AIRCREW WEAPONS DELIVERY MANUAL (NONNUCLEAR) B … 1B-52H-34-2-8 1-Jun-06 Scrib… · t.o. 1b-52h-34-2-8 1 december 2003 change 3 – 1 june 2006 aircrew weapons delivery manual (nonnuclear)

T.O. 1B-52H-34-2-8

1 DECEMBER 2003CHANGE 3 – 1 JUNE 2006

AIRCREW WEAPONS DELIVERY MANUAL(NONNUCLEAR)

B-52/AGM-158 JASSMUSAF

SERIESAIRCRAFTWEAPONSB-52/AGM-158 JASSM

THE BOEING COMPANYF34601-98-C-0002F34601-03-D-0066

This manual contains unverified procedures. Refer to the validation/verification sta-tus page(s) prior to performing any operation or maintenance procedure.

THIS PUBLICATION IS INCOMPLETE WITHOUT CLASSIFIED SUPPLEMENT T.O. 1B-52H-34-2-8-1.

SEE T.O. 0-1-CD-1 FOR CURRENT STATUS OF FLIGHT MANUALS, SAFETY SUPPLEMENTS, OPERATIONAL SUPPLEMENTS, ANDFLIGHT CREW CHECKLISTS.

COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTION OF ALL AIR FORCE PERSONNELCLEARED FOR OPERATION OF SUBJECT AIRCRAFT.

DISTRIBUTION STATEMENT E – Distribution authorized to the Department of Defense Components only, due to Direct Military Support, 29October 1996. Other requests shall be referred to 327 BMSG/EN, Tinker AFB, OK 73145-3021.

WARNING –This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.)or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et seq. Violations of these export laws are subject to severecriminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

HANDLING AND DESTRUCTION NOTICE – Comply with distribution statement and destroy by any method that will prevent disclosure ofcontents or reconstruction of the document. Demil code D.

PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE AIR FORCE

INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

*The asterisk indicates pages changed, added, or deleted by the current change.

Dates of issue for original and changed pages are:

NOTE: The portion of the text affected by the changes is indicated by avertical line in the outer margins of the page.

LIST OF EFFECTIVE PAGES

Upon receipt of the second and subsequent changes to this technical order, personnel responsible for maintaining this publication in currentstatus will ascertain that all previous changes have been received and incorporated. Action should be taken promptly if the publication isincomplete.

T.O. 1B-52H-34-2-8

A Change 3 USAF

ADDITIONAL COPIES OF THIS PUBLICATION MAY BE OBTAINED BY USAF ACTIVITIES IN ACCORDANCE WITH T.O. 00-5-1.

Technical orders are normally distributed promptly after printing. Date(s) shown on the title page (lower right corner) are for identification only. Theseare not distribution dates. Processing time sometimes causes distribution to only appear to have been delayed.

Original 0 1 Dec 03 Change 1 1 Dec 04 Change 2 1 Jul 05 Change 3 1 Jun 06

TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 256 CONSISTING OF THE FOLLOWING:

Page Change Page Change Page Change Page Change No. No. No. No. No. No. No. No.

* Title 3. . . . . . . . . . . . . . . . . . . . . * A 3. . . . . . . . . . . . . . . . . . . . . . .

V/VS-1 – V/VS-7 Added 2. . . V/VS-8 Blank Added 2. . . . . .

* Flyleaf 1 3. . . . . . . . . . . . . . . . . Flyleaf 2 Blank 0. . . . . . . . . . . i 0. . . . . . . . . . . . . . . . . . . . . . . . ii – iii 2. . . . . . . . . . . . . . . . . . . .

* iv 3. . . . . . . . . . . . . . . . . . . . . . . 1-1 0. . . . . . . . . . . . . . . . . . . . . 1-2 Blank 0. . . . . . . . . . . . . . .

* 1-3 3. . . . . . . . . . . . . . . . . . . . . 1-4 – 1-5 0. . . . . . . . . . . . . . . . 1-6 1. . . . . . . . . . . . . . . . . . . . . 1-7 – 1-9 0. . . . . . . . . . . . . . . . 1-10 Blank 0. . . . . . . . . . . . . . . 1-11 – 1-13 2. . . . . . . . . . . . . . 1-14 0. . . . . . . . . . . . . . . . . . . . 1-15 2. . . . . . . . . . . . . . . . . . . . 1-16 – 1-18 0. . . . . . . . . . . . . . 1-19 – 1-20 2. . . . . . . . . . . . . . 1-21 0. . . . . . . . . . . . . . . . . . . .

* 1-22 3. . . . . . . . . . . . . . . . . . . . 1-23 – 1-24 0. . . . . . . . . . . . . .

* 1-25 3. . . . . . . . . . . . . . . . . . . . 1-26 0. . . . . . . . . . . . . . . . . . . . 1-27 – 1-30 2. . . . . . . . . . . . . . 1-30A – 1-30F Added 2. . . . . 1-31 – 1-35 2. . . . . . . . . . . . . .

* 1-36 3. . . . . . . . . . . . . . . . . . . . 1-37 – 1-38 2. . . . . . . . . . . . . .

* 1-39 3. . . . . . . . . . . . . . . . . . . . 1-40 1. . . . . . . . . . . . . . . . . . . .

1-41 2. . . . . . . . . . . . . . . . . . . . * 1-42 3. . . . . . . . . . . . . . . . . . . .

1-43 – 1-44 2. . . . . . . . . . . . . . * 1-45 3. . . . . . . . . . . . . . . . . . . .

1-46 2. . . . . . . . . . . . . . . . . . . . * 1-47 3. . . . . . . . . . . . . . . . . . . .

1-48 – 1-52 2. . . . . . . . . . . . . . 1-52A – 1-52G Added 2. . . . . 1-52H Blank Added 2. . . . . . . 1-53 – 1-55 0. . . . . . . . . . . . . . 1-56 – 1-61 2. . . . . . . . . . . . . .

* 1-62 3. . . . . . . . . . . . . . . . . . . . 1-62A Added 2. . . . . . . . . . . . .

* 1-62B – 1-62D 3. . . . . . . . . . . 1-63 2. . . . . . . . . . . . . . . . . . . . 1-64 0. . . . . . . . . . . . . . . . . . . .

* 1-65 3. . . . . . . . . . . . . . . . . . . . 1-66 2. . . . . . . . . . . . . . . . . . . .

* 1-67 3. . . . . . . . . . . . . . . . . . . . 1-68 2. . . . . . . . . . . . . . . . . . . . 1-68A – 1-68D Added 2. . . . . 1-69 0. . . . . . . . . . . . . . . . . . . . 1-70 – 1-73 2. . . . . . . . . . . . . . 1-74 0. . . . . . . . . . . . . . . . . . . .

* 1-75 – 1-76 3. . . . . . . . . . . . . . 1-77 – 1-78 2. . . . . . . . . . . . . . 1-79 0. . . . . . . . . . . . . . . . . . . .

* 1-80 3. . . . . . . . . . . . . . . . . . . . 2-1 0. . . . . . . . . . . . . . . . . . . . . 2-2 Blank 0. . . . . . . . . . . . . . . . 2-3 2. . . . . . . . . . . . . . . . . . . . . 2-4 – 2-6 0. . . . . . . . . . . . . . . . 2-7 2. . . . . . . . . . . . . . . . . . . . .

2-8 0. . . . . . . . . . . . . . . . . . . . . 2-9 2. . . . . . . . . . . . . . . . . . . . .

* 2-10 3. . . . . . . . . . . . . . . . . . . . 2-11 – 2-12 0. . . . . . . . . . . . . .

* 2-13 3. . . . . . . . . . . . . . . . . . . . 2-14 – 2-17 0. . . . . . . . . . . . . . 2-18 1. . . . . . . . . . . . . . . . . . . . 2-19 – 2-21 0. . . . . . . . . . . . . . 2-22 2. . . . . . . . . . . . . . . . . . . . 2-23 0. . . . . . . . . . . . . . . . . . . . 2-24 Blank 0. . . . . . . . . . . . . . . 3-1 – 3-2 0. . . . . . . . . . . . . . . . 3-3 – 3-4 2. . . . . . . . . . . . . . . .

* 3-5 3. . . . . . . . . . . . . . . . . . . . . 3-6 – 3-7 0. . . . . . . . . . . . . . . . 3-8 Blank 0. . . . . . . . . . . . . . .

* 4-1 3. . . . . . . . . . . . . . . . . . . . . 4-2 0. . . . . . . . . . . . . . . . . . . . .

* 4-3 3. . . . . . . . . . . . . . . . . . . . . 4-4 0. . . . . . . . . . . . . . . . . . . . . 5-1 – 5-6 0. . . . . . . . . . . . . . . . 6-1 – 6-6 0. . . . . . . . . . . . . . . . 6-7 2. . . . . . . . . . . . . . . . . . . . . 6-8 0. . . . . . . . . . . . . . . . . . . . . 7-1 0. . . . . . . . . . . . . . . . . . . . . 7-2 – 7-3 2. . . . . . . . . . . . . . . . 7-4 – 7-5 0. . . . . . . . . . . . . . . . 7-6 Blank 0. . . . . . . . . . . . . . . .

* 7-7 3. . . . . . . . . . . . . . . . . . . . . 7-8 2. . . . . . . . . . . . . . . . . . . . . 7-9 0. . . . . . . . . . . . . . . . . . . . .

* 7-10 3. . . . . . . . . . . . . . . . . . . .

7-11 0. . . . . . . . . . . . . . . . . . . . * 7-12 3. . . . . . . . . . . . . . . . . . . .

7-13 0. . . . . . . . . . . . . . . . . . . . 7-14 – 7-15 2. . . . . . . . . . . . . . 7-16 Blank 0. . . . . . . . . . . . . . .

* 7-17 3. . . . . . . . . . . . . . . . . . . . 7-18 2. . . . . . . . . . . . . . . . . . . .

* 7-19 – 7-20 3. . . . . . . . . . . . . . * 7-20A – 7-20B 3. . . . . . . . . . . . * 7-20C – 7-20D Deleted 3. . . .

7-21 – 7-22 0. . . . . . . . . . . . . . 7-23 2. . . . . . . . . . . . . . . . . . . . 7-24 0. . . . . . . . . . . . . . . . . . . .

* 7-25 3. . . . . . . . . . . . . . . . . . . . 7-26 – 7-27 0. . . . . . . . . . . . . . 7-28 Blank 0. . . . . . . . . . . . . . . 7-29 – 7-45 0. . . . . . . . . . . . . . 7-46 2. . . . . . . . . . . . . . . . . . . . 7-47 – 7-49 0. . . . . . . . . . . . . . 7-50 – 7-52 2. . . . . . . . . . . . . . 7-52A Added 2. . . . . . . . . . . . . 7-52B Blank Added 2. . . . . . . 7-53 2. . . . . . . . . . . . . . . . . . . .

* 7-54 – 7-55 3. . . . . . . . . . . . . . 7-56 – 7-68 2. . . . . . . . . . . . . . 7-68A – 7-68D Added 2. . . . . 7-69 2. . . . . . . . . . . . . . . . . . . . 7-70 – 7-73 0. . . . . . . . . . . . . . 7-74 Blank 0. . . . . . . . . . . . . . . Glossary-1 – Glossary-2 0. . . Index-1 – Index-3 2. . . . . . . . . Index-4 Blank 0. . . . . . . . . . . .

CURRENT ABBREVIATED CHECKLIST

AGM-158 JASSM Abbreviated Flight Crew Checklist T.O. 1B-52H-34-2-8CL-1 1 Dec 03 Change 3 - 1 Jun 06

T.O. NO. PTO CHANGE NO. – DATE

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(B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)

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BASIC DATE CHANGE NO. – DATE

This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accor-dance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage toequipment.

WARNING

V/VS-1

T.O. 1B-52H-34-2-8 1 DEC 03 CHANGE 2 - 1 JUL 2005 AMI

TCTO Listings (P, PG iv) 1 Mar 04 AOffensive Avionics System (OAS)Interface (P, PG 1-11 ) 1 Mar 04 AWeapon Control PanelInterface (P, PG 1-11 ) 1 Mar 04 AMissile Data Flow (Typical)(F: 1-4, PG 1-13) 1 Mar 04 AWeapon Control Panel(F: 1-5, 2 /2, PG 1-15) 1 Mar 04 AJASSM IKB Commands(F: 1-9, 1/2, PG 1-19) 1 Mar 04 AJASSM IKB Commands(F: 1-9, 2/2, PG 1-20) 1 Mar 04 AWeapon Jettison(P, PG 1-22) 1 Mar 04 AAJCP Commanded Jettison(P, PG 1-22) 1 Mar 04 APilot’s Bmb Bay & Missile Jett ContrlSwitch Commanded Jett (P, PG1-25) 1 Mar 04 AJASSM SMO Software(P, PG 1-27) 1 Mar 04 ASMO MFD Displays(P, PG 1-27 – 1-28) 1 Mar 04 APrime Mission Data(P, PG 1-28) 1 Mar 04 AWeapon Supervision Menu (CF-5)(P, PG 1-30) 1 Dec 04 APART SIM Mode Command (CF-51)(P, PG 1-30) 1 Dec 04 AFULL SIM Mode Command (CF-52)(P, PG 1-30) 1 Dec 04 AJASSM Supervision Menu (CF-57)(P, PG 1-30A) 1 Mar 04 AJASSM Control Function (CF)Commands (F: 1-16, PG 1-30B) 1 Mar 04 ACF Menu(F: 1-17, 1/2, PG 1-30C) 15 Mar 04 ACF Menu(F: 1-17, 2/2, PG 1-30D) 15 Mar 04 AWeapon Supervision Menu (CF-5)(F: 1-18, 1/2, PG 1-30E) 15 Mar 04 A



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V/VS-2


Weapon Supervision Menu (CF-5)(F: 1-18, 2/2, PG 1-30F) 15 Mar 04 AClassified Data Erase Command(CF-575) (P, PG 1-31) 1 Mar 04 AJASSM Auto Targeting Mode(CF-580) (P, PG 1-31) 1 Mar 04 AMissile Tgt Assign(Manual Targeting)Display (CF-586) (P, PG 1-31) 1 Mar 04 AJASSM Supervision Menu (CF-57)(F: 1-18, 1/2, PG 1-32) 15 Mar 04 AJASSM Supervision Menu CF-57(F: 1-18, 2/2, PG 1-33) 1 Mar 04 AJASSM Targeting Menu (CF-58)(F: 1-20, 1/2, PG 1-34) 1 Mar 04 AJASSM Targeting Menu (CF-58)(F: 1-20, 2/2, PG 1-35) 1 Mar 04 AMissile Target Assignment Display (CF-586) (F: 1-21, 1/3, PG 1-36) 1 Mar 04 AMissile Target Assignment Display(CF-586) (F: 1-18, 2/3, PG 1-37) 1 Mar 04 AMissile Target Assignment Display(CF-586) (F: 1-18, 3/3, PG 1-38) 1 Mar 04 ADirect Target Definition Display(CF-588,n) (P, PG 1-39) 1 Mar 04 ARetarget-All Command (CF589)(P, PG 1-41) 1 Mar 04 ADirect Tgt Definition Disp (CF-588,n)(P, 1-22, 2/4, PG 1-43) 1 Mar 04 ACF-62 SMO Menu(P, PG 1-46) 1 Mar 04 ACF-65 Data Record(P, PG 1-46) 1 Mar 04 ACF-67 Shutdown(P, PG 1-47) 1 Mar 04 ACF-68 ECU Power Override(P, PG 1-47) 1 Mar 04 ACF-69A & CF-69B ACU Shutdown(P, PG 1-47) 1 Mar 04 AFCP Supervision Menu (CF-6)(F: 1-23, 1/2, PG 1-48) 1 Mar 04 AFCP Supervision Menu (CF-6)(F: 1-23, 2/2, PG 1-49) 1 Mar 04 A



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V/VS-3


SMO Load Menu (CF-62)(F: 1-24, PG 1-50) 1 Mar 04 AMission Supervision Menu(P, PG 1-51) 15 Mar 04 AB-52 Mission Data Load Command(P, PG 1-51) 1 Dec 04 AWeapon Group Load Display(CF-82A, CF-82C)(P, PG 1-52) 1 Mar 04 AMission Supervision Menu(F: 1-25, 1/2, PG 1-52A) 15 Mar 04 AMission Supervision Menu(F: 1-25, 2 /2, PG 1-52B) 15 Mar 04 AB-52 Mission Data Load Display(CF-81)(F: 25A, 1/2, PG 1-52C) 15 Mar 04 AB-52 Mission Data Load Display(CF-81)(F: 25A, 2/2, PG 1-52D) 1 Mar 04 AWpn Grp Load Menu (F: 1-25B, 1/2, PG 1-52E) 1 Mar 04 AWpn Grp Load Menu (F: 1-25B, 2/2, PG 1-52F) 1 Mar 04 ATargeting Completion Command (CF-DD) (P, PG 1-52G) 1 Mar 04 ADirect Target Copy Command (CF-Dn)(P, PG 1-52G) 1 Mar 04 AFormat (FRMT) Displays(P, PG 1-56) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(P, PG 1-56) 1 Mar 04 AJASSM Status & Invent Disp w/ Sel Sta Status (FRMT-7xy)(P, PG 1-57) 1 Mar 04 AWeapon Assignment Data Display(P, PG 1-57) 1 Mar 04 AStores Inventory Summary Display(FRMT-77)(P, PG 1-57) 1 Mar 04 AJASSM Format Commands(F: 1-28, PG 1-57) 1 Mar 04 AJASSM FRMT (Format) Menu(F: 1-29, 1/2, PG 1-58) 1 Mar 04 AJASSM FRMT (Format) Menu(F: 1-29, 2/2, PG 1-59) 1 Mar 04 APME Status Display (FRMT-6)(F: 1-30, 1/2, PG 1-60) 1 Mar 04 A



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PME Status Display (FRMT-6)(F: 1-30, 2/2, PG 1-61) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(F: 1-31, 1/6, PG 1-62) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(F: 1-31, 2/6, PG 1-62A) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(F: 1-31, 3/6, PG 1-62B) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(F: 1-31, 4/6, PG 1-62C) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(F: 1-31, 5/6, PG 1-62D) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(F: 1-31, 6/6, PG 1-63) 1 Mar 04 AJASSM Stat & Invent Disp w/ Sel StaStatus (F: 1-32, 2/5, PG 1-65) 1 Mar 04 AJASSM Stat & Invent Disp w/ Sel StaStatus (F: 1-32, 3/5, PG 1-66) 1 Mar 04 AJASSM Stat & Invent Disp w/ Sel StaStatus (F: 1-32, 4/5, PG 1-67) 1 Mar 04 AJASSM Stat & Invent Disp w/ Sel StaStatus (F: 1-32, 5/5, PG 1-68) 1 Mar 04 AWeapon Assignment Data Display(F: 1-32A, 1/2, PG 1-68A) 1 Mar 04 AWeapon Assignment Data Display(F: 1-32A, 2/2, PG 1-68B) 1 Mar 04 AStores Inventory Display(F: 1-32B, Sheet 1/2, PG 1-68C) 1 Mar 04 AStores Inventory Display(F: 1-32B, Sheet 2/2, PG 1-68D) 1 Mar 04 AWeapon Summary Display(P, PG 1-70) 1 Mar 04 AWeapon Summary Display(F: 1-34, 1/3, PG 1-71) 1 Mar 04 AWeapon Summary Display(F: 1-34, 2/3, PG 1-72) 1 Mar 04 AWeapon Summary Display(F: 1-34, 3/3, PG 1-73) 1 Mar 04 AProgram Display (PRGM)(F: 1-36, 3/6, PG 1-77) 1 Mar 04 AProgram Display (PRGM)(F: 1-36, 4/6, PG 1-78) 1 Mar 04 A



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V/VS-5


General (Procedures)(P, PG 2-3) 1 Mar 04 AAfter Engine Start(P, PG 2-7) 1 Mar 04 AMIssile Power Application(P, PG 2-9 - 2-10) 1 Mar 04 APost Strike/ Abort Procedures(P, PG 2-22) 1 Mar 04 ASelective Jettison Using WCP/SMO(P, PG 3-3) 1 Mar 04 ASelective Jettison Using AJCP(P, PG 3-4) 1 Mar 04 AEmergency Jettison(P, PG 3-5) 1 Mar 04 ATelemetry Power Off Command (CF-57B) (Test Only)(P, PG 4-3) 1 Mar 04 AMIssion Planning Considerations(P, PG 6-7) 1 Mar 04 AOAS/JASSM Operation(P, PG 7-3) 1 Mar 04 AWCE Power Application(P, PG 7-7) 1 Mar 04 AMissile Power Application(P, PG 7-8) 1 Mar 04 AMissile and Ejector Status(P, PG 7-10 - 7-11) 1 Mar 04 ALaunch Point Target Number(P, PG 7-12) 1 Mar 04 AMissile GPS Alignment Quality(P, PG 7-12) 1 Mar 04 AJASSM Status & Inventory Display(FRMT-7)(F: 7-4, PG 7-14) 1 Mar 04 AMissile Mission Data and Targeting(P, PG 7-17) 1 Mar 04 AMissile Targeting Methods(P, PG 7-17) 1 Mar 04 AAutomatic Targeting(P, PG 7-17) 1 Mar 04 AJASSM Tgt Assign (Manual Targeting)Disp(CF-586)(F: 7-6, 1/2, PG 7-19) 1 Dec 04 ADirect Target Definition Disp(CF-586)(F: 7-7, 2/2, PG 7-20A) 1 Dec 04 A



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Missile/Tgt Assign (Man Targeting)Data Entry Proced (P, PG 7-23) 1 Mar 04 AAutomatic Launch Determination(P, PG 7-46) 1 Mar 04 AMissile Jettison(P, PG 7-50) 1 Mar 04 ASimulation Capabilities(P, PG 7-51) 1 Mar 04 ASimulated Missile Loadout(P, PG 7-51) 1 Mar 04 ASimulated Targeting Operations(P, PG 7-51) 1 Mar 04 ASimulated WCE Responses(P, PG 7-51) 1 Mar 04 ASimulated Ranging(P, PG 7-51) 1 Mar 04 ASMO Termination(P, PG 7-52) 1 Mar 04 ASMO Restart(P, PG 7-52) 1 Mar 04 AJASSM Master Faults(F: 7-19, 1/17, PG 7-53) 1 Dec 04 AJASSM Master Faults(F: 7-19, 2/17, PG 7-54) 1 Mar 04 AJASSM Master Faults(F: 7-19, 3/17, PG 7-55) 1 Mar 04 AJASSM Master Faults(F: 7-19, 4/17, PG 7-56) 1 Dec 04 AJASSM Master Faults(F: 7-19, 5/17, PG 7-57) 1 Mar 04 AJASSM Master Faults(F: 7-19, 6/17, PG 7-58) 1 Dec 04 AJASSM Master Faults(F: 7-19, 7/17, PG 7-59) 1 Mar 04 AJASSM Master Faults(F: 7-19, 8/17, PG 7-60) 1 Dec 04 AJASSM Master Faults(F: 7-19, 9/17, PG 7-61) 1 Dec 04 AJASSM Master Faults(F: 7-19, 10/17, PG 7-62) 1 Mar 04 AJASSM Master Faults(F: 7-19, 11/17, PG 7-63) 1 Dec 04 A



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V/VS-7/(V/VS-8 blank)


JASSM Master Faults(F: 7-19, 12/17, PG 7-64) 1 Dec 04 AJASSM Master Faults(F: 7-19, 13/17, PG 7-65) 1 Dec 04 AJASSM Master Faults(F: 7-19, 14/17, PG 7-66) 1 Mar 04 AJASSM Master Faults(F: 7-19, 15/17, PG 7-67) 1 Mar 04 AJASSM Master Faults(F: 7-19, 16/17, PG 7-68) 1 Dec 04 AJASSM Master Faults(F: 7-19, 17/17, PG 7-68A) 1 Dec 04 AJASSM Advisories(F: 7-20, 2/3, PG 7-68C) 1 Dec 04 AJASSM Advisories(F: 7-20, 3/3, PG 7-68D) 1 Dec 04 AJASSM Status Messages(F: 7-21, PG 7639) 1 Mar 04 ASafe Release Advisories(F: 7-22, PG 7-69) 1 Mar 04 A

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STATUS OF SAFETY AND OPERATIONAL SUPPLEMENTS

This supplement status page is based on information available to the manual editor as of the date ofthis publication. The information may not be current as it must be updated by any subsequent supple-ment status pages and by reference to T.O. 0-1-CD-1.

SUPPLEMENTS IN THIS CHANGE

Number Date Short Title Section Affected

OUTSTANDING SUPPLEMENTS

Number Date Short Title Section Affected

SS-1(I) 30 September 03 Recycle Weapon Power After Targeting II, VII

SS-4(I) 27 January 06 JASSM Launch Criteria II, V, VI

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T.O. 1B-52H-34-2-8

i

Table of Contents

SECTION I DESCRIPTION 1-1

SECTION II NORMAL AIRCREW PROCEDURES 2-1

SECTION III EMERGENCY AIRCREW PROCEDURES 3-1

SECTION IV SUPPLEMENTARY DATA 4-1

SECTION V OPERATING LIMITATIONS 5-1

SECTION VI MISSION PLANNING 6-1

SECTION VII SYSTEMS OPERATION 7-1

GLOSSARY GLOSSARY 1

ALPHABETICAL INDEX INDEX 1

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ii Change 2

INTRODUCTION

SCOPE. This manual provides aircrews with descriptive and procedural information requiredfor delivery of the AGM-158 Joint Air-To-Surface Standoff Missile (JASSM) from B-52H air-craft modified with Integrated Conventional Stores Management System (ICSMS), and theStandoff Weapon Stores Management Overlay loaded.

CHECKLISTS. Abbreviated checklists for the procedures given in this manual are contained ina stand alone Weapon Delivery Checklist. This checklist is identified by a T.O. number that isidentical to that of the applicable weapon delivery manual except for the addition of the let-ters CL (checklist).

ARRANGEMENT. This manual is divided into seven sections as follows:

Section I, DESCRIPTION – Locates, identifies, and functionally describes the weaponand aircraft components which directly concern the aircrew in the control and deliv-ery of the JASSM.

Section II, NORMAL AIRCREW PROCEDURES – Contains partially illustrated am-plified checklists for performance of normal aircrew weapon delivery procedures frompreflight through after landing and procedures applicable in the event a mission isaborted.

Section III, EMERGENCY AIRCREW PROCEDURES – Contains weapon jettisonprocedures. No attempt is made to regulate or define conditions under which the mis-sion will be aborted.

Section IV, SUPPLEMENTARY DATA – Contains information on operational test sys-tems.

Section V, OPERATING LIMITATIONS – Contains important weapon and weaponsystem limitations that must be taken into account during planning and accomplish-ment of a mission.

Section VI, MISSION PLANNING – Contains information on transportation of dan-gerous material, inflight emergency notification, and inflight mission data changesthat can be accomplished by the flightcrew.

Section VII, SYSTEMS OPERATION – Contains additional material regarding theoperation of the aircraft, JASSM systems. Theory of guidance system operation, guid-ance performance, and malfunction analysis are included.

PRECEDENCE. Compliance with procedures herein is mandatory. In all instances, only thoseoperations which are within the scope of the current applicable safety rules may be per-formed.

SAFETY POLICIES. The procedures in this manual reflect the latest applicable rules and poli-cies. Aircrew compliance with these procedures and policies is mandatory.

Mission planning shall provide maximum protection to friendly and neutral areas consistentwith operational requirements. Selection of launch point and type of maneuver shall beguided by the possible effect upon friendly or neutral areas of a missile guidance or controlsystem failure. Since launch point and type of maneuver are sufficiently flexible to allow forinflight decisions, aircrews shall be briefed concerning the potential disaster hazard tofriendly or neutral areas.

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Change 2 iii

REFERENCES. The following publications, available to using commands, should be used togain more comprehensive information on subjects referred to in this technical order:

1B-52H-1 Flight Manual1B-52H-1-1 Flight Manual - Appendix 1, Performance Data1B-52H-1-12 Radar Navigator’s/Navigator’s Manual1B-52H-1-13 Electronic Warfare Officer’s Manual1B-52H-2-31GA-1 General Aircraft/Bomb Release System B-52H1B-52H-33-2-1 Nonnuclear Munitions Loading Procedures1B-52H-34-2-1 Aircrew Weapon Delivery Manual (Nonnuclear) B-521B-52H-34-2-7 Aircrew Weapon Delivery Manual (Nonnuclear) B-52/AGM-154 JSOW1B-52H-34-2-8-1 B-52H/AGM-158 Aircrew Weapons Delivery Manual

Classified Supplement1B-52H-34-2-9 Aircrew Weapon Delivery Manual (Nonnuclear) B-52/AGM-86C/D1B-52H-5 Basic Weight Checklist and Loading Data B-52H1-1M-34 Aircrew Weapons Delivery Manual (Nonnuclear) JMEM Joint Munition Employment Manual

SAFETY AND OPERATIONAL SUPPLEMENTS. Information involving flightcrew safety and di-rectly pertaining to the information contained herein will be promptly forwarded to you bySafety Supplements issued against this manual. Safety Supplements covering loss of life willget to you in 48 hours by message (called Interim Safety Supplements) and those concerningserious damage to equipment within 15 days by mail (in a formal printed form). Operationalinformation not involving safety but of an urgent nature will be forwarded to you by Opera-tional Supplements issued against this manual. These will be forwarded by message (inter-im) or by mail (formal), depending on the urgency of the information. Interim supplementsare normally replaced by formal printed supplements at an early date. Formal printed sup-plements are identified by red letters “SS” for safety supplements and black letters “OS” foroperational supplements printed around the borders of the pages. The currency of safety andoperational supplements affecting your manual can be determined by referring to the WeeklyIndex of Bomber Aircraft Safety Supplements (T.O. 0-1-CD-1). The title block of each supple-ment and the title page of this manual should also be checked to determine the effect theymay have on existing supplements. You must remain constantly aware of the status of allsupplements – current supplements must be complied with, but there is no point in restrict-ing your operation by complying with a replaced or rescinded supplement. As a further aid asupplement summary is included in this manual, following the A pages, for both safety andoperational supplements: however, this summary can only be as current as this manual.Safety and operational supplements will be filed in accordance with Section VI of the AirForce Technical Order System, T.O. 00-5-1.

WARNINGS, CAUTIONS, AND NOTES. The following definitions apply to “Warnings,” “Cautions,”and “Notes” found throughout the manual.

Operating procedures, techniques, etc, which could result in personal injury or lossof life if not carefully followed.

Operating procedures, techniques, etc, which could result in damage to equipmentif not carefully followed.

NOTE

An operating procedure, technique, etc, which is considered essential to emphasize.

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iv Change 3

SHALL, WILL, SHOULD, and MAY. The following definitions apply to the words:

SHALL or WILL The instructions or procedures prefaced by “shall” or “will” aremandatory.

SHOULD Normally used to indicate a preferred but nonmandatorymethod of accomplishment.

MAY An acceptable or suggested means of accomplishment.

CHANGE SYMBOLS. Changes to existing material and addition of new material are indicatedby one of three types of symbols determined by the nature of the material affected. Text ma-terial utilized a vertical line in the margin adjacent to the affected area. New illustrations(figures) utilize a vertical line in the outer margin of the page. Line drawings use a miniaturepointing hand to highlight the affected area. Change symbols are not used for blank spaceresulting from deletions, indexes, and tabular data where changes cannot be identified, relo-cation of material, or correction of minor inaccuracies unless such correction changes themeaning.

RESPONSIBLE AGENCY. Every effort is made to keep this manual current. Review conferenceswith operating personnel and a constant review of reports assure inclusion of the latest datain this manual. Comments, corrections, and questions regarding this manual should be sub-mitted on AF Form 847 through the local standardization/evaluation unit and routed to 327BMSG/EN, 3001 Staff Drive Suite 2AF193A, Tinker AFB, Oklahoma 73145-3021.

RETROFIT CODING. The following code symbols along with the word ‘‘Less’’ are used todistinguish information related to aircraft that have the described retrofit changeincorporated from that which is applicable to aircraft not yet retrofitted. This list containsonly TCTO’s currently active. Those known to be completed are not included.

SYMBOL T.O. NO. TITLE

CS

1B-52H-753

1B-52H-756

⎧⎨⎩

Installation of Global Positioning System (GPS) on B-52HAircraft (ECP 0109)

Installation of Integrated Conventional Stores Management System (ICSMS)on B-52H Aircraft (ECP 0109)

[AMI] 1B-52H-830 Replacement of Ballistics Computer Set AN/AYQ-10 and Inertial NavigationSystem AN/ASN-136 on B-52H Aircraft.

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Description section I

table of contents page

PART 1 – B-52/AGM-158 JASSM SYSTEM DESCRIPTION 1-3

B-52/JASSM WEAPON SYSTEM 1-3

B-52 CARRIER EQUIPMENT 1-3

JOINT AIR-TO-SURFACE STANDOFF MISSILE (JASSM) 1-3

JASSM SUSPENSION SYSTEM 1-7

JASSM COVER 1-7

PART 2 – OFFENSIVE AVIONICS SYSTEM 1-11

OFFENSIVE AVIONICS SYSTEM (OAS) INTERFACE 1-11

OAS/WEAPON SYSTEM RELATED CONTROLS AND DISPLAYS 1-11

WEAPON JETTISON 1-22

PART 3 – JASSM SMO SOFTWARE 1-27

SMO MFD DISPLAYS 1-27

RELEASE ADVISORY DISPLAY 1-27

PRIME MISSION DATA 1-29

CONTROL FUNCTION (CF) DISPLAYS 1-29

FORMAT (FRMT) DISPLAYS 1-56

PROGRAM (PRGM) DISPLAYS 1-74

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PART 1 - B-52/AGM-158 JASSM SYSTEM DESCRIPTION

B-52/JASSM WEAPON SYSTEM

The B-52 Joint Air to Surface Standoff Missile(JASSM) weapon system consists of a ConventionalEnhancement Modification (CEM) modified B-52with OAS, and the JASSM. The B-52 aircraft hasthe capability of releasing 12 JASSM missiles, sixfrom each Heavy Stores Adapter Beam (HSAB)mounted on an Integrated Conventional StoresManagement System (ICSMS) external pylon.

B-52 CARRIER EQUIPMENT

The offensive avionics system (OAS) controls powerapplication, programming, and launch of missiles.The OAS also provides signal processing, storageavionics, control and display panels, missile super-vision, regulated dc power conversion, and monitorsenvironmental control equipment in the aircraft.The OAS interfaces with the carrier electricalsources, and panel lighting. Primary missile controland monitor is provided through the OAS weaponcontrol panel (WCP), integrated keyboard (IKB)and the multifunction displays (MFD).

The B-52, when configured for JASSM carriage andrelease, is equipped with the following equipment:OAS Hardware; OAS Software, including the JointAir-To-Surface Standoff Missile Stores Manage-ment Overlay (JASSM SMO); and Less [AMI] thepilots’ moving map display, which depicts both theIn-Range and In-Zone Launch Acceptability Re-gions (LARs) for the JASSM. For information onthe pilots’ moving map display see GPS IU/TACANEMULATION in T.O. 1B-52H-1.

JOINT AIR-TO-SURFACE STANDOFF MISSILE(JASSM)

The AGM-158A JASSM, figure 1-1, is an air-launched, medium range autonomous cruise mis-sile. JASSM is designed as a launch and leaveweapon system, in that once launched, the missilewill navigate to and engage its planned target withno further control communication from the launch-ing aircraft or other command agency. The use ofthe Infrared (IR) seeker in the nose of the missile isoptional based on target requirements. The missileuses a tightly coupled Global Positioning System(GPS) aided Inertial Navigation System (INS) formid-course and terminal area navigation. A GPS

anti-jam capability is also provided to ensure robustperformance. The no-seeker mission option providesexcellent performance against soft targets usingGPS/Inertial guidance to target impact. The seekeris employed against targets requiring high impactprecision. The no-seeker mission option can be usedin a GPS/Inertial terminal guidance mode.

The JASSM is trapezoidal in cross section. The fu-selage is constructed from composite shells of asandwiched foam core construction. An internalhardback assembly and several bulkheads providestructural strength. A pair of folding lugs with 30inch spacing is provided for mating to the ejectorrack. Flight surfaces (wings) are stowed in a foldedlocation under the fuselage and are pyrotechnicallydeployed after launch. A single vertical tail surfaceassists in steering control. The vertical tail surfaceis stowed in a folded position and is also pyrotechni-cally deployed after launch. Electrical connection tothe B-52 is made via a MIL-STD-1760 cable inter-face through the missile umbilical connector just aftof the rear launch lug. After release, pyrotechnicsare fired to deploy both the flight surfaces and thevertical tail. Propulsion is provided by a liquidfueled (JP-10) Teledyne 370 series turbojet engine.JASSM uses a 1000-pound class WDU-42/B war-head with a FMU-156B fuze. The aircraft MIL-STD-1760 cable connection to the missile umbilicalis the only electrical connection to the missile. Allmissile arming and flight transition actions areelectronically controlled within the missile aftermissile release. No other lanyards or release de-vices are required between the host aircraft and theJASSM.

JASSM physical characteristics are as follows:

Length 168 inchesWidth 24.9 InchesHeight 20.4 InchesLug Spacing 30 inchesWing Span (fully deployed) 120 inchesEngine Teledyne 370 series

TurbojetWeight 2250 poundsSeeker InfraredGuidance GPS/InertialWarhead WDU-042

One Thousand Pound Class

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1-4

Joint Air to Surface Standoff Missile (JASSM)

Figure 1-1

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1-5

FUSELAGE

The fuselage has a pointed nose with a trapezoidalcross section. Two covers close out the bottom of thefuselage. The forward cover encloses the IR seeker,Inertial Measuring Unit (IMU), Missile ControlUnit (MCU), warhead and the wing section, whilefitting around the forward inlet lips; the aft coverencloses the propulsion section and aft fuel tankand test instrumentation kit areas.

The fabricated skins are constructed of stiffenedfoam cores contained between composite panels.The bulkheads consist of a superframe assemblyand 2 conventional frames. The superframe assem-bly supports the launch lug, ejector and sway braceloads, and missile retention. The aft lower bridgeencloses the warhead below the aft lug. The mainsuperframe and the wing carry-through are fabri-cated from stainless steel. The superframe assem-bly is split horizontally to allow the installation ofthe warhead late in the assembly process. The com-posite forward frame provides stiffness. The engine/tail frame secures the engine to the upper fuselage,the vertical fin actuator and the vertical fin root.

WINGS

The missile has two deployable wings. The wingshave a constant chord and thickness except at thewing fuselage intersection where the upper wingsurface transitions to a flat surface for the wingpivot integration. Mechanical latches hold thewings next to the missile fuselage until launch toprevent flutter during captive carriage. The wingsare deployed in a two step process, using a two-stage pyrotechnic actuator. The wings are com-manded to extend to 75 degrees when clear of thelaunch aircraft. This first deployment position in-creases pitch stability to aid separation from thehost aircraft. The wings move from 75 degrees to a45 degree sweep position for cruise when initialpitch stability is achieved. The 45 degree sweepposition aids longitudinal stability and contributesa large dihedral effect. The wing deployment mech-anism connects both the left and right wings to en-sure symmetrical deployment.

An elevon located on the outer portion of each wingprovides pitch and roll control. The elevons are noteffective until the wings are deployed to 45 degrees.Roll control is provided by differential elevon deflec-tions and pitch control by symmetrical deflection.Electro-mechanical actuators mounted inside thewing spars drive the elevons.

VERTICAL TAIL

The vertical tail is constructed similar to the wings.Prior to launch the tail is folded over 135 degreesand held in place by a mechanical latch. Afterlaunch a pyrotechnic actuator located in the foldedtail fires to erect and latch the tail. The entire verti-cal tail pivots on a metallic shaft for yaw control.The electro-mechanical rotary yaw actuator is lo-cated inside the aft fuselage. The Bomb Impact As-sessment (BIA) antenna is located in the verticalfin.

BLOW OFF WEDGES

Two expendable wedges are located on the under-side of each aft strake and held in place by pyro-technic retention pins. The wedges insure the mis-sile makes a clean separation from the aircraft andare jettisoned from the missile after a fixed delayfollowing launch. Wedge separation occurs afterwings are deployed.

WARHEAD

The WDU-42/B warhead provides the hard targetpenetration, detonation, and blast/fragmentationdamage capabilities for the JASSM. The warheadconsists of the loaded case, containing PBX(AF)-757insensitive munition fill, and an FMU-156/B fuze.The warhead is capable of penetrating and defeat-ing hardened underground facilities as well as de-stroying soft targets. Arming power is provided onlyfrom the JASSM engine alternator. The FMU-156/Bis a programmable fuze. The fuze is installed in theaft well of the warhead case and secured with a re-taining ring. The FMU-156/B modes of operationare BIT, arm, impact fire and command fire. Thecommand fire delay times are instantaneous, 10, 1520, 30, 40, 50 and 120 milliseconds. Fuze settingsare established during mission planning and can bechanged in flight.

FUEL SYSTEM

Fuel (JP-10) is carried in four fuselage fuel tanksmade of aluminum. The fuel system distributes fuelfrom the tanks to the engine, transfers fuel betweentanks, and vents the tanks during filling. The fueltanks are pressurized by engine bleed air duringmissile powered flight. Fuel from the tanks is fed tothe fuel pump where pressure is boosted to thepressure level required by the engine for enginestart.

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1-6 Change 1

ENGINE

A Teledyne turbojet powers the vehicle. The flushlower surface mounted inlet has full line of sightblockage. The nozzle also provides for an ejectorflow to aid engine compartment cooling. A pyrotech-nic cartridge starts the engine. The engine has avariable throttle for optimal cruise or airspeed con-trol to meet the time on target requirement.

AIR DATA SYSTEM

The air data system is composed of an Air DataProbe (ADP), one Flush Static Port (FSP), and re-lated sensor cards as part of the avionics package.

The air data system is equipped with anti-ice heat-ers on both the ADP and FSP. Weapon (115VAC)power for missile loaded locations applies warmuppower to these heaters. Warm-up time may take upto 13 minutes depending on ambient temperature.The heaters remain on as long as 115 VAC power isapplied. Temperatures for these heaters can reach250 degrees F. Heaters are on during any WIU op-erations.

Without proper warm-up time, icing can de-grade the missile pitot-static system suchthat mission failure could occur. Ensure theJASSM heater power is applied (WIU ON)at least 15 minutes prior to launch. If icingconditions are encountered prior to 15 min-utes of heater operation, then a minimumwarm-up time of 30 minutes is requiredprior to launch.

AVIONICS

The JASSM Avionics consists of the Missile ControlUnit (MCU), Seeker Assembly, JASSM Anti-jamGlobal Positioning System Receiver (JAGR or JAGR-S), and associated antennas. The seeker assemblyconsists of the gimbaled IR imaging sensor and IMU.

Missile Control Unit (MCU)

The MCU provides electrical power distributionalong with centralized communication, timing, con-trol and processing for the operation of the missile,and generates telemetry data. Its functional ele-ments consist of a squib and power distributionCCA, a system interface and processing CCA, andactuator control CCA; and air data transducer as-sembly; a BIA transmitter; and an ElectromagneticInterference (EMI) filter assembly.

IR Seeker Assembly

The IR seeker assembly consists of a dual axis line-of-sight gimbal assembly, a sensor assembly; optics,reference wheel assembly; a squib activated gasbottle for cooling the sensor to cryogenic tempera-tures; and an Inertial Measurement Unit (IMU).The IMU is attached to the seeker assembly to en-sure dynamic alignment.

JASSM Anti-Jam Global Positioning System Receiver(JAGR) and JAGR-S Selective Availability Anti-SpoofingModule (SAASM)

The JAGR provides the MCU with GPS measure-ment data computed from GPS satellite data col-lected in a jamming environment. Critical functionsperformed by the JAGR include: acceptance of init-ialization data, acceptance of inertial aiding datafrom the MCU, receiving GPS satellite and jammersignals from the antenna, minimization of the jam-mer to GPS signal ratios, satellite selection, GPSreceiver control, computation of GPS data, and BIT.

The JASSM Anti-Jam GPS Receiver-SAASM (JAGR-S) is a high fidelity Anti-Jam GPS receiver. Itachieves its Anti-Jam performance through the in-tegration of a multi-channel analog RF Front End,the implementation of Space-Time Adaptive signalprocessing algorithms in digital nuller/front beam-former electronics and GPS measurement algorithmsin a digital receiver back-end. The JAGR-Ss criticaltask is to provide GPS satellite line-of-sight (LOS)Range and Delta-range measurements to the Naviga-tion functions algorithms in the MCU. In order toprovide these measurements, the JAGR-S receivesPosition, Time and Velocity Initialization data and in-ertial aiding data from the MCU and tracks GPS sat-ellite signals from the GPS satellite through a Con-trollable Radiation Pattern (CRPA) antenna. In thecase of operation in a jamming environment, the digi-tal beamformer/nuller adaptively and dynamicallynulls signals in the direction of the jammers while si-multaneously steering multiple higher gain produc-ing signal reception beams in the known directions ofthe GPS satellites. This provides interference-freeLOS measurements to the MCU’s navigation func-tion.

Bomb Impact Assessment (BIA) System

The BIA system’s primary function is to transmitmissile terminal engagement status and missilehealth data just prior to target impact. The trans-mitter provides 25 watts of output power and is ca-pable of transmitting data at 2400 Bps rate to aline-of-sight airborne platform such as the RC-135(RIVET JOINT) aircraft. The BIA transmitter isconnected to an antenna mounted in the tail for tac-tical operation. The BIA begins sending repeatedmessages approximately 10 seconds prior to impact.

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1-7

JASSM SUSPENSION SYSTEM

JASSMs are carried externally on CEM modifiedwing pylon weapon suspension assemblies whichare attached to the wing pylon adapter. Up to 6JASSMs can be carried on each B-52 wing pylon.Figure 1-2 illustrates the JASSM suspension sys-tem.

Each suspension assembly consists of the following:Stub Pylon (Modified Wing Pylons)Heavy Stores Adapter Beam (HSAB)MAU-12 Ejector Racks (6 JASSM)

The HSAB is attached to the stub pylon on each wingand houses the wire harnesses for missile control andrelease. The adapter beam has provisions for carrying6 JASSMs on stations 1, 2, 3, and 6, 7, 8.

The MAU-12 ejector rack (figure 1-3) is used to sus-pend and release the missiles. Each rack isequipped with two hooks and four sway braceswhich hold and support the missile. Two ejectorfeet, one near each hook between each pair of swaybraces, ejects the missile when release is comman-ded. The rack has provisions for a ground safetylockpin and an inflight safety lock. An extensionhas been added to the rack which contains the um-bilical restraint. This restraint is a cable which

holds the umbilical cable in position to help ensurea clean missile separation when the missile is re-leased. Electrical circuits to the inflight safety lockare available but not used. Therefore, a bolt withnut is installed in the inflight safety lockout pinhole of each MAU-12 rack. The ground safety lock-pin is used to prevent operation of the racks whileon the ground.

JASSM COVER

The missile is covered with an environmental cover,whenever it is outside the shipping and storage con-tainer, which includes when loaded on externalstores stations for ground alert and other “extendedperiods”. The environmental cover serves to protectair data probe ports, static ports, and engine open-ings from dirt, debris and any other hazards thatmay be the result of poor environmental conditions.The environmental cover is required, due to war-ranty considerations.

The effects of environmental contaminationon weapon reliability and accuracy are un-known.

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1-8

Heavy Stores Adapter Beam JASSM Configuration

Figure 1-2

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MAU-12 Ejector Rack With Extension

1 INFLIGHT SAFETY LOCKOUT PIN2 QUICK RELEASE PIN3 LANYARD CHANNEL4 QUICK RELEASE PIN5 UMBILICAL RESTRAINT A HOLE6 UMBILICAL RESTRAINT B HOLE

7 UMBILICAL RESTRAINT C HOLE8 CAMLOCK FASTENER9 LEFT PLATE ASSEMBLY

10 FORWARD CABLE LANYARD11 UMBILICAL CABLE LANYARD12 CENTER CHANNEL ASSEMBLY

Figure 1-3

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Change 2 1-11

PART 2 - OFFENSIVE AVIONICS SYSTEM

OFFENSIVE AVIONICS SYSTEM (OAS) INTERFACE

Less [AMI] The B-52 Integrated ConventionalStores Management System (ICSMS) provides OAScontrol for release of JASSM. The ICSMS opera-tional computer program consists of a GroundMaintenance Computer Program (GMCP) andFlight Computer Program (FCP). The GMCP is notdiscussed. The FCP consists of the Flight Manage-ment System (FMS) and JASSM Stores Manage-ment Overlay (JASSM SMO). For further informa-tion regarding ICSMS and basic SMO functions, re-fer to INTEGRATED CONVENTIONAL STORESMANAGEMENT SYSTEM, T.O. 1B-52H-1-12.

Less [AMI] The JASSM SMO software controlsJASSM functions. The Navigation and Weapon De-livery (NAWD) ACU executes the navigation andweapon delivery functions for the SMO. The Con-trols and Displays (CAD) ACU executes the controlsand displays function along with a majority of theBIT (Built In Test) processing.

[AMI] The B-52 OAS provides control for program-ming and release of JASSM. The operational com-puter program consists of a Ground MaintenanceComputer Program (GMCP) and Flight ComputerProgram (FCP). The GMCP is not discussed. TheFCP consists of the Flight Management System(FMS), Common Stores Processing (CSP), andJASSM Stores Management Overlay (JASSMSMO). For further information regarding OAS andbasic SMO functions, refer to T.O. 1B-52H-1-12.

[AMI] The OAS provides the capability for control-ling and monitoring more than one type of weaponsystem at a time. This is accomplished by the CSPand loading multiple weapon SMOs. Currently, onlythe CALCM SMO may be loaded with the JASSMSMO. With the CALCM and JASSM SMOs loaded,MIU/WIU power, environmental conditioning andmonitor capabilities are available to all the CALCMand JASSM weapons. However, all other weaponfunctions are available only to those weapons con-trolled by the Primary SMO.

NOTE

• [AMI] With JASSM designated as the Pri-mary SMO (CF-62x), all JASSM weaponfunctions are available. The JASSM can bepowered, aligned, monitored, targeted,ranged, launched and jettisoned (throughOAS).

• [AMI] If the JASSM SMO is not the Prima-ry SMO, only WIU power, heating and mon-itoring functions (FRMT 7A, 7C and 77) areavailable for the missiles.

• [AMI] If the JASSM SMO is not the Prima-ry SMO and a mission planned JASSMlaunch point is 30 minutes away, a JASSMEVENT advisory message will be displayed.

• [AMI] If the JASSM SMO is not the Prima-ry SMO and a mission planned JASSMlaunch point is 25 minutes away, a JASSMEVENT master fault will be displayed.

OAS/WEAPON SYSTEM RELATED CONTROLS AND DISPLAYS

Operator controls and displays for weapon releasesystem control are located at the pilots’ and naviga-tors’ stations. The munitions consent panel is lo-cated at the pilots’ station. The Weapon ControlPanel (WCP), OAS Power Control Panel (OASPCP), keyboards, MFD, and computer control panelare located at the navigators’ station. See figure 1-4for OAS/weapon data flow.

Weapon Control Panel

The Weapon Control Panel (WCP) (figure 1-5), lo-cated on the navigator’s front panel, provides con-trols for missile power application, missile powerremoval, missile jettison, or missile abort. Missilesare selected with the LOCATION (LP and RP) andSTATION (1, 2, 3, 6, 7, 8, and ALL) switches. TheWCP station switches are enabled only when one orboth pylon locations have been selected. If no loca-tion is selected when either the ALL station switchor an individual station switch has been selected,the advisory message LOCATION?? will be dis-played on each MFD. If the bay location is selectedthe advisory B: LOCATION will be displayed oneach MFD. If an invalid station (4 or 5) is selected,the advisory Less [AMI] STATION??, [AMI]JASSM STATION?? will be displayed on each MFD.

T.O. 1B-52H-34-2-8

1-12 Change 2

WEAPON CONTROL PANEL ABNORMAL PROCEDURES

An advisory WCP on the MFD indicates malfunc-tion on the WCP. The operator will use CF-E (figure1-26) to back up actions accomplished on the WCP.This will allow the operator to work around certainfailures of the WCP and OAS PCP.

NOTE

With a total WCP failure prior to accom-plishing hardwired function, (LOCK-UN-LOCK) missile release is not possible.

CF-E may be used in conjunction with an opera-tional WCP and OAS PCP to operate the system.The operators may use keyboard entries to performfunctions mechanized on these panels at any timeregardless of the panels go/no-go status. The OASwill treat the keyboard command as if it had origi-nated from the WCP or OAS PCP. The lock-unlockfunction is not available on the CF-E backup. Thedisplay is laid out in basically the same arrange-ment as the panel. To accomplish a backup actionfor the malfunctioning panel switch, the operatorenters CF-E and the symbols associated with theswitch on the keyboard in the same sequence thatnormal switch operation would occur. See CF-E thissection for further discussion of the CF-E functions.

Pilot’s Munitions Consent Panel

The pilot’s munitions consent panel (figure 1-6) con-tains the PREARM-OFF and LOCK-UNLOCKswitches. The panel provides unlock consent forpowering the weapon ejectors. The PREARM func-tion of the pilot’s switch is not used with JASSM.The LOCK-UNLOCK switch is guarded in theLOCK position.

OAS Power Control Panel

The OAS Power Control Panel (PCP) (figure 1-7) lo-cated on the navigators’ front panel provides powercontrol for the OAS and the WIU (Weapon InterfaceUnit). All legends are backlighted green whenpower is on. The MIU switches which commandpower to the WIU are alternate action pushbuttons

and will remain latched if the WIU loses power or isshut down by the OAS. The light in the switch issoftware controlled and will go out when WIUpower is removed regardless of switch position. Toreapply power to the WIU when they have beenshut down by other than the operator, the switchmust be pressed and released to reset the switchand then pressed a second time to reapply WIUpower. If PCP switches malfunction, the navigatoror radar navigator can select CF-E which providesa display of the PCP switches.

Keyboard

The keyboards (figure 1-8) located at the naviga-tor’s and radar navigator’s stations, provide inter-face with the control of the OAS and weapon sys-tem. The keyboard and MFD provide operator in-terface with the missiles through the selection offormat (FRMT), control function (CF), program(PRGM), and modify (MDFY) commands. The selec-tion of FRMT results in the display of a specificOAS and missile data presentation on the selectedMFD. Control function selection results in displayof a specific OAS data display or initiates the entryinto a specific operating mode. If WCP switchesmalfunction, the navigator or radar navigator canselect CF-E which provides a display of the WCPswitches and the MIU power switches.

IKB commands associated with the JASSM arelisted in figure 1-9.

MULTIFUNCTION DISPLAYS

The multifunction display (MFD) (figure 1-10) is aCRT display unit. The MFD displays scan con-verted radar video, electro-optical viewing system(EVS) video, and alphanumeric mission data. TwoMFDs are located at the navigator’s station and twoat the radar navigator’s station.

MFD DISPLAY FIGURES

In the MFD display figures in this T.O., the itemsmodifiable by the operator or the SMO are repre-sented in the display explanations as lower case(non-capital) letters. The labels which are not modi-fiable are presented in all capital letters.

T.O. 1B-52H-34-2-8

Change 2 1-13

Missile Data Flow (Typical)

Figure 1-4

T.O. 1B-52H-34-2-8

1-14

Weapon Control Panel

NAVIGATOR’S FRONT PANEL

Figure 1-5 (Sheet 1 of 2)

T.O. 1B-52H-34-2-8

Change 2 1-15

NO. CONTROL/INDICATOR FUNCTION

1 WPN JETTISON SEL (Weap-on Jettison Select) Switch

Spring-loaded to NORM (off) position. Used with unlock consent from pilot’sweapon consent panel and WCP NUCLEAR LOCK-UNLOCK switch.

SEL – Jettisons missiles selected on location and station switches.

2 STATION Switches Used with location switches to select individual pylon weapon stations 1 thru8 (4 and 5 not used) or all (ALL) stations at the selected location for missile op-erational functions

3 WPN PWR (Weapon Power)Switch

Three position, spring-loaded to neutral (N).

ON – Commands power be applied to the missiles selected by the location andstation switches on the WCP.

OFF – Commands power be removed from the missiles selected by the WCP.

4 LAMP TEST Switch When pressed all panel lights will come on.

5 MSTR (Master FAULTLight

Indicates a fault has occurred. More information is available on the MFD.Pressing acknowledges receipt of message, turns light off, and erases mes-sage.

6 MISSILE MAN LNCH (ManualLaunch) Switch

In manual launch mode, pressing the switch commands launch of the selectedJASSM at the current JASSM launch point or the currently selected direct tar-get. If no launch point/direct target is selected or the selected missile is notready for launch the command is ignored. The light in the switch comes onwhen the command is accepted and goes out on completion of the launch se-quence.

NOTE

For JASSM, deselecting the MISSILE MAN LAUNCH duringmanual launch sequence will result in an abort.

7 MISSILE LNCH MODE(AUTO/MAN) Switch

The switch selects Automatic (AUTO) or Manual (MAN) missile launch mode.The system is initialized in MAN.

NOTE

Switching the MISSILE LAUNCH MODE switch from AUTO toMAN during the launch countdown may result in an abort.

8 LOCATION Switches Used with station select switches to select missiles for missile operation functions.

LP (Left Pylon) – Selects left pylon missiles.

RP (Right Pylon) – Selects right pylon missiles.

BAY (Bay) – Non functional with JASSM.

9 NUCLEAR LOCK-UNLOCKSwitch

Guarded two position switch used with pilot’s consent to apply power to weap-on interface unit to allow operation of the ejectors for release or jettison.

NOTE

In SIM Mode a momentary UNLOCK CONSENT message will bedisplayed each time the NUCLEAR LOCK-UNLOCK switch ispositioned. The message will clear automatically.


T.O. 1B-52H-34-2-8

1-16

Pilot’s Munition Consent Panel

PILOT’S SIDE PANEL

Figure 1-6

T.O. 1B-52H-34-2-8

1-17

OAS Power Control Panel

NAVIGATOR’S FRONT PANEL


1 LAMP TEST Switch Tests all lights on the Power Control Panel.

2 Weapon Interface UnitSwitches (3)

MIU/LP – Commands power to the left pylon weapon interface unit.MIU/BAY – Not used for JASSMMIU/RP – Commands power to the right pylon weapon interface unit.

3 MASTER POWER Switch ON (light on) – Sends master power to:• OAS• WEAPON CONTROL PANEL• ARMAMENT INTERFACE UNIT (AIU)• Enable MIU POWER switches

For all other functions, refer to the applicable flight manual.

Figure 1-7

T.O. 1B-52H-34-2-8

1-18

Integrated Keyboard (IKB)

MISSILE RELATED KEYS AND SWITCHES


1 0 – 9 Keys Enter the respective number in the data/command to be transferred. Whenused in conjunction with upper corner key, gives N, S, E, W, +, –, and comma(,).

2 ENTER Key Completes the operator sequence. When pressed, data/commands will betransferred to OAS and displayed on MFD.

3 Message (MSG) Switch Acknowledges an existing message after being displayed on all four MFDs.

4 A – F Keys Enter respective letter in data/command to be transferred.

5 Return (RTN) Key Places the MFD cursor to the first operator-changeable position in the row des-ignated.

6 Backspace (←) and Advance(→) Keys

Keys move the cursor on the MFD to the left and right respectively.

7 Upper Corner (UC) Key When pressed, the number keys enter the symbols in the upper left corner ofthe key.

8 Display Select Keys (4) PRGM displays current event program or selected event program.

CF displays OAS mode supervision menu or initiates entry into specific OASmode.

MDFY initiates operator changes to MFD displayed data.

FRMT displays video and/or data.

9 L MFD and R MFD SelectionSwitches

Select either MFD for display of data inputs from the keyboard.

Figure 1-8

T.O. 1B-52H-34-2-8

Change 2 1-19

JASSM IKB CommandsCOMMAND DESCRIPTION

ADVISORY ACKNOWLEDGMENT

MSG Control Function Menu Request

COMMAND MENU DISPLAY REQUESTS

CF- Control Function Menu Request

CF-5 Weapon Supervision Menu Request

CF-5A [AMI] JASSM Supervision Menu (CF-57) Request for Left Pylon (All JASSM SMO Controlled Locations)

CF-5C [AMI] JASSM Supervision Menu (CF-57) Request for Right Pylon (All JASSM SMO Controlled Locations)

CF-57 JASSM Supervision Menu Request

CF-58 JASSM Targeting Menu Request

CF-6 FCP Supervision Menu Request

CF-62 SMO Load Menu Request

CF-8 Mission Supervision Menu Request

CF-82 [AMI] Weapons Load Menu Request

CF-82A [AMI] Weapon Group Load Menu (Left Pylon)

CF-82C [AMI] Weapon Group Load Menu (Right Pylon)

CF-E Weapon Control Panel Backup Display Command

FRMT- Format Menu Request

SYSTEM STATUS DISPLAY REQUESTS

CF-DB [AMI] Display Previous Weapon Assignment Data (from FRMT-7, 7A, or 7C)

CF-DF [AMI] Display Next Weapon Assignment Data (from FRMT-7, 7A, or 7C)

FRMT-6 PME Status Display Request

FRMT-7 JASSM Status and Inventory Display Request

FRMT-7A [AMI] JASSM Status and Inventory Display Request (Left Pylon - All JASSM SMO Controlled Locations)

FRMT-7C [AMI] JASSM Status and Inventory Display Request (Right Pylon - All JASSM SMO Controlled Locations)

FRMT-7xy JASSM Status and Inventory with Selected Station xy Display Request

FRMT-77 [AMI] Stores Summary Display Request

PRGM- Program Display Request

PRGM-nn Destination View Command for Destination nn

PRGM-Dn Direct Target Selection Command for Direct Target n

DESTINATION AND TARGETING DISPLAY REQUESTS

CF-586 Missile/Target Assignment Request (Manual Targeting)

CF-588,n Direct Target Definition Display Request For Direct Target n

CF-Dn Copy Current Direct Target to Direct Target n

CF-DB Display Previous Weapon Summary (FRMT-12)

CF-DF Display Next Weapon Summary (FRMT-12)

FRMT-12 Display Weapon Summary

FRMT-10,nn Destination Table Display Request

FRMT-12,nn Missile Summary Display Request for Launch Point nn

FRMT-12,Dn Direct Target Missile Summary Display Request for Direct Target n


T.O. 1B-52H-34-2-8

1-20 Change 2

JASSM IKB Commands (Cont)

COMMAND DESCRIPTION

SENSOR DATA REQUESTS

FRMT-1 Radar Display Data Request

FRMT-2 Radar with PMD Display Data Request

FRMT-4 EVS Display Data Request

FRMT-5 EVS Full Display Data Request

SYSTEM CONTROL COMMANDS

CF-50 STRIKE Mode Command

CF-51 [AMI] PART SIM Mode Command

CF-52 FULL SIM Mode Command

CF-57A Telemetry ON Command for Selected Missile(s) (Flight Test Only)

CF-57B Telemetry OFF Command for Selected Missile(s) (Flight Test Only)

CF-57C,xy Flight Termination System (FTS) Enable/Disable Command for Missile xy (Flight Test Only)

CF-57D FTS Power Source Command (Flight Test Only)

CF-57E,xy TXA (Transfer Alignment) Halt Command for Missile xy (Flight Test Only)

CF-57F,xy TXA (Transfer Alignment) Re-Initialize Command for Missile xy (Flight Test Only)

CF-571 Go/No-Go Test Command (Maintenance Only)

CF-572 SIT Command (Maintenance Only)

CF-575 Classified Data Erase Command For Selected Missiles

CF-580 [AMI] Auto Target Enable/Disable

CF-589 Retarget-all Command

CF-62,n Less [AMI] SMO Load Menu

CF-62x [AMI] Primary SMO Selection by Location x

CF-65 SMO Mission Event Recording Command

CF-66 Clear PME Faults Command

CF-67 OAS Shutdown Command

CF-68 ECU Fault Override Command

CF-81,n Read B-52 Sortie Mission Data Command

CF-82,nn [AMI]

CF-82,n [AMI]Select Weapon Group

TARGETING PROCESS COMPLETION COMMANDS

PRGM-Dn Target Selection Command for Direct Target n

CLR-D Selected Weapon Event Deselection Command

TARGETING PROCESS COMPLETION COMMANDS

CF-DD Download Data to Selected Missiles for Targeting

CF-DE Exit Without Downloading Data

MODIFY DATA COMMANDS

MDFY-n Modify Line Identified by Number n


T.O. 1B-52H-34-2-8

1-21

Multifunction Displays

TYPICAL MFD RADAR NAVIGATOR’S AND NAVIGATOR’S FRONT PANELS

CRITICAL DESIGNATION/RELEASE EVENT DATAOR

OAS SUPERVISORY MENUS, MISSION DATA TABLES,AND WEAPON/PME STATUS

OAS ADVISORY DATA AREA

KEYBOARD DATA INPUTSMASTER FAULT MESSAGES NUCLEAR CAUTION MESSAGE PME FAULT MESSAGES

QUESTIONS REQUIRING YES – NO RESPONSEOAS ADVISORY MESSAGES AND SELECTED WEAPON STATION STATUS

PRIME MISSION DATA (PMD)

GENERAL DISPLAY ARRANGEMENT

Figure 1-10

T.O. 1B-52H-34-2-8

1-22 Change 3

WEAPON JETTISON

Weapon jettison for JASSM SMO controlled weap-ons is accomplished by one of three methods: thenavigator’s weapon jettison select switch on theWCP, the Alternate Jettison Control Panel (AJCP)at the navigator’s station or the pilots’ Bomb Bayand Missile Jettison Control switch. All methods re-quire unlock consent.

Less [AMI] The OAS must be operational with theJASSM SMO loaded and WIU power must be on forjettison of JASSMs when using the WCP or the pilots’switch.

[AMI] The OAS must be operational with theJASSM SMO loaded and selected as the PrimarySMO and WIU power must be on for jettison ofJASSMs when using the WCP or the pilots’ switch.

Only weapons for the SMO loaded will be jetti-soned. (i.e. if JASSMs are being carried externally,and CALCMs on the CSRL internal, only the weap-ons of the loaded SMO will be jettisoned). This doesnot apply to jettison mixed loads with 1760 andGWD SMO weapons, as GWD SMO weapon re-leases/jettisons are not WIU/SMO controlled.

Less [AMI] With OAS or WIU off, or a SMO otherthan the JASSM SMO loaded, jettison of JASSMscan only be accomplished using the AJCP.

[AMI] With OAS or WIU off, or a SMO other thanthe JASSM SMO loaded as the Primary SMO, jetti-son of JASSMs can only be accomplished using theAJCP.

The pilots’ Bomb Bay and Missile jettison switchhas the same effect as if all locations and all sta-tions were selected on the WCP and then the WPNJETTISON switch was selected.

Circuit breakers applicable to weapons jettison arecontained in figures 1-11 and 1-12.

• The pilots’ Bomb Bay & Missile JettisonControl switch jettisons all GWD and ac-tive/primary SMO controlled weaponsloaded on the aircraft and will only be usedas a backup to jettison by the Radar Navi-gator. If jettison is commanded using the pi-lots’ Bomb Bay & Missile Jettison Controlswitch, all GWD weapons and, with OASoperating and MIUs/WIUs powered, all ac-tive/primary SMO controlled weapons willbe jettisoned. Proper separation clearance

between weapons and between weaponsand aircraft cannot be ensured.

• The JASSM SMO has no interlocks prevent-ing jettison on the ground. With unlock con-sent, and power applied to the OAS and theWIU, actuation of jettison switches while onthe ground will result in weapon jettison.

• For OAS controlled weapons, if the blockingdiode in the jettison system fails, the RadarNavigator ’s Bomb Bay Jettison Controlswitch will function in the same manner asthe pilot’s Bomb Bay & Missile jettisonswitch. Normally, the radar navigator ’sBomb Bay Jettison Control switch is excludedfrom operation with the SMO. A blockingdiode prevents signal travel between the ra-dar navigator’s switch and the OAS. If thediode fails, the signal will be sent through theOAS to both internal and external weapons.The only method to determine if this diodehas failed is to perform a jettison test usingthe radar navigators switch and monitoringthe weapon stations for a jettison signal.

• If an OAS reconfiguration occurs duringJASSM jettison, the jettison command will beretained and the jettison will continue afterreconfiguration.

• If there is a retained/HUNG center stationstore, launching/jettisoning an adjacentshoulder station may result in a Store-to-Store contact. When a center station storeis retained/HUNG, operators will retain theadjacent shoulder station stores.

OAS Commanded Jettison

The preferred method of jettison for SMO controlledweapons uses the OAS and the JASSM SMO throughthe LOCATION/STATION switches and the WEAP-ON JETTISON SEL switch on the Weapon ControlPanel (figure 1-5) to selectively jettison weapons.CF-E Weapon Control Panel Backup display (Figure1-26) can also be used for selective jettison.

AJCP Commanded Jettison

The second method of jettison for JASSMs uses theAlternate Jettison Control Panel (AJCP) located atthe navigator’s station, figure 1-13. The AJCP allowsselective jettison of JASSMs without the OAS opera-tional, when a SMO other than the JASSM SMO isloaded ([AMI] as the Primary SMO), or when WCPjettison is not possible. The AJCP will selectively jet-tison the missiles, one at a time.

T.O. 1B-52H-34-2-8

1-23

The AJCP has no interlocks preventing jet-tison on the ground. With unlock consentand power applied to the aircraft, actuationof AJCP switches while on the ground willresult in weapon jettison.

NOTE

The OAS SMOs cannot detect AJCP jettisoncommands and interprets the commands asuncommanded EED power available faults.Therefore if the AJCP is used for jettisonwith the SMO loaded, the SMO will inter-pret the command as a fault and removeWIU power at the affected station.

Circuit Breaker Panels

RIGHT FORWARD BNS CIRCUIT BREAKER PANEL

Figure 1-11

Circuit Protection

CIRCUITBREAKER

NOMENCLATUREAMPERERATING LOCATION TYPE FUNCTION

WEAPONSJETTISON

JETTISON POWER 15 Right fwd BNSoverhead CBpanel

DC Pilot’s jettisonswitch power

JETTISON CONTROL 10 Right fwd BNSoverhead CBpanel

DC Pilot’s jettisonswitch power

Figure 1-12

T.O. 1B-52H-34-2-8

1-24

Alternate Jettison Control Panel

The AJCP has no interlocks preventing jettison on the ground. With unlock con-sent, actuation of AJCP switches while on the ground with power applied to theaircraft will result in weapon jettison.


1 POWER and STORES Jettison Light

Two part light:

PWR – Comes on when the pylon power (No. 2) switch is placed to either LEFTor RIGHT indicating power is applied to the AJCP.

JET – Comes on when any jettison switch (No. 3) is placed up to commandjettison.

2 PYLON POWER Switch Applies Jettison power to the selected pylon.

3 JETTISON Switch (8) Switches 1 thru 8 command jettison at the respective HSAB ejector location.

Figure 1-13

T.O. 1B-52H-34-2-8

Change 3 1-25

PILOTS’ BOMB BAY & MISSILE JETTISON CONTROLSWITCH COMMANDED JETTISON

Jettison using the pilots’ Bomb Bay and Missile jet-tison switch (figure 1-14) should be used only if jet-tison by the other methods is not possible. Pressingthe pilots’ Bomb Bay & Missile jettison controlswitch jettisons all weapons on the aircraft. ForOAS SMO controlled weapons the OAS must be upand running ([AMI] with the JASSM SMO loadedas the primary SMO) with the WIU powered for jet-tison of JASSM with this switch. The JETTISONPOWER and JETTISON CONTROL circuit break-ers on the Right Forward BNS circuit breaker panelmust be in for the pilots’ jettison switch to function.

• The pilots’ Bomb Bay & Missile JettisonControl switch jettisons all GWD and ac-tive/primary SMO controlled weaponsloaded on the aircraft and will only be usedas a backup to jettison by the Radar Navi-

gator. If jettison is commanded using the pi-lots’ Bomb Bay & Missile Jettison Controlswitch, all GWD weapons and, with OASoperating and MIUs/WIUs powered, all ac-tive/primary SMO controlled weapons willbe jettisoned. Proper separation clearancebetween weapons and between weaponsand aircraft cannot be ensured.

• The JASSM SMO has no interlocks pre-venting jettison on the ground. With unlockconsent, and power applied to the OAS andthe WIU and ([AMI] with the JASSM SMOloaded as the primary SMO), actuation ofthe pilots’ Bomb Bay & Missile jettison con-trol switch while on the ground will resultin weapon jettison.

• If there is a retained/HUNG center stationstore, launching/jettisoning an adjacentshoulder station my result in a Store-to-Store contact. When a center station storeis retained/HUNG, operators will retain theadjacent shoulder station stores.

Jettison Control Switches


T.O. 1B-52H-34-2-8

1-26

Jettison Control Switches (Cont)


RADAR NAVIGATOR’S BOMB BAY JETTISON CONTROL (Cont)

1 BOMB BAY Jettison ControlSwitch

The jettison switch is a button type with unmarked jettison and off positions withthe depressed position being jettison. The switch is spring-loaded to OFF posi-tion and is recessed in the panel to discourage inadvertent actuation. Momen-tary actuation of the switch to RELEASE position for non OAS Controlledweapons will energize the jettison circuits.

Power is supplied by means of aft battery power through circuit breakersmarked JETTISON CONTR and JETTISON PWR on the right forward BNScircuit breaker panel. When the jettison circuits are energized, the bomb dooropen circuits will be energized and if unlock consent is present, all the weap-ons (internal and external) will be released in a safe configuration. The bombdoors will be held open while the jettison circuits are energized.

For OAS controlled weapons (nuclear and SMO controlled) the switch will notfunction. If the blocking diode in the switch’s jettison circuits has failed, theswitch will send a jettison signal to the OAS. If OAS receives this signal, withOAS and WIU power on, all weapons at powered locations will be jettisoned.

2 INTERNAL STORES RELEASE Light

Store jettisoned lights come on while the jettison circuit is energized. Powersource for the lights is the same as for the jettison switches.

PILOTS’ BOMB BAY & MISSILE JETTISON CONTROL

3 BOMB BAY & MISSILE Jettison Control Switch

The jettison control switch is a button type with unmarked jettison and off posi-tions with the depressed position being jettison. The switch is spring-loadedto off position and is recessed in the panel to discourage inadvertent actuation.Momentary depression of the switch for non OAS controlled weapons will jetti-son weapons at all locations.

For OAS controlled weapons the switch will send a jettison command to OAS.If OAS is operating, OAS will respond to the jettison command by sending ajettison all command to those locations with powered WIUs.


T.O. 1B-52H-34-2-8

Change 2 1-27

PART 3 - JASSM SMO SOFTWARE

The OAS controls the programming and launch orrelease of JASSMs using the flight computer pro-gram (FCP). The FCP consists of the flight manage-ment system (FMS) and stores management over-lay (SMO) and [AMI] Common Stores Processing(CSP). The FMS controls navigation, radar, controlsand displays, and supports the JASSM SMO. TheJASSM SMO contains all weapon control deliveryfunctions required with JASSMs. [AMI] The CSPincorporates common stores/weapon capabilitiesand provides multi-SMO operation. The SMO menucan be displayed to allow the operator to select theappropriate SMO. Up to 10 SMOs can be listed oncontrol function CF-62, the SMO Load Menu.

Functions performed by the SMO include weaponcontrol processing, simulation processing, and con-trols and displays processing. To perform its re-quired functions, the SMO interfaces with existingaircraft weapon system components, the OASsources of navigation, steering, controls and dis-plays processing, mission data, and with the globalpositioning system (GPS) hardware.

• [AMI] With JASSM designated as the PrimarySMO (CF-62x), all JASSM weapon functions areavailable. The JASSM can be powered, aligned, moni-tored, targeted, ranged, launched and jettisoned.

• [AMI] When the CALCM and the JASSM SMOsare loaded at the same time, CALCM will be automat-ically selected as the primary SMO by the OAS.

• [AMI] If the JASSM SMO is not the PrimarySMO, only WIU power, heating and monitoringfunctions are available for the missiles.

• [AMI] If the missiles are targeted with theJASSM SMO primary, the missiles will retain thetargeting information while the JASSM SMO is sec-ondary.

• [AMI] If the JASSM SMO is primary, settingthe JASSM SMO to secondary will be inhibited ifweapon power is on or if any process is active thatcannot be accomplished in the secondary SMOmode.

SMO MFD DISPLAYS

Displays can be requested on each MultifunctionDisplay (MFD) which contain SMO data and areused to interface with the operator for JASSM op-erations. Several of the displays are defined andupdated primarily by the FCP for which the SMOprovides additional data for display. Some of thedisplays are completely unique to the SMO opera-tion for which it provides all of the data.

The display commands ending in xy (i.e. CF-57Cxy,FRMT-7xy, etc.) require an xy entry representingthe location and station of the applicable weapon.The x represents the location and is entered as Afor the left pylon and C for the right pylon. The yrepresents the station and is entered as 1,2,3,6,7, or8 for the respective JASSM Launch station.

In this manual, discussion of display items/keyboardentries has been standardized. If numbers or capitalletters are shown on a display, they are as actuallydisplayed on the MFD. Lower case (small) letters in-dicate variable entries. An a is an alphabetical entry,an n is a number, mm:ss are minutes and seconds, ddare degrees, xy is station/location, etc.

The following displays are affected wholly or in partby the SMO:

• All Displays Release Advisory Display.• CF Control Function.• CF-5 Weapon Supervision Menu.• CF-5A [AMI] Weapon Supervision

Menu (Left Pylon).• CF-5C [AMI] Weapon Supervision

Menu (Right Pylon).• CF-57 JASSM Supervision Menu.• CF-58 JASSM Targeting Menu.• CF-586 Weapon/Target Assignment

(manual targeting) Display• CF-588,n Direct Target Definition

Display for Target n.• CF-6 FCP Supervision Menu.• CF-62 SMO Load Menu.• CF-8 Mission Supervision Menu.• CF-82 [AMI] Weapons Load Menu.• CF-82A [AMI] Weapons Group Load

Menu (Left Pylon).• CF-82C [AMI] Weapons Group Load

Menu (Right Pylon).• CF-E WCP Backup Display.• CF-DB/DF [AMI] With FRMT-7, 7A, 7C

Displays Previous/Next WeaponAssignment Data (LP-RP).

• FRMT- Format Menu.• FRMT-1 Radar Display Data.• FRMT-2 Radar Display Data with PMD.• FRMT-4 EVS Display Data.• FRMT-5 EVS Full Display Data.• FRMT-6 PME Status Display.• FRMT-7 JASSM Status and Inventory

Display.

T.O. 1B-52H-34-2-8

1-28 Change 2

• FRMT-7A [AMI] JASSM Status andInventory Display - Left Pylon(All JASSM SMO Controlled

Locations).• FRMT-7C [AMI] JASSM Status and

Inventory Display - Right Pylon(All JASSM SMO Controlled

Locations).• FRMT-7xy JASSM Status and Inventory

Display with Selected StationStatus.

• FRMT-77 [AMI] Stores Summary Display.• FRMT-10,nn Destination Table Display.• FRMT-12,nn Weapon Summary Display.• PRGM Program Display.• PRGM-Dn Program Display

Selection for Direct Target n.• PRGM-nn Program Display for

Destination nn.

RELEASE ADVISORY DISPLAY

When weapons are declared launched, jettisoned,aborted, or hung, the Location/Station number andthe appropriate status of each affected weapon willbe shown as a Weapon Release advisory as indi-cated in figure 1-15. The Weapon Release Advisorydisplay will be shown on all MFDs that do not cur-rently have data displayed on the bottom of theMFD. Release advisories can be displayed for up to4 weapons. When more than 4 advisories are dis-played, release advisory window locations will beupdated from left to right with subsequent weaponsrelease advisories. There is no operator command to

cause the Weapon Release advisory to be displayed.The data will remain on the MFDs for five secondsafter the release or attempted release of the lastweapon in the sequence.

PRIME MISSION DATA

Less [AMI] The prime mission data (PMD) is dis-played anytime a MFD is displaying FRMT-2,FRMT-4, FRMT-5, FRMT-6, FRMT-8, FRMT-9,FRMT-10, or a PRGM display. PMD is displayedany time an MFD is displaying CF, CF-E, CF-1through CF-8, CF-61, CF-62, CF-67, FRMT,FRMT-0, or FRMT-7xy display, provided PMD waspreviously displayed. PMD is not displayed when aMFD is displaying CF-57, CF-58, CF-586, CF-588,FRMT-1 (time to go current destination only),FRMT-3, or FRMT-12 display. The SMO providesthe destination label for the current destinationwhen the destination is a JASSM initial point.

[AMI] The prime mission data (PMD) is displayedanytime a MFD is displaying FRMT-2, FRMT-4,FRMT-5, FRMT-6, FRMT-8, FRMT-9, FRMT-10, ora PRGM display. PMD is displayed any time anMFD is displaying CF, CF-E, CF-1 through CF-8,CF-57, CF-58, CF-61, CF-67, FRMT or FRMT-0 dis-play, provided PMD was previously displayed. PMDis not displayed when a MFD is displaying CF-586,CF-588, CF-62, CF-81, CF-82, FRMT-1 (time to gocurrent destination only), FRMT-3, or FRMT-12 dis-play. FMS provides the destination label for thecurrent destination. FRMT-7xy will display only thefirst line of the PMD.

T.O. 1B-52H-34-2-8

Change 2 1-29

Release Advisory Display

WINDOW DISPLAY FUNCTION

1 Location/StationIdentifier

Location and station of each weapon launched.

xy x = L for left pylon stations and R for right pylon stations.y = Station number 1, 2, 3, 6, 7 or 8.

The location and station of each weapon launched will be displayed in the nextavailable window 1 from left to right in preferred launch sequence. If release advi-sories exist for more than 4 weapons, the first 4 advisories will appear in windows1 and 2 for 5 seconds, then go to the next four weapons. The remaining advisorieswill appear after the windows will be updated from left to right with the releaseadvisories.

2 Weapon Release StatusABORTAWAY_HUNG_

JETT_

A weapon release abort occurred.The weapon was successfully launched.The weapon umbilical and/or ejector status indicate that the weapon was notreleased.The weapon was successfully jettisoned.

Figure 1-15

T.O. 1B-52H-34-2-8

1-30 Change 2

CONTROL FUNCTION (CF) DISPLAYS

Pressing the CF key on the IKB will display the CFMENU display (figure 1-17). The JASSM relatedselections from this menu are; CF-5 which com-mands display of the JASSM supervision menu,CF-6 which commands display of the FCP supervi-sion display, CF-8 MSN SUPV which commandsdisplay of the mission supervision menu, and CF-Ewhich commands display of the weapon controlpanel backup display. The JASSM CF commandsare listed in figure 1-16.

WEAPON SUPERVISION MENU (CF-5)

The Weapon Supervision Menu, commanded byCF-5, is shown in figure 1-18, and is available in allSMOs and provides four common SMO functions.The common functions are:

• Displays current SMO mode status (i.e.,STRIKE, FULL SIM and [AMI] PART SIM).

• Identifies operator commands to changebetween STRIKE (CF-50), FULL SIM (CF-52)and [AMI] PART SIM (CF-51) modes.

• Identifies the operator command to requestthe JASSM Supervision Menu (CF-57).

• Identifies the operator command to requestthe JASSM Targeting Menu (CF-58).

• [AMI] Displays the twenty-four characterSMO identifier next to the assigned location(LP, Bay and RP).

When the Weapon Supervision Menu is displayed,the current SMO mode (i.e., STRIKE, FULL SIM[AMI] or PART SIM), followed by the loaded missiontype (i.e., WAR, TLI, OTL, FERRY or CC) is dis-played, similar to the Control Function Menu (CF-).

STRIKE Mode Command (CF-50)

Operator entry of CF-50 will command the SMOfrom SIM mode into STRIKE mode. If the commandis entered while the SMO is in STRIKE mode, itwill be ignored. The SMO will reject a CF-50 com-mand and display it in reverse video if simulatedpower is applied to either WIU, Go/No-Go testoption is active, or SIT is active.

NOTE

After SIM mode is exited by commandingSTRIKE mode, the B-52 mission data andthe SMO must be reloaded to guaranteeproper operation of the system.

Less [AMI] SIM Mode Command (CF-52)

Operator entry of CF-52 will command the SMOfrom STRIKE mode into SIM mode. If the commandis entered while the SMO is in SIM mode, it will beignored. The SMO will reject a CF-52 command anddisplay the command in reverse video if any of thefollowing conditions exist:

• Power is applied to either WIU.• B-52 mission data is for an operational (WAR)

mission.• B-52 mission data is for a timeline integration

(TLI) mission.• Actual Go/No-Go test mode is active.• Actual SIT test mode is active.• 28 VDC T/R power discrepancy fault exists.• AIU Communications fault (cyclic status mes-

sage exists).

[AMI] PART SIM Mode Command (CF-51)

Operator entry of CF-51 will command the SMOfrom STRIKE mode into PART SIM mode. If thecommand is entered while the SMO is in PART SIMmode, it will be ignored. The CF-51 command willbe rejected and displayed it in reverse video if oneor more of the following conditions are true:

• The system is in FULL SIM mode.• Mission data is for an operational (strike/war)

mission or a timeline integration (TLI) mis-sion.

• Power is applied to either MIU or to anyweapon.

• Actual Go/No-Go test mode is active.• Actual System Integrity Test (SIT) test mode

is active.• 28 VDC T/R Power Discrepancy fault exists.• AIU (cyclic status message 5C23) Communica-

tion fault exists.

[AMI] FULL SIM Mode Command (CF-52)

Operator entry of CF-52 will command the the weap-on system from STRIKE mode into FULL SIM mode.If the command is entered while the SMO is in FULLSIM mode, it will be ignored. The CF-52 commandwill be rejected and displayed it in reverse video if oneor more of the following conditions are true

• The system is in PART SIM mode.• Mission data is for an operational (strike/war)

mission or a timeline integration (TLI) mission.• Power is applied to either MIU or to any

weapon.• Actual Go/No-Go test mode is active.• Actual System Integrity Test (SIT) test mode

is active.• 28 VDC T/R Power Discrepancy fault exists.• AIU (cyclic status message 5C23) Communica-

tion fault exists.

T.O. 1B-52H-34-2-8

Change 2 1-30A

JASSM Supervision Menu (CF-57)

The JASSM Supervision Menu, commanded byCF-57, is shown in figure 1-19.

When the JASSM Supervision Menu is displayed,the current OAS mode and current mission typeand the IKB commands which can be used to moni-tor and control the weapons are displayed just as onthe Control Function Menu (CF-) and the WeaponSupervision Menu (CF-5).

[AMI] Although designated for weapons on the leftand right pylons, respectively, CF-5A and CF-5Cprovide the same display as CF-57 for all JASSMSMO controlled weapons. That is, if carryingJASSM and CALCM and the CALCM SMO isprime, CF-57 is selectable, but will not be displayedon the CF-5 menu. However, CF-5A and CF-5C areselectable options and will display the JASSM Su-pervision Menu no matter which SMO is prime. Al-though the JASSM Supervision Menu is selectablewhen the JASSM SMO is not prime, none of optionson the menu are available.

The control function commands that are unique tothe SMO are of the form CF-57x, where x repre-sents any of several alphanumeric characters thatmay or may not be followed by a comma and addi-tional alphanumeric characters. The JASSM Super-vision Menu displays the control function com-mands of this form that are accepted by the SMOand the function commanded by each. [AMI] Thecontrol function commands are not unique to theJASSM SMO and thus these commands will only beacted upon if JASSM is the primary SMO.

In addition to identifying the CF-57X commands,the JASSM Supervision Menu (CF-57) also identi-fies other SMO commands, not identified on otherJASSM displays.

Telemetry Power ON Command (CF-57A), Teleme-try Power OFF Command (CF-57B), FTS Enable/Disable Command (CF-57C,xy), FTS Power SourceCommand (CF-57D), Transfer Alignment (TXA)Halt Command (CF-57E,xy), and Transfer Align-ment (TXA) Re-Init Command (CF-57F,xy) are testonly commands and are discussed in Section IV.

T.O. 1B-52H-34-2-8

1-30B Change 2

JASSM Control Function (CF) CommandsCOMMAND DESCRIPTION

CF Control Function Menu Request

CF-5 Weapon Supervision Menu Request

CF-5A [AMI] JASSM Supervision Menu (CF-57) Request for LP (All JASSM SMO Controlled Locations)

CF-5C [AMI] JASSM Supervision Menu (CF-57) Request for RP (All JASSM SMO Controlled Locations)

CF-50 STRIKE Mode Command

CF-51 [AMI] PART SIM Mode Command

CF-52 FULL SIM Mode Command

CF-57 JASSM Supervision Menu Request

CF-57A Telemetry ON Command for selected weapon(s) (Test Only)

CF-57B Telemetry OFF Command for selected weapon(s) (Test Only)

CF-57C,xy Flight Termination System (FTS) Enable/Disable Command for Weapon xy (Test Only)

CF-57D FTS Power Source Command (Test Only)

CF-57E,xy TXA (Transfer Alignment) Halt Command for Weapon xy (Test Only)

CF-57F,xy TXA (Transfer Alignment) Re-Initialize Command for Weapon xy (Test Only)

CF-571 Go/No-Go Test Command (Maintenance Only)

CF-572 SIT Command (Maintenance Only)

CF-575 Classified Data Erase Command For Selected Weapons

CF-58 JASSM Targeting Menu Request

CF-580 [AMI] Auto Target Enable/Disable

CF-586 Weapon/Target Assignment Request (Manual Targeting)

CF-588,n Direct Target Definition Display Request For Direct Target n

CF-589 Retarget-all Command

CF-6 FCP Supervision Menu Request

CF-62,n Less [AMI] SMO Load Menu

CF-62x [AMI] Primary SMO Selection

CF-65 SMO Mission Event Recording Command

CF-66 Clear PME Faults Command

CF-67 OAS Shutdown Command

CF-68 ECU Fault Override Command

CF-8 Mission Supervision Menu Request

CF-81,n Read B-52 Sortie Mission Data Command

CF-82 [AMI] Weapons Load Menu Request

CF-82A [AMI] Weapons Group Load Menu (LP)

CF-82C [AMI] Weapons Group Load Menu (RP)

CF-82,n [AMI]

CF-82,nn [AMI]Select Weapon Group

CF-DB Display Previous Weapon Summary (FRMT-12, [AMI] FRMT-7, 7A and 7C)

CF-DD Download Data to Selected Weapons for Targeting

CF-DE Exit Without Downloading Data

CF-Dn Copy Current Direct Target to Direct Target n

CF-DF Display Next Weapon Summary (FRMT-12, [AMI] FRMT-7, 7A and 7C)

CF-E Weapon Control Panel Backup Display Command

CLR-D Selected Weapon Event Deselection Command

Figure 1-16

T.O. 1B-52H-34-2-8

Change 2 1-30C

Control Function (CF) MenuLess [AMI]

[AMI]


T.O. 1B-52H-34-2-8

1-30D Change 2

Control Function (CF) Menu (Cont)WINDOW DISPLAY MODI-

FIABLEFUNCTION

1 Operational Mode NO

FULL SIM (BrightVideo)

Operational mode is full simulation of the WIU and weapons.

[AMI] PART SIM(Bright Video)

Operational mode is partial simulation of the WIU and weapons.

STRIKE (Bright Video) Operational mode is STRIKE.

2 Loaded B-52 MissionType

NO

WAR JASSM War mission is loaded.

OTL JASSM Operational Test Launch (OTL) mission is loaded.

CC JASSM Captive Carry (CC) mission is loaded.

FERRY JASSM Ferry mission is loaded.

TLI JASSM Timeline Integration (TLI) mission is loaded.

(blank) No mission is loaded, or the current mission is not recognized by theJASSM SMO.


T.O. 1B-52H-34-2-8

Change 2 1-30E

Weapon Supervision Menu (CF-5)Less [AMI]

[AMI]

− − − −CF - 5

5C RP WPN SUPV5B BAY WPN SUPV5A L P WPN SUPV5 9 BAY DOORS5 8 J ASSM TARGET I NG

5 7 J ASSM SUPV

5 2 FUL L S I M5 1 PART S I M5 0 STR I KE

5 WPN SUPV 1

34

44

B40808

PMD

2


T.O. 1B-52H-34-2-8

1-30F Change 2

Weapon Supervision Menu (CF-5) (Cont)

WINDOW DISPLAY MODI-FIABLE

FUNCTION


PART SIM [AMI](Bright Video)

Operational mode is simulation of the WIU and weapons.

FULL SIM (Bright Video)

Operational mode is simulation of the WIU and weapons.



NO






(blank) No mission is loaded, or the current mission is not recognized by theJASSM SMO.

3 Bomb Bay Door Status NO

OPEN The bomb bay doors are open.

CLSD The bomb bay doors are closed.

4 [AMI] SMO ID NO 28 Character ID of SMO assigned to specified location (LP, Bay, RP)


T.O. 1B-52H-34-2-8

Change 2 1-31

Classified Data Erase Command (CF-575)

Operator entry of CF-575 commands the SMO toperform a classified data erase for the selected mis-siles. When a classified data erase is performed, thefollowing data is erased from missile memory:

• Target Data Set.• GPS Crypto Keys.• Less [AMI] Missile Assignments.

Prior to initiating classified data erase, the SMOseeks confirmation by displaying the confirmationprompt CLSF DATA ERASE? (YES/NO). A YES re-sponse will result in classified data erase being ini-tiated, while a NO response will terminate the re-quest. After Less [AMI] 60 seconds, [AMI] 120 sec-onds, the default response of NO will be assumed.

After the classified data erase is performed, themissile is powered off, unassigned and untargeted.Reloading B-52 mission data, performing a ManualTargeting operation, or commanding Retarget Allcan restore missile assignments. However, powermust be applied to the missiles for targeting to beinitiated.

NOTE

• A classified data erase initiated by the SMOdue to a permanent fatal fault (rather thanthe operator) results in missile assignmentsbeing maintained. However, the missile willbe untargeted.

• Do not initiate classified data erase until INstatus is achieved.

• Do not initiate classified data erase while atargeting operation is in progress (prior toCF-DD).

The SMO will reject a CF-575 command and dis-play the advisory LOC/STA?? ([AMI] JASSM LOC/STA??) if no Location(s)/Station(s) have been se-lected on the WCP or PCP/WCP backup. TheCF-575 command will be displayed in reverse videowhen it is rejected. The SMO will also reject aCF-575 command, if another confirmation promptis displayed.

If a CF-575 command is accepted, but the selectedweapon(s) cannot be accessed (weapon not present,weapon powered off, etc.), the advisory LOC/STA??([AMI] JASSM LOC/STA??) will be displayed. A de-scription of each failure and the corresponding cor-rective action is listed in figure 7-20.

CDE COMPLT ([AMI] JASSM CDE COMPLT) willbe displayed when classified data erase has been com-pleted for all selected missiles.

JASSM Targeting Menu (CF-58)

The JASSM Targeting menu commanded by CF-58 isshown in figure 1-20. The JASSM Targeting menudisplays targeting options that are available. Op-tions available are Missile/Target Assignment(manual targeting), Direct Target definition, and Re-target-all.

[AMI] JASSM Auto Targeting Mode (CF-580)

Operator entry of CF-580 toggles between com-manding the Auto Targeting mode ON and OFF.The current status of the Auto Target mode is dis-played on the JASSM Targeting Menu (CF-58). Thedefault state for Auto Targeting is ON.

Missile/Target Assignment (Manual Targeting) Display(CF-586)

The Missile/Target Assignment Display command-ed by CF-586 is shown in figure 1-21. The Missile/Target Assignment (Manual Targeting) display al-lows the operator to download pre-planned target-ing data to selected missile(s). The operator will se-lect a missile launch point along with a correspond-ing mission group. If the mission group field is leftblank, mission group A will be assumed. After alaunch point and mission group have been identi-fied, the operator will then select the desired mis-sile to receive targeting data.

The SMO will reject a CF-586 command and dis-play the command in reverse video if any of the fol-lowing conditions are true:

• Targeting is active.• A direct targeting operation is in progress.• Less [AMI] A missile mission DTUC is not

available.• B-52 mission data is in the process of being

loaded.• Less [AMI] CAD processor reconfiguration is

in progress.

Manual targeting (CF-586), requires data item entry/modification by the operator initiated by MDFY-n,where n represents the MFD line number associatedwith the data to be entered/modified. Several dataitems are common to the CF-586 Manual Targetingand CF-588 Direct Target Definition displays (SeeTarget Data Items). The operator will use the samemissile selection process for manual targeting and di-rect target assignment. If the operator enters an in-valid command through the IKB, the command willbe displayed in reverse video. If the operator entersinvalid data values, the affected data fields will bedisplayed in reverse video.

T.O. 1B-52H-34-2-8

1-32 Change 2

JASSM Supervision Menu (CF-57)([AMI] CF-57, CF-5A, CF-5C)


FUNCTION


[AMI] PART SIM(Bright Video)

Operational mode is partial simulation of the WIU and missiles.

FULL SIM (BrightVideo)

Operational mode is full simulation of the WIU and missiles.



NO






(blank) No mission is loaded, or the current mission is not recognized by the JASSMSMO.


T.O. 1B-52H-34-2-8

Change 2 1-33


FUNCTION

3 GO/NOGO Test Status

OFF (Bright Video)

NO

Go-NoGo quick test mode is not active.

ON (Bright Video) Go-NoGo quick test mode to determine proper umbilical connection is ac-tive.

ON (Reverse Video) Go-NoGo quick test mode was in progress, but was terminated due to aninvalid condition (aircraft is airborne).

4 SIT Test Status

OFF (Bright Video)

NO

SIT is not commanded.

ON (Bright Video) SIT mode is active.

ON (Reverse Video) SIT mode was in progress, but was terminated due to an invalid condition(aircraft is airborne).

5 FTS Power Enable/Disable Identifier (Test Only)

NO

xy Location/station of the missile with FTS enabled/disabled.x = L for left pylon stations and R for right pylon stations.y = Station number 1, 2, 3, 6, 7 or 8.

xy (Reverse Video) FTS enable/disable is commanded and an activate FTS fault exists.

(blank) No missile has FTS enabled.

6 FTS Power TransferPower Source(Test Only)

NO

CARR (Bright Video) Aircraft is commanded as the power source to missile FTS (initial valuewhen FTS is enabled).

CARR (Reverse Vid-eo)

Aircraft is commanded as the power source to missile FTS and an activateFTS fault exists.

MSL (Bright Video) Missile battery is source of FTS power.

MSL (Reverse Video) Missile battery is commanded as the source of FTS power and an activateFTS fault exists.

(blank) FTS is not enabled.


T.O. 1B-52H-34-2-8

1-34 Change 2

JASSM Targeting Menu (CF-58)

Less [AMI]


T.O. 1B-52H-34-2-8

Change 2 1-35

[AMI]

5 8 J ASSM TARGET I NG

5 8 6 WPN / TGT ASSGN

5 8 8 , N D I R TGT N= 1− 6

5 8 9 RETGT AL L

− − − −CF - 5 8

B40811

PMD

5 8 0 AUTO TGT 1


FUNCTION

1 [AMI] Auto TargetingStatus

NO Auto targeting status.

ON (Bright Video) Auto targeting is enabled.

OFF (Bright Video) Auto targeting is disabled.


T.O. 1B-52H-34-2-8

1-36 Change 3

Missile/Target Assignment Display (CF-586)

Less [AMI]


T.O. 1B-52H-34-2-8

Change 2 1-37

[AMI]


FUNCTION

1 Targeting Data Loading Status

COMPLT

NO

Data has been successfully downloaded to the missile.

COMPLT(Reverse Video)

Failure to download data.

LOADING(Bright-Blinking Video)

Waiting for data to be downloaded to the missile.

(Blank) Targeting operation is not active or transfer of data to the missile(s) hasnot been initiated via a CF-DD command.

2 JASSM Launch PointNumbernn

YES

JASSM launch point number where nn = _1 to 99 and is a valid target.

(blank) Prior to operator entry or targeting operation is not active.

3 Mission Group Identifiera

YES

Mission group identifier where a = A to F.

3A [AMI] JASSM WeaponGroup

NO

28 Character Label Selected Weapon Group for specified location.

(Blank) No Weapon Group selected for specified location.


T.O. 1B-52H-34-2-8

1-38 Change 2

Missile/Target Assignment Display (CF-586) (Cont)WINDOW DISPLAY MODI-

FIABLEFUNCTION

4 Location/StationSelection StatusE

YES

The corresponding location or station is currently selected.

0 The corresponding location or station is not selected.

(blank) The corresponding missile is not present or is unavailable for assign-ment due to a permanent fatal fault.

5 Location/Station Identifierxy

NO

Location/station of each missile present on the aircraft and available forselection that is not currently assigned and targeted to any target.

xy (BrightUnderlined Video)

Location/station of each missile present on the aircraft and available forselection that is currently assigned and targeted to this target or toanother target.

xy (NormalBlinking Video)

Location/station of each missile that does not have power applied andis available for selection.

xy (Reverse Video) Location/station of each missile that was not successfully targeted aftera CF-DD command.

(blank) The corresponding missile is not present or is unavailable for selectiondue to a permanent fatal fault.

x = L for left pylon stations and R for right pylon stations.y = Station number 1, 2, 3, 6, 7 or 8.Each location and station that is displayed will be displayed in a dedi-cated screen location for that missile. The positions are assigned fromleft to right across the screen in the preferred launch sequence.

6 Missiles Selected NO

__n Remaining missiles to be selected. n = 0 or 1.

–nn (Reverse Video) More missiles are selected than are required for the mission. nn = 1 to 11.

(blank) When any of the following conditions is true:•Targeting operation is not active.•When manual targeting is active, prior to selection of JASSM launchpoint destination and mission group identifier.

7 Missiles Required NO

_n Quantity of required missiles. _n = 1.

(blank) When manual targeting is active, prior to selection of JASSM launchpoint destination and mission group identifier or targeting operation isnot active.


T.O. 1B-52H-34-2-8

Change 3 1-39

Direct Target Definition Display (CF-588,n)

The Direct Target Definition display, commandedby CF-588,n is shown in figure 1-22. The DirectTarget Definition display allows the operator to de-fine targets that are not contained Less [AMI] onthe missile mission DTUC, [AMI] in the weapongroup on the DTC.

Operator entry of CF-588,n, where n is an operator-defined direct target, commands the Direct TargetDefinition display for that direct target. The SMOwill reject a CF-588,n command and display thecommand in reverse video if any of the followingconditions is true:

• n is not a valid direct target identifier.• [AMI] Targeting is active.• Any of the following targeting operations are ac-

tive:a. Manual targeting.b. Retarget-all.c. Automatic targeting.d. Direct targeting operation is in progress foranother direct target other than the one beingrequested.

• B-52 mission data is in the process of being loaded.

The SMO will accept operator entry of CF-588 (ex-cluding ,n) to command the Direct Target Definitiondisplay to be displayed only when the direct targetoperation is in progress. Otherwise, the SMO willreject the CF-588 command and display the com-mand in reverse video.

Direct target definition (CF-588) requires data itementry/modification by the operator initiated byMDFY-n, where n represents the MFD line numberassociated with the data to be entered/modified.Several data items are common to the CF-586Manual Targeting and CF-588 Direct Target Defini-tion displays. The operator will use the same mis-sile selection process for manual targeting and di-rect target assignment. If the operator enters an in-valid command through the IKB, the command willbe displayed in reverse video. If the operator entersinvalid data values, the affected data fields will bedisplayed in reverse video.

Target Data Items

Manual Targeting (CF-586) and Direct Targeting(CF-588) require data item entry/modification bythe operator. The following are the Target Dataitems.

LAUNCH POINT NUMBER

In order to manually target a missile, the operatormust select the launch point number associatedwith the target. The launch point number is en-tered on the Manual Targeting display (CF-586)(figure 1-21). The input is numeric and ranges from01 to 99. Only the JASSM launch points defined bythe loaded B-52 mission are valid.

MISSION GROUP IDENTIFIER

Along with the selected launch point, the missiongroup identifier associated with that launch point isentered on the Manual Targeting display (CF-586)(figure 1-21). Valid IKB input entries for window 3are A, B, C, D, E, F, or it may be left blank. If it isleft blank, the default mission group A will be as-sumed. The range of valid alpha characters (A-F) isdependent on the quantity of mission groups associ-ated with the launch point and missile type cur-rently loaded.

TARGET LOCATION

The target location is the geographical position andelevation which a missile is to strike. The targetlocation data fields appear on the Direct TargetDefinition screen (CF-588) (figure 1-22). The posi-tion entry key fields are:

• Target point reference latitude in degrees,minutes, and ten-thousandths of a minute.

• Target point reference longitude in degrees,minutes, and ten-thousandths of a minute.

• Target point reference elevation in feet (MSL).• Target point reference elevation ([AMI] MSL;

Less [AMI] MSL or HAE) in feet.• Less [AMI] Target point elevation reference

(HAE or MSL).

T.O. 1B-52H-34-2-8

1-40 Change 1

BEARING TO TARGET

The bearing to target specifies the weapon’s termi-nal ground track to the target. The bearing to tar-get is entered on the Direct Target screen (CF-588)(figure 1-22). The valid input values are from 0 to360 degrees (0 is North), and 999, which indicatesthe missile will determine bearing to target as anangle from the aircraft to the target at point of rele-ase. The default value for this field is 999.

TARGET IMPACT ANGLE

The target impact angle specifies the angle in de-grees, relative to local level plane at the target. Theimpact angle is entered on the Direct Target Defini-tion display, (CF-588) (figure 1-22). The default im-pact angle is 60 degrees. Valid input values arefrom 0 (level) to 90 (vertical) degrees, however, themissile will only use an impact angle ranging from20 to 70 degrees.

NOTE

If less than 20 degrees is entered onCF-588, the missile will use a built-in mini-mum impact angle value of 20 degrees. Ifmore than 70 degrees is entered on CF-588,the missile will use a built-in maximum val-ue of 70 degrees. FRMT-12 displays the im-pact angle actually being used by the mis-sile. While in SIM mode, the FRMT-12 im-pact angle displayed is the same as theCF-588 value input.

CRUISE ALTITUDE

The cruise altitude indicator on the JASSM DirectTargeting display (CF-588) (figure 1-22) is used tospecify a cruise altitude (MSL) for the JASSM. Val-id entries for this field range from 0 to 45000 feetand 99999, the default value, displayed prior to op-erator entry. The default cruise altitude is 15,000feet and, although the field range is 0 to 45,000feet, the maximum altitude the missile will fly isapproximately 22,000.

FUZE MODE

The fuze mode indicator on the JASSM Direct Tar-geting display (CF-588) (figure 1-22) is used to spec-ify a fuze mode of either soft impact referenced toCrush Switch, or hard impact referenced to G-forceSensor. The operator can select a fuze mode of Soft

by entering 1 or a fuze mode of Hard by entering 2.The text SOFT or HARD will be displayed, depend-ing on the fuze mode selected. A default value of 1(Soft) will be displayed prior to operator entry.

FUZE DELAY

Fuze delay milliseconds can be specified by enter-ing a corresponding delay entry on the JASSM Di-rect Targeting display (CF-588) (figure 1-22). A fuzedelay will delay detonation from the time of impactby the specified time value. Valid entries for thisfield and their corresponding time values are listedin the following table. A default value of 0 will bedisplayed prior to operator entry.

FUZE DELAYS

VALID ENTRIES MILLISECOND DELAY

0 0

1 10

2 15

3 20

4 30

5 40

6 50

7 120

MISSILE SELECTION INDICATOR

The missile selection indicator appears above thelocation/station identifier for each available missileon the JASSM Direct Targeting display (CF-588)(figure 1-22). The missile selection identifier is usedwhen selecting missiles during a manual targetingor direct target definition operation. Valid entriesare E and 0 (zero), where E indicates that the corre-sponding missile is selected for targeting and 0 in-dicates the missile is not selected. The missile selec-tion indicator window will be blank when any of thefollowing conditions are true:

• The missile is not present.• The missile is not selected and is unavailable

for selection due to a permanent fatal fault prior to a CF-DD command.

• The missile is not present or is unavailable for selection due to a permanent fatal fault following a CF-DD command and is not a selected missile.

T.O. 1B-52H-34-2-8

Change 2 1-41

Retarget-all Command (CF-589)

Operator entry of CF-589 (figure 1-20) will result inthe targeting of missiles as directed by the B-52mission that is loaded. Once CF-589 is accepted, allmissiles will become unassigned. The SMO willthen restore the missile assignment data to theoriginal values of the B-52 mission that is loaded.This will result in the loss of modified targetingdata previously transferred to the missiles. All mis-siles not assigned to a JASSM Launch Point by theB-52 mission that is loaded will remain unassignedand considered untargeted by the SMO.

NOTE

A retarget-all command requires approx-imately 2 minutes per JASSM.

The SMO will reject a CF-589 command and dis-play the command in reverse video if any of the fol-lowing conditions exist:

• B-52 mission data is in the process of beingloaded.• Less [AMI] Another confirmation prompt is

active.• Less [AMI] A missile mission DTUC is not ac-

cessible.

Prior to initiating targeting of all missiles, the SMOwill seek confirmation by displaying the confirma-tion prompt RETARGET ALL? (YES/NO). A YESresponse will result in the halting of any targetingin progress, and proceed with the untargeting of allmissiles, while a NO response will terminate the re-quest. After Less [AMI] 60 seconds, [AMI] 120 se-conds, the default response of NO will be assumed.

When a valid CF-589 command is entered any ofthe following targeting operations will be termi-nated, if active:

• Manual targeting.• Direct targeting.• Automatic targeting.

T.O. 1B-52H-34-2-8

1-42 Change 3

Direct Target Definition Display (CF-588,n)

Less [AMI]


T.O. 1B-52H-34-2-8

Change 2 1-43

[AMI]

D I RECT TGT

CF - DD=DONE CF - DE =ESC CF - DN=COPY TO D I R TGT ( D 1−D6 )

WPNS TO SEL ECT

OF− − − −CF - 5 8 8 n

’

1 3 1 4 1 56

1 2

A75613

12(ALL TOP BOXES)

ENTER E TO SEL ECT OR 0 TO DEL ETE

1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3

TGT PT

BRNG TO TGT

FUZE DE

L AT LONG AL T’1

2

3

4

5

4 53

’6

7o

I MPACT ANGL E 8o

CRU I SE AL T

FUZE MODE 1 09 1−SOF T 2 −HARD

L AY ( 0 − 7 )1 1


FUNCTION

1 Direct Target Numbern

NODefined Direct Target. n = 1 to 6.

(blank) Targeting operation is not active.

2 Data Loading Status

COMPLT

NO

Data has been successfully downloaded to the missile.

COMPLT (ReverseVideo)

Failure to download data.

LOADING (Bright-Blinking Video)

Assigned mission data is downloading to the missile.

(Blank) Targeting operation is not active or transfer of data to the missile(s) hasnot been initiated via a CF-DD command.

3 Direct Target Latitude

add°mm.mmmm

YES

Target point latitude in degrees, minutes and ten-thousandths of a minute.a = N for north and S for south. Limits are S90.00.0000 through N90.00.0000.

ITEM VALID INPUT RANGE Degrees (d) S90 to N90 Minutes (m) 00.0000 to 59.9999



T.O. 1B-52H-34-2-8

1-44 Change 2

Direct Target Definition Display (CF-588,n) (Cont)WINDOW DISPLAY MODI-

FIABLEFUNCTION

4 Direct Target Longitude YES

addd°mm.mmmm Target point longitude in degrees, minutes and ten-thousandths of a minute.a = E for east and W for west. Limits are W 180.00.0000 through E 179.59.9999

ITEM VALID INPUT RANGE Degrees (d) W180 to E179 Minutes (m) 00.0000 to 59.9999


5 Direct Target Altitude YES

fffff Target point altitude (MSL): –328 to 32810 in feet.


6 Direct Target MissileCruise Altitude

YES

nnnnn Cruise altitude for JASSM Direct Targets where nnnnn = 0 to 45000’ MSLor 99999, the default value, displayed prior to operator entry. Although val-ues up to 45000 are valid, the missile’s actual maximum cruise altitude isapproximately 22,000 feet MSL. The missile uses 15,000 feet MSL as thedefault altitude (99999).


7 Direct Target MissileBearing to Target

YES

bbb Bearing to target where bbb = 0 to 360 (0 being true north) or 999 where mis-sile will determine BTT from A/C to target at time of launch. A 999 is displayed prior to operator entry.


8 Direct Target MissileImpact Angle

YES

dd Target impact angle (0 - level to 90 - vertical) degrees relative to local levelhorizontal plane at target impact. 60 is displayed on CF-588 prior to operatorentry.


9 Fuze Mode YES

n Fuze mode selector where n is used to specify whether to reference thedelay time from a crush switch (soft target) or g-force sensor (hard target).A 1 is displayed prior to operator entry.

VALID INPUT TARGET TYPE1 Soft Impact2 Hard Impact

(blank) Direct targeting is not active.

10 Fuze Target Type NO

HARD Selected Fuze Mode is function on impact referenced to G-Force Sensor(Hard target).

SOFT Selected Fuze Mode is function on impact referenced to Crush Switch(Soft target). SOFT is displayed prior to operator entry, or if Fuze Mode in-valid.



T.O. 1B-52H-34-2-8

Change 3 1-45


FUNCTION

11 Fuze Function Delay YES

m Fuze function delay setting where m = 0 to 7. A 0 is displayed prior to opera-tor entry, or if Fuze Mode invalid.


12 Location/StationSelection Status

YES

E The corresponding location or station is currently selected.

0 The corresponding location or station is not selected.

(blank) The corresponding missile is not present or is unavailable for assignmentdue to a permanent fatal fault.

13 Location/Station Identifier

NO

xy Location/station of each missile present on the aircraft and available forassignment that is not currently assigned and targeted to any target.

x = L for left pylon stations and R for right pylon stations.y = Station number 1, 2, 3, 6, 7 or 8.Each location and station that is displayed will be displayed in a dedicatedscreen location for that missile. The positions are assigned from left to rightacross the screen in the preferred launch sequence.

xy (Bright Underlined Video)

Location/station of each missile present on the aircraft and available forassignment that is currently assigned and targeted to this target or toanother target.

xy (Normal BlinkingVideo)

Location/station of each missile that does not have power applied and isavailable for assignment.

xy (Reverse Video) Location/station of each missile that was not successfully targeted aftera CF-DD command.

(blank) The corresponding missile is not present or is unavailable for selectiondue to a permanent fatal fault.

14 Weapons Remaining NO

__n Remaining missiles to be selected. n = 0 or 1.

–nn (Reverse Video) More missiles are selected than are required for the mission. nn = 1 to 11.

(blank) When any of the following conditions is true:•Targeting operation is not active.•When manual targeting is active, prior to selection of JASSM launchpoint destination and mission group identifier.

15 Weapons Required NO

_n Quantity of required missiles. _n = 1.

(blank) When manual targeting is active, prior to selection of JASSM launch pointdestination and mission group identifier or targeting operation is not active.

16 Direct Target ElevationReference Less [AMI]

YES Target elevation reference in MSL or HAE.

n Valid Input Elevation Measurement n= 0 Mean Sea Level n= 1 Height Above Ellipsoid



T.O. 1B-52H-34-2-8

1-46 Change 2

FCP SUPERVISION MENU (CF-6)

The FCP Supervision Menu, commanded by CF-6,is shown in figure 1-23. Much of the data displayedon the FCP Supervision Menu is related to the FMSand is contained in T.O. 1B-52H-1-12.

CF-61 Startup

CF-61 commands OAS startup. The procedure forstarting up the OAS is the same as for any otherOAS startup and is contained in T.O. 1B-52H-1-12.

Less [AMI] CF-62 SMO Menu

Operator entry of CF-62 will result in an FMS dis-play of the SMOs available on the OCP DTUC (Fig-ure 1-24). Operator entry of CF-62,n will result inthe FMS loading the SMO indicated by n. A num-ber followed by the text AGM-158 XXXXXXX, iden-tifies the number to be entered to load the SMO.XXXXXXX is the version information extractedfrom the CPIN number. While the SMO is active,the SMO will delay a CF-62,n command to have theFMS load a new SMO until the following conditionshave been met:

• All WIU and missile power removal complete.• Classified data erase (CF-575) is completed.• DTU input/output is complete if a Fault Data

Recorder Cartridge (FDRC) DTUC is installed.

The SMO is automatically initialized and beginsexecution immediately upon loading the SMO intothe ACUs. The procedure for loading the SMO intothe ACUs is equivalent to loading any other CWISMO. The JASSM SMO, if it exists on the OCPDTUC, is identified on the CF-62 menu. The statusmessage SMO LOAD CMPLT will be displayed oneach MFD following completion of a SMO load. Theprocedure for loading the SMO, (the same as forloading any other SMO) is contained in T.O.1B-52H-1-12.

[AMI] CF-62 SMO Menu

SMO Load Menu (CF-62) (figure 1-24) allows theoperator to select and load a SMO for left pylon, bay(not used with JASSM), or right pylon. The primarySMO is selected from the SMO’s loaded on left py-lon, bay, or right pylon.

While the SMO is active, the SMO will inhibit loadinga new SMO until the following conditions have beenmet:

• All WIU and missile power removal complete.• Classified data erase is completed (software

initiated).

• DTS input/output is complete if a DTC isinstalled.

With the CF-62 menu displayed the operator willenter MDFY-11 to copy the following text to the bot-tom of the MFD for modification:

11 SMO LOAD LP__ BAY__ RP__

The operator will then enter the number of the de-sired SMO number into the field that correspondsto the location that the SMO is to control and pressthe ENTER key. The location: LP (left pylon), BAYnot used with JASSM), or RP (right pylon) is de-fined by the cursor which can be moved using thearrow keys on the IKB. The primary SMO will bethe first SMO loaded until a primary is chosen.

To select a SMO as the primary SMO, the operatorwill enter CF-62x where x is either A, B or C to se-lect the SMO that controls the left pylon, bay orright pylon, respectively.

The procedure for loading SMOs is contained inT.O. 1B-52H-1-12.

CF-64 CLSF Memory Erase

CF-64 commands the erasure of OAS classified me-mory. The procedure for classified memory erase isthe same as contained in T.O. 1B-52H-1-12.

CF-65 Data Record

CF-65 DATA RECORD indicates a CF-65 commandcan be used to record mission event data. When aSMO is loaded, the missile modes, safe conditionsand pertinent information are recorded along withFMS mission event data. Operator entry of CF-65will result in a DTUC/DTC recording of navigationand mission parameters, missile mode switches,time to go, and LAR status.

CF-66 Erase PME Faults

CF-66 ERASE PME FAULTS indicates a CF-66command can be used to erase fault indicationsthat are no longer valid from the PME Status Dis-play (FRMT-6). The SMO will indicate to the FMSwhich of its fault indications should be erased. Op-erator entry of CF-66 will result in erasure of allpast fault indications shown on the PME StatusDisplay (FRMT-6, figure 1-33). Any WIU commu-nication faults and ECU faults will be cleared. Anyexisting faults will cause a fault recording and thefault indication will continue to be displayed inreverse video.

T.O. 1B-52H-34-2-8

Change 3 1-47

CF-67 Shutdown

CF-67 SHUTDOWN indicates a CF-67 commandcan be used to shutdown FMS and SMO processingin the ACUs. Operator entry of CF-67 will result inthe shutdown of the FMS and SMO. The SMO willdelay compliance of the shutdown request until alloutstanding SMO faults have been recorded (Less[AMI] if an FDRC is installed) and until powerdown of all WCE and missiles is complete. The pro-cedure for shuting down the OAS with the SMOloaded is the same as for any other shutdown and iscontained in T.O. 1B-52H-1-12.

CF-68 ECU Power Override

Less [AMI] CF-68 ECU PWR ORIDE indicates aCF-68 command can be used to override faults asso-ciated with non-availability of Environmental Con-trol Unit (ECU) power. The current state of theoverride is displayed (ON or OFF). The SMO willnot reject a CF-68 command.

[AMI] CF-68 ECU PWR ORIDE serves as an ON-OFF toggle switch for overriding faults associatedwith non-availability of Environmental ControlUnit (ECU) power. The current state of the overrideis displayed (ON or OFF) on CF-6. The SMO willnot reject a CF-68 command.

During WIU power on and initialization, the ECU,which supplies cooling air to the WIUs, is com-manded on. If aircraft status indicates ECU poweris not available when commanded, the WIU poweron process is terminated. Additionally, if an Envi-ronmental No-Go fault is detected from the ECUafter ECU power has been applied for 2 minutes,power will be removed from all missiles and bothWIUs unless the operator activates the ECU poweroverride option.

Less [AMI] Operator entry of CF-68 will commandthe OAS to activate the ECU power override optionand ignore any ECU faults. If an EnvironmentalNo-Go fault is detected, an ECU master fault willbe displayed. If the CF-68 command is enteredwithin 1 minute of the time that the fault isdetected, missile and WIU power will remain on,otherwise missile and WIU power will be removed.If WIU and/or missile power is removed because ofa fault, the CF-68 command can be entered prior tore-applying WIU power and the ECU fault will beignored.

[AMI] Operator entry of CF-68 will command theOAS to activate the ECU power override option andignore any ECU faults. If an ECU AC Discrepancyfault is detected, ECU PWR will be displayed, andECU will be displayed on the Weapon Status and

Inventory Display (FRMT-7) and an X will be dis-played next to ECU text on the PME Status Dis-play (FRMT-6). If an ECU Environmental No-Gofault is detected, X will be displayed by CSP next toECU text on the PME Status Display (FRMT-6) andECU will be displayed on the Weapon Status AndInventory Display (FRMT-7). If an EnvironmentalNo-Go fault is detected, an ECU master fault willbe displayed. If the CF-68 command is enteredwithin 1 minute of the time that the fault isdetected, missile and WIU power will remain on,otherwise missile and WIU power will be removed.If WIU and/or missile power is removed because ofa fault, the CF-68 command can be entered prior tore-applying WIU power and the ECU fault will beignored.

While in ECU power override, the WIU may be op-erated using a 30 minute on, 15 minute off, 30 min-ute on cycle.

With an ECU fault present, damage toequipment may occur if WIU power re-mains on continuously as a result of select-ing ECU Power Override.

Less [AMI] The ECU power override option willbecome inactive only if the SMO is reloaded or if alogoff is commanded and the system is restarted.The current status of the ECU power overrideoption, whether it is active or inactive, is displayedon the FCP Supervision Menu (CF-6).

[AMI] The ECU power override option will becomeinactive only if CF-68 is commanded when the ECUpower override is active. The operator will be given1 minute from the time the CF-68 command wasentered to reenter the CF-68 command if an ECUfault is still in effect otherwise weapon and WIUpower will be removed. A system logoff and restartof the system will also deactivate the ECU override.The current status of the ECU power override op-tion, whether it is active or inactive, is displayed onthe FCP Supervision Menu (CF–6).

[AMI] CF-69A and CF-69B ACU Shutdown Commands

Primary ACU shutdown is initiated by entering aCF-69A command and secondary ACU shutdown isinitiated by entering a CF-69B command. When theprimary ACU is shutdown, the secondary ACU willbe reconfigured to become the primary ACU if it isoperational. The ACU shutdown process is de-scribed in T.O. 1B-52H-1-12.

T.O. 1B-52H-34-2-8

1-48 Change 2

FCP Supervision Menu (CF-6)Less [AMI]

B40814

66 1 STARTUP6 2 SMO MENU

6 4 CL SF MEM ERASE6 5 DATA RECORD6 6 ERASE PME FAUL TS6 7 SHUTDOWN6 8 ECU PWR OR I DE

CF - 6

FCP SUPV

2

PMD

[AMI]

6 FCP SUPV6 1 STARTUP

6666

4567

CDES

LARH

STAU

FAST

ED

MR

O

EEPW

MCMN

OE

ER

RASEDF AUL TS

− − − −CF - 6

6 2 SMO MENU

SMO :

PMD

6 9 SHUTDOWNA PR I MARY ACU6 9 SHUTDOWNB SECONDA Y A

FCP APPL I CAT I ONS

R CU

PR I MARY 1

6 8 CU PWR OR DE I E 2

B40815


T.O. 1B-52H-34-2-8

Change 2 1-49


FUNCTION

1 Primary SMO Title NO

24 Character Label Primary SMO title.

2 ECU Power Override NO

OFF ECU power override is not commanded.

ON ECU power override is commanded.


T.O. 1B-52H-34-2-8

1-50 Change 2

SMO Load Menu (CF-62)Less [AMI]

[AMI]

Figure 1-24

T.O. 1B-52H-34-2-8

Change 2 1-51

Less [AMI] MISSION SUPERVISION MENU (CF-8)

The Mission Supervision Menu, commanded byCF-8, is shown in Figure 1-25. Much of the datadisplayed on the Mission Supervision Menu isrelated to the flight management system and iscontained in T.O. 1B-52H-1-12. The SMO operationitems include the current B-52 mission type (i.e.,WAR, TLI, OTL, FERRY or CC) and the missilegroup ID from the loaded missile DTUC.

Less [AMI] Read B-52 Sortie Mission Data Command(CF-81,n)

Operator entry of CF-81,n will initiate reading ofB-52 mission n data. The SMO will inhibit loading ofthe mission data and the command displayed in re-verse video if any of the following conditions exist:

• The B-52 sortie mission file format is not inconventional (ICSMS) format.

• There is a missile in launch countdown.• Jettison is in progress for any missile.• SIT is active.• Go-NoGo test is active.• The SMO is operating in SIM mode.

If the mission type of the loaded sortie mission isnot a conventional mission, the nonfatal masterfault MSN DATA?? will be displayed.

The JASSM SMO and a sortie mission must beloaded in order to successfully apply power to theWIUs. If a B-52 sortie mission is not loaded WIUpower application will be inhibited and the nonfatalmaster fault MSN DATA ?? will be displayed.

If the sortie mission data that is loaded does notidentify a WIU as the Stores Management InterfaceUnit (SMIU) at a location where power is applied,power will be removed from that WIU and all mis-siles at that location, and the nonfatal master faultMSN DATA?? will be displayed.

Once the WIU is powered on, weapons may be pow-ered. Weapons are automatically assigned launchpoints if the sortie mission has JASSM launchpoints. When the weapons are powered on, weapontypes are verified and valid weapons are targeted tothe assigned launch points. When sortie missiondata is changed, valid weapons that are not directtargeted are automatically targeted.

Weapon store mismatches with sortie mission datacan be discerned by observing the FRMT-7 Missiletype window in combination with a fault such asXY:STORE ID or XY:WPN PRSNT.

If the missile type identified by mission data is notthe same as that identified by the previously loadedmission and subsequently power is applied to themissile(s), a xy:STORE ID transient fatal masterfault will be displayed.

If the missile type identified by mission data is not thesame as that identified by the previously loaded mis-sion and if either WIU is operational, power will be re-moved from each WIU that is powered and a MSNDATA?? master fault will be displayed. However, ifthe missile type identified by the previous missionwas a JASSM, the power will not be removed.

NOTE

Manual Targeting, Direct Targeting, or Auto-matic Targeting, if active, will be terminatedwhen a valid CF-81,n command is entered.

For an in-depth discussion of mission data opera-tions see MISSION DATA in Section VII.

[AMI] MISSION SUPERVISION MENU (CF-8)

The Mission Supervision Menu, commanded byCF-8, is shown in Figure 1-25. Much of the datadisplayed on the Mission Supervision Menu isrelated to the flight management system and iscontained in T.O. 1B-52H-1-12. The screen displaysthe sortie, mission type (i.e., WAR, TLI, OTL,FERRY or CC), and weapon group for the left py-lon, bay and right pylon loaded in the OAS.

[AMI] B-52 Mission Data Load Command (CF-81)

The B-52 Mission Data Load Display (CF-81), fig-ure 1-25A, displays the primary SMO, loaded sor-tie, mission and primary SMO weapon group, num-ber of sorties available on the DTC, and a list ofmissions available for each sortie. The display alsoprovides the capability of selecting the sortie anddisplaying the command to load a mission.

NOTE

The resident sortie and mission windows atthe top of the CF-81 display will remain blankor display the previously loaded sortie andmission identifiers until a mission/new mis-sion is loaded.

The operator can select a sortie from one of threeways, Either CF-DF to select the next sortie, CF-DB to select the previous sortie, or MDFY-1, enterthe desired sortie number and press the ENTERkey. The selected sortie number will be displayedalong with the sortie title and the associated mis-sions will be listed below them.

T.O. 1B-52H-34-2-8

1-52 Change 2

Operator entry of CF-81,n will initiate reading ofB-52 mission n data. The JASSM SMO will inhibitloading of the mission data and the command dis-played in reverse video if any of the following condi-tions exist:

• The B-52 sortie mission file format is not inconventional format.

• There is a missile in launch countdown.• Jettison is in progress for any missile.• SIT is active.• Go-NoGo test is active.• The SMO is operating in SIM mode.• The B-52 sortie mission file currently loaded

is a captive carry mission and one or bothWIUs have power applied.

If the mission type of the loaded sortie mission isnot a conventional mission, the nonfatal masterfault JASSM MSN DATA?? will be displayed.

A sortie mission must be loaded in order to success-fully apply power to the WIUs. If a B-52 sortie mis-sion is not loaded WIU power application will be in-hibited and the nonfatal master fault JASSM MSNDATA ?? will be displayed.

If the sortie mission data that is loaded does notidentify a WIU as the Stores Management InterfaceUnit (SMIU) at a location where power is applied,power will be removed from that WIU and all mis-siles at that location, and the nonfatal master faultJASSM MSN DATA?? will be displayed.

Once the WIU is powered on, weapons may be pow-ered. Weapons are automatically assigned launchpoints if the sortie mission has JASSM launchpoints. When the weapons are powered on, weapontypes are verified and valid weapons are targeted tothe assigned launch points. When sortie missiondata is changed, valid weapons that are not directtargeted are automatically retargeted when autotargeting is not enabled.

Weapon store mismatches with sortie mission datacan be discerned by observing the FRMT-7 Missiletype window in combination with a fault such asxy:STORE ID or xy:WPN PRSNT.

If the weapon type identified by mission data is aJASSM and subsequently power is applied to theweapon(s), and the weapon indicates it is not aJASSM the transient fatal master fault XY:STOREID will be displayed and power will be removedfrom the weapon.

If the weapon type identified by B-52 sortie missiondata is a JASSM and the weapon identifies itself asa JASSM and subsequently a B-52 sortie mission isloaded that does not identify JASSMs the masterfault JASSM MSN DATA?? will be displayed

NOTE

Any of the following targeting operationswill be terminated, if active, when a validCF-81,n command is entered.

• Manual Targeting

• Direct Targeting

• Automatic Targeting

For an in-depth discussion of mission data opera-tions see MISSION DATA in Section VII.

[AMI] Weapon Group Load Display (CF-82A, CF-82C)

The JASSM Weapon Group Load Display (CF-82Aand CF-82C), figure 1-25B, shows the sortie, missionand weapon group (for the pylons) that are loadedinto the OAS. The display also depicts the numberavailable and a listing of the JASSM weapon groups.

There can be up to 30 JASSM weapon groups on aDTC. The CF-82A and CF-82C displays can show amaximum of nine weapon groups at a time. CF-DFand CF-DB commands are used to page forward orback to the page containing the desired weapongroup.

The operator can select and load a weapon groupinto the OAS with a CF-82,nn or CF-82,n com-mand, where nn or n represents the weapon groupnumber as shown on the CF-82A or CF-82C display.

NOTE

• Although depicted as LP and RP WPNGROUPs, CF-82A and CF-82C represent allthe JASSM SMO controlled weapons. ACF-82,nn or CF-82,n command from eitherthe CF-82A or CF-82C display will load theselected (nn or n) weapon group for all theJASSMs.

• The CF-82,nn and CF-82,n commands willbe ignored, if CF-82A or CF-82C is not dis-played on the current MFD.

T.O. 1B-52H-34-2-8

Change 2 1-52A

Mission Supervision Menu (CF-8)Less [AMI]

[AMI]

- - - - CF - 8

B52478

B 5 2 DATAS T I EORS ENTI DRE

S ENTI DRE B− 5 2 DATA

8 MSN SUPV

8 1

PMD

8 2 A L P WPNSELECTED WEAPON GROUP

8 2C RP WPN8 2B BAY WPN

34

5

5

GRPGRP

GRP

1


T.O. 1B-52H-34-2-8

1-52B Change 2

Mission Supervision Menu (CF-8) (Cont)WINDOW DISPLAY MODI-

FIABLEFUNCTION


NO







2 Less [AMI] MissileMission Data Tape

NO

28 Character ASCIITitle

Missile mission data tape label.

(blank) When no missile DTUC is installed; title on mission data tape contains allblanks.

3 [AMI] Sortie Title NO

28 Characters Title of the sortie loaded into the ACU.

(Blank) No mission is loaded into the ACU or mission data load is in progress.

4 [AMI] Mission Title NO

28 Characters Title of the mission loaded into the ACU.


5 [AMI] Weapon GroupTitle

NO

28 Characters Title of the weapon group assigned to the associated location.


T.O. 1B-52H-34-2-8

Change 2 1-52C

B-52 Mission Data Load Display (CF-81)[AMI]


FUNCTION

1 Primary SMO Title NO

24 Character Label Primary SMO title.

2 Sortie Title NO

28 Character Label Title of the sortie loaded into the ACU.


3 Mission Title NO

28 Character Label Title of the mission loaded into the ACU.


4 PRIMARY SMOGROUP(Bright UnderlinedVideo)

NO The text, PRIMARY SMO GROUP, will appear when a weapon group hasbeen loaded for the primary SMO.

(Blank) No weapon group has been loaded for the primary SMO.

5 Primary SMO WeaponGroup

NO

28 Character Label Title of the weapon group loaded for the primary SMO.

(Blank) No weapon group has been loaded for the primary SMO.

Figure 1-25A (Sheet 1 of 2)

T.O. 1B-52H-34-2-8

1-52D Change 2

B-52 Mission Data Load Display (CF-81) (Cont)


FUNCTION

6 Sortie No. Select YES

n Selected sortie number (1 - 8).

6A Loaded B-52 MissionType

NO







7 DTC Sortie Count NO

0 No DTC is installed or no sorties are resident on the DTC.

n Number of sorties resident on the DTC.

8 Selected Sortie No. NO

n Selected sortie number (1 - 8).

9 Selected Sortie Title NO

28 Character Label Title of selected sortie on the DTC.

(Blank) No DTC is available.

10 DTC Mission Title NO

28 Character Label Title of each mission data file in the DTC for the selected sortie.

(Blank) No DTC is available.


T.O. 1B-52H-34-2-8

Change 2 1-52E

Weapon Group Load Menu (CF-82A, CF-82C)

[AMI]

Figure 1-25B (Sheet 1 of 2)

T.O. 1B-52H-34-2-8

1-52F Change 2

Weapon Group Load Menu (CF-82A, CF-82C) (Cont)


FUNCTION

1 Selected Sortie Title NO

28 Character Label Title of the sortie resident in the ACU.


2 Selected Mission Title NO

28 Character Label Title of the mission resident in the ACU.


3 Selected WeaponGroup

NO

28 Character Label Title of the weapon group loaded into the ACU for the selected location.

(Blank) No weapon group loaded into the ACU for the selected location.

4 Number of WeaponGroups Available

NO

n or nn Number of JASSM weapon groups available to load.

5 Weapon GroupNumber

NO

n or nn JASSM weapon group number.

6 Weapon GroupTitle

NO

28 Character Label JASSM weapon group title.


T.O. 1B-52H-34-2-8

Change 2 1-52G/(1-52H blank)

TARGETING PROCESS CONTROL (CF-DD AND CF-DE)

There are two commands (CF-DD and CF-DE) thatallow an operator to control the completion processwhen one of the following requests is active:

• Manual Targeting (CF-586).• Direct Target Definition (CF-588).

The targeting process completion command, CF-DD, initiates the downloading of target data to theselected missile(s). The other command used to con-trol the targeting process is the CF-DE command,and is used to exit targeting process without down-loading data to the missile(s).

Targeting Completion Command (CF-DD)

Operator entry of CF-DD will conclude the currenttargeting request. If either the manual targeting ordirect targeting operation is being performed and ifmissiles are selected, transfer of targeting data tothe selected missiles will be initiated. The currenttargeting process will then be concluded if DirectTargeting is active.

The SMO will reject a CF-DD command and displayit in reverse video if any of the following conditionsexist:

• The manual targeting or direct target defini-tion operation is not active.

• The display associated with the active target-ing operation is not present on the selected MFD.

• The data items required have not been en-tered for the active targeting operation.

• Less [AMI] Manual targeting operation is ac-tive and a missile mission DTUC is not available.

• [AMI] Manual targeting operation is activeand a weapon mission group is not available.

Exit Targeting Process Command (CF-DE)

Operator entry of CF-DE command will exit the re-quest without initiating the transfer of targetingdata or saving direct target that has been changed.

The SMO will reject a CF-DE command and displayit in reverse video if any of the following conditionsexist:

• The manual targeting or direct target opera-tion is not active.

• The display associated with the active target-ing operation is not present on the selected MFD.

DIRECT TARGET COPY COMMAND (CF-Dn)

Operator entry of CF-Dn, will result in the directtarget data currently displayed being copied to di-rect target n. n represents the number of the directtarget to receive the copied direct target data. Aconfirmation prompt, OVERWRITE DATA? (YES/NO) will be displayed requesting confirmation tooverwrite the existing direct target data for directtarget n with the current direct target data. A YESresponse to the confirmation prompt will result inoverwriting the target data for direct target n andmissiles previously assigned/targeted to direct tar-get n will be unassigned/untargeted. A NO responseto the confirmation prompt will result in abandon-ing the CF-Dn command, leaving the direct target ndata and missile assignment and targeted statesunchanged. If the confirmation prompt is unan-swered after Less [AMI] 60 seconds, [AMI] 120seconds the default answer of NO will be assumed.

The SMO will reject a CF-Dn command and displayit in reverse highlight if any of the following condi-tions exist:

• Direct Target operation is not currently active.• Direct target n is the same as the currently

displayed direct target.• n is not a valid direct target number.• There is another confirmation prompt pend-

ing.• Direct Target display is not displayed on the

same MFD on which the copy command was en-tered.

MISSILE CONTROL PANEL BACKUP DISPLAY (CF-E)

CF-E, shown in figure 1-26, can be used by the op-erator to enter missile commands in lieu of enteringthe commands via the WCP. The CF-E commandsassociated with the JASSM SMO are contained infigure 1-27. Input of commands using CF-E is con-tained in Section III of T.O. 1B-52H-1-12.

SELECTED DIRECT TARGET DESELECTION COM-MAND (CLR-D)

If a direct target has been selected via PRGM-Dn,operator entry of CLR-D will command the SMO todeselect that direct target for launch. If a direct tar-get is not currently selected for launch, CLR-D willbe rejected and displayed in reverse video. The se-lected direct target will also be exited if auto launchmode is selected or a fly-to command is entered.

BLA

T.O. 1B-52H-34-2-8

1-53

Missile Control Panel Backup Display (CF-E)

PMD

WPN JET TSEL =EE 1

PWRW I UL P / =E 9A

/RP =E 9CEN HW SWCH=E 9D

L AUNCH/ MODE =E 7

=ECD =E 1 1

WPN PWRON =E 6 AOF F =E 6B

ENTER E 3’ ’ THEN ENTER ’ ’A TO SEL ECT OR 0 TO CL EAR’ ’LOCAT I ON + STAT I ON = E 3

CF E

2

2

1

1

34 5

6

7 8 9 1 2 3 6 7 8

11 11 11 11 11

10

A67182


FUNCTION

1 WIU Power Status NO

ON WIU power is off.

ON (Bright Underlined Video)

WIU power is on.

2 WIU Power Status NO

OFF WIU power is on.

OFF (Bright Under-lined Video)

WIU power is off.

3 Master Fault Status NO

MSTRFAULT

A master fault is not displayed.

MSTRFAULT (Bright Underlined Video)

A master fault is displayed.

4 AUTO Launch ModeStatus

NO

AUTO Launch mode is manual.

AUTO (Bright Underlined Video)

Launch mode is automatic.


T.O. 1B-52H-34-2-8

1-54

Missile Control Panel Backup Display (CF-E) (Cont)


FUNCTION

5 MAN Launch ModeStatus

NO

MAN Launch mode is automatic.

MAN (Bright Underlined Video)

Launch mode is manual.

6 MAN Launch Command

NO

MAN LAUNCH Manual launch has not been commanded or has completed.

MAN LAUNCH (Bright Underlined Video)

Manual launch has been commanded and launch is in progress.

7 Location Identifier NO

LP Left pylon is not selected.

LP (Bright UnderlinedVideo)

Left pylon is selected.

8 Location Identifier

RP

NO

Right pylon is not selected.

RP (Bright UnderlinedVideo)

Right pylon is selected.

9 Station Identifier

ALL

NO

ALL station switch is not selected.

ALL (Bright UnderlinedVideo)

ALL station switch is selected.

10 Station Identifier

Station Number 1 Thru 8

NO

Station is not selected (Stations 4 and 5 are not used).

Station Number 1 Thru 8 (Bright Underlined Video)

Station is selected (Stations 4 and 5 are not used).

11 CF-E3 Status

A

YES

CF-E3 was the last command entered and the corresponding location or sta-tion is currently selected. When ‘A’ is displayed, the location/station identifierabove it will be displayed in Bright Underline Video.

0 CF-E3 was the last command entered and the corresponding location or sta-tion is not selected. When ‘0’ is displayed, the location/station identifierabove it will be displayed in Normal Video.

(blank) CF-E3 was not the last command entered or corresponding location or sta-tion is not currently selected.


T.O. 1B-52H-34-2-8

1-55

Commands for OAS Power Control Panel and MissileControl Panel (CF-E)

OAS PCP/WCP SWITCH CF-E COMMAND PURPOSE

WPN JETT SEL CF-EE1 Jettisons Selected missile(s)

WPN LNCH MODE CF-E7 Switches AUTO/MAN Launch Function

MIU/LP CF-E9A Power ON/OFF for Left Pylon WIU

MIU/RP CF-E9C Power ON/OFF for Right Pylon WIU

EN HW SWCH CF-E9D Enable Commands to be Entered Via PCP/WCP subsequent toCF-E9A or CF-E9C Commands

MAN LNCH CF-ECD Command Manual missile Launch

MSTR FAULT CF-E11 Acknowledge Master Faults

Locations:L PYLNR PYLN

Stations:1, 2, 3, 6, 7, 8, and ALL

CF-E3 Allows Selection of Location(s) and Station(s)

WPN PWR ON CF-E6A Power ON for Selected missile(s)

WPN PWR OFF CF-E6B Power OFF for Selected missile(s)

Figure 1-27

T.O. 1B-52H-34-2-8

1-56 Change 2

FORMAT (FRMT) DISPLAYS

The FRMT display displays the format menu shownin figure 1-29. FRMT-6 PME Status, FRMT-7 missileData, ([AMI] FRMT-7A LP Weapon Data, FRMT-7CRP Weapon Data and FRMT-77 Stores Summary)FRMT-10 DEST/OAP table, and FRMT-12 WeaponSummary displays are applicable to JASSM opera-tions. Operator entry of FRMT will cause the FormatMenu to be displayed on the selected MFD at the sta-tion where the command was entered. The formatcommands are shown in figure 1-28.

Radar/Electro-Optical Viewing System (EVS) Displays

Discussion of the Radar and EVS displays, com-manded by FRMT-1, FRMT-2, FRMT-4, or FRMT-5,is contained in T.O. 1B-52H-1-12. The SMO willprovide the destination label for these displayswhen the destination is a JASSM launch point.

PME Status Display (FRMT-6)

Figure 1-30 shows FRMT-6, the PME Status dis-play. Much of the data displayed on the PME Statusdisplay is common OAS equipment and is containedin T.O. 1B-52H-1-12.

The operator can review the operational status ofthe AIU, ECU, left WIU and right WIU via thePME Status display. The PME Status displayshows AIU and WIU A bus and C bus communica-tion status and AIU, ECU and WIU failure status.AIU will be displayed in reverse video, if the AIUhas failed; ECU will be displayed in reverse video,if the ECU has failed; and WIU will be displayed inreverse video for the left or right WIU respectively,if either the WIU communication or the WIU havefailed. The AIU, ECU or WIU failure status is alsodisplayed on the JASSM Status and Inventory dis-play (FRMT-7). Each failure display on FRMT-7 willbe removed if the associated failure status clears

Operator entry of FRMT-6 will cause the PME Sta-tus Display to be displayed on the selected MFD atthe station where the command was entered.

JASSM Status and Inventory Display (FRMT-7)

Less [AMI] The JASSM Status and Inventory dis-play, commanded by FRMT-7, is shown in Figure1-31. This display is used to view WCE and missilestatus data.

[AMI] The Weapon Status and Inventory displaycan be requested with or without the Selected Sta-

tion Status displayed in the advisory area. TheWeapon Status and Inventory display without theSelected Station Status is requested on the selectedMFD at an operator station by entering a FRMT-7command when the JASSM SMO is the primarySMO. The Weapon Status and Inventory displaycan also be requested when the JASSM SMO is sec-ondary SMO by entering a FRMT-7A commandwhen the JASSM SMO is assigned to the left pylonor a FRMT-7C command when the JASSM SMO isassigned to the right pylon.

NOTE

[AMI] The CF-DF = PAGE FWD, CF–DB =PAGE BACK label is in the advisory areaand will be overwritten if FRMT-7XY isentered and when release advisories aredisplayed.

The items which can be reviewed on the JASSMStatus and Inventory Display are contained in thefollowing list:

• Armament Interface Unit (AIU) fault indica-tion.

• ECU fault indication.• Left and right WIU, GPS receiver, IU, and

DTU/DTR fault indications.• Missile identification type and sub-type.• Missile power state.• Missile faults.• Ejector status (on selected station status only).• Missile targeting status.• Missile alignment status.• Missile GPS data transfer status.• Telemetry status (on selected station status

only).• Manual launch required status (on selected

station status only).• Crypto key presence indicators.• Missile power on/off countup timer (on se-

lected station status only).• Store missile type (on selected station status

only).• Configuration ID (on selected station status

only).• Carrier navigation mode status.• In-Range/In-Zone status.

Operator entry of FRMT-7 will cause the JASSM Sta-tus and Inventory Display to be displayed on theselected MFD at the station where the command wasentered.

T.O. 1B-52H-34-2-8

Change 2 1-57

JASSM Status and Inventory Display Request with Se-lected Station Status (FRMT-7xy)

Operator entry of FRMT-7xy, where xy represents asingle valid location and station selection, willcause the JASSM Status and Inventory displaywith selected station status display, figure 1-32, tobe displayed on the selected MFD along with statusfrom the selected location and station. A single val-id location and station is selected on an IKB by en-tering ‘A’ or ‘C’ followed by a number 1, 2, 3, 6, 7, or8. Numbers 4 and 5 are invalid stations for JASSM.The characters ‘A’ and ‘C’ represent the left or rightpylon location respectively. The numbers representthe selected station on the identified pylon. As anexample, a FRMT-7A3 command would request theFRMT-7 display to appear with detailed station sta-tus for left pylon station 3 being displayed on thebottom of the selected MFD at the station wherethe command was entered.

[AMI] Weapon Assignment Data Display(CF-DF or CF-DB From FRMT-7, 7A, 7C or 7xy)

The JASSM Weapon Assignment Data display (fig-ure 1-32A), is requested by paging forward (CF-DF)or backward (CF-DB) from the Weapon Status andInventory displays (FRMT-7, 7A, 7C or 7xy). In addi-tion to common FRMT-7 data, such as station num-ber, weapon type/subtype, and the launch point/tar-get identifier, the Weapon Assignment Data displayprovides the weapon group id, selected sortie, andselected B-52 mission. Paging forward from FRMT-77A, 7C or 7xy, the Weapon Assignment Data dis-

plays are presented in the order of assigned JASSMlocations; Left Pylon, Right Pylon and back to thestarting FRMT-7,7A, 7C or 7xy display. Paging back-ward from the FRMT-7, 7A, 7C or 7xy will presentthe Weapon Assignment Data displays in the re-verse sequence.

NOTE

Although not displayed (overwritten withJASSM xy data), CF-DF and CF-DB com-mands are available on the FRMT-7xy dis-play, allowing the operator to request theWeapon Assignment Data displays.

[AMI] Stores Inventory Summary Display (FRMT-77)

Operator entry of FRMT-77 displays the Stores In-ventory Summary (figure 1-32B). The Stores Inven-tory Summary display provides generic store/weap-on information for all locations. All data on this dis-play is controlled by the CSP and none of the datafields are modifiable.

Destination Table Display (FRMT-10,nn)

The Destination Table display, commanded by FMScommand FRMT-10,nn is shown in figure 1-33. TheSMO will provide the destination label, JASSM LP,for each destination in figure 1-33 when the respec-tive destination is a JASSM launch point. The SMOwill not allow modification of a turn short indication,latitude, longitude, and altitude for a JASSM LP.

JASSM Format CommandsCOMMAND DESCRIPTION

FRMT Format Menu Request.

FRMT-6 PME Status Display Request.

FRMT-7 JASSM Status and Inventory Display Request.

FRMT-7A [AMI] JASSM Status and Inventory Display Request.

FRMT-7C [AMI] JASSM Status and Inventory Display Request.

FRMT-7xy JASSM Status and Inventory Display Request with Selected Station xy.

FRMT-77 [AMI] Stores Inventory Summary Display

FRMT-10,nn Destination Table Display. nn = current or selected destination.

FRMT-12,nn Weapon Summary Display. nn = direct target (Dn) or launch point (nn).

CF-DF or CF-DB FromFRMT-7, 7A, 7C or 7xy [AMI] JASSM Weapon Assignment Data Display Request.

Figure 1-28

T.O. 1B-52H-34-2-8

1-58 Change 2

JASSM FRMT (Format) MenuLess [AMI]

FRMT MENU1 RDR2 RDR+PMD3 EVS4 EVS+PMD5 EVS FUL L6 PME STATUS7 WPN DATA (XY )8 EMERG DATA9 F XPT TBL

1 0 DEST / OAP TBL

+ XH POS I T I ON

NN= J ASS L AUNCH PO I NT 1− 9 9 ) OR D I R TGT ( D 1−D6 )− −FRMT -

(XY= LOC / STA )

A67183

PMD

M (

1 2 WEAPON SUMMARY ( NN )

[AMI]

FRMT MENU1 RDR2 RDR+PMD3 EVS4 EVS+PMD5 EVS FUL L6 PME STATUS

8 EMERG DATA9 F XPT TBL

1 0 DEST / OAP TBL

− −FRMT -

B40819

7 A L P WPN DATA7B BAY WPN DATA7C RP WPN DATA

+ XH POS I T I ON

7 7 STORES SUMMARY

7 PR I MARY WEAPON DATA

1 2 WEAPON SUMMARY ( NN )NN= J ASSML AUNCH PT ( 1− 9 9 ) ORD I R TGT ( D 1−D6 )

1

1

PMD


T.O. 1B-52H-34-2-8

Change 2 1-59


FUNCTION

1 SMO ID NO

24 Character ASCII ID ID of SMO assigned to specified location.

24 Character ASCII ID (Bright Underline Video)

ID of SMO assigned to specified location and SMO is primary.

(blank) No SMO assigned to location.


BUS PME FL T BUS PME FL T BUS PME FL T UB S PME FL T

DEURSCRVRRNKBNKB

R I UAHRSRDR

CD I UCSCPRNMPWCP

A I URADOORECU

L W I UR W I U

T - 6MRF

A47310

PMD

ACU ABC

1234

DTU

12

I ME

DVSE I U

ACU

DTU

ACU

DTUDTU

I ME

--

I UGPSS URPKBNPKB 1 2 3

1 2 3

3A

1 2 3

T.O. 1B-52H-34-2-8

1-60 Change 2

PME Status Display (FRMT-6) Less [AMI]

[AMI]

Figure 1-30 Sheet (1 of 2)

T.O. 1B-52H-34-2-8

Change 2 1-61


FUNCTION

1 Device A Bus Test NO

A The corresponding device has failed the A Bus test since the last timefaults were cleared (CF-66), but is currently passing the A Bus test.

A (Reverse Video) The corresponding device is currently failing A Bus test.

(Blank) The corresponding device has not failed the A Bus test since the last timefaults were cleared.

2 Device C Bus Test NO

C The corresponding device has failed the C Bus test since the last timefaults were cleared (CF-66), but is currently passing the C Bus test.

C (Reverse Video) The corresponding device is currently failing the C bus test.

(Blank) The corresponding device has not failed the C Bus test since the lasttime faults were cleared.

3 Device Fault NO

X The corresponding device has failed since the last time faults werecleared (CF-66), but is currently not faulted.

X (Reverse Video) The corresponding device is currently faulted.

(Blank) The corresponding device has not failed since the last time faults werecleared.


T.O. 1B-52H-34-2-8

1-62 Change 3

JASSM Status and Inventory Display (FRMT-7)(FRMT-7, FRMT-7A, FRMT-7C)

Less [AMI]

R I GHT 8R I GHT 6

R I GHT 7

R I GHT 3R I GHT 1

R I GHT 2

L EF T 3

L EF T 8

L EF T 7

L EF T 6

− −FRMT − 7

2 M1−GO /

M

1

1

6

7

3

8

2

31

7

86

2 −/

3 / 4 5

8

A75616

SAMPLE

1

PMD

10 11 12 13 14 15 16 17

9

6 7

0 1 / G Z

0C

NOTE

• Details of the LEFT 1 station inventory defined in the following table, LEFT 2 dis-play is shown as a sample. The other station data displays are identical.

• Stations 4 and 5 are not used with JASSMs.


T.O. 1B-52H-34-2-8

Change 2 1-62A

[AMI]

R I GHT 8R I GHT 6

R I GHT 7

R I GHT 3R I GHT 1

R I GHT 2

L EF T 3

L EF T 8

L EF T 7

L EF T 6

− −FRMT - 7

M

6

7

3

8

2

31

7

86

B41366

SAMPLE

10 11 12 13 14 15 16 17

9

0 1 / G Z2M1−GO / 10C

1 2 −/

3 / 4 5

8

1

6 7

C F - DF =PAGE FWD C F - DB =PAGE BACK

PMD

NOTE• Details of the LEFT 1 station inventory defined in the following table, LEFT 2 dis-

play is shown as a sample. The other station data displays are identical.• Stations 4 and 5 are not used with JASSMs.


FUNCTION

1 Crypto Key Status NO

NO KEYS(Reverse Video)

Crypto keys are not available.

(blank) Crypto keys are available.

2 Missile Type NO

M1 Weapon power is off and mission data indicates weapon is anAGM-158A.

Weapon power is on and both weapon and mission data agree weapon isan AGM-158A.

M1 (Reverse Video) Weapon is on and indicates that the weapon is an AGM-158A. Mission datadisagrees. Not a JASSM mission.


T.O. 1B-52H-34-2-8

1-62B Change 3

JASSM Status and Inventory Display (FRMT-7)(FRMT-7, FRMT-7A, FRMT-7C) (Cont)


FUNCTION

2 (Cont) M NO Weapon is on and indicating it is a variant.

Weapon is off and mission data indicates weapon is a variant.A carrier mission is not loaded and the weapon is a JASSM. (SIT and Go/No-Go test only)

M (Reverse Video) Weapon power is on and indicating it is a variant, and mission data is indisagreement.

P Weapon is present, but it is of unknown type. JASSM MSN data indicatesempty station. (WPN PRSNT master fault)

P (Reverse Video) Non-JASSM weapon (displayed after power on attempt)

(blank) WIU power is off for the location, or a missile is not present at the station.

3 Weapon Status NO

CL Captive Carry missile launched (simulated launch).

GO Mission capable: Safe to Release with launchable alignment state. Manuallaunch required.

GO (Bright UnderlineVideo)

Fully Mission capable: All Up Round ready with launchable alignment state.

NG (Reverse Video) Permanent fatal fault has occurred for this missile. Missile power is inhibited.

OF WIU power is on for this pylon and missile power is off for this missile.

ON Missile power is on for this missile.

X Missile is not present and no missile presence discrepancy exists.

X (Reverse Video) Missile is not present and a missile presence discrepancy exists.

(blank) WIU power for this pylon is off.


T.O. 1B-52H-34-2-8

Change 3 1-62C


FUNCTION

4 Target Data NO

Dn Direct target has been assigned to missile where n = 1 to 6, or the missilehas been launched against the target.

Dn (Bright Video) Direct target has been assigned to the missile and targeting is in progress,or the weapon has been powered off after targeting. n = 1 to 6.

Dn (Bright UnderlineVideo)

Direct target has been assigned to the missile, targeting data has been as-signed, loaded, and verified.

Dn (Reverse Video) Targeting failure.

nn Launch point number has been assigned to the missile, or the missile hasbeen launched against the target. nn = 1 to 99.

nn (Bright Video) Launch point number has been assigned to the missile and targeting is inprogress, or the weapon has been powered off after targeting. nn = 1 to 99.

nn (Bright UnderlineVideo)

Launch point has been assigned to the missile, targeting data has been as-signed, loaded and verified.

nn (Reverse Video) Targeting failure.

(blank) Missile is not assigned, WIU power is not applied, or the missile has beenjettisoned.

5 Mission Group NO

a Mission group associated with the launch point that has been assigned to themissile, or the missile has been launched against the target.a = A to F.

a (Bright Video) Mission group associated with the launch point that has been assigned tothe missile and targeting is in progress. a = A to F.

a (Bright UnderlineVideo)

Mission group associated with the launch point that has been assigned to themissile, targeting data has been assigned, loaded and verified. a = A to F.

a (Reverse Video) Targeting failure for mission group associated with the launch point.a = A to F.

(blank) WIU power is off, the missile is not assigned, the missile is assigned to a di-rect target prior to targeting or missile has been jettisoned.

6 Transfer AlignmentQuality

NO

nn Transfer alignment quality. nn= 1 to 10.

nn (Reverse Video) Transfer alignment quality. nn= 10. Reverse video indicates a failure hasLess [AMI] occurred; [AMI] persisted for a minimum of 10 minutes.

(blank) WIU or missile power off, missile is not present, or transfer alignment not ini-tiated.


T.O. 1B-52H-34-2-8

1-62D Change 3

JASSM Status and Inventory Display (FRMT-7)(FRMT-7, FRMT-7A, FRMT-7C) (Cont)


FUNCTION

7 Missile Status NO

BT Missile is in IBIT.

ER Mission data successfully erased.

ER (Normal BlinkingVideo)

Mission data erase in progress.

ER (Reverse Video) Mission data erase failure.

IN Missile is in GPS Initialization.

NOTE

IN can also indicate the combined loss of crypto keys, AUR ready,and minimum GPS.

IN (Reverse Video) Missile is in GPS initialization and Time Received fault has occurred.

MG Missile has received minimum GPS data to acquire GPS after launch.

MG (Reverse Video) Missile has received minimum GPS data and Ephemeris Received fault oc-curred.

TK Missile is tracking at least 4 satellites (test launch only).

WU Missile is in Warmup. Prior to missile power application, indicates heaterpower is applied (115 VAC). Subsequent to missile power application,indicates missile is in warm-up.

WU (Reverse Video) Heater power fault has occurred (while missile power on or off) or warm upfault has occurred (while missile power on).

(blank) WIU is off, or missile 115 VAC and 28 VDC #1 is off.

8 Ranging/In-Zone NO

R In-Range.

[AMI] R (ReverseVideo)

In-Range with launch inhibited.

Z In-Zone.

[AMI] Z (ReverseVideo)

In-Zone with launch inhibited.

(blank) WIU or missile power is off, or neither In-Range nor In-Zone.

9 Missile Fault Display NO When a missile fault exists, the fault text is displayed.(See FRMT-7 missile Faults in Section VII).

10 L WIU Fault Indicator NO

WIU (Reverse Video) A WIU fault indication has been received which may preclude missile launchfrom the left pylon or communication with the left WIU has failed.

(blank) No fault is present for the left WIU.


T.O. 1B-52H-34-2-8

Change 2 1-63


FUNCTION

11 Carrier Nav Mode NO

DPLR/AHRS(Reverse Video)

Carrier nav mode is DPLR/AHRS. ([AMI] Over land only)

DPLR-NAV Carrier nav mode is DPLR-NAV.

GPS/AHRS(Reverse Video)

Carrier nav mode is GPS/AHRS.

GPS-NAV Carrier nav mode is GPS-NAV.

NAV Carrier nav mode is NAV.

NAV INVALD(Reverse Video)

Invalid nav mode.

(blank) No prime nav mode data available.

12-16 Fault/Status Indicators

12 [AMI] DTC (BlinkingVideo)

NO SMO is accessing DTC.

DTU ([AMI] DTC)(Reverse Video)

The I/O with the missile Mission DTUC/DTC failed (GPS initialization or mis-sile Mission Data attempt).

(blank) No fault is present or [AMI] SMO is not accessing the DTC.

13 IU (Reverse Video) NO The I/O with the Interface Unit failed (GPS Almanac or Crypto Keys Accessattempt).

(blank) No fault is present.

14 GPS (Reverse Video) NO The IU has faulted the GPS receiver.


15 ECU (Reverse Video) NO An ECU fault indication has been received from the AIU.


16 AIU (Reverse Video) NO An AIU fault indication has been received which may preclude missilelaunch or communication with the AIU has failed.


17 R WIU Fault Indicator NO

WIU (Reverse Video) A WIU fault indication has been received which may preclude missile launchfrom the right pylon or communication with the right WIU has failed.



14

R I GHT 8R I GHT 6

R I GHT 7

R I GHT 3R I GHT 2

R I GHT 2

L EF T 3

L EF T 8

L EF T 7

L EF T 6

− −FRMT − 7

2 M1−GO / 1 00 1 / MG Z

6

7

3

8

2

31

7

86

XY

L EF T1

2

E JTLMY 8 9

1 07311

21 65/4

/ 1312

A75617

PMD

SAMPLE

1 6T I ME1 5

C

T.O. 1B-52H-34-2-8

1-64

JASSM Status and Inventory Display with SelectedStation Status (FRMT-7xy)

NOTE

Stations 4 and 5 are not used with JASSMs.


FUNCTION

1 Selected Location

x (Bright Video)

NO

x = Pylon Location L or R.L = Left pylon location of missile selected.

R= Right pylon location of missile selected.

2 Selected Station

y (Bright Video)

NO

y = Station number of missile selected; 1, 2, 3, 6, 7 or 8.


T.O. 1B-52H-34-2-8

Change 3 1-65


FUNCTION

3 Missile Type IDpossible:

NO Store Identification for selected station.

AGM-158A An AGM-158A JASSM is present.

(blank) WIU is off; power has never been applied to the weapon; or weapon isnot present.

4 JASSM Status NO


GO Mission capable: Safe to Release with launchable alignment state. Manu-al launch required.


Fully Mission capable: All Up Round ready with launchable alignmentstate.

NG (Reverse Video) Permanent fatal fault has occurred for this missile. Missile power is inhib-ited.






5 Direct Target/LaunchPoint Number

NO




Direct target has been assigned to the missile, targeting data has beenloaded and verified.


nn Launch point number has been assigned to the missile, or the missile hasbeen launched against the target. nn = _1 to 99.

nn (Bright Video) Launch point number has been assigned to the missile and targeting is inprogress, or the weapon has been powered off after targeting. nn = 1 to 99.


Launch point or target number has been assigned to the missile,loaded and verified.


(blank) Missile is not assigned; WIU power is not applied; or the missile has beenjettisoned.


T.O. 1B-52H-34-2-8

1-66 Change 2

JASSM Status and Inventory Display with SelectedStation Status (FRMT-7xy) (Cont)


FUNCTION

6 Mission Group NO

a Mission group associated with the launch point that has been assigned tothe missile, or the missile has been launched against the target. a = A to F.

a (Bright Video) Mission group associated with the launch point that has been assigned tothe missile and targeting is in progress. a = A to F.

a (Bright UnderlineVideo)

Mission group associated with the launch point that has been assigned tothe missile, targeting data has been assigned, loaded and verified. a = Ato F.

a (Reverse Video) Targeting failure for mission group associated with the launch point. a = Ato F.

(blank) WIU power is off, the missile is not assigned, the missile is assigned to adirect target prior to targeting or missile has been jettisoned.

7 Missile Fault Display NO When a missile fault exists, the fault text is displayed.(See FRMT-7 missile Faults in Section VII).

8 Telemetry Power Status(Flight Test Only)

NO

OFF Telemetry is commanded off.

ON Telemetry is commanded on.

(blank) Less [AMI] WIU power is off.

9 Manual LaunchRequired Indication

NO

MAN LNCH REQ(Reverse Video)

Missile requires manual launch and missile power is on.

(blank) Weapon power is on with no fault requiring manual launch existing or weap-on power is off.

For Test Only: In addition to the MAN LNCH REQ the window will display the following:

TXA HALT Missile transfer alignment halt test is commanded (test only).

TXA HLT/REIN Missile transfer alignment halt and reinitialization tests are both com-manded (test only).

TXA REINIT Missile transfer alignment reinitialization test is commanded (test only).

(blank) Missile power is off and TXA halt is not commanded, or missile is notpresent.

10 Ejector Status NO

NOT UNLKD (ReverseVideo)

Illegal ejector status is detected.

UNLOCKD Ejector is unlocked.

(blank) Missile is not present or WIU power for this pylon is off.

11 Missile Configuration ID NO

xxxxxx Missile Configuration ID.

(blank) Less [AMI] WIU power off. [AMI] Power has never been applied to eitherthe WIU or the weapon, or weapon is not present.


T.O. 1B-52H-34-2-8

Change 3 1-67


FUNCTION

12 Transfer AlignmentQuality

NO

nn Transfer alignment quality. nn= 1 or 10 (1 = Aligned;10 = NOT Aligned).

nn (Reverse Video) Transfer alignment quality. nn= 10. Reverse video indicates a failure hasLess [AMI] occurred; [AMI] persisted for a minimum of 10 minutes.

(blank) WIU or missile power off, missile is not present, or transfer alignment not ini-tiated.

13 Weapon Data/GPSStatus

NO

BT Missile is in IBIT.

ER Mission data successfully erased.

ER (Normal BlinkingVideo)

Mission data erase in progress.

ER (Reverse Video) Mission data erase failure.

IN Missile is in GPS Initialization.

NOTEIN can also indicate the combined loss of crypto keys, AUR ready,and minimum GPS.

IN (Reverse Video) Missile is in GPS Initialization and Time Received fault has occurred.

MG Missile has received minimum GPS data to acquire GPS after launch.

MG (Reverse Video) Missile has received minimum GPS data and Ephemeris Received fault oc-curred.

TK Missile is tracking at least 4 satellites (test launch only).

WU Missile is in Warmup. Prior to missile power application, indicates heaterpower is applied (115 VAC). Subsequent to missile power application,indicates missile is in warm-up.

WU (Reverse Video) Heater power fault has occurred (while missile power on or off) or warm upfault has occurred (while missile power on).

(blank) WIU is off, or missile 115 VAC and 28 VDC #1 is off.

14 Crypto Key Status NO

K Status received from the missile indicates crypto-keys are present. This in-dication will remain displayed even if missile subsequently fails to indicatekeys present.

K (Reverse Video) Missile indicates crypto-keys are in error or have not been received.

(blank) Missile is powered off or prior to download.


T.O. 1B-52H-34-2-8

1-68 Change 2


FUNCTION

15 Missile Power/Overheat Status

NO

The effects of weapon overheat on weapon reliability and accura-cy are unknown.

HOT (Reverse Video) Label indicating that Overheat Caution has been issued for missile thathas power applied.

HOT (Reverse BlinkingVideo)

Label indicating that Overheat Warning has been issued for missile thathas power applied.

OFF (Bright Video) Label indicating that missile is powered OFF.

ON (Bright Video) Label indicating that missile is powered ON and neither an OverheatWarning nor an Overheat Caution exist.

(blank) Less [AMI] WIU power is off, or missile not present, or power has neverbeen applied to missile. [AMI] Power has never been applied to eitherthe WIU or the weapon, or the weapon is not present.

16 Missile Overheat Monitor Time

NO

hh:mm Time in hours and minutes that missile has been powered ON, poweredOFF, or had either an Overheat Warning or an Overheat Caution issuedwhile powered on. Time pertains to status displayed in Missile Power/Overheat Status window.Range 00:00 – 99:59 (Hours:Minutes).

(blank) Less [AMI] WIU power is off, or missile not present, or power has neverbeen applied to missile. [AMI] Power has never been applied to eitherthe WIU or the weapon, or the weapon is not present.


T.O. 1B-52H-34-2-8

Change 2 1-68A

Weapon Assignment Data Display(CF-DF or CF-DB From FRMT-7, 7A, 7C or 7xy)

[AMI]


FUNCTION

1 JASSM Location NOLP(Bright Underlined)

Displayed weapon assignment data is for the left pylon.

RP(Bright Underlined)

Displayed weapon assignment data is for the right pylon.

2 Selected Sortie Title NO28 Character Label ID of sortie loaded into ACU.(blank) No sortie is loaded into ACU.

3 Selected Mission Title NO28 Character Label ID of B-52 mission loaded into ACU.

(blank) No B-52 mission is loaded in ACU.

4 Missile Type NO

M1 Weapon power is off and mission data indicates weapon is anAGM-158A.

Weapon power is on and both weapon and mission data agree weapon isan AGM-158A.

M1 (Reverse Video) Weapon is on and indicates that the weapon is an AGM-158A. Mission datadisagrees. Not a JASSM mission.


T.O. 1B-52H-34-2-8

1-68B Change 2

Weapon Assignment Data Display(CF-DF or CF-DB From FRMT-7, 7A, 7C or 7xy)

(Cont)WINDOW DISPLAY MODI-

FIABLEFUNCTION

4 (Cont) M Weapon is on and indicating it is a variant.

Weapon is off and mission data indicates weapon is a variant.A carrier mission is not loaded and the weapon is a JASSM. (SIT and Go/No-Go test only)

M (Reverse Video) Weapon power is on and indicating it is a variant, and mission data is indisagreement.

P Weapon is present, but it is of unknown type. JASSM MSN data indicatesempty station. (WPN PRSNT master fault)

P (Reverse Video) Non-JASSM weapon (displayed after power on attempt)

(blank) WIU power is off for the location, or a missile is not present at the station.

5 Target Data NO


Dn (Bright Video) Direct target has been assigned to the missile and targeting is in progress.n = 1 to 6.


Direct target has been assigned to the missile, targeting data has been as-signed, loaded, and verified.



nn (Bright Video) Launch point number has been assigned to the missile and targeting is inprogress. nn = 1 to 99.


Launch point has been assigned to the missile, targeting data has been as-signed, loaded and verified.



6 Selected WeaponGroup

NO

28 Character Label(Bright Underlined)

ID of weapon group, loaded into ACU and used for targeting data.

(blank) No targeting data is currently assigned to the weapon.


T.O. 1B-52H-34-2-8

Change 2 1-68C

Stores Inventory Summary Display (FRMT-77)

[AMI]

− −FRMT

B42831

1 1 11 2 3 4 5

2

3

4

5

6

7

8

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

3 4 521

2

3

4

5

6

7

8

2 3 4 5

- 7 7

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

321 4 5

2

3

4

5

6

7

8

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

2 3 4 5

PMD


FUNCTION

1 SMO Title NO

17 Characters SMO title assigned to the location (truncated to 17 characters).

17 Characters (BrightUnderlined Video)

Primary SMO title (truncated to 17 characters).

(blank) No SMO assigned to the location.

2 Weapon Type NO

aa Weapon type as provided by the loaded aircraft mission data (No SMOloaded at the location or the SMO cannot confirm the actual store type.)aa = JA (JASSM) or CL (CALCM)

aa (Bright UnderlinedVideo)

Weapon type as provided by the loaded aircraft mission data, that hasbeen confirmed by the weapon.

aa (Reverse Video) The SMO has confirmed that the weapon type as provided by the loadedaircraft mission data does not match the actual weapon type.

(blank) No SMO is assigned to the location and there is no mission loaded.

(Blank) (ReverseVideo)

No store indicated by mission data but weapon is present.


T.O. 1B-52H-34-2-8

1-68D Change 2

Stores Inventory Summary Display (FRMT-77) (Cont)


FUNCTION

3 Weapon Status NO


GO Mission capable: Safe to Release with launchable alignment state. Manual launch required.


Fully Mission capable: All Up Round ready with launchable alignmentstate.

NG (Reverse Video) Permanent fatal fault has occurred for this missile. Missile power is inhibited.






4 Target Data NO




Direct target has been assigned to the missile, targeting data has beenassigned, loaded, and verified.



nn (Bright Video) Launch point number has been assigned to the missile and targeting isin progress, or the weapon has been powered off after targeting. nn = 1to 99.


Launch point has been assigned to the missile, targeting data has beenassigned, loaded and verified.



5 Time To In-Range NO

mm:ss The time in minutes and seconds required for the aircraft to reach a pointthat is within range of the target if the aircraft continues flying at the currentGS, altitude and ground track. This condition is termed “time-to-go (TTG)to in-range”. Maximum value is 59:59 if greater than one hour.

mm:ss (Reverse Video) Weapon unable to provide valid in-range data, launch is inhibited, or air-craft is inside Min range circle. Number indicated is based on the last validdata or 59:59 if greater than one hour.

00:00 Aircraft is in-range.

(blank) In-range is unachievable, or no selected weapon event.

(blank) (Reverse Video) Not ranging and weapon unable to provide valid in-range data.


1234

OAP − 1− 2− 3− 4

1234

−−−−

1234

− −FR T − 1 0M’

1

1

A75618

PMD

nn

T.O. 1B-52H-34-2-8

1-69

Destination Table Display (FRMT-10,nn)


FUNCTION

1 Destination ID NO

JASSM LP Destination is a JASSM Launch Point (LP).

Figure 1-33

T.O. 1B-52H-34-2-8

1-70 Change 2

Weapon Summary Display (FRMT-12, FRMT-12,nn orFRMT-12,Dn)

The Weapon Summary display, commanded byFRMT-12, FRMT-12,nn or FRMT-12,Dn is shown infigure 1-34. The FRMT-12 display provides a sortedsummary of targeting data for up to 12 missiles. Amaximum of 4 missiles will be shown on one dis-play, requiring scrolling to view targeting data forother missiles. CF-DB and CF-DF will allow the op-erator to scroll backwards and forwards betweenmissiles in groups of four. The sorted targeting datawill be displayed in the order of: JASSM stores tar-geted to launch points, followed by stores targetedto direct targets, and ending with the status of mis-siles not targeted or having no assignment.

The FRMT-12 command will sort the targeting dataand request the Weapon Summary display startingwith the first missile identified by the sort. TheFRMT-12,nn command will sort the targeting dataand request the Weapon Summary display begin-ning with the missile assigned to JASSM launchpoint nn. JASSM launch point nn can be a numberfrom _1 to 99. The FRMT-12,Dn command will sortthe targeting data and request the Weapon Sum-mary display beginning with the missile assigned toJASSM direct target D1. JASSM launch point Dncan be a direct target from D1 to D6. The sort is ex-ecuted once upon entry of the FRMT-12,nn orFRMT-12,DN command. If a missile assignmentchange occurs while the FRMT-12 screen is dis-played, all location/stations will be displayed in re-verse video in the location/station window. This pro-vides an indication to the operator that the target-ing data displayed may not be accurate. Therefore,re-entry of the FRMT-12,nn command is requiredafter targeting is complete to resort and refresh dis-played targeting data. The following four conditionswill cause a FRMT-12 command to be rejected anddisplayed in reverse video.

• A FRMT-12,nn command was entered and nnis not a valid JASSM launch point.

• A FRMT-12,Dn command was entered and nis not a valid JASSM Direct target.

• No missile is assigned to the requestedJASSM launch point.

• A FRMT-12,nn command was entered and theapplicable carrier mission is not loaded.

NOTE

Discrepancies can occur between an impactangle displayed on FRMT-12 display andCF-588 Direct Targeting display. The Mis-sile will use a built in minimum impactangle of 20 if less than 20 is entered. Themissile will use a built in maximum impactangle value of 70 if a value greater than 70is entered. Therefore, while in strike modethe impact angle displayed on FRMT-12represents the missile’s value. While in SIMmode the impact angle displayed is thesame as the value input.

DISPLAY PREVIOUS WEAPON SUMMARY (CF-DB)

Entry of CF-DB while the Weapon Summary dis-play is active will cause the targeting data for thefour previous missiles to be displayed in the pre-ferred launch sequence. The SMO will reject a CF-DB command and display the command in reversevideo if the Weapon Summary Display is not activeon the selected MFD or if there are no previous mis-sile targets points to be displayed.

NOTE

CF-DB will not display targeting data pre-vious to missile target nn if FRMT-12,nnwas entered, or previous to missile targetDn if FRMT-12,Dn was entered.

DISPLAY NEXT WEAPON SUMMARY (CF-DF)

Entry of CF-DF while the Weapon Summary dis-play is active will cause the targeting data for up tofour missiles to be displayed in the preferredlaunch sequence. The SMO will reject a CF-DFcommand and display the command in reverse vid-eo if the Weapon Summary display is not active onthe selected MFD or if there are no more missiletargets to be displayed.

T.O. 1B-52H-34-2-8

Change 2 1-71

WEAPON SUMMARY DISPLAY(FRMT-12,nn/FRMT-12,Dn)

Less [AMI]

[AMI]

J ASSM WEAPON SUMMARYI D /L S L AT LONG EL EV AL T TGT ANG

CRU I SE BRG I MP

PTOF FUZE MODE DEL AY




’’

’ ’

’ ’

’ ’

1 1 N4 1 3 4 . 5 6 7 8 W1 1 8 3 4 . 5 6 7 8 1 0 7 4 9 9 9 9 9 9 2 7 0 3 0

o o

oo

o o o o

o o

− −FRMT - 1 2 , NN

L 7 SKR 1 0 0 : 2 5 SOF T 3

91 2 3 4 5 6 78 10 11

1 2 38 9 10

4 5 6 711

1 2 3 4 5 6 7111098

A86436

12

12

12

MP D

CF - DF =PAGE FWD CF - DB= PAGE BACK


T.O. 1B-52H-34-2-8

1-72 Change 2

WEAPON SUMMARY DISPLAY(FRMT-12,nn/FRMT-12,Dn) (Cont)


FUNCTION

1 Current Event No. NO

nn JASSM launch point. nn = _1 to 99.

Dn Direct Target. n = 1 to 6.

0 Missile displayed in window is not assigned to any launch point or direct tar-get.

2 Latitude NO

add°mm.mmmm Target point latitude in degrees, minutes and ten-thousandths of a minute.a = N for north and S for south. Limits are S90.00.0000 through N90.00.0000.

ITEM VALID INPUT RANGE Degrees (d) S90 to N90 Minutes (m) 00.0000 to 59.9999

3 Longitude NO

addd°mm.mmmm Target point longitude in degrees, minutes and ten-thousandths of a minute. a = E for east and W for west.

Limits are W 180.00.0000 through E 179.59.9999 ITEM VALID INPUT RANGE Degrees (d) W180 to E179 Minutes (m) 00.0000 to 59.9999

4 Target Point Elevation NOfffff Target elevation (MSL or HAE, as designated in mission planning, for pre-

planned targets; MSL for direct targets): –328 to 32810 in feet. DisplayedMSL can vary up to 10 feet due to HAE conversion in mission planning sys-tems.

5 Missile Cruise Altitude NOnnnnn Missile Cruise Altitude for Direct Targets. nnnnn = 0 to 45000 (MSL) or

99999. A 99999 is displayed prior to operator entry of a value.

6 Missile Impact Azimuth NO

bbb Bearing to Target (Impact Azimuth) in degrees true. bbb = 0 to 360 (0 =North); bbb = 999 where the missile will determine BTT from aircraft to targetat time of launch. A 999 is displayed prior to operator entry of a value.

7 Missile Impact Angle NOdd Target Impact Angle in degrees relative to local level horizontal plane at

target impact. dd = 0 (level) to 90 (vertical) degrees. A value of 60 is dis-played prior to operator entry of a value.

NOTE

Discrepancies can occur between an impact angle displayed onFRMT-12 display and CF-588 Direct Targeting display. The Mis-sile will use a built in minimum impact angle of 20 if less than 20is entered. The missile will use a built in maximum impact anglevalue of 70 if a value greater than 70 is entered. Therefore, whilein strike mode the impact angle displayed on FRMT-12 representsthe missile’s value. While in SIM mode the impact angle displayedis the same as the value input.



T.O. 1B-52H-34-2-8

Change 2 1-73


FUNCTION

8 Location/StationIdentifier

NO

xy Location and Station of each missile.

xy (Reverse Video) Target data displayed for this location/station may not be accurate.Re-entry of Weapon Summary Display FRMT-12 command is recom-mended.

x = L for left pylon stations and R for right pylon stations.y = Station number 1, 2, 3, 6, 7 or 8.Each location and station that is displayed will be displayed in a dedicatedscreen location for that missile.

9 Seeker Requirement NO

SKR Seeker is required for the target.

(blank) Seeker is not required for the target.

10 Missile Planned TimeOf Flight (PTOF)

NO

mmm:ss JASSM Planned Time Of Flight (PTOF) when a missile Time on Target(TOT) is required. mmm:ss = Minutes and Seconds 00:00 to 143:10.

(blank) The missile time on target is not required.

11 Fuze Target Type NO

SOFT (Bright Underlined Video)

Selected Fuze Mode is function on impact referenced to Crush Switch(Soft target). SOFT is displayed prior to operator entry, [AMI] or if fuzemode invalid.

HARD (Bright Underlined Video)

Selected Fuze Mode is function on impact referenced to G-Force Sensor(Hard target).

12 Fuze Function Delay

m

NO

Fuze function delay setting where m = 0 to 7. A 0 is displayed prior tooperator entry.

0 0 = Fuze mode is invalid.


T.O. 1B-52H-34-2-8

1-74

PROGRAM (PRGM) DISPLAYS

The Program Display, commanded by the FMS com-mand PRGM-, is shown in figure 1-36. This com-mand allows the operator to review certain missionparameters prior to and during launch. In addition,the Program display also shows pertinent launch,ranging, and missile status data in preparation forlaunch. The data displayed at the top and bottom ofthe Program display is common OAS navigationand B-52 mission data and is contained in T.O.1B-52H-1-12. However, the items contained in themiddle of the screen, commonly designated asGroup III data, relate to JASSM launch events. Theitems regarding JASSM operation are:

• Current launch point identifier.• In-Zone indication for current launch point.• In Range indication for current launch point.• Time to Go (TTG) to In-Range for current

launch point.• In-Range time remaining for current launch

point.• TTG to In-Zone for current launch point.• In-Zone time remaining for current missile

event.• Steering cue to In-Range for current missile

event.• Steering cue to In-Zone for current missile

event.• Missile Time on Target (TOT).• Seeker retained indicator.• Safe launch advisories.• Manual launch required, or LCD status.• Identification and launch status of missile(s)

associated with current launch point.• SMO identified mission event indicator.

NOTE

Safe launch advisories and ranging times onthe Program display are calculated by the air-craft. In-Range and In-Zone indications onthe display are independently calculated bythe weapon. Because of the independent cal-culation and data latency, it is possible for thesafe launch advisories and aircraft calculatedranging indications to differ from the In-Range and In-Zone indications. The In-Range and In-Zone indications describe thestatus of the weapon, and will be honored bythe weapon when launched.

Operator entry of PRGM will cause the ProgramDisplay (Figure 1-36) for the current destination tobe displayed on the selected MFD at the stationwhere the command was entered. There are severalPRGM commands which will specify a certainlaunch point to be displayed.

Selected Destination Program Display (PRGM-nn)

Operator entry of PRGM-nn, where nn representsdestination nn, will cause the Program Display forthe specified carrier destination to be displayed onthe selected MFD.

Direct Target Program Display (PRGM-Dn)

Operator entry of PRGM-Dn, where n represents adirect target number n, will cause the Program Dis-play for the specified direct target to be displayedon the selected MFD This will initiate ranging onmissile Dn. The SMO will reject a PRGM-Dn com-mand and display it in reverse highlight if any ofthe following conditions exist:

• n is not a valid direct target number.• No missiles are assigned to the designated di-

rect target.

JASSM SMO Program Commands

COMMAND DESCRIPTION

PRGM Program Display Request

PRGM-nn Target Selection Command for JASSM Target nn

PRGM-Dn Target Selection Command for Direct Target n

Figure 1-35

T.O. 1B-52H-34-2-8

Change 3 1-75

PROGRAM DISPLAY (PRGM)[AMI]

PMD

1 CPA

PTA

D 1

2 2 2 2 2 2

4

10

3511

612

713

1416

D D

PTAETE

− −PRGM−

A75619

1

8

15

9

Less [AMI]


T.O. 1B-52H-34-2-8

1-76 Change 3

PROGRAM DISPLAY (PRGM) (Cont)WINDOW DISPLAY MODI-

FIABLEFUNCTION

1 Destination Type NO

JASSM LP SMO identified destination type. Current or next destination is a JASSMLaunch Point.

2 Direct Target Number

NO

Dn A missile is assigned to the direct target n, it has not been released andthe direct target is not in range. n = 1 to 6.

Dn (Bright-Underlined Video)

A missile is assigned to the direct target n, it has not been released andthe direct target is in range.

(blank) No missile is assigned to the direct target n or the assigned missile hasbeen released.

3 Current Event Number

NO

LPnn Current event is JASSM launch point number. nn = _1 to 99.

Dn__ Current event is JASSM Direct Target point number. Dn = D1 to D6.

(blank) No launch point or direct target selected.

4 Location/Station NO

xy Location and station of each missile (displayed in preferred launch se-quence) assigned to the current launch point that is targeted and ready forlaunch.

x = L for left pylon stations and R for right pylon stations.y = Station number 1, 2, 3, 6, 7 or 8.

xy (Normal Blinking Video)

Location and station of each missile assigned to the current launch point thatcannot be launched because power is not applied or targeting has not beencompleted.

xy (Bright UnderlinedVideo)

Location and station of each missile assigned to the current launch point thatis ready for launch and is In-Range.

xy (ReverseVideo)

Location and station of each missile assigned to the current launch point thatcannot be launched due to a WIU, AIU, or missile fault.

(blank) (ReverseVideo)

Displayed once for each missile that is required for the selected target bymission data, but no missile is assigned.

(blank) (Normal Video) The missile that was displayed in this MFD area was launched or missile notassigned to this launch point or direct target.

5 In-Range Status NO

RANGE (BrightUnderlined Video)

The missile currently indicates In-Range.

TTG-R The missile currently indicates not In-Range but is achievable.

TTG-R (ReverseVideo)

The missile currently indicates not In-Range and In-Range not achievable, or is not targeted.

(blank) No selected launch point.


T.O. 1B-52H-34-2-8

Change 2 1-77


FUNCTION

6 Time-to-Go to In-Range NO

mm:ss Time-to-Go (TTG) to In-Range. The time in minutes and seconds requiredfor the aircraft to reach a point that is within range of the target if the aircraftmaintains current ground speed, altitude, and ground track. Maximum valueis 59:59 if greater than 1 hour.

mm:ss (ReverseVideo)

The missile is unable to provide valid In-Range data, [AMI] launch is inhib-ited or aircraft is inside min range circle. Number displayed is based on thelast valid data, or 59:59 if greater than 1 hour.

00:00 Aircraft is In-Range.

(blank) In-Range is not achievable, or no selected launch point.


Invalid data. [AMI] Not ranging and weapon not able to provide in-rangedata.

7 In-Range RemainingTime

NO

mm:ss Remaining In-Range time in minutes and seconds if the aircraft maintainscurrent ground speed, altitude, and ground track. Maximum value is 59:59if greater than 1 hour.


The missile is unable to provide valid In-Range data, [AMI] launch is inhib-ited or aircraft is inside min range circle. Number displayed is based on thelast valid data, or 59:59 if greater than 1 hour.

(blank) In-Range is not achievable, or no selected launch point.


Invalid data. [AMI] Not ranging and weapon not able to provide in-rangedata.

8 TOT Label NO

TOT The TOT label is displayed when JASSM ranging is active.

TOT (Bright, Under-lined Video)

Mission requires Time on Target.

(blank) Ranging is not active or Less [AMI] no missile time of flight is being re-ceived from the missile.

9 Missile Time on Target NO

hh:mm:ss Missile Time on Target (TOT) determined by adding the current UTC andthe time of flight data from the weapon (00:00:00 to 23:59:59).

hh:mm:ss(Reverse Video)

Missile unable to provide valid Time of Flight data or [AMI] or launch isinhibited. The number displayed is based on the last valid data.

(blank) No missile time of flight is being received from the missile.


T.O. 1B-52H-34-2-8

1-78 Change 2


FIABLEFUNCTION

10 In-Range TrackIndicator

NO

→ The aircraft is not on track and needs to steer to the right in order toachieve In-Range for the selected direct target.

← The aircraft is not on track and needs to steer to the left in order toachieve In-Range for the selected direct target.

(blank) The aircraft is on track to achieve In-Range or the aircraft is past thepoint of closest approach for In-Range or no selected direct target event.

11 In-Zone Status NO

TTG-Z The missile currently indicates not In-Zone but is achievable.

TTG-Z (ReverseVideo)

The missile currently indicates not In-Zone and In-Zone unachievable, orthe missile is not targeted.

ZONE (BrightUnderlined Video)

The missile currently indicates In-Zone.

(blank) No selected launch point, (Less [AMI] launch point has no waypoints) ordirect target is active event.

12 Time-to-Go to In-Zone NO

mm:ss The time in minutes and seconds required for the aircraft to reach a pointthat is within zone of the first waypoint if the aircraft continues flyingtowards the first waypoint at the current ground speed, altitude, andground track. This condition is termed Time-to-Go (TTG) to In-Zone.Maximum value is 59:59 if greater than 1 hour.


The missile is unable to provide valid In-Zone data. Number indicated isbased on the last valid data or 59:59 if greater than 1 hour.

00:00 Aircraft is In-Zone.

(blank) In-Zone is not achievable, or no selected launch point.


Invalid data. [AMI] Not ranging and weapon unable to provide valid in-zonedata.

13 In-Zone RemainingTime

NO

mm:ss Remaining In-Zone time in minutes and seconds if the aircraft maintainscurrent ground speed, altitude, and ground track. Maximum value is59:59 if greater than 1 hour.


The missile is unable to provide valid In-Zone data. Number displayed isthe last valid time or 59:59 if greater than 1 hour.

(blank) In-Zone is not achievable, or no selected launch point.


Invalid data. [AMI] Not ranging and weapon unable to provide valid in-zonedata.


T.O. 1B-52H-34-2-8

1-79


FUNCTION

14 Safe Release andWeapon LaunchAdvisories

NO Safe release and weapon launch advisories are shown below in the order ofhighest priority.

Weapon LaunchAdvisories:

CLIMB (Blinking, BrightUnderlined Video)

Aircraft altitude is at, below, or within 500 feet of the minimum altitude forrelease. Applicable when the aircraft is In-Zone or In-Zone is achievable.

ACCEL (Blinking, BrightUnderlined Video)

Aircraft speed is at, below, or within 0.02 Mach of the minimum Mach forrelease. Applicable when the aircraft is In-Zone or In-Zone is achievable.

DIVE (Blinking, BrightUnderlined Video)

Aircraft altitude is at, above, or within 500 feet of the maximum altitude forrelease. Applicable when the aircraft is In-Zone or In-Zone is achievable.

DECEL (Blinking, BrightUnderlined Video)

Aircraft speed is at, above, or within 0.02 Mach of the maximum Mach forrelease. Applicable when the aircraft is In-Zone or In-Zone is achievable.

HDG TOL(Blinking Video)

Current aircraft heading is within 6° to 9° of heading tolerance limits. Applicable when the aircraft is not In-Zone, but In-Zone is achievable.

HDG TOL (Blinking,Bright Video)

Current aircraft heading is within 3° to 6° of heading tolerance limits. Applicable when the aircraft is not In-Zone, but In-Zone is achievable.

HDG TOL (Blinking,Bright UnderlinedVideo)

Current aircraft heading is within 3° or outside of heading tolerance limits.Applicable when the aircraft is not In-Zone, but In-Zone is achievable.

TRN LEFT(Blinking Video)

Aircraft heading is within 6° to 9° of the right heading tolerance limit for re-lease. (Turn LEFT to correct.) Applicable when the aircraft is In-Zone only.

TRN LEFT(Blinking, Bright Video)

Aircraft heading is within 3° to 6° of the right heading tolerance limit for re-lease. (Turn LEFT to correct.) Applicable when the aircraft is In-Zone only.

TRN LEFT (Blinking,Bright Underlined Video)

Aircraft heading is within 3° or outside of the right heading tolerance limitfor release. (Turn LEFT to correct.) Applicable when the aircraft is In-Zoneonly.

TRN RIGHT(Blinking Video)

Aircraft heading is within 6° to 9° of the left heading tolerance limit for re-lease. (Turn RIGHT to correct.) Applicable when the aircraft is In-Zone only.

TRN RIGHT(Blinking, Bright Video)

Aircraft heading is within 3° to 6° of the left heading tolerance limit for re-lease. (Turn RIGHT to correct.) Applicable when the aircraft is In-Zone only.

TRN RIGHT (Blinking,Bright Underlined Video)

Aircraft heading is within 3° or outside of the left heading tolerance limit forrelease. (Turn RIGHT to correct.) Applicable when the aircraft is In-Zoneonly.

(blank) No weapon launch advisories exist or no selected launch point.

Safe ReleaseAdvisories:

Safe release advisories do not inhibit launch. Possible collisionbetween weapons and between weapon and aircraft can occurif weapon is launched with a release advisory displayed.

ROLL Aircraft roll angle and/or roll rate is too high for safe launch.

PITCH Aircraft pitch angle and/or pitch rate is too high for safe launch.

LEVL_OFF Aircraft vertical velocity and/or vertical acceleration is too high for safelaunch.

YAW Aircraft yaw rate is too high for safe launch.

(blank) No safe release advisories exist or no selected launch point.


T.O. 1B-52H-34-2-8

1-80 Change 3


FIABLEFUNCTION

15 Seeker Status NO

SKR (ReverseVideo)

The missile mission requires seeker and either a terminal guidance fault ex-ists or the missile has no seeker.

(blank) The missile has seeker guidance capability.

16 Countdown/ManualLaunch Indicator

NO

MAN LNCH REQ(Bright Video)

Manual launch required for missile assigned to current launch point.

COUNTDOWN n(Bright Video)

In LCD. n = TTG to launch ranging from 2 down to 0.

(blank) Not in LCD and not in manual launch mode or no selected launch point.

17 CLR-D=EXIT DIR TGTMODE Less [AMI]

NO Displayed when Direct Target mode selected.


T.O. 1B-52H-34-2-8

2-1/(2-2 blank)

Normal Aircrew Procedures section II


GENERAL 2-3

PREFLIGHT PROCEDURES 2-3

BEFORE EXTERIOR INSPECTION (POWER OFF) (RN/N) 2-3

EXTERIOR INSPECTION (POWER OFF) (RN/N) 2-3

AFTER ENGINE START (AIRCRAFT POWER AND COOLING AIR AVAILABLE) 2-7

MISSILE CHECK (RN/N) 2-7

INFLIGHT PROCEDURES 2-9

AFTER TAKEOFF (RN/N) 2-9

MISSILE POWER APPLICATION (N) 2-9

MISSILE TARGETING PROCEDURES (RN-N) 2-10

MISSILE/TARGET ASSIGNMENT (MANUAL TARGETING) PROCEDURES 2-10

DIRECT TARGETING DEFINITION DATA ENTRY PROCEDURES 2-13

LAUNCH PROCEDURES 2-17

MISSILE PREPARATION FOR LAUNCH (RN-N) 2-17

MISSILE LAUNCH PROCEDURES 2-18

BEFORE LAUNCH CHECK (RN) 2-18

AUTOMATIC MISSILE LAUNCH CHECKLIST (RN-N) 2-19

MANUAL MISSILE LAUNCH CHECKLIST (RN-N) 2-20

POST STRIKE/ABORT PROCEDURES 2-22

POST STRIKE/ABORT (RN/N) 2-22

AFTER LANDING PROCEDURES 2-23

GROUND SAFEING PROCEDURES (RN-N) 2-23

BLA

T.O. 1B-52H-34-2-8

Change 2 2-3

GENERAL

Detailed normal operating procedures for theAGM-158 JASSM are contained in this section. Theprocedural checklists are grouped in PREFLIGHTPROCEDURES, AFTER ENGINE START (Powerand Cooling Air Available), INFLIGHT PROCE-DURES, and AFTER LANDING PROCEDURESsubsections.

The step procedures are the call-response type inwhich code letters appear after each response to in-dicate which member of the crew is to accomplishthat step. Identification symbols are used after eachresponse, except when the entire checklist is accom-plished by a single crewmember, such as pilot ornavigator. Code letters are as follows: (P) pilot, (CP)copilot, (N) navigator, and (RN) radar navigator.

NOTE

[AMI] On missions with mixed weapons loads, the JASSM SMO must beloaded and selected as the primary SMO in order to power, align, target,range and launch JASSMs.

PREFLIGHT PROCEDURES

BEFORE EXTERIOR INSPECTION (POWER OFF) (RN/N)

1. Jettison Power & Jettison Control Circuit Breakers – Out

2. Pilot’s Munitions Consent Panel: (RN)

a. LOCK-UNLOCK Switch – Guard closed

3. Weapon Control Panel: (N)

a. WPN JETTISON Switch – Guard closed

b. NUCLEAR LOCK-UNLOCK Switch – Guard closed

4. Alternate Jettison Control Panel: (N)

a. PYLON POWER Switch – OFF, Guard closed

b. POWER Light – Off

5. Proceed to aircraft EXTERIOR INSPECTION (POWER OFF) checklist (RN/N)

EXTERIOR INSPECTION (POWER OFF) (RN/N)

NOTE

• If any discrepancies are found, notify munitions personnel.

• Accomplish step 1 for each loaded HSAB, step 2 for each loadedMAU-12, and step 3 for each missile.

1. External Heavy Stores Adapter Beam & Pylon General Condition – Checked

Check the general condition of the pylon for surface damage. Check pylon and HSAB fairings areinstalled, the relay access door is fastened, and the pylon is configured for ICSMS.

T.O. 1B-52H-34-2-8

2-4

EXTERIOR INSPECTION (POWER OFF) (RN/N) (Cont)

2. MAU-12 (Each missile Loaded Station):1.

a. Inflight Safety Lockout Pin Hole – Bolt and nut installed

b. Sway Braces & Ejector Feet – Seated and locked

Check sway brace lockout is tight and both ejector feet are against the missile.

c. Ground Safety Lock Pin(s) – Removed, counted, and stowed

There should be one pin per missile.

If undue resistance is encountered when removing a lockpin, cease fur-ther action and call munitions personnel.

d. Sensing Switch Plunger – Checked

MAU-12 EJECTOR RACK

3. JASSM Missiles Checked :

The following steps should be accomplished for each missile. 2.3.

a. Leading Edge of Wings – Undamaged

b. Missile Skin – Smooth and undamaged

c. Missile Outer Coating – Undamaged

Accept or reject based on mission requirements.

d. Exhaust Nozzle – Undamaged and unobstructed

T.O. 1B-52H-34-2-8

2-5

e. Tail Fin Assembly – Undamaged and secure

f. IR Window – Checked

No visible scratches, cracks, or dirt.

g. Air Data Probe & Static Port Plate – Checked

No dents or obstructions.

h. Missile 1760 Umbilical Connector – Connected between pylon and missile

i. Umbilical Restraint – Closed, Cam lock fastener secure.

j. Umbilical Lanyard – Quick release pin inserted in B hole

T.O. 1B-52H-34-2-8

2-6

EXTERIOR INSPECTION (POWER OFF) (RN/N) (Cont)

With WIU power applied, extremely hightemperatures exist on the air data probeand static port plate.

T.O. 1B-52H-34-2-8

Change 2 2-7

AFTER ENGINE START (Aircraft Power and Cooling Air Available)

MISSILE CHECK (RN/N)

NOTE

For proper operation, the JASSM requires GPS almanac data to be less than twoweeks old to be considered valid. Since the primary source of almanac data forthe missile is the B-52 GPS Interface Unit, which retrieves the data from the GPSreceiver’s non-volatile memory, the crew should ensure that the GPS receivercontains the current almanac data prior to applying missile power (28 vdc #1)to any JASSM missile. If the GPS almanac data age is unknown, or the GPS IUhas not been operated within the last two weeks, the crew should accomplishsteps 1 through 4.

1. GPS Power – On (if required) (N)

Apply power to the GPS and GPS IU in accordance with GPS Power Turn-on in OAS, EVS, andRADAR TURN-ON CHECKLIST of T.O. 1B-52H-1-12.

Wait a minimum of 12.5 minutes after the receiver indicates tracking of satellites. This allows the receiv-er to complete the initialization process and store current almanac data in its non-volatile memory.

2. GPS Power – Cycle (if required per Note above) (N)

Cycle GPS IU power. This causes the IU to retrieve the almanac data from the GPS receiver.

3. GPS Crypto Keys – Load (if required) (N)

Load weekly crypto keys into the IU in accordance with GPS Initialization OAS, EVS, AND RADARTURN-ON CHECKLIST of T.O. 1B-52H-1-12.

4. Less [AMI] JASSM SMO – Reload (CF-62,n) (if required) (N)

4. [AMI] JASSM SMO – Reload (CF-62) (if required) and checked primary (N)

5. PKB KEYS Indication – KEYS PRESENT (N)

Ensure keys are validated by observing the PRESENT indication on the PKB.

6. Simulation Mode (CF-52 or [AMI] CF-51) – Entered (if applicable) (N)

The system must be in STRIKE (CF-50) mode to enter simulation mode.

7. MISSILE LNCH MODE Switch – As briefed (N)

8. FRMT-7 – Entered

T.O. 1B-52H-34-2-8

2-8

MISSILE CHECK (RN/N) (CONT)

9. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – ON

Apply WIU power to missile loaded locations.

• Due to overheating of the Non-Interruptible Direct Current (NDC) power sup-ply, WIU operation on the ground without cooling air being supplied directly tothe right wing root is limited to 2 minutes.

• To reapply WIU power on the ground without cooling air being supplied tothe right wing root, a minimum cool down period (power off) of 20 minutesis required between power applications.

Status windows for each missile will be blank before WIU power is turned ON and, while WIUpower is ON, will show weapon type as M1 and status of OF (off).

10. WCP Location/Station (Missile Loaded Stations) – Selected

11. WCP Weapon Power Switch – ON

12. Missile Type – Checked (all missiles)

13. WIU & Ejector Faults Not Present – Checked

14. WCP Location/Station (Missile Loaded Stations) – Selected

15. WCP Weapon Power Switch – OFF

16. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – Off

T.O. 1B-52H-34-2-8

Change 2 2-9

INFLIGHT PROCEDURES

AFTER TAKEOFF (RN/N)

1. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – ON (if required)

Applying WIU power (without JASSM weapon power) with the JASSM SMO loaded provides 115VAC anti-ice heater power to the JASSM.

Without proper warm-up time, icing can degrade the missile pitot-static sys-tem such that mission failure could occur. Ensure the JASSM heater power isapplied (WIU ON) at least 15 minutes prior to launch. If icing conditions areencountered prior to 15 minutes of heater operation, then a minimum warm-up time of 30 minutes is required prior to launch.

MISSILE POWER APPLICATION (N)

1. [AMI] JASSM SMO – Primary (CF-62x), if not previously accomplished.

NOTE

The prime OAS navigation mode must be GPS-aided inertial, Doppler-aidedinertial, or free inertial prior to missile power application. If the alternatenavigation model is commanded as prime during missile alignment, JASSMmissile alignment is interrupted, weapon power is removed and a correspond-ing xy:COMM NOGO JASSM master fault is displayed for each missile.

2. Missile Status Check: (N)

a. FRMT-7 – Entered

NO KEYS, in reverse video, is displayed in the Crypto Key Status until validated during initiali-zation.

b. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – ON

Ensure WIU power is available to missile loaded locations.

c. Missile Type – Checked (all missiles)

Status windows for each missile will be blank before WIU power is turned ON and, while WIUpower is ON, will show WEAPON TYPE as M1 and WEAPON STATUS of OF (off).

d. WIU & Missile Faults Not Present – Checked

Check for missile related faults; transient faults are possible.

T.O. 1B-52H-34-2-8

2-10 Change 3

MISSILE POWER APPLICATION (Cont)

3. Weapon Control Panel:

a. Desired Location(s) – Selected

b. Desired Station(s) – Selected

c. WPN PWR Switch – ON

The WEAPON TYPE on FRMT-7 shows M1 for the missile and the WEAPON STATUS changesfrom OF to ON. The WEAPON/GPS STATUS changes from WU to BT (IBIT) to IN and then toMG. It may take up to 13.5 minutes after WIU power application for warmup to complete. IBITwill not begin until warmup is complete. See Section VII for warmup and IBIT times. FollowingIBIT, WEAPON STATUS changes from ON to GO.

NOTE

Exposure of the JASSM to ambient skin temperatures below –49° F (–45° C)may result in weapon BIT [FAIL] indications and/or missile failures. Refer toJASSM LOW TEMPERATURE OPERATIONS, Section VI.

4. Missile Auto Targeting – Checked

a. [AMI] AUTO TGT (CF-58) – Checked ON

b. FRMT-7 – Entered

When a missile has been assigned to a launch point number and targeting has been initiated, thestatus changes from blank to nn (nn = JASSM launch point number 1 to 99), and is displayed in brightvideo. Once targeting data has been loaded and verified nn changes to bright underlined video. Mis-sion group number changes from blank to a (where a = A to F).

MISSILE TARGETING PROCEDURES (RN-N)

NOTE

• Upon completion of missile warm up, the automatic targeting process cantake up to 24 minutes (2 minutes per missile) and cannot be interrupted.

• An in depth discussion of missile targeting procedures is contained in Section VII.

MISSILE/TARGET ASSIGNMENT (MANUAL TARGETING) PROCEDURES

NOTE

• A CF-DE command can be entered to abandon the manual targeting operationat any time. When a CF-DE command is entered, the manual targeting operationis terminated, and all associated targeting displays will remain displayed andupdated. Data modification will be inhibited. The targeting availability statusfor each location/station will continue to be displayed. All remaining windowswill be blank.

• The manual targeting operation is active from the time that a valid CF-586 com-mand is entered until a CF-DE command is entered or until the manual targetingdisplay is replaced by another display on all MFDs where the manual targetingdisplay is selected. A CF-DD command will not terminate the manual targetingoperation. When the selected missiles have been targeted following a CF-DDcommand, another or the same launch point can be selected for manual targetingby entering a MDFY-1 command and repeating this process.

• Only one manual targeting process may be active at a time. Use caution whenmodifying the same manual target on multiple screens, as data input by one oper-ator can be overwritten by the other operator.

T.O. 1B-52H-34-2-8

2-11

1. MISSILE LNCH MODE Switch – MAN2. CF-586 – Entered

Upon entry of a valid CF-586 command, the CF-586 display will be presented on the selected MFD.The location and station of each missile that is present will be displayed on MFD. The columnlocations are assigned from left to right across the screen in the preferred launch sequence (figure2-1). The video mode of the field indicates the missile’s targeting availability status. This status iscontinually updated while the manual targeting display is present on an MFD.

3. MDFY-1 – EnteredEnter MDFY-1 to copy line 1 to the MFD command line for modification.The information contained on line 1 will be copied to the MFD command line as:

1 LAUNCH POINT (1 - 99) nn MISSION GROUP (A–F) a

NOTE

Modifiable fields are shown in boldface for convenience, but are highlightedas defined when displayed on the MFD.

4. Desired JASSM Launch Point Number, nn, & Desired Mission Group Identifier, a – Entered

Key in JASSM Launch Point Number, nn (nn = 01 to 99), and Mission Group identifier, a (a = A to F).After the desired data is keyed in, press the ENTER key.

5. MDFY-6 – Entered

6. Location/Station of Missile to be Retargeted – E or 0 entered (as required)Location/Station Selection Status on Missile/Target Assignment Display indicates an E to reflectmissile selected and an 0 to reflect missiles not selected.

Entry of CF-586 and selection of a JASSM does not prevent that missile frombeing launched at the target to which it was previously assigned if the missileis in LAR prior to a CF-DD command.

NOTE

If more than one weapon is selected, all selected weapons will have ranginginhibited, until corrected by the operator. The operator should either correctthe desired missile entry, using CF-DE, or leave the CF-586 screen to removethe inhibit.

7. CF-DD – Entered

If the missile selected is the missile to be targeted enter CF-DD to initiate the transfer of the target-ing data to the selected missiles.

8. FRMT-12 – EnteredDetermine if the selected missiles are to receive the targeting data associated with the designatedmissile launch point and mission group. This is done by viewing each location/station displayed incombination with the corresponding missile selection indicator. The possible display combinationsand the Select/Deselect process are described in Section VII.

9. FRMT-7 – EnteredWhen a missile has been assigned to a JASSM launch point number and retargeting has been initi-ated, the status changes from blank to nn (nn = JASSM launch point number 1 to 99), and is dis-played in bright video. Once retargeting data has been loaded and verified, nn changes to brightunderlined video. Mission group identifier a (where a = A to F) changes to bright video.

T.O. 1B-52H-34-2-8

2-12

Missile Preferred Launch Sequence

If there is a retained/HUNG center station store, launching/jettisoning an ad-jacent shoulder station may result in a Store-to-Store Contact. When a centerstation store is retained/HUNG, operators will retain the adjacent shoulderstation stores.

Figure 2-1

T.O. 1B-52H-34-2-8

Change 3 2-13

DIRECT TARGETING DATA ENTRY PROCEDURES

NOTE

• To perform the direct targeting operation, the Direct Target Definition Dis-play (CF-588,n) must be displayed on the selected MFD.

• Only one direct target may be modified at a time. Use caution when modifyingthe same direct target on multiple screens, as data input by one operator can beoverwritten by the other operator.

• A CF-DE command can be entered to exit the direct target definition opera-tion without downloading data to the missile at any time prior to entry of aCF-DD command. When a CF-DE command is entered, the direct target defi-nition operation is terminated, data modification is inhibited, and the speci-fied direct target number will remain displayed on the top of the MFD. Thetargeting availability status for each location/station will continue to be statu-sed. All remaining windows are blanked. The direct target data will not besaved if a CF-DE command is entered. The previous direct target data ismaintained.

• Performing direct targeting for an already targeted weapon while CDE is inprogress will result in a misleading FRMT-7 display. Allow the CDE to com-plete, then recommand the desired targeting operation after re-powering onthe weapon.

1. MISSILE LNCH MODE Switch – MAN

2. CF-588,n – Entered

n (1 to 6) is the number of the direct target to be defined.


The information contained on line 1 is copied to the MFD command line as follows:

1 TGT PT addomm.mmmm adddomm.mmmm fffff ’ Less [AMI] r

NOTE

Modifiable fields are shown in boldface for convenience, but are highlightedas defined when displayed on the MFD.

4. Desired Target Point Latitude, Longitude, Elevation, Less [AMI] and Elevation Reference – Entered

addomm.mmmm is the target latitude in degrees, minutes, and ten-thousandths of a minute. a =N for North and S for South. dd = degrees from 0 to 90. mm.mmmm = minutes from 00 to 59 andten-thousandths of a minute from 0000 to 9999.

adddomm.mmmm is the target longitude in degrees, minutes, and ten-thousandths of a minute. a= E for East and W for West. ddd = degrees from West 180 to East 179. mm.mmmm = minutes from00 to 59 and ten-thousandths of a minute from 0000 to 9999.

fffff is the target point elevation in feet (MSL Less [AMI] or HAE). Input ranges from –328 to 32810feet.

Less [AMI] r is the target elevation reference. Valid input is 0 or 1. 0 represents a measurementof MSL for the target point elevation while 1 indicates HAE.

The entered latitude, longitude, elevation, and Less [AMI] target elevation reference will be dis-played on line 1.

T.O. 1B-52H-34-2-8

2-14

DIRECT TARGETING DATA ENTRY PROCEDURES (Cont)


The information contained on line 2 is copied to the MFD command line as:

2 CRUISE ALT fffff’

6. Desired Cruise Altitude – Entered

fffff is the desired cruise altitude in feet MSL. Valid input range is from 0 to 45000 ft. Prior tooperator entry the default value of 99999 (representing 15000 ft) is displayed.

The entered cruise altitude is displayed on line 2.



3 BRNG TO TGT bbb° IMPACT ANGLE dd°

8. Desired BRNG TO TGT & Impact Angle – Entered

bbb° is the missile’s Bearing to Target in degrees. Valid input range is from 0 to 360 degrees true(0 = North) or 999. The default value of 999 is displayed prior to operator entry. The default valueindicates the missile will determine it’s bearing to target from the aircraft to the target at time oflaunch.

NOTE

If 360 is entered by the operator, the resulting display will be 0.

dd° is the desired impact angle for the missile. Valid input range is from 0 (level) to 90 (vertical)degrees, however, the missile will only use an impact angle ranging from 20 to 70 degrees. Thedefault angle of 60° is displayed prior to operator input.

NOTE

If less than 20 degrees is entered on CF-588, the missile will use a built-inminimum impact angle value of 20 degrees. The missile will use a built-inmaximum value of 70 degrees, if more than 70 degrees is entered on CF-588.FRMT-12 displays the impact angle actually being used by the missile. Whilein SIM mode, the FRMT-12 impact angle displayed is the same as the CF-588value input.

The entered Range on Bearing and Bearing to Target is displayed on line 2.



4 FUZE MODE n XXXX

10. Desired Fuze Mode Identifier – Entered

n is the missile’s fuze impact setting. Valid inputs for fuze mode are 1 (Soft Impact) and 2 (HardImpact). The default value of 1 will be displayed prior to operator entry.

The entered fuze mode will be displayed on line 4. The corresponding fuze mode of SOFT or HARDwill also be displayed.

T.O. 1B-52H-34-2-8

2-15




5 FUZE DELAY n (0-7)

12. Desired Fuze Delay – Entered

n is a single digit that corresponds to themissile’s fuze delay in milliseconds. Validinput values for fuze delay are 0 through 7.The millisecond delay corresponding to thenumber is listed in the figure to the right.


0 0

1 10

2 15

3 20

4 30

5 40

6 50

7 120

Select/Deselect Missile(s) to be assigned to the designated target as follows:


The information contained on line 6 is copied to the MFD command line.

14. Missiles – Selected

For each missile that is to be selected, overwrite the 0 with an E. For each missile that is to bedeselected, overwrite the E with a 0. Selected missiles are not assigned to a direct target until aCF-DD command is entered.

NOTE

If more than one weapon is selected, all selected weapons will have ranginginhibited, until corrected by the operator. The operator should either correctthe desired missile entry, using CF-DE, or leave the CF-586 screen to removethe inhibit.

If more than one missile is selected, the difference is displayed in the Missiles Selected window asa negative number in reverse video. If fewer missiles were selected than required, the difference isdisplayed in normal video. The contents of the display will be updated to show which missiles areassigned.

If more missiles are selected than required, the least preferred missiles will be deselected by the SMOto reduce the number of missiles selected to the number of missiles required for the designated targetwhen a CF-DD command is entered. The data is updated with a 0 displayed in normal video, and willthen be updated to show which missiles are assigned.

T.O. 1B-52H-34-2-8

2-16


15. CF-Dn Direct Target Copy – Entered (if required)

Copy direct target information to direct target, as required.

16. CF-DD – Entered

If no other missile is to be selected, enter CF-DD to save the direct target data and initiate thedownloading of the targeting data to the selected missile.

NOTE

If no missiles are selected and a CF-DD command is entered, the data for thedesignated direct target is saved, but the direct target will not be defined.

Selected missile is set as untargeted.

NOTE

Selected missile will no longer be targeted to its previous target.

The SMO will initiate the transfer of the targeting data to the selected missile. Selected missilesthat do not have power applied are assigned but not targeted. The order of selected missiles is basedon the preferred launch sequence.

Data modification is inhibited and associated targeting displays will remain displayed and updatedas follows:

LOADING is displayed in bright blinking video while the data is being downloaded to a missile.

The specified direct target number will remain displayed, The targeting availability status for eachlocation/station window will continue to be statused. All remaining windows are blanked out.

17. FRMT-7 – Entered, if desired

The targeting process of each selected missile can be monitored on the FRMT-7 display. The CF-588display is updated as follows:

If the transfer of targeting data to all selected missiles completes successfully:

If direct targeting data is subsequently modified. an * will be displayed to the right of theMission Group Identifier.

COMPLT is displayed in normal video. The location/station of assigned missiles is displayedin bright underline video in the appropriate window. All modifiable windows and the WPNSTO SELECT window will be blank.

If the transfer of targeting data to any of the selected missiles completes unsuccessfully:

COMPLT is displayed in reverse video and a corresponding advisory/master fault messageis displayed to indicate which failure occurred. The location/station of each missile that wasnot successfully targeted is displayed in reverse video in the appropriate window. Data willremain displayed in all modifiable windows and in the WPNS TO SELECT windows. Themissile will retain the previously selected targeting data.

T.O. 1B-52H-34-2-8

2-17

LAUNCH PROCEDURES

MISSILE PREPARATION FOR LAUNCH (RN-N)

NOTE

• These checklists should be completed prior to the HEW, IP (high altitudelaunch), or descent (low altitude launch).

• A transfer alignment maneuver is not required for JASSM operation.

1. Cabin Pressurization – COMBAT (if applicable) (CP)

2. Personal Locator Beacon Lanyards – Set as briefed (All)

3. Exterior Lights – As briefed (P)

4. Jettison Power & Jettison Control Circuit Breakers – In (RN)

5. Missile Status Check: (N)

a. FRMT-7 – Entered

b. Missile Targeting - Checked

A missile has been assigned to a launch point number and targeting has occurred, the statusdisplays nn or Dn (nn = JASSM launch point number 1 to 99, Dn = JASSM direct target numberD1 to D6), in bright underlined video. Mission group number displays an a (where a = A to F)in bright video.

c. Missile Status - Checked

The missile should be powered on and should indicate a GO status.

T.O. 1B-52H-34-2-8

2-18 Change 1

MISSILE LAUNCH PROCEDURES

BEFORE LAUNCH CHECK (RN)

1. Fuel Transfer – Accomplished (if required) (RN, CP)

2. HAC/LAC – Cross checked

B-52 Operators must be aware that the Inertial/GPS aided munitionsuse the transfer alignment data (latitude, longitude, altitude, etc.) ofthe aircraft prime navigation model. Buffers are not incorporated/transferred to the Inertial/GPS aided munitions. This navigation trans-fer applies to a prime navigation model with, or without, GPS aiding.Failure to recognize this condition may result in weapons impactingother than the intended target or failing to release due to LAR consid-erations. Refer to MAJCOM or Theater specific guidance for degradedweapon release ROE.

3. Circuit Breakers – Checked (RN-N)

Check all lower deck circuit breakers. Ensure all release associated circuit breakers are in the properconfiguration for the planned launch.

4. Prime NAV Mode – Selected (RN)


6. Missile Launch – Review (All)

Review number of missiles and data for each missile including missile location, total time to launchmissile, run in heading, turn direction, altitude, airspeed, launch mode, and egress maneuver, ifapplicable.


NOTE

During In-Zone JASSM launch operations, it is highly recommended thatcrews use the AUTO launch feature. The JASSM SMO incorporates an 8 sec-ond “look back” feature to preclude the system from falling into In-Range (i.e.,a heading tolerance problem) just prior to launch. If the aircraft was In- Zoneduring the 8 seconds prior to the at or abeam launch point, the weapon willfly the planned In-Zone mission. If the missile was to fly an In-Range profile,all preplanned autorouting data would be lost, as the missile determines it’sown profile.

T.O. 1B-52H-34-2-8

2-19

AUTOMATIC MISSILE LAUNCH CHECKLIST (RN-N)

1. Pilot’s Munitions Consent Panel LOCK/UNLOCK Switch – UNLOCK (P)

2. Master Fault Light – ON (RN)

3. WCP LOCK/UNLOCK Switch – UNLOCK (RN)

4. Master Fault Light – OFF (RN)

5. FLY-TO nn – Entered (as required)

6. Missile Status – GO (N)

7. PRGM – Entered (N)

a. Ranging – Monitor

Ranging is being performed for the current JASSM launch point.

b. TTG-Z – Monitor

TTG-Z (Time-To-Go to In-Zone) decreases to zero and changes to ZONE 00:00 in bright under-lined video to indicate the missile is in zone. The time remaining In-Zone will be displayed inthe window immediately to the right of the ZONE 00:00, and will begin to decrease. In theAutomatic launch mode, the JASSM will begin launch countdown to launch at, or the closestpoint of approach to, the planned launch point.

8. MISSILE LNCH MODE Switch – AUTO

• During a weapon launch, do not enter PRGM-Dn or CLR-D until the weaponAWAY advisory has been displayed or the launch may be aborted.

• Switching the MISSILE LNCH MODE switch from AUTO to MAN during thelaunch countdown may result in an ABORT.

9. Launch Countdown – Monitored (N)

NOTE

Launch will take 3.5 seconds maximum from countdown entry to AWAY.

10. Missile Status Indication – xy AWAY

xy AWAY is displayed for 5 seconds at the bottom of the MFDs.

11. Notify Crew – “Missile Away” (RN)

12. Egress Maneuver As Briefed – Called after release of the missile (N); Performed (P)

13. MISSILE LNCH MODE Switch – As required

T.O. 1B-52H-34-2-8

2-20

MANUAL MISSILE LAUNCH CHECKLIST (RN-N)

NOTE

Manual Launch is required if:• The missile is targeted to a Direct Target.• The missile has no waypoint data.• The aircraft is beyond the closest point of approach and is still In-Zone.

1. Pilot’s Munitions Consent Panel LOCK/UNLOCK Switch – UNLOCK (P)


3. WCP LOCK/UNLOCK Switch – UNLOCK (RN)



6. Missile Status – GO (N)

7. PRGM/PRGM Dn – Entered (N)

a. Ranging – Monitor

Ranging is being performed on the selected (PGRM or PGRM Dn) JASSM target event.

b. TTG-R – Monitor

TTG-R (Time-To-Go to In-Range) decreases to zero and changes to RANGE 00:00 in bright under-lined video to indicate the missile is in range. The time remaining In Range will be displayedin the window immediately to the right of the RANGE 00:00, and will begin to decrease. In theManual launch mode, JASSM launch of a GO missile can be commanded upon entering RANGE00:00.

c. TTG-Z – Monitor

TTG-Z (Time-To-Go to In-Zone) decreases to zero and changes to ZONE 00:00 in bright under-lined video to indicate the missile is in zone. The time remaining In Zone will be displayed inthe window immediately to the right of the ZONE 00:00, and will begin to decrease. In theManual launch mode, JASSM launch of a GO missiles can be commanded upon entering ZONE00:00.

Pressing the MAN LNCH switch more than once during step 8 may stop thelaunch countdown and result in an ABORT.

8. MISSILE MAN LNCH Switch – Pressed

During a weapon launch, do not enter PRGM-Dn or CLR-D until the weaponAWAY advisory has been displayed or the launch may be aborted.

9. Launch Countdown – Monitored (N)

NOTE

Launch will take 3.5 seconds maximum from countdown entry to AWAY.

T.O. 1B-52H-34-2-8

2-21

MANUAL MISSILE LAUNCH CHECKLIST (RN-N) (Cont)

10. Missile Status Indication – xy AWAY

xy AWAY is displayed for 5 seconds at the bottom of the MFDs.

11. Notify Crew – “Missile Away” (RN)

12. Egress Maneuver As Briefed – Called after release of missile (N); Performed (P)

T.O. 1B-52H-34-2-8

2-22 Change 2

POST STRIKE/ABORT PROCEDURES

POST STRIKE/ABORT (RN/N)

NOTE

• Accomplish the following for mission abort when no further launchesare to be attempted.

• The MASTER CAUTION light will come on and remain on any timethere is a disagreement between the pilot and navigator unlockswitches.

1. Weapon Control Panel LOCK/UNLOCK Switch – LOCK (RN)


3. Munitions Consent Panel LOCK/UNLOCK Switch – LOCK (P)



6. Jettison Power & Jettison Control Circuit Breakers – Out (RN)

7. FRMT-7 – Entered

8. LP & RP Location & ALL Station – Selected

9. Classified Data Erase (CF-575):

a. CF-575 – Entered

b. CLSF Data Erase Question – Answer YES

A CDE COMPLT ([AMI] JASSM CDE COMPLT) message will be displayed below each missileon FRMT-7 and at the bottom of the MFD when classified data erase is complete. Missiles willbe automatically powered off.

10. Missile Status – Checked

Missile status should change to OF, alignment status and targeting status should be blank.

NOTE

If any JASSM remains aboard, but is not hung, delay step 11 until after landing.

11. MIU Power Switches – OFF

T.O. 1B-52H-34-2-8

2-23/(2-24 blank)

AFTER LANDING PROCEDURES

GROUND SAFEING PROCEDURES (RN-N)

Flight crew will notify ground crew personnel and will use caution regardingpotential hot spots on the missile at the air data probe and static plate. Con-tacting these hot spots with unprotected skin should be avoided. Requiredcool down time is comparable to that for the aircraft pitot tubes.

NOTE

If missiles are retained on the aircraft and qualified maintenance personnelare not available, missile release system safeing procedures must be accom-plished by the navigator and radar navigator using the following checklist.Do not apply power until ground safety lockpins are installed.

1. MAU-12 Ground Safety Lockpin(s) – Installed

BLA

T.O. 1B-52H-34-2-8

3-1

Emergency Aircrew Procedures section III


INTRODUCTION 3-1

MISSILE JETTISON 3-2

SELECTIVE JETTISON USING THE WCP/SMO 3-3

SELECTIVE JETTISON USING THE AJCP 3-4

EMERGENCY JETTISON 3-5

NOTIFICATION PROCEDURES - DANGEROUS MATERIALS 3-6

FIREFIGHTING AND EVACUATION CRITERIA 3-7

INTRODUCTIONEmergency procedures listed in this section are spe-cific to the JASSM. If a weapon malfunction or air-craft emergency occurs, contact a command authori-ty, if necessary, and proceed as directed. If contactcannot be made and jettison is required, see MISSILEJETTISON checklists. The JASSM jettison envelopeis contained in Section V.

NOTE

When a JASSM is retained/HUNG it shouldbe monitored visually, if possible, until jetti-soned or, if not jettisoned, it should be peri-odically monitored visually (when possible)until after landing.

T.O. 1B-52H-34-2-8

3-2

MISSILE JETTISON

Missile Preferred Jettison Sequence


Figure 3-1

T.O. 1B-52H-34-2-8

Change 2 3-3

SELECTIVE JETTISON USING THE WCP/SMO

• The weapon SMO has no interlocks preventing jettison on the ground. Withunlock consent, and power applied to the OAS and the WIU, actuation ofWeapon Control Panel Jettison Select switch while the aircraft is on theground will result in jettison of the selected weapon(s).

• If there is a retained/HUNG center station store, launching/jettisoning anadjacent shoulder station may result in a Store-to-Store Contact. When acenter station store is retained/HUNG, operators will retain the adjacentshoulder station stores.

NOTE

Selective jettison using the WCP is the preferred method of jettison whenOAS is loaded and operating with the weapon SMO loaded [AMI] as the pri-mary SMO.

1. Crew – Alerted (RN)

2. Command Authority – Contacted, if necessary (P)

3. Impact Area – Cleared (P-CP-RN)

Clear area visually and/or by radar to the maximum extent possible.

4. OAS Master Power – ON (N)

5. Processors – Loaded (N)NOTE

The OAS and the JASSM SMO must be loaded ([AMI] as the primary SMO) andoperating to enable jettison.

6. [AMI] JASSM SMO – Primary (CF-62x) (N)

7. MIU Power Switches – ON (pylon location of weapon(s) to be jettisoned) (RN)

8. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – UNLOCK (P)


10. WCP Nuclear LOCK-UNLOCK Switch – UNLOCK (RN)


12. Location & Station Switches (Weapon(s) To Be Jettisoned) – Selected (RN)

13. Classified Data Erase (CF-575):a. CF-575 – Enteredb. CLSF Question – Answer YES

A CDE COMPLT ([AMI] JASSM CDE COMPLT) message will be displayed below each weaponon FRMT-7 and at the bottom of the MFD when classified data erase is complete. Missiles willbe automatically powered off.

14. Location & Station (Weapon(s) To Be Jettisoned) – Selected (RN)

15. WCP Jettison Select Switch – Select (1 second) (RN)

16. Jettison Monitored – Weapon(s) AWAY (RN)

17. WCP Nuclear LOCK-UNLOCK Switch – LOCK (RN)


19. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – LOCK (P)


T.O. 1B-52H-34-2-8

3-4 Change 2

SELECTIVE JETTISON USING THE AJCP

• The AJCP has no interlocks preventing jettison on the ground. With unlockconsent, and power applied to the aircraft, actuation of AJCP switches whileon the ground will result in weapon jettison.


NOTE

• Selective jettison using the WCP is the preferred method of jettison if theOAS is loaded and operating with the weapon SMO loaded [AMI] as theprimary SMO.

• If AJCP jettisons are commanded with OAS loaded and operating with theweapon SMO loaded and the WIU(s) powered, the WIU will be powered offby the OAS. An uncommanded EED power available fault will be displayedby OAS.









8. AJCP Pylon Power Switch (Location Of Weapon To Be Jettisoned) – LEFT or RIGHT selected (N)

POWER and STORES jettison light, PWR, will be on while the PYLON POWER Switch is in theleft or right position.

9. AJCP JETTISON Station Select Switch (Weapon To Be Jettisoned) – Actuated (N)

POWER and STORES jettison light, JET, will be on while the JETTISON Switch is in the left orright position.





T.O. 1B-52H-34-2-8

Change 3 3-5

EMERGENCY JETTISON

• The pilots’ Bomb Bay & Missile Jettison Control switch jettisons all GWD andactive/primary SMO controlled weapons loaded on the aircraft and will only beused as a backup to jettison by the Radar Navigator. If jettison is commandedusing the pilots’ Bomb Bay & Missile Jettison Control switch, all GWD weaponsand, with OAS operating and MIUs/WIUs powered, all active/primary SMO con-trolled weapons will be jettisoned. Proper separation clearance between weap-ons and between weapons and aircraft cannot be ensured.

• The JASSM SMO has no interlocks preventing jettison on the ground. Withunlock consent and power applied to the OAS and the WIU, actuation of thepilots’ Bomb Bay & Missile jettison control switch while on the ground willresult in weapon jettison.






4. Jettison Control & Jettison Power Circuit Breakers (2) – In (RN/N)

5. OAS Master Power – ON (N)

6. Processors – Loaded (N)

NOTE

The OAS and the JASSM SMO must be loaded, [AMI] as the primary SMO, andoperating to enable jettison.

7. [AMI] JASSM SMO – Primary (CF-62x) (N)

8. MIU Power Switches – ON (pylon location of weapon(s) to be jettisoned) (RN)





13. Pilots’ Bomb Bay & Missile Jettison Switch - Pressed (momentarily) (P)

NOTE

After weapons have been released perform the following.

14. Jettison Monitored - Weapons AWAY (RN)





19. Jettison Control & Jettison Power Circuit Breakers (2) – Out (RN/N)

T.O. 1B-52H-34-2-8

3-6

NOTIFICATION PROCEDURES – DANGEROUS MATERIALS

Procedures for alerting the fire department andother base support elements for aircraft carryingdangerous materials are as follows:

DEFINITION OF TERMS

Definitions of some of the terms used in communi-cations are as follows:

• Dangerous Materials: Any material that isflammable, corrosive, an oxidizing agent, explosive,toxic, radioactive, nuclear, unduly magnetic, or bio-logically infective or any other material that (be-cause of its quantity, properties, or packaging) mayendanger human life or property.

• Firefighting Time: A period that begins whenthe material becomes enveloped in flames and ter-minates when the material can be expected to deto-nate, deflagrate, or begin burning.

• Withdrawal Distance: The minimum permissi-ble distance, between firefighters, rescue, and/ornonessential personnel and the site of the accident(fire/detonation), without protective barricades.

• Department of Transportation (DOT) Classifica-tions: Classifications established by DOT for handl-ing dangerous materials in transit. They defineclasses of dangerous materials.

• Inert Devices: Devices containing no dangerousmaterial but closely resembling nuclear or explosiveitems that are classified as dangerous.

• Net Explosive Weight (NEW): The actual (orhigh explosive equivalent) weight of explosive sub-stances contained within a munition/weapon to beused when applying quantity – distance criteria orother standards.

NORMAL NOTIFICATION PROCEDURES

It is the responsibility of the major command con-cerned to ensure that all required information istransmitted to departure and destination (primary/alternate) bases far enough in advance to ensureadequate preparation before the departure/arrivalof aircraft carrying dangerous materials.

AIRCRAFT COMMANDER’S RESPONSIBILITIES

The aircraft commander must ensure that his crewmembers thoroughly understand the operationalmission requirements and procedures governing thedangerous materials to be airlifted. He will complywith applicable backup and emergency inflight no-tification procedures, plan flight routes to avoidoverflight of heavily populated or otherwise criticalareas, and refuse to accept any ATC clearance that,in the aircraft commander’s judgment, would inter-fere with operational necessity or flight safety. Foreach flight ‘‘Dangerous Cargo,’’ ‘‘Inert Devices,’’ orboth (as appropriate) will be entered in the ‘‘Re-marks’’ section of the DD Form 175 or ‘‘Other Infor-mation’’ section of the DD Form 1801 (ICAO FlightPlan) unless prohibited by regulations governingthe area of operation.

BACKUP NOTIFICATION PROCEDURES

If the ETE is less than 1 hour or if other known cir-cumstances will preclude timely receipt of informa-tion, the aircraft commander will contact the baseof intended landing by priority telephone and pro-vide tactical call sign, ETA, DOT class of dangerousmaterial aboard, DOD quantity-distance class(when applicable), NEW (total weight in pounds ofall DOT Class A and Class B explosives on board),withdrawal distance and firefighting time (if as-signed), request for special handling (if required),inert devices (when applicable) and line numbersand quantities (if applicable).

INFLIGHT NOTIFICATION PROCEDURES

At least 30 minutes (or as soon thereafter as practi-cal) before the ETA, the aircraft commander willcontact the base operations dispatcher, control tow-er, approach control, or other agency specified inthe applicable FLIP announcing that he has dan-gerous material and to verify receipt of arrival noti-fication. If advance notice has not been received, re-quest that the information stated in backup notifi-cation procedures, be relayed to the military baseoperations or civil airport manager to pass to appro-priate base support elements (Example: ‘‘Bird 51,ETA – 1200Z, DOT Class A explosives, DOD class7, ‘‘NEW’’ four zero pounds, four zero zero zero feet,3 minutes, request isolated parking, four each M-XXX bombs in bomb bay. Please relay immediatelyto fire department and other base support ele-ments.’’)

T.O. 1B-52H-34-2-8

3-7/(3-8 blank)

INFLIGHT EMERGENCY NOTIFICATION PROCEDURES(WORLD WIDE)

Under inflight emergency conditions or for un-scheduled landings, the aircraft commander will in-form the appropriate Air Traffic Control Facility ofthe nature of the emergency, his intentions, and, aspracticable, the information as stated in backup no-tification procedures. (Example: ‘‘Bird 51, 60 mileseast of intended landing base – Nest AFB, No. 1and 2 engines out; six personnel, forward section ofaircraft; have dangerous cargo in bomb bay of air-craft, four zero pounds of DOT class A explosives; ifexplosives become enveloped in flames, detonationmay be expected after 3 minutes; withdrawal dis-tance is 2000 feet; 10,000 gallons of fuel remaining,apply emergency procedures accordingly.’’)

Inert Devices

If inert devices are carried, the radio call will besimilar to inflight emergency notification proce-dures (world wide), identifying the devices as inert,that they present no hazard, and including theamount of fuel remaining. (Example: ‘‘Bird 51, 60miles east of intended landing base – Next AFB,No. 1 and 2 engines shut down, six personnel for-ward compartment, inert cargo in bomb bay of air-craft; no hazard; 10,000 gallons fuel remaining; ap-ply emergency procedures accordingly.’’)

CONUS Civil Airports

When aircraft must land at a CONUS civil airportwhich has no control tower, information in inflightemergency notification procedures (world wide), asapplicable, will be furnished to the nearest FAAFlight Service Station.

Aircraft Ditching/Abandonment

If the aircraft must be ditched or abandoned, recordthe coordinates and descriptive location of aban-doned cargo for later use by appropriate authori-ties.

FIREFIGHTING AND EVACUATION CRITERIA

These emergency procedures consist of actions totake if munitions are involved in a fire. The aircrewshould be thoroughly familiar with these instruc-tions.

Aircraft fires involving conventional munitions can-not be definitized to any one set of circumstancesand environmental conditions. This precludes de-velopment of reliable standardized test criteria andreliable specific item firefighting and withdrawaltimes. The conclusion to be reached from availabledata is that a munitions reaction to fire is a func-tion of case thickness and type of explosive fillerwhich can be varied by environmental conditions.Since the circumstances of a fire cannot be pre-dicted, specific item by item firefighting and with-drawal times cannot be determined with any degreeof reliability.

Normally, aircraft fire involving munitions occursunder a set of circumstances wherein it is impossi-ble to know immediately the specific missile, bomb,or BLU model number. Such information is abso-lutely essential for specific firefighting and with-drawal times. Therefore, these times are presentedfor family groups only; i.e., bombs, BLUs, missile,etc.

• Bombs: See T.O. 1B-52H-34-2-1• CBUs: See T.O. 1B-52H-34-2-1• Missiles: Missiles normally react in a propul-sion, detonation, or both between +45 seconds and2 minutes. A propulsion hazard (missile flight) ex-ists within 45 seconds and a major hazard to envi-ronment and firefighting capability exists after 1minute. Approach the fire, if necessary, from theside of the aircraft. See figure 3-2 for specificAGM-158 data.

The firefighting guidance provided in AFI 91-201will be utilized in all instances. There is no specificwithdrawal time assigned to items which do notalign into one of the family groups mentionedabove.

Fire Fighting and Evacuation Criteria

NOMENCLATUREWITHDRAWAL DISTANCE (FT) FIRE

NONESSENTIAL PERSONNEL SYMBOL

AGM-158A 4000 1

Figure 3-2

BLA

T.O. 1B-52H-34-2-8

Change 3 4-1

Supplementary Data section IV


TEST INSTRUMENTATION KIT (TIK) 4-1

JASSM SMO FLIGHT TEST SOFTWARE COMMANDS 4-1

TEST INSTRUMENTATION KIT (TIK)

The TIK is a limited use package installed only foruse on designated flight test ranges. It provides te-lemetry of the missile in-flight data parameters andprovides for destructive flight termination in thecase of range footprint limitations being exceeded.

The TIK consists of the following major components:• Telemetry package• Transponder• Flight Termination System (FTS)

(Destruct ring, safe & arms, receivers, logicunits, battery packs)

• Antennas• Sensors• Missile aft bottom cover (TIK cover assembly)

JASSM SMO FLIGHT TEST SOFTWARE COMMANDS

NOTE

If it becomes necessary to reload theJASSM SMO and mission data, reload theSMO first.

JASSM SUPERVISION MENU (CF-57)

The JASSM Supervision Menu commanded by CF-57is shown in Figure 1-18. When the JASSM Supervi-sion Menu is displayed, the current SMO mode is dis-played just as on the Control Function Menu (CF-)and the Weapon Supervision Menu (CF-5).

NOTE

The displayed status of CF-57 commands isthe commanded state in the OAS, not themissiles status. The actual status of themissile may or may not be the same.

The control function commands that are unique tothe SMO are of the form CF-57x, where x repre-sents any of several alphanumeric characters thatmay or may not be followed by a comma and addi-tional alphanumeric characters. The JASSM Super-vision Menu displays the control function com-mands of this form that are accepted by the SMOand the function commanded by each. In addition toidentifying the CF-57x commands, the JASSM Su-pervision Menu (CF-57) also identifies other SMOcommands not identified on other JASSM displays.

TELEMETRY POWER ON COMMAND (CF-57A)(TEST ONLY)

Operator entry of CF-57A will result in enablingthe Telemetry (TM) Radio Frequency (RF) trans-mitter for selected weapon(s). The SMO will reject aCF-57A command to enable telemetry power, dis-play the command in reverse video, and display theadvisory Less [AMI] LOC/STA??, [AMI] JASSMLOC/STA??, if no location/station(s) have been se-lected on the WCP or PCP/WCP backup. The SMOwill ignore a CF-57A command to enable telemetrypower for each selected weapon where telemetrypower is already ON. The SMO will retain a validTelemetry Power On command for a selected weap-on that does not have power applied. The commandwill be processed for the selected weapon after theweapon is powered on.

If a CF-57A command is accepted, but the selectedweapon(s) cannot be accessed (for example: weaponnot present), the advisory Less [AMI] LOC/STA??,[AMI] JASSM LOC/STA??, will be displayed. A de-scription of each failure and the corresponding cor-rective action is listed in figure 7-20.

Due to RF hazards when TM power is ap-plied, ensure personnel avoid the TM an-tenna area by at least two feet.

NOTE

If either TM or FTS is commanded on andthe missile has an uncommanded powerdown, the TM and/or FTS may transition tointernal battery power. Re-applying missilepower will automatically power off the TM/FTS battery.

T.O. 1B-52H-34-2-8

4-2

JASSM Telemetry Antenna

Figure 4-1

T.O. 1B-52H-34-2-8

Change 3 4-3

TELEMETRY POWER OFF COMMAND (CF-57B)(TEST ONLY)

Operator entry of CF-57B will result in disablingthe TM RF transmitter for selected weapon(s). TheSMO will reject a CF-57B command to disable pow-er, display the command in reverse video, and dis-play the advisory Less [AMI] LOC/STA??, [AMI]JASSM LOC/STA??, if no location/station has beenselected on the WCP or PCP/WCP backup. TheSMO will ignore a CF-57B command to disable te-lemetry power OFF for each selected weapon wheretelemetry power is already OFF. The SMO will re-tain a valid Telemetry Power Off command for a se-lected weapon that does not have power applied.The command will be processed for the selectedweapon after the weapon is powered on.

If a CF-57B command is accepted, but the selectedweapon(s) cannot be accessed (for example: weaponnot present), the advisory Less [AMI] LOC/STA??,[AMI] JASSM LOC/STA??, will be displayed. A de-scription of each failure and the corresponding cor-rective action is listed in figure 7-20.

FTS ENABLE/DISABLE COMMAND (CF-57C,xy)(OTL ONLY)

Operator entry of CF-57C,xy, where xy represents avalid location/station, will result in the Flight Ter-mination System (FTS) being enabled/disabled forthe selected weapon. The FTS Enable is a test com-mand that allows the operator to terminate a weapontest flight if it is determined the weapon is posing asafety risk. If the command is entered while FTS En-able is active for the selected weapon, FTS will be-come disabled for the selected weapon. A single validlocation and station is selected on an IKB by enteringA or C followed by a number 1, 2, 3, 6, 7 or 8. The char-acters “A” and “C” represent the left or right pylonlocation respectively. The numbers represent the se-lected station on the identified pylon. The SMO willreject a CF-57C,xy command to enable FTS and dis-play the command in reverse video if any of the follow-ing conditions exist:

• Location entered is other than A (left pylon)or C (right pylon).

• Station number entered is not 1, 2, 3, 6, 7, or 8.• Weapon is not present at selected station.• Weapon is not operational selected station.• Carrier mission is not live launch with Telem-

etry (TIK) package.• Another weapon has FTS enabled.

If a CF-57C,xy command is accepted, but the selectedweapon(s) cannot be accessed (for example: weaponnot present), the advisory LOC/STA?? will be dis-played. A description of each failure and the corre-sponding corrective action is listed in figure 7-20.

The SMO will also reject a CF-57C,xy command todisable FTS and display the command in reversevideo if any of the following conditions exist:

• Location entered is not A or C.• Station number entered is not 1, 2, 3, 6, 7, or 8.

The FTS default state is disabled.

FTS POWER SOURCE COMMAND (CF-57D) (OTL ONLY)

Operator entry of CF-57D will result in FTS powersource being toggled between aircraft (carrier) pow-er and the missile’s battery power for the missilewith FTS enabled. The SMO will reject a CF-57Dcommand and display the command in reverse vid-eo, if no location/station has FTS enabled.

The FTS default power source for an enabled weap-on is aircraft power.

For Operational Test Launch (OTL) missions, theJASSM SMO will automatically command TM andFTS power off, including removal from internal bat-tery power, prior to removing initialization powerfrom the weapon in all cases, except for a normallaunch sequence. However, it is recommended thatFTS power source be manually commanded to air-craft power, and TM and FTS be manually com-manded off prior to weapon power down.

NOTE

If either TM or FTS is commanded on andthe missile has an uncommanded powerdown, the TM and/or FTS may transition tointernal battery power. Re-applying missilepower will automatically power off the TM/FTS battery.

T.O. 1B-52H-34-2-8

4-4

TRANSFER ALIGNMENT (TXA) HALT COMMAND(CF-57E,xy) (CAPTIVE CARRY ONLY)

Operator entry of CF-57E,xy while Transfer Align-ment (TXA) Halt is inactive, where xy represents avalid location/station, will result in the weapon ig-noring transfer alignment. If the command is en-tered while TXA Halt is active for the selectedweapon, TXA Halt will become inactive for the se-lected weapon. A single valid location and station isselected by IKB entry. The letters A and C are usedon the IKB to enter the left or right pylon locationrespectively. The numbers 1, 2, 3, 6, 7, or 8 are usedon the IKB to enter the selected station on the iden-tified pylon. The SMO will reject a CF-57E,xy com-mand to activate TXA Halt and display the com-mand in reverse video if any of the following condi-tions exist:


• Station number entered is not 1, 2, 3, 6, 7 or 8.• Carrier mission is not captive carry.• Weapon is not present at selected station.• Weapon has a permanent fatal fault.

The SMO will also reject a CF-57E,xy command to de-activate TXA Halt and display the command in re-verse video if any of the following conditions exist:


• Station number entered is other than 1, 2, 3,6, 7 or 8.

The SMO will retain a valid TXA Halt command fora selected weapon that does not have power ap-plied. The command will be processed for the se-lected weapon after the weapon is powered on.

TRANSFER ALIGNMENT (TXA) RE-INIT COMMAND(CF-57F,xy) (CAPTIVE CARRY ONLY)

Operator entry of CF-57F,xy, where xy represents asingle valid location/station, will result in the rein-itialization of missile transfer alignment for thatlocation/station. A single valid location and stationis selected on an IKB by entering A or C followed bya number 1, 2, 3, 6, 7 or 8. The characters A and Crepresent the left or right pylon location respective-ly. The numbers represent the selected station onthe identified pylon.

The SMO will reject a CF-57F,xy command to re-initialize TXA and display the command in reversevideo if any of the following conditions exist:


• Station number entered is other than 1, 2, 3,6, 7 or 8.

• Carrier mission is not captive carry.• Weapon is not present at selected station.• Weapon has a permanent fatal fault.

The SMO will retain a valid TXA Re-Init commandfor a selected weapon that does not have power ap-plied. The command will be processed for the se-lected weapon after the weapon is powered on.

T.O. 1B-52H-34-2-8

5-1

Operating Limitations section V


WING FLUTTER AIRSPEED LIMITATIONS 5-1

JASSM ANTI-ICE OPERATION 5-1

JASSM JETTISON AND LAUNCH ENVELOPE 5-1

JASSM LAUNCH OR JETTISON WITH OPEN BAY DOORS 5-1

JASSM SAFE SEPARATION AND DECONFLICTION 5-2

WING FLUTTER AIRSPEED LIMITATIONS

The wing flutter airspeed limitations when carryingJASSMs are contained in T.O.1B-52H-1, Section V.

JASSM ANTI-ICE OPERATION

JASSMs are equipped with anti-ice heaters on boththe air data probe and the flush static port. Powerto the anti-ice heaters is automatically appliedwhenever the SMO is loaded and MIU power is on.MIU power for missile heaters should be applied toall missiles for a minimum of 15 minutes prior toweapon release or entering icing conditions. MIUpower may be removed during flight when required,however it should be re-applied as soon as practical.When heater power is off, flight through icingshould be avoided.

If flight through icing conditions with MIUpower off is unavoidable, re-apply MIUpower for a minimum of 30 minutes priorto release.

JASSM JETTISON AND LAUNCH ENVELOPES

JASSM Jettison and Launch envelopes are shownin figure 5-1.

• Launch or jettison of an AGM-158 in excessof the speeds shown in figure 5-1 may resultin collision between the JASSM and the air-craft.

• The JASSM jettison and launch envelopelimits, detailed in figure 5-1, reflect a vari-able relationship between altitude, machnumber, gross weight, and carriage posi-tion. Operators must be familiar with all as-pects of the jettison and launch envelopesand use care when operating near the pe-rimeters of the envelope.

JASSM LAUNCH OR JETTISON WITH OPENBOMB BAY DOORS

In an emergency, launch or jettison of JASSM may beattempted with the bomb bay doors open; however,consideration should be given to possible aircraftdamage due to a weapon to aircraft impact. Plannedrelease of JASSM is not authorized with the bomb baydoors open.

The pilot’s Bomb Bay & missile Jettison controlswitch jettisons all weapons loaded on the aircraft.If jettison is commanded using this switch, thebomb bay doors will open and would likely result inaircraft/JASSM collision during jettison.

Release of JASSM with the bomb bay doorsopen may result in damage to the aircraft.

T.O. 1B-52H-34-2-8

5-2

JASSM SAFE SEPARATION AND DECONFLICTION

The MAU-12 ejector rack imparts a safe separationvelocity to the JASSM to allow the weapon to meetthe following safe separation requirements:

• The JASSM normally maintains a minimumof two inches clearance from adjacent stores/struc-ture during all releases (launch or jettison).

If there is a retained/HUNG center stationstore, launching/jettisoning an adjacentshoulder station may result in a Store-to-Store contact. When a center station storeis retained/HUNG, operators will retain theadjacent shoulder station stores.

• The JASSM does not eject any items duringand after separation until the weapon has achievedsafe clearance from the aircraft.

• The JASSM has positive movement away fromthe aircraft such that no portion of the weaponpenetrates a determined interference boundary ofthe aircraft and/or remaining suspension systemsand stores. The interference boundary is defined asa four foot envelope around the fuselage, wings, en-gines, and tail during launch and jettison.

To further ensure safe separation, launch advisorieswill be issued when the required aircraft flight pa-rameters are exceeded, refer to PGRM WeaponLaunch Advisories in Section VII.

Deconfliction reduces the possibility of an in-flightcollision between the JASSM and the aircraft dur-ing separation and the JASSM’s flight to the first

waypoint. At launch detection, weapon flight pathcriteria are evaluated to determine if the directiontoward the first waypoint is within three degrees ofthe horizontal flight path and if the altitude of thefirst waypoint requires the weapon to climbthrough the launch altitude. If this scenario doesnot exist, then no special considerations are neces-sary to ensure the weapon does not penetrate thekeep out zone around the aircraft. However, whensuch a scenario does exist, the following operationstake place:

• The latitude and longitude of the firstwaypoint are adjusted to create an offset of 1400feet (1000 feet requirement + 400 feet navigationuncertainty) normal to the computed azimuth.

• The altitude command is set at least 500 feet(100 feet requirement + 400 feet navigation uncer-tainty) below the launch altitude.

• The heading command is biased by three de-grees.

Modification of waypoint information and desiredheading is necessary to avoid an impending flightpath conflict with the aircraft, which is assumed tocontinue on its flight path at release.

To avoid conflict with the aircraft, the JASSM will:

• Achieve a minimum lateral separation of 1000feet, to the right of the aircraft, before climbingthrough the aircraft’s altitude at release.

• Achieve a minimum vertical separation of 100feet below the aircraft’s altitude at release beforecrossing the aircraft’s flight path.

• When crossing the aircraft’s flight path, main-tain 100 feet minimum vertical separation belowthe aircraft’s altitude at release until lateral sepa-ration of 1000 feet is reached.

T.O. 1B-52H-34-2-8

5-3

JASSM Jettison and Launch EnvelopesSTATIONS L1 and R3

0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 0.55 0.60 0.65 0.70 0.75 0.80 0.85 0.90 0.95 1.000

5

10

15

20

25

30

35

40

45

50

True Mach Number

Pre

ssu

re A

ltit

ud

e −

1000

Fee

t

B46518

Top View

Buf

fet

Max

imum

Allo

wed

um

be

r

be

r

45,000 Ft.

Launch AndJettison

Prohibited

200 ,

000

L

Launch AndJettison

Prohibited

0.8

4In

dic

ate

dM

ach

N

390KIA

S340KIA

S

0.8

1In

dic

ate

dM

ach

Nu

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171KIA

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300,

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Lb

0.4

5In

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JettisonOnly

400,

000

Lb

Launch AndJettison

488,000

Lb


T.O. 1B-52H-34-2-8

5-4

JASSM Jettison and Launch Envelopes (Cont)STATIONS L8 and R6

0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 0.55 0.60 0.65 0.70 0.75 0.80 0.85 0.90 0.95 1.000

5

10

15

20

25

30

35

40

45

50

True Mach Number

Pre

ssu

re A

ltit

ud

e −

1000

Fee

t

B46517

0.4

5In

dic

ate

dM

ach

Nu

mb

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Buf

fet

Max

imum

Allo

wed

200 ,

000

Lb

0.8

4In

dic

ate

dM

ach

Nu

mb

er

390KIA

S

Top View

d

00,0

00Lb

3

400,

000

Lb

JettisonOnly

171KIA

S

45,000 Ft.

Launch AndJettison

Prohibited

340KIA

SLaunch An

Jettison

Prohibite

d

488,000

Lb

Launch AndJettison


T.O. 1B-52H-34-2-8

5-5

STATIONS L2, L3, L7 and R1, R2, R7

0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 0.55 0.60 0.65 0.70 0.75 0.80 0.85 0.90 0.95 1.000

5

10

15

20

25

30

35

40

45

50

B46519

True Mach Number

Pre

ssu

re A

ltit

ud

e −

1000

Fee

t

Top View

Buf

fet

340 KIAS

Max

imum

Allo

wed

200 ,

000

Lb

390KIA

S

Launch AndJettison

Prohibited

0.8

4In

dic

ate

dM

ach

Nu

mb

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MI=

0.8

1

45,000 Ft.

Launch AndJettison

Prohibited

171KIA

S

300,

000

Lb

400,

000

Lb

JettisonOnly

0.4

5In

dic

ate

dM

ach

Nu

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T.O. 1B-52H-34-2-8

5-6

JASSM Jettison and Launch Envelopes (Cont)STATIONS L6 and R8

0.15 0.20 0.25 0.30 0.35 0.40 0.45 0.50 0.55 0.60 0.65 0.70 0.75 0.80 0.85 0.90 0.95 1.000

5

10

5

20

25

30

35

40

45

50

Pre

ssu

re A

ltit

ud

e −

1000

Fee

t

True Mach NumberB46520

Top View

Buf

fet

Max

imum

Allo

wed

200 ,

000

Lb

340 KIAS

Launch AndJettison

Prohibited

0.8

4In

dic

ate

dM

ach

Nu

mb

er

39

S

0KIA363

KIAS

MI=

0.8

1

45,000 Ft.

Launch AndJettison

Prohibited

171KIA

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300,

000

Lb

400,

000

Lb

JettisonOnly

0.4

5In

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Launch AndJettison


T.O. 1B-52H-34-2-8

6-1

Mission Planning section VI


GENERAL 6-1

MISSION PLANNING MODULES 6-3

REPF MISSION PLANNING 6-4

UNIT MISSION PLANNING INTEGRATION 6-4

MISSION PLANNING TIMELINES 6-4

MISSION PLANNING CONSIDERATIONS 6-7

GENERAL

Mission Planning is the key component in the effec-tive operational use of a weapon system, especiallywith the advent of launch and leave precisionguided munitions. These weapons require the mis-sion planner to provide both the routing and target-ing information used to autonomously guide theweapon to the desired impact point with high preci-sion.

The low-observable JASSM missile uses GPS-aidedinertial guidance, updated with an imaging in-frared (IIR) terminal area seeker to provide highprecision terminal guidance to engage heavily de-fended and/or hardened targets requiring greaterimpact point precision. The terminal seeker re-quires the mission planning system to provide theterminal attack plan, including reference materialfor locating and tracking the target, JASSM termi-nal trajectory, weapon fusing and Bomb Impact As-sessment (BIA) data. Extended range weapons suchas JASSM also require a launch aircraft launch ac-ceptability region (LAR), weapon route waypoints,and time of flight information to achieve desiredtime on target. JASSM simplifies missile routeplanning by flying midcourse at high altitude,avoiding terrain obstacles.

The JASSM mission begins with the Air TaskingOrder (ATO) defining specific targets, delivery air-

craft and mission details. JASSM planning is de-signed to conform to ATO planning cycleconstraints. During the ATO process, desired tar-gets as well as desired effects are coordinated witha JASSM Rear Echelon Production Facility (REPF).

The REPF is responsible for designing, building,and maintaining the primary target database, theprimary element of which is:

• Target Area Model (TAM) – A wire frame ren-dering of a target complex, utilizing DigitalPoint Position Database (DPPDB) as the prin-ciple source of reference imagery, selection ofweapon type data, and specification and eval-uation of the attack trajectory and azimuth.REPF planners use a Precision TargetingModule (PTM) workstation online with cur-rent Intel sources to achieve the model. TheTAM provides the ability to utilize the JASSMseeker, if desired. The TAM can also be ma-nipulated if a DMPI adjust is desired.

The other key target database incorporated inJASSM planning is:

• PGMTDB – A standard database for precisetarget information. Using targets from thisdata set does not allow for seeker use.PGMTDB targets may also be manipulated toachieve desired effects. Planners may manual-ly enter desired DMPI information at the unitlevel.

T.O. 1B-52H-34-2-8

6-2

Effects-based targeting then occurs, utilizing thesetwo formats, at the AOC, and, if the targets are notreadily available in a database, the desired targetmodels are requested from the REPF. Once theTAM is built and verified, the REPF and/or theAOC will pass the resulting appropriate target dataset (TDS) to the tasked unit with instructions.Since the JASSM’s effectiveness lies mainly in highvalue, fixed targets, it is highly desired that a cur-rent, coordinated baseline TAM database be avail-able prior to deployment to minimize the time need-ed for target material generation during an ATOcycle. Large-scale operations should utilize pre-planned sortie data from operational plans con-ceived far in advance of hostilities.

Once target tasking is received, a JASSM missionplan is assembled at the tasked unit level. Thismission consists of an enroute plan, release points,Target Area Model (TAM) or Precision GuidedMunition Target Database (PGMTDB) target datasets, and terminal engagement trajectory for thedesired weapon effect. DMPI manipulation may berequired at the unit level by a qualified JASSMplanner. Alternate missions may also be specified ifdesired (up to 5 per launch point). The JASSM mis-sion plans are then integrated with the delivery air-craft flight plan and transferred to the aircraft us-ing a data transfer cartridge (DTC). The ability tocarry multiple JASSM missions on the aircraftDTUC allows great flexibility in striking targets,and appropriate strike planning should incorporateprocedures to use the various options.

USAF JASSM Mission Planning Module

Figure 6-1

The JASSM system mission planning is performedwithin the existing or planned infrastructure andusing existing or planned data products, formatsand hardware. Design infrastructure includes theREPF, and should be implemented with acentralized management system, such as TheaterBattle Management Core System (TBMCS), or likesystem located at the AOC, wing and units. FinalJASSM mission planning uses the tasked units’ AirForce Mission Support System (AFMSS) MissionPlanning System (MPS) workstations for weaponand aircraft routing.

Target materials used in terminal planning androute planning include:

• Target descriptions (BE#, DMPI, TAM ID).• Weapon data (Fuzing, Impact Angle, Azi-

muth).• DMPI identification (Short written descrip-

tion, Imagery).• Geopositional reference data (Latitude, Longi-

tude, Elevation).• Digital imagery with support data.• Digital terrain elevation data (DTED, Terrain

Clobber Analysis).• Threat information.• Weather conditions.

T.O. 1B-52H-34-2-8

6-3

JASSM planning utilizes the skills of personnelcurrently responsible for performing targeting androute planning functions. The approach also meetsthe targeting timeline where the target area, TAMDMPI selection, and associated reference modelconstruction and terminal attack planning must beperformed in 15 minutes (average). DMPI reviewand manipulation, and weapon routing must beperformed in 5 minutes (average). The approachprovides significant flexibility to the planners in theuse of existing data and the ability to plan/replan atboth the force and unit levels to meet a variety oftargeting circumstances, including emerging tar-gets. The overall Mission Planning flow and parti-tioning to planning workstations is shown in figure6-2.

MISSION PLANNING MODULES

The REPF planners use the Precision TargetingModule to produce the Terminal Area Model, whichcontains the terminal attack plan data (Seeker ref-erence, DMPI and weapon data). The PTM supports

all functions of planning the terminal attack includ-ing designation of the DMPI and seeker aim point,construction and evaluation of the seeker referencemodel using national asset products, selection ofweapon type data, specification of the attack trajec-tory and azimuth and evaluation of the attack plan.The PTM provides archiving and transfer ofJASSM TAM files with associated TAM ID toAFMSS.

The tasked unit mission planners use the WeaponPlanning Module (WPM), which is an AFMSS A/W/E hosted on the AFMSS workstation. The WPMsupports reading of archived JASSM TAM files, re-view and revision of DMPI’s and terminal attackplans; weapon auto route and manual modificationplanning, time-on-target planning, LAR deconflic-tion, association of a JASSM with the aircraftroute, AFMSS based multi-JASSM route deconflic-tion; and constraint checking, and transfer of re-quired weapon data to the aircraft A/W/E fordownload to the Data Transfer Device (DTD).

Mission Planning Flow and Partitioning

TBMCS or DIWS

Stereo Work Station(Force / Unit Level)

AFMSS or TAMPS

Work Station(Unit Level)

Weapon Type

Threat data

Target Materials

– Target area imagery

– DMPI

– seeker reference

– performance

Target Data – DMPI coordinates

– Imagery

Weapon selection

Launch A/C routing

Weapon Materials

– A/C routing

– Weapon routing

– Terminal data

(TOT, Fusing settings, etc)

– Seeker reference

DTD Aircraft / Weapon

Precision

Targeting

Module

Target Data

Weapon

Planning

Module

Missile and A/C route

planning and loadout

Terminal attack

planning

JASSM Target

Material

Tasking

Figure 6-2

T.O. 1B-52H-34-2-8

6-4

REPF MISSION PLANNING

To develop a TAM, the REPF mission planner viewsthe stereo data on the PTM to perform imageryanalyses. He/she can use the Digital Point Position-ing Data Base (DPPDB) imagery as the principlesource of reference imagery and National TechnicalMeans (NTM) NITF 2.0 imagery to augment theDPPDB data. A target nomination list is then ac-cessed to identify target areas of interest via usingother Intel application and databases such as theMIDB (modern integrated intelligence database) onthe TBMCS workstation. The planner can view ex-isting JASSM target seeker reference databasemodels for review and refinement or build a newmodel. If he/she chooses to build a new model, thereference imagery is accessed either by loading atape or accessing a previously loaded DPPDB seg-ment on his system. Once the imagery is displayed,the three dimensional data is used to locate anddesignate a DMPI. Once the Designated MeanPoint of Impact (DMPI) is chosen, building a seekerreference model can begin. A 3D reference wire-frame (WF) is constructed using the visible edges inthe reference imagery. While the building the WF,the user can perform a reference evaluation processthat provides a quantitative assessment of the mo-del. The completed model can be archived in a TAMfor future use, a feature useful in prewar planning.

The operator may also choose to select and use anexisting TAM. A TAM is selected from the databaseand opened for review of the terminal planningdata. Then the existing reference model with its as-sociated reference imagery can be viewed. The usermay update the original reference model by bring-ing in new NTM imagery to use with the originalreference imagery (DPPDB or other NTM imagery).The operator can tie the DPPDB and NTM imagerytogether in support of reference model update. He/she can overlay the original wireframe on the NTMimage and update it as required. The referencemodel update is performed using drawing tools toconstruct wireframes of objects in the NTM image.The modified reference wireframe can be evaluatedagainst the new, up to date, NTM imagery. Oncethe update is complete, a DMPI can be added ormodified using a target location description corre-sponding to a viewable location in the update imag-ery.

Once the reference model is ready, terminal plan-ning is performed. An attack trajectory and fuzedelay time is selected based on the target to be at-tacked. An attack azimuth range is selected by theplanner based on the attack trajectory, terminalarea imagery, and target characteristics. For eachazimuth selected the seeker reference model is com-

piled and performance effectiveness is evaluated forthe selected azimuth range and provided to the op-erator. The terminal planning could potentially beperformed at stereo capable Sun/UNIX worksta-tions within the DODIIS CSE or TBMCS/DIICOEenvironment.

The resulting attack plan including a reference ste-reo image pair and NTM imagery is exported as aTAM and passed to the unit for use in the WPM onan AFMSS workstation.

UNIT MISSION PLANNING INTEGRATION

The mission plan is then available to the unit levelplanner along with the ATO for weapon routing.The Weapon Route Planning functional flow is alsoshown in figure 6-3. Using the JASSM A/W/E mod-ule on the AFMSS workstation, the planner reads-in the JASSM TAM file. He/she reviews the attackplan and can modify weapon data and DMPI’s onthe 3D reference model. The reference image is dis-played to support DMPI review and adjustment.With modified DMPI’s, the terminal attack planwill be reevaluated to verify that the reference mod-el supports the new DMPI. Missile information isentered including BIA and TOT data when appli-cable. The operator also reviews and updates weap-on fuze settings and impact angle and which of theterminal profiles is to be used for the target.

The unit planner then builds the weapon route. Theoperator displays or enters the DMPI coordinates.He/she then, guided by JASSM range rings on theAFMSS display, selects either a waypoint one (plan-ning scenarios one and two) or an aircraft releasepoint (planning scenario three). He/she can thendisplay a LAR. He/she has now completed defini-tion of a stick route. The operator then selects auto-routing using the Common Low-observable AutoRouter (CLOAR) selection. Either a time-on-targetor non time-on-target (not time critical) flyout pro-file will be used by the auto-router. Once the auto-route has been performed, the operator may per-form manual modifications of the route, if desired.

The resulting weapon data, weapon route, terminaltrajectory, seeker reference and BIA settings are ac-cessed via calls to the JASSM A/W/E by the aircraftA/W/E on the AFMSS system for download to theData Transfer Device.

MISSION PLANNING TIMELINES

The mission planning timelines are shown in figures6-4 and 6-5 for the PTM and WPM respectively.

T.O. 1B-52H-34-2-8

6-5

Mission Planning Functional Flow

Target Materials

Nominations– DTM

– MIDB

Generate TerminalAttack Plan and

Evaluate

Designate DMPI’sModify / Generate

Reference Model

IMINT

– DPPDB– Updatel Imagery

Archive / TransmitJASSM Target

Materials

Precision TargetingModule

Review terminal

attack plan andmodify DMPI’s

JASSM Weapon– Seeker

– Non–seeker

Weapon Route Plan

Determine A/C LAR

Weapon Planning Module

Integrate A/C andWeapon Mission

Plans (A/C AWE)

DownloadWeapon MissionPlan to DTD

JASSM Target Materials

Repeat each weapon– Move DMPI’s– Analyze attack

Threat DataDTED

Wx

Evaluate

Reference Model

Evaluate Route

OpenWF Model

ArchiveWF Model

Archive Plan

Figure 6-3

T.O. 1B-52H-34-2-8

6-6

PTM Timeline Definition

Figure 6-4

WPM Timeline Definition

Figure 6-5

T.O. 1B-52H-34-2-8

Change 2 6-7

MISSION PLANNING CONSIDERATIONS

Since JASSM requires the use of time sensitive ma-terials, such as GPS crypto data, the planner mustensure the most current data is used at all times tomaximize mission effectiveness. If B-52 missionduration will extend across any crypto expirationboundary, the following period’s data should beloaded to ensure the JASSM receiver has sufficientinformation. For example, a B-52 mission will startat 2000 hrs GMT/ZULU and end at 0900 hrs. Dur-ing the sortie there is a new GPS crypto issued. Ifthe GPS/IU keyboard has failed, or the crew doesnot have the new keys available, the only othersource is the weapon or aircraft mission DTUC/DTC.

NOTE

The following steps may be used to correctfor GPS rollover:

• (RN-N) CF-61 entered.• Correct date is input on the MFD, but not en-

tered into the system.• (RN-N) Monitor for GPS date to rollover to in-

correct date.• Enter Key pressed to insert the correct date.• A missile health status check occurs.

Other Items to Consider When Preparing toEmploy JASSM:

• JASSM MPS security/environment• Height Above Ellipsoid (HAE) – JASSM uses

HAE for all altitude computations (launch,cruise, target). This closely mirrors the OASHA altitude for launch operations, and shouldbe a consideration if determining deconflictionfrom other platforms.

• Coordinate format – JASSM uses DDMMSS.SSS for higher fidelity. Planning on MPS canbe done in DDMM.MMMM, since data is con-verted in the MPS to give the missiles the cor-rect format.

• GPS Crypto Data Currency – Weekly keys re-quired. Recommend that current and follow-ing week keys always be loaded on DTC.

• AS/SV Data Currency• BIA Data – BIA frequencies used must be

coordinated with the AOC, Intel, and ELINTplatforms to assure missile health data is re-ceived and matched against the proper missilemission, if desired.

• GPS Almanac Data – Should be current, or atleast within 14 days of mission.

• Intel feed – Coordinated with unit Intel sec-tion for current threat database and otherflight restrictions.

• Divert and Staging base security – Appropri-ate to support the highest levels security forplanning systems, communication nodes, andthe assets themselves. Foreign controlledbases should be avoided and only used foremergencies.

• Divert and Staging base logistics support –Load equipment, missile storage (includingenvironmental needs), and planning systemsupport should be examined as far in advanceas possible.

• Direct targeting ROEs – Theater or Opera-tional commanders must drive use, due to lim-ited number of assets, cost, range, etc.

• Integration with other JASSM platforms – Acentralized, coordinated plan for JASSMstrikes that includes all JASSM capable air-craft is highly recommended. Mass JASSMlaunch scenarios will occupy copious amountsof airspace, and the ATO must sanitize spacefor missile launch(s).

• LAR Tolerances – Must be thoroughly briefed toensure planned IN ZONE launches are achieve-d. Aircraft flying a pressure altitude, for exam-ple, could be off the HAE altitude enough to beout of IN ZONE launch tolerances.

JASSM Operations Near the Poles

The JASSM SMO great circle distance equation isapproximate when operating close to or at thepoles. This will affect the times-to-go to enter andexit ranging indications on the PRGM screen. Thiswill not affect the actual In-Range/In-Zone statusreported by the weapon. To minimize the distanceerror when planning sortie destinations to eitherpole, ensure the following:

• Aircraft route follows the same longitude asthe launch point destination, and

• Center of range circle, center of zone arcs, andlaunch point destination are on the same sideof the pole.

Planning for JASSM Safe Separation and Deconfliction

For planning of a low altitude or co-altitude launch,it should be noted that the JASSM will require aminimum 5 degree offset to the right of the aircraftheading to avoid conflict with the aircraft. The mis-sile will achieve a minimum lateral separation of1000 feet to the right of the aircraft before climbingthrough the aircraft altitude at release. The JASSMwill also achieve a minimum vertical separation of100 feet below the aircraft altitude at release beforecrossing the aircraft’s flight path. This combinationwill assure the missile will maintain a minimumvertical separation of 100 feet below the aircraft’saltitude at release until lateral separation of 1000feet is reached.

T.O. 1B-52H-34-2-8

6-8

JASSM Low Temperature Flight Operations

The JASSM missile is designed for captive carriageand free flight down to a minimum ambient skintemperature (Ts) of –49 degrees F (–45 deg. C). Ex-posure of the JASSM missile to ambient skin tem-peratures below –49 degrees F could result in BIT[FAIL] indications and or missile failures. Sincewind friction warming affects the JASSM skin dur-ing external carriage, low temperature exposureshould not be an operational concern unless theJASSM is carried in the bomb bay or if loaded onthe aircraft for alert during extreme cold weather

conditions. JASSM missile skin temperature (Ts)during external carriage is defined as:External Carriage and Free Flight:

Ts = (OAT + 460)(1+0.18M2) – 460

Where Ts = Missile skin temperature (degrees F);OAT = True ambient air temperature (degrees F);M = True flight Mach number.

For example, a JASSM mission profile of FL 370 at0.76 mach should produce JASSM skin tempera-tures of approximately –25 degrees F.

T.O. 1B-52H-34-2-8

7-1

Systems Operation section VII


OAS/JOINT AIR TO SURFACE STANDOFF MISSILE OPERATION 7-3

JASSM EMPLOYMENT OVERVIEW 7-3

MISSILE MISSION TYPES 7-3

WEAPON MONITOR AND POWER CONTROL 7-7

WEAPON CONTROL EQUIPMENT (WCE) STATUS 7-7

WCE POWER APPLICATION 7-7

WCE POWER REMOVAL 7-8

MISSILE POWER APPLICATION 7-8

MISSILE AND EJECTOR STATUS 7-10

MISSILE POWER REMOVAL 7-15

MISSILE MISSION DATA AND TARGETING 7-17

MISSILE TARGETING METHODS 7-17

TARGETING TECHNIQUES 7-22

TARGET RANGING 7-29

IN-RANGE LAR 7-31

IN-ZONE LAR 7-36

TARGET RANGING INDICATIONS 7-43

IN-RANGE/IN-ZONE INDICATION 7-43

WEAPON LAUNCH ADVISORIES 7-43

SAFE RELEASE ADVISORIES 7-44

MISSILE LAUNCH 7-45

MISSILE LAUNCH PROCESS 7-45

AUTOMATIC LAUNCH DETERMINATION 7-46

MANUAL LAUNCH DETERMINATION 7-47

MISSILE LAUNCH TERMINATION 7-47

PREFERRED LAUNCH/JETTISON SEQUENCE 7-48

MISSILE LAUNCH RESTRICTIONS 7-48

JASSM FREE FLIGHT SEQUENCE 7-48

T.O. 1B-52H-34-2-8

7-2 Change 2

page

MISSILE JETTISON 7-50

SIMULATION CAPABILITIES 7-51

SIMULATED MISSILE LOADOUT 7-51

SIMULATED TARGETING OPERATIONS 7-51

SIMULATED WCE RESPONSES 7-51

SIMULATED RANGING 7-51

SMO TERMINATION 7-52

SMO RESTART 7-52

MESSAGES 7-52A

MASTER FAULTS 7-52A

ADVISORIES AND STATUS MESSAGES 7-52A

SAFE RELEASE AND WEAPON LAUNCH ADVISORIES 7-52A

FRMT-7 MISSILE FAULTS 7-52A

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Change 2 7-3

OAS/JOINT AIR TO SURFACE STANDOFF MISSILE OPERATIONThe B-52 OAS provides the operator interface forcontrol, targeting, and release of JASSMs.

Operation of the JASSM while carried by the B-52is made up of six major functions. These functionsare:

• Missile Monitor and Power Control• Mission Data and Targeting• Transfer Alignment• Target Ranging• Missile Launch• Missile Jettison

NOTE

[AMI] In order to accomplish any of the sixmajor functions listed above, the JASSMSMO must be designated as the primarySMO (CF-62x).

JASSM EMPLOYMENT OVERVIEW

At a specified time prior to arriving at the aircraftmissile launch point, initialization power is appliedto the missile, initiated BIT is run, mission dataand GPS Crypto keys are downloaded, and the se-lected missile mission number is designated by theaircrew. When aircraft transfer alignment is com-plete, the missile is ready for launch at the speci-fied release point.

After missile launch (autonomous missile flight),missile navigation to the target is accomplished viapredetermined three-dimensional waypoints. In-gress is at an optimum altitude condition to achievethe desired range and enhance survivability. At aspecified distance from the target the JASSM de-scends to a selected altitude above ground level forfinal target ingress which will enable the missile toachieve the desired terminal impact angle. The ter-minal profile depends on target orientation (verticalor horizontal) and hardness. Impact velocity ismaintained to achieve the required penetration ofhard targets. The terminal dive starts approximate-ly 3 km from the target with a pushover maneuverto the desired impact angle. An imaging infraredseeker is used to reduce terminal area guidance er-ror for hardened targets requiring greater impactpoint precision. When the seeker line-of-sight ispointed at the target area, an algorithm which de-termines if the JASSM is above or below the cloudceiling is initiated.

Once the seeker Line-of-Sight (LOS) is clear, an Au-tomatic Target Correlator (ATC) algorithm providestarget aim point error corrections for terminal guid-ance. The ATC uses a preloaded target area refer-

ence model which was developed using the JASSMmission planning system.

The missile is designed to operate under adverseweather conditions of 1500 ft. ceiling and 3 nauticalmile visibility. If weather conditions preclude theseeker from acquiring the target, the system willguide to the target using the inertial navigationsystem and target coordinates it received via mis-sion planning. During the terminal trajectory, aBomb Impact Assessment (BIA) subsystem trans-mits missile position and status information in anunencrypted format to an airborne receiving plat-form.

MISSILE MISSION TYPES

There are two types of JASSM missions, pre-planned missions and direct target missions (alsocalled Target of Opportunity missions by JASSM).There are two types of preplanned missions, thosethat require a Time on Target (TOT) and those thatdo not require a TOT.

All preplanned missions are planned as In-Zone re-leases, but can be released In-Range, if the In-Zoneconditions cannot be achieved by the host aircraft.

All Target of Opportunity (TOO) missions are re-leased In-Range, there is not an In–Zone region as-sociated with a TOO.

Altitudes can be mission planned, aircrew definedvia cockpit controls or missile default.

Preplanned Missions

Preplanned missions require at least one waypointto define the route of flight and flight altitudes. Therequirement for TOT required missions is set bymission planning and must be launched In-Zone.Using missile throttle adjustments the missile fliesthe planned route within ± 5 seconds of the CurrentTime Of Flight (CTOF), giving it a TOT which isalso ± 5 seconds of planned TOT assuming the mis-sile was launched on time and at the preplanned re-lease point. If the TOT requirement is not set, themissile flies the preplanned route without throttleadjustments. If a TOT required missile is launchedIn-Range, but not In-Zone, it deviates from theplanned route of flight and does not attempt tomake the required TOT, but still maintains all pre-planned terminal conditions. See figure 7-1 forFlight Profile Summary and figure 7-2 for JASSMFlight Profiles.

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7-4

JASSM Flight Profile SummaryMISSION TYPE LAUNCH WAYPOINTS SEEKER TOT

REQUIREDPTOF

TOLERANCEJASSM FLIES

TO

PREPLANNED In-Zone Yes Used, If Required Yes ± 5 Seconds Waypoint 1

PREPLANNED In-Zone Yes Used, If Required No Not Required Waypoint 1

PREPLANNED In-Range No Used, If Required Yes Not Used Target Azimuth

PREPLANNED In-Range No Used, If Required No Not Required Target Azimuth

DIRECT TARGET In-Range No Not Used N/A Not Required Target Azimuth

Figure 7-1

PREPLANNED, LAUNCHED IN-ZONE

In-Zone launched missions use a static Launch Ac-ceptability Region (LAR). This preplanned staticLAR defines the zone around the launch point fromwhich the missile will be able to intercept the mis-sile mission at the first waypoint and fly the pre-planned route (See Target Ranging this section).

In-Zone launches have the following parameters:• Can be with or without seeker terminal guid-

ance.• Missile flies the preplanned route of flight (in-

cluding all waypoints and altitudes).• For non-TOT missions, the nominal cruise al-

titude is 22000 feet MSL, until transitioningto the terminal area. During the mission plan-ning process, the user can change the cruisealtitude ± 500 feet in 50 feet increments, rela-tive to the nominal altitude. For example, ac-ceptable mission planned entries are 21500,21550, 21600, etc.

• For TOT missions, the nominal cruise altitudeis 12000 feet MSL until transitioning to theterminal area. During the mission planningprocess, the user can change the cruise alti-tude ± 500 feet in 50 feet increments, relativeto the nominal altitude. For example, accept-able mission planned entries are 11500,11550, 11600, etc.

• Impacts the target under preplanned condi-tions.

• Preplanned data items cannot be changed.

PREPLANNED, LAUNCHED IN-RANGE

For preplanned missions launched In-Range, themissile does not attempt to make the planned way-points nor planned timing. Instead the missile will

fly directly to meet the target azimuth into the tar-get.

In-Range launches have the following parameters:

• The missile will generate its own route to in-tercept target azimuth.

• Proceeds to 22,000 feet MSL and remainsthere until descending to the terminal area.

• Since the route from the last waypoint to tar-get did not change it can be with or withoutseeker terminal guidance as planned.

• Since the route from the last waypoint to tar-get did not change it impacts the target underpreplanned conditions.

• Preplanned data items cannot be changed.

Direct Targeted Missions/Target of Opportunity (TOO)

Direct target function allows the operator to specifya target that is not included as a preplaned mis-sion. TOO missiles can only be launched In-Range.

TOO launches have the following parameters:• Waypoints cannot be specified for a direct tar-

get.• A direct target can be assigned to a specific

missile.• Target latitude, longitude, and elevation must

be entered.• The missile will fly cruise altitude until tran-

sitioning to the terminal area. The cruise alti-tude can be specified from 0 to 22,000 feetMSL (defaults to 15,000 feet MSL).

• Bearing to target and impact angle can bespecified.

• Fuze mode of soft impact or hard impact canbe specified. Defaults to soft.

• Fuze delay time can be specified.

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7-5/(7-6 blank)

JASSM Flight Profiles

Figure 7-2

BLA

T.O. 1B-52H-34-2-8

Change 3 7-7

WEAPON MONITOR AND POWER CONTROL

The Weapon Control Equipment (WCE), which con-sists of the Armament Interface Unit (AIU), Environ-mental Control Unit (ECU) and Weapon InterfaceUnits (WIUs) must be powered on to enable the opera-tor to power on, control, and release any missiles. TheAIUs supply power to the ECU and WIUs. The ECUssupply cooling air to the WIUs. The WIUs enable pow-er application to the missile(s), perform data trans-missions with the missile(s), and provide ejector con-trol. AIU power is supplied when OAS master poweris turned on. ECU and WIU power are supplied powerwhen WIUs are turned on.

Subsequent to applying power to the WIU on a pylon,initialization power can be commanded on for anymissile(s) on that pylon via the WCP. Missile initiali-zation power must be applied to enable the SMO toverify the weapon type, missile operational and LARstatus, and to transmit missile initialization, GPS,alignment, and targeting data to the missile(s) priorto launch.

WEAPON CONTROL EQUIPMENT (WCE) STATUS

The operator can review the operational status of theAIU, ECU, left WIU (L WIU) or right WIU (R WIU)using the PME Status Display (FRMT-6). The SMOcommunicates with these LRUs using OAS 1553 databuses A and C. The PME Status Display (FRMT-6)shows AIU and WIU A bus and C bus communicationstatus and AIU, ECU and WIU failure status. If aWIU A bus communication failure has occurred, an Awill be displayed for the respective WIU. If a WIU Cbus communication failure has occurred, a C will bedisplayed for the respective WIU. If an LRU failurehas occurred, an X will be displayed for the ECU or re-spective WIU. In a similar manner, FMS will displayan A or a C next to AIU if an AIU A bus or C bus com-munication failure has occurred and an X next to AIUif an AIU failure has occurred. The format of the textindicates whether or not the failure currently exists.If the failure currently exists, the text (A, C, or X) willbe displayed in reverse video. If the failure does notcurrently exist, the text (A, C, or X) will be displayedin normal video.

To clear unwanted data from the PME Status Display(FRMT-6), the operator can enter CF-66 Erase PMEFaults, to delete the display of all failures which nolonger exist. When the CF-66 command is entered, allfailure text displayed in normal video will be blankedand any text displayed in reverse video will remain.The AIU, ECU or WIU failure status is also displayedon the JASSM Status and Inventory Display(FRMT-7). AIU will be displayed in reverse video ifthe AIU has failed. ECU will be displayed in reverse

video if the ECU has failed. WIU will be displayed inreverse video for the left or right WIU respectively, ifeither the WIU communication or the WIU have fai-led. Each failure displayed on FRMT-7 will be re-moved if the associated failure status clears.

WCE POWER APPLICATION

WIU power will be applied when the operatorpresses the WIU power switch (MIU/LP or MIU/RP)to the depressed (Power On) position. When theswitch is in the depressed position it illuminates af-ter a short delay. If the switch was in the depressedposition when the SMO was loaded or restarted, theswitch must be cycled to command power to theWIU. The MIU/BAY switch is not recognized byJASSM SMO. If it is selected the advisory messageB: LOCATION will be displayed. Power will be ap-plied to the WIU and then the WIU will be initial-ized for the selected location.

If the SMO is unable to complete the WIU power-onsequence it will be terminated, the appropriatefault will be displayed, and any power which hasbeen applied will be removed. However, for an ECUfault, if ECU Power Override is currently active,the SMO will continue with the power-on sequence.The operator can verify completion of the WIU pow-er on sequence by viewing FRMT-7.

When the sequence is complete, the following dis-play changes will occur on FRMT-7 next to eachWIU station number (1, 2, 3, 6, 7, and 8)(4 and 5are not recognized by the JASSM SMO):

• The weapon type window will indicate eitherM1 to identify there is a weapon present at the sta-tion or blank to indicate that no weapon is present.

• The missile status window will change fromblank to OF, X, NG, or CL, to indicate missile state.See FRMT-7 in Section I for a description of thedisplay options.

1. OF will be displayed to indicate that missileinitialization power is not applied at thestation.

2. X will be displayed if both the ejector andumbilical status show no missile is presentat the station.

3. NG will be displayed in reverse video if apermanent fatal fault has occurred for themissile.

4. CL will be displayed if the missile is a cap-tive carry launched (Flight Test Only).

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7-8 Change 2

• The missile fault display window will display afault indication if a missile is present and any faultshave been detected at the station. All faults are listedand described at the end of this Section. If no missileis present the fault window will remain blank.

• The JASSM launch point number (1 to 99) andmission group (A to F) will be displayed as assignedper B-52 mission data.

Missile Warm-up

Upon application of power to the WIU, 115-volt acpower is applied to the missiles to thermally condi-tion the missiles air data systems (requires up to13.5 minutes). When takeoff and climb-out throughicing conditions is anticipated, heater power shouldbe applied prior to take-off and remain on for aminimum of 15 minutes or until clear of icing condi-tions, whichever occurs last. Flight through icingconditions should be avoided.

The missile will set an Overtemperature Cautionindicating the probability of the missile overheatingbefore completing its mission, if the missile is notlaunched in approximately ten minutes.

The missile will set an Overtemperature Warningindicating the probability of the missile overheatingbefore completing its mission if the missile is notlaunched in approximately one minute.

If, as a result of an Overtemperature Caution orWarning, the operator removes missile power nodamage will occur. If missile power is removed dueto an overtemperature condition, a cool down periodof approximately 45 minutes should be allowed be-fore missile power is reapplied.

The effects of weapon overheat on weaponreliability and accuracy are unknown.

WCE POWER REMOVAL

WIU power will be removed from the selected loca-tion when the operator presses the desired WIUpower switch (MIU/LP or MIU/RP) and allows it toreturn to the out (non-depressed) position. Nofaults will be displayed during WIU power removal.

The operator can verify completion of the WIU pow-er off sequence by viewing FRMT-7, CF-E and/orthe OAS Power Control Panel. When the sequenceis complete, the selected WIU power switch (LWIUor RWIU) will no longer be lit and all data containe-d on FRMT-7 for each station at that WIU locationwill be blanked within 3 seconds.

MISSILE POWER APPLICATION

After applying power to the WIU on a pylon, powerapplication can be commanded for any missile(s) onthat pylon. Missile power must be applied in orderfor the SMO to verify the weapon type, missile op-erational and LAR status, and to transmit missileinitialization, GPS Crypto Keys (weekly), GPS Al-manac (less than 2 weeks old), alignment, and tar-geting data to the missile(s) prior to launch.

Missile Initialization power (28-volt DC-1) powerwill be applied when the operator depresses the de-sired Location (left and/or right) and Station (1, 2,3, 6, 7, and/or 8 or ALL) switches on the WCP andmomentarily moves the WPN PWR switch to theON position. Missile power can also be applied us-ing CF-E. Subsequently, the selected missile(s) willbe powered on and initialized. See figure 7-3 for aninitialization timeline.

The OAS provides GPS data to the JASSM throughthe WIU in order to prepare the weapon GPS receiverto acquire satellites after separation from the air-craft. The GPS data provided includes: Almanac data,Anti-Spoofing Status/Space Vehicle Configuration(AS/AV) data, GPS Crypto Keys, Time data, Ephem-eris. GPS data transfer occurs after warm up andbuilt in test. The JASSM must have weekly cryptokeys that are current for the duration of the mission.

The crew should ensure that the weapon missionDTUC/DTC contains GPS Almanac Data (less than 2weeks old) and GPS Crypto Keys (weekly) sufficientto support the mission since the B-52 SMO uses theweapon mission DTUC/DTC as backup.

If the GPS almanac data age is unknown, or theGPS has not been operated within the last twoweeks, it should be updated in accordance with pro-cedures in Section II of this T.O.

The SMO can acquire crypto key data from eitherthe GPS interface unit (IU) or the weapon missionDTUC. The primary source of crypto key data is theGPS IU. If the GPS receiver validates the cryptokey data, the SMO loads the validated crypto dataanytime after SMO start-up. After power initializa-tion is complete, the crypto key data is transferredto any weapon requiring the data.

If the crypto key data in the IU is not validated ornot available, the data can be obtained from theweapon mission DTUC/DTC. When weapon powerinitialization is complete, the SMO retrieves thecrypto key data from the weapon mission DTUC/DTC and transfers the data to the weapon(s).

T.O. 1B-52H-34-2-8

7-9

JASSM Initialization Timeline

Figure 7-3

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7-10 Change 3

MISSILE AND EJECTOR STATUS

The operator can review the operational status ofeach JASSM via the JASSM Status and Inventorydisplay (FRMT-7) figure 7-4 or FRMT-7xy figure7-5. The JASSM Status and Inventory Displayshows missile presence, missile power, missile stateand missile fault status for each station (1, 2, 3, 6,7, and 8) on each pylon (left and right). The stationstatus windows are grouped together for each sta-tion. The station number is displayed immediatelyto the left of the weapon type window.

If the SMO is unable to complete any of the stepsfor a missile, the missile power on sequence will beterminated for that missile, the appropriate faultwill be displayed and any missile power which hasbeen applied to that missile will be removed. Whenthe power on sequence is complete, the followingdisplay changes will occur within 2 seconds onFRMT-7 or FRMT-7xy next to each selected WIUstation number (1, 2, 3, 6, 7, or 8) where power wasapplied:

• Missile type will change from blanks to M1 whenthe missile is determined to be a JASSM or it willremain M1 if the missile has previously been deter-mined to be a JASSM. P will be displayed if thesystem detects a missile at the station but cannotidentify the type.• Weapon Status will change from OF to ON, toindicate missile initialization power is available atthe station. If the missile is a captive carry missile,CL, will be displayed when the missile is launched.• Missile Fault display will display a fault indica-tion if any missile faults have been detected at thestation. All missile faults are listed and describedat the end of this section.

The following conditions must exist:

• The JASSM SMO must be the primary SMO.• The associated WIU must have power appliedand be initialized.• The missiles selected must be pylon stations 1, 2,3, 6, 7, or 8; or ALL.• The missiles selected must be present and pow-ered off.• Carrier mission stores table is loaded.• The missiles selected must not have any perman-ent fatal faults. If a fatal fault exists for a missile,NG will be displayed in reverse video.

In addition, the operator can review the operationalstatus of a selected station ejector and additional

missile status via the JASSM Status and Inventorywith Selected Station Status display (FRMT-7xy).See FRMT-7xy in Section I for a description of thedisplay windows and the data that will be displayedat the bottom of the requesting MFD.

• Window 1 (figure 7-5), will display the location ofthe selected missile with L signifying the Left pylonor R signifying the Right pylon.• Window 2 (figure 7-5), will display the station(1-3, 6-8) of the selected missile.• Window 3 (figure 7-5), indicates the missile type(e.g. AGM-158A) of the selected missile.• Window 8 (figure 7-5), will display ON or OFF toindicate whether or not missile telemetry power hasbeen commanded.

NOTE

The telemetry command is initialized to offand the command state is displayed any-time the display is requested, regardless ofWIU or missile power status.

• Window 9 (figure 7-5), will display MAN LNCHREQ if the missile does not meet the requirementsfor launching the missile in automatic launch mode.

A manual launch will be required if any of the fol-lowing occurs:

1. Selected missile has a non-fatal fault requir-ing manual launch.

2. Selected missile does not indicate AURREADY = TRUE (SAFE TO RELEASE =TRUE).

3. Selected missile indicates In-Range LAR =TRUE and In-Zone LAR = FALSE.

4. Selected missile indicates In-Range LAR =TRUE and In-Zone LAR = TRUE and pastthe closest point of approach.

• Window 10 (figure 7-5), will display station ejec-tor status as either blank, UNLOCKD orNOT_UNLKD to indicate the ejector status at thestation.

1. The field will be blank if no weapon is pres-ent or WIU power for this pylon is off.

2. UNLOCKD will appear if the ejector lockedstatus is false and unlocked status is true.

3. NOT_UNLKD will appear if an illegal ejec-tor status is detected.

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7-11

• Window 11 (figure 7-5), displays the configurationID of the selected missile.• Window 14 (figure 7-5), will display a K in nor-mal video to indicate keys are present in the mis-sile. If the missile fails to indicate Crypto KeysPresent subsequent to a successful Crypto KeyPresent indication, the SMO will resend the keysand the normal video K will remain displayed. TheK in reverse video indicates keys are in error orhave not been received. A blank window indicatesthe missile is powered off or no targeting data hasbeen downloaded to the missile.• Window 15 (figure 7-5), will display ON, OFF, orHOT to indicate the missile timer status.

1. ON will be displayed, if the missile is cur-rently powered on and neither an OverheatWarning nor an Overheat Caution exist forthe missile.

2. OFF will be displayed, if the missile is cur-rently powered off.

3. HOT will be displayed in reverse video, ifthe missile is currently powered on andthere is an Overheat Caution issued for themissile. This indicates the missile may over-heat during its mission, if not releasedwithin 10 minutes.

4. HOT will be displayed in blinking reversevideo, if the missile is currently powered onand there is an Overheat Warning issuedfor the missile. This indicates the missilemay overheat during its mission, if not re-leased within 1 minute.

• Window 16 (figure 7-5), will indicate the hoursand minutes that the missile has been either ONor OFF, or the elapsed time since either an Over-heat Caution or an Overheat Warning was issued.

The text and associated indications for station sta-tus on the JASSM Status and Inventory display areoutlined in the following paragraphs. All of thesefields will be blank for a station if either the WIU isnot powered on for that pylon or if no missile ispresent at the station.

Weapon Type

The weapon presence field, window 2, on FRMT-7the JASSM Status and Inventory display (figure7-4), indicates what the SMO identifies as presentat the umbilical based on the data available fromthe ejector, WIU and missile.

TEXT VIDEO INDICATION

M1 Normal Prior to initial weapon power ap-plication, loaded sortie missionidentifies missile type isAGM-158A;

orAfter initial weapon power applica-tion, both loaded sortie mission andweapon identify the same missiletype as AGM-158A.

M1 Reverse Sortie mission identifies anAGM-158A but the missile at sta-tion is a different variant;

orA non-JASSM sortie is loaded afterthe missile type was identified asan AGM-158A.

M Normal A sortie mission is not loaded andafter weapon power application,the missile is a JASSM (SIT andGo/No-Go test only);

orA different JASSM variant sortiemission is loaded prior to initialweapon application;

orA different JASSM variant sortiemission is loaded and after weaponpower application, the weapon isan AGM-158A.

M Reverse A non-JASSM sortie mission isloaded and after initial weaponpower is applied, the weapon pres-ent is a JASSM;

orAn AGM-158A sortie mission isloaded with no weapon identifiedfor this location and after initialweapon power is applied, theweapon present is a JASSM (WPNPRSNT master fault).

P Normal Prior to initial weapon power ap-plication during SIT or Go/NoGotesting with no sortie missionloaded, a weapon is present, but isof unknown type.

P Reverse Prior to initial weapon power ap-plication a non-JASSM sortie mis-sion is loaded;

orPrior to initial weapon power ap-plication JASSM mission data indi-cates an empty station (WPNPRSNT master fault);

orAfter weapon power application isattempted a non-JASSM weaponis present (STORE ID masterfault).

Blank Location WIU power Off or weaponpower Off.

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7-12 Change 3

Missile Status

The missile status field, window 3, on the FRMT-7,JASSM Status and Inventory display (figure 7-4),indicates the status of the missiles.


OF Normal WIU Power for the Location is Onand missile power for specific mis-sile is Off. (115-volt ac power is ap-plied to the missile. 28-volt dc #1power is off)

ON Normal Missile power is On for specificmissile. (Both 28-volt dc #1 and115-volt ac power are applied to themissile.)

NG Reverse Permanent Fatal Fault has oc-curred for this missile or abort hasbeen commanded prior to releaseattempt. All power (both 28-volt dc#1 and 115-volt ac power) has beenremoved from the missile. Powerapplication is inhibited.

GO Normal Mission capable missile. Safe to re-lease with launchable alignmentstatus. Manual launch required.(Both 28-volt dc #1 and 115-volt acpower are applied to the missile.)

GO Bright/Underline

Fully Mission capable missile. AllUp Round Ready with launchablealignment status. (Both 28-volt dc#1 and 115-volt ac power are ap-plied to the missile.)

CL Normal Captive Carry missile launched(simulated launch). (Both 28-voltdc #1 and 115-volt ac power are ap-plied to the missile.)

X_ Normal Weapon not present and no pres-ence discrepancy exists.No power applied.

X_ Reverse Weapon not present and Weaponpresence discrepancy exists. No power applied.

Blank WIU Power for the Location is Off.

Launch Point/Target Number Indicator

The missile launch point/target number field, win-dow 4, on the FRMT-7, JASSM Status and Inventorydisplay (figure 7-4), indicates the launch point or di-rect target number for the specified missile. In con-junction with windows 4 and 7, window 12 (DTU/DTC) indicates the missile mission DTUC/DTC hasfailed anytime a missile is operational when the SMOrequests GPS almanac, GPS AS status/SV configura-tion data, GPS crypto keys, or missile TDS.


nn Normal The missile is assigned to launchpoint nn (nn= _1 to 99) or the mis-sile has been launched against thetarget.

nn Bright The missile is in the process of being targeted to launch point nn.

nn Bright/Underline

The missile has been successfullytargeted to launch point nn

nn Reverse The missile has failed to target suc-cessfully.

Dn Normal The missile is assigned to Directtarget Dn (n= 1 to 6) or the missilehas been launched against the di-rect target.

Dn Bright Direct target Dn has been assignedto the missile and targeting hasbeen initiated.

Dn Bright/Underline

Direct target Dn has been assignedto the missile and targeting hasbeen loaded and verified.

Dn Reverse The missile has failed to target suc-cessfully.

Blank The missile has not started the tar-geting process.

Missile GPS Alignment Quality

The missile alignment quality field, window 6, onFRMT-7, the JASSM Status and Inventory display(figure 7-4), indicates the quality of GPS data. Themissile transfer alignment quality field will display1 or 10 indicating the quality of each missile’s align-ment. Display of the transfer alignment quality inreverse video indicates an alignment failure has oc-curred and [AMI] persisted for a minimum of 10minutes.

NOTE

A transfer alignment quality of 1 is re-quired for launch.

In conjunction with window 6, the FMS primarynavigation mode used to align the missile is dis-played in window 11.

NOTE

In order to achieve good missile alignmentquality (1), an INS/INU must be selected asthe primary FMS navigation mode.

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7-13

Missile Data GPS Status

The missile GPS status field, window 7, onFRMT-7, the JASSM Status and Inventory display(figure 7-4), indicates the status of missile GPSdata. If a missile has successfully completed a clas-sified data erase ER is displayed in window 7. If theclassified data erase was unsuccessful, the ER willbe in reverse video. BT is displayed when the mis-sile is in IBIT. If a missile indicates a combined lossof crypto keys, AUR ready, and minimum GPS, thetext IN will be displayed in window 7. The missilestatus indicators that may be displayed in window7 are listed below.


BT Normal Missile is in IBIT.

ER Normal Missile Mission data is erased.

ER Blinking Missile Mission data erase in progress.

ER Reverse Missile Mission data erase failure.

IN Normal Missile is in Initialization.

IN Reverse Initialization fault has occurred.

MG Normal Missile has received minimumGPS.

MG Reverse Minimum GPS received andEphemeris Received fault oc-curred.

TK Normal Missile is tracking at least 4 satellites.(Test launch only).

WU Normal Missile in Warm-up.

WU Reverse Warm-up fault or missile heaterpower fault has occurred.

Blank WIU or missile power has not beenapplied.

In conjunction with window 7, window 13 (IU) indi-cates the IU has failed or there is no communica-tion with the IU any time the WIU is operationalwhen the SMO requests GPS almanac, ephemeris,GPS time mark, or crypto key data.

In conjunction with window 7, window 14 (GPS) in-dicates the GPS is faulted by the IU any time theWIU is operational.

Missile Fault Status

The missile fault field, window 9 on FRMT-7,JASSM Status and Inventory display (figure 7-4),indicates any missile faults present. The highestpriority fault will be displayed in window 9 if morethan one fault exists. The missile faults, which maybe displayed in window 7 on FRMT-7xy, the JASSMStatus and Inventory display with Selected StationStatus (figure 7-5), and their description are pro-vided in the Station Master Faults, this section.

Missile In-Range/In-Zone Status

The missile In-Range/In-Zone status field, window8, on FRMT-7, the JASSM Status and Inventorydisplay (figure 7-4), indicates the In-Range/In-Zonestatus of the missiles.


R Normal Missile is In-Range.

Z Normal Missile is In-Zone.

Blank Otherwise.

Ejector State

The ejector state field, window 10, on FRMT-7xy,the JASSM Status and Inventory display with Se-lected Station Status (figure 7-5), indicates thestate of missile ejectors.


UNLOCKD Normal Ejector locked status indicatesunlocked.

NOTUNLKD

Reverse Ejector status cannot be de-termined.

Blank Missile is not present or WIUpower for the location is off.

T.O. 1B-52H-34-2-8

7-14 Change 2

JASSM Status and Inventory Display (FRMT-7)Less [AMI]

R I GHT 8R I GHT 6

R I GHT 7

R I GHT 3R I GHT 1

R I GHT 2

L EF T 3

L EF T 8

L EF T 7

L EF T 6

− −FRMT − 7

2 M1−GO /

M

1

1

6

7

3

8

2

31

7

86

2 −/

3 / 4 5

8

A75616

SAMPLE

1

PMD

10 11 12 13 14 15 16 17

9

6 7

0 1 / G Z

0C

[AMI]

R I GHT 8R I GHT 6

R I GHT 7

R I GHT 3R I GHT 1

R I GHT 2

L EF T 3

L EF T 8

L EF T 7

L EF T 6

− −FRMT - 7

M

6

7

3

8

2

31

7

86

B41366

SAMPLE

10 11 12 13 14 15 16 17

9

0 1 / G Z2M1−GO / 10C

1 2 −/

3 / 4 5

8

1

6 7

C F - DF =PAGE FWD C F - DB =PAGE BACK

PMD

Figure 7-4

14

R I GHT 8R I GHT 6

R I GHT 7

R I GHT 3R I GHT 2

R I GHT 2

L EF T 3

L EF T 8

L EF T 7

L EF T 6

− −FRMT − 7

2 M1−GO / 1 00 1 / MG Z

6

7

3

8

2

31

7

86

XY

L EF T1

2

E JTLMY 8 9

1 07311

21 65/4

/ 1312

A75617

PMD

SAMPLE

1 6T I ME1 5

C

T.O. 1B-52H-34-2-8

Change 2 7-15/(7-16 blank)

JASSM Status and Inventory Display with SelectedStation (FRMT-7,xy)

Figure 7-5

MISSILE POWER REMOVAL

Missile initialization power will be removed whenthe operator depresses the desired Location (leftand/or right) and Station (1, 2, 3, 6, 7 and/or 8 orALL) switches on the WCP and momentarily movesthe WPN PWR switch to the OFF position. Subse-quently, the selected missile(s) will be powered off.Missile heater power (115-volt ac) will remain on aslong as the respective WIU remains powered.

The operator can verify completion of the missileinitialization power off sequence by viewingFRMT-7 or FRMT-7xy. When the sequence is com-plete, the following display changes will occur onFRMT-7 or FRMT-7xy next to each selected WIUstation number within 2 seconds:

• The missile status window will change to OF in-dicating missile initialization power is not availableat the station.

• The missile fault display window will continue todisplay the highest priority fault indication if anymissile faults have been detected at the station. Allmissile faults are listed and described at the end ofthis Section.

The following limitations apply to missile power re-moval:

• The missiles selected cannot be pylon stations 4or 5.• A missile must be present at selected station.• Missile power removal will not be performed forany missile to which an Commit To Separate (CTS)command has been issued.• Missile CDE is not in progress.

BLA

T.O. 1B-52H-34-2-8

Change 3 7-17

MISSILE MISSION DATA AND TARGETING

Prior to launching a missile, targeting data must beprovided to the missiles. JASSM missions are pre-planed and loaded onto a B-52 DTUC/DTC and Less[AMI] associated missile DTUC(s). Subsequently themissile targeting data is downloaded to the missilesprior to launch. In addition, the operator may performdirect targeting as required.

MISSILE TARGETING METHODS

This paragraph describes the types of missile target-ing requests, targeting data items, and the processesfor entering, modifying, and reviewing missile target-ing data. The SMO supports four types of missile tar-geting requests as described in the following para-graphs:

• Automatic targeting.• Manual targeting (CF-586).• Retarget-all (CF-589).• Direct targeting (CF-588,n).

Only one targeting request is allowed to be in prog-ress at any one time.

The following targeting operations will be termi-nated, if active, when a valid Retarget-all (CF-589) ora Load B-52 Mission Data (CF-81,n) is entered.

• Manual targeting.• Direct targeting.• Automatic Targeting.

Less [AMI] Reconfiguration of the Hot Spare as theControls and Display (CAD) or Navigation and Weap-on Delivery (NAWD) processor will terminate any ac-tive targeting operations and update any targetingdisplay associated with that targeting operation to in-dicate targeting did not complete. The operator is re-quired to re-enter the appropriate command to re-start the targeting operation. If a CF-DD commandwas entered for a Direct Targeting operation, the tar-get assignment will be removed from each missilepreviously selected.

[AMI] Reconfiguration of the processor will termi-nate any active targeting operation and update anytargeting display associated with that targeting op-eration to indicate targeting did not complete. The op-erator is required to re-enter the appropriate com-mand to restart the targeting operation. If a CF-DDcommand was entered for a Direct Targeting opera-tion, the target assignment will be removed from eachmissile previously selected.

NOTE

Targeting may take up to two minutes. Aweapon may fail if the OAS is transferringdata to the weapon. Attempt to retarget theweapon.

Automatic Targeting

Each missile must be targeted prior to launch. Mis-sile target data set is automatically transferred to amissile when:

• Missile power application and initialization iscomplete.

• A B-52 mission is loaded which containsJASSM targets, the JASSM SMO is loaded,and missiles are assigned to the appropriatelaunch points.

• Less [AMI] A missile mission DTUC associat-ed with the B-52 mission is accessible.

• [AMI] A weapon mission group associatedwith the B-52 mission is accessible.

• The missile is not currently targeted.• No other targeting operation is active.• Automatic Targeting is enabled on CF-58.

Less [AMI] If a missile mission DTUC is not acces-sible, automatic targeting will remain suspendeduntil a missile DTUC is accessible. If the missilemission DTUC becomes unaccessible while auto-matic targeting is in progress, targeting will re-sume when the missile mission DTUC is accessibleagain and no other targeting operations are active.

[AMI] If a weapon mission group is not accessible,automatic targeting will remain suspended until aweapon mission group is accessible. If the weaponmission group becomes inaccessible while automat-ic targeting is in progress, targeting will resumewhen the weapon mission group is accessible againand no other targeting operations are active. If thefaults JASSM WPN DATA?? and xy:WPN NOGOoccur in conjunction, the operator must selectanother weapon group.

If missiles have been targeted and a B-52 mission issubsequently reloaded, all missiles that wereloaded with preplanned targeting data will be con-sidered untargeted and automatic targeting will beperformed on those missiles. Missiles that havebeen loaded with direct targeting data will not beretargeted. A Retarget All command (CF-589) ormanual targeting Missile Target Assign (ManualTargeting) command (CF-586) will be necessary toretarget missiles that have been direct targeted.

T.O. 1B-52H-34-2-8

7-18 Change 2

The missiles are targeted with specific targetingdata as directed by the B-52 mission that is loaded.After power is applied and initialization is completefor a missile, targeting data will be transferred tothat missile. If power is applied to several missiles,targeting data will be transferred to missiles as di-rected by the B-52 mission. While targeting data isbeing transferred, the launch point or target num-ber associated with the targeting data being trans-ferred will be displayed bright video in window 4for that missile on the FRMT-7 display (figure 7-4).The mission group identifier will be displayed inwindow 5. After the transfer of targeting data hascompleted successfully, the launch point or targetnumber will be displayed in bright underline videoin window 4. Automatic retargeting of all missilescan be initiated manually by entering a CF-589command.

JASSM Target Assignment (CF-586) (Manual Targeting)

The manual targeting request allows the operatorto command the transfer of targeting data associat-ed with specific launch points to selected missile(s).This is initiated by operator entry of CF-586. TheManual Targeting display as shown in figure 7-6,will be displayed on the selected MFD. The operatorwill then select a launch point and mission groupidentifier of the targeting data to be transferred,via a MDFY-1 command. Subsequently, the opera-tor will choose the missile to receive the targetingdata via a MDFY-6 command. A CF-DD commandwill initiate the transfer of designated targeting

data to the selected missile. A CF-DE command willexit the current targeting request without transfer-ring targeting data to any missile. The active tar-geting operation may also be deactivated by remov-ing the display associated with the current target-ing request from all MFDs, prior to CF-DD.

Retarget All (CF-589)

The operator can initiate the transfer of pre-planned targeting data to all missiles as directed bythe currently loaded B-52 mission by entering aCF-589 command.

Once a CF-589 command is accepted, all missileswill become untargeted and the SMO will halt anytargeting in progress. The SMO will then restorethe missile assignment data to the original valuesof the B-52 mission that is loaded and initiate auto-matic targeting of all missiles assigned to a launchpoint or target with the pre-planned targeting data.This will result in the loss of targeting data pre-viously transferred to the missiles. Targeting datawill not be transferred unless the same conditionsexist as for automatic targeting. Missiles that donot have power applied or have not completed thepower-on sequence will be targeted when missilepower is applied.

NOTE

A retarget-all command requires approxi-mately 2 minutes per JASSM on the aircraft.

T.O. 1B-52H-34-2-8

Change 3 7-19

JASSM Target Assignment (Manual Targeting)Display (CF-586)

[AMI]

Less [AMI]

Figure 7-6

T.O. 1B-52H-34-2-8

7-20 Change 3

Direct Targeting (CF-588,n)

Direct target definition and assignment allows theoperator to specify a target that is not included as apreplaned mission. This process is initiated by the op-erator entering CF-588,n. The Direct Target screen,figure 7-7, will be displayed on the selected MFD. Amissile assigned to a direct target will generate itsown route to intercept target azimuth. Waypointscannot be specified for a direct target. The direct tar-get request allows the operator to specify a direct tar-get to be assigned to a missile. The operator can enterthe target latitude, longitude, elevation, and Less[AMI] target elevation reference, by entering aMDFY-1 command. The missile’s cruise altitude canbe specified by entering a MDFY-2 command. TheMDFY-3 command allows the operator to enter abearing to target and impact angle. The fuze mode ofsoft impact or hard impact can be specified by enter-ing a MDFY-4 command. The fuze delay time can bespecified by entering a MDFY-5 command. By enter-ing a MDFY-6 command, the operator can choose themissile to receive the direct target data.

Operator entry of CF-Dn, where n represents thenumber of the direct target to receive the copied direct

target data, will result in the Direct Target currentlydisplayed being copied to direct target n. A confirma-tion prompt, OVERWRITE DATA? (YES/NO) will bedisplayed requesting confirmation to overwrite theexisting direct target data for direct target n with thecurrent direct target data. A YES response to the con-firmation prompt will result in overwriting the targetdata for direct target n and any missiles previouslyassigned/targeted to direct target n will be unas-signed/untargeted. A NO response to the confirma-tion prompt will result in abandoning the CF-Dn com-mand, leaving the direct target n data and missile as-signment and targeted states unchanged. If the con-firmation prompt is unanswered after 60 seconds, thedefault answer of NO will be assumed.

A CF-DD command with missiles selected, will initi-ate the transfer of the direct target data to the se-lected missile. A CF-DD command without a missileselected will save the data without transferring datato any missile or changing the assignment status ortargeting status of any missile. A CF-DE commandwill exit this targeting request and not transfer thetargeting data.

T.O. 1B-52H-34-2-8

Change 3 7-20A

Direct Target Definition Display (CF-588,n)Less [AMI]

[AMI]

D I RECT TGT

CF - DD=DONE CF - DE =ESC CF - DN=COPY TO D I R TGT ( D 1−D6 )

WPNS TO SEL ECT

OF− − − −CF - 5 8 8 n

’

1 3 1 4 1 56

1 2

A75613

12(ALL TOP BOXES)

ENTER E TO SEL ECT OR 0 TO DEL ETE

1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3 1 3

TGT PT

BRNG TO TGT

FUZE DE

L AT LONG AL T’1

2

3

4

5

4 53

’6

7o

I MPACT ANGL E 8o

CRU I SE AL T

FUZE MODE 1 09 1−SOF T 2 −HARD

L AY ( 0 − 7 )1 1

Figure 7-7

T.O. 1B-52H-34-2-8

7-20B Change 3

Targeting Data Items

Direct target definition (CF-588) and manual tar-geting (CF-586), require data item entry/modifica-tion by the operator initiated by MDFY-n, where nrepresents the MFD line number associated withthe data to be entered/modified. Several data itemsare common to the Manual Targeting and DirectTarget Definition displays. The operator will usethe same missile selection process for manual tar-geting and direct target assignment. If the operatorenters an invalid command through the IKB, thecommand will be displayed in reverse video. If theoperator enters invalid data values, the affecteddata fields will be displayed in reverse video.

LAUNCH POINT NUMBER

In order to manually target a missile, the operatormust select the launch point number associatedwith the target. The launch point number is en-tered in window 2, (figure 7-6) of the Manual Tar-geting display (CF-586). The input is numeric andranges from 1 to 99. Only the numbers of launchpoints defined by the B-52 mission to be launchpoints for the SMO that is loaded are valid.

MISSION GROUP IDENTIFIER

Along with the missile event selected in window 2,(figure 7-6) the mission group identifier associatedwith that launch point is entered in window 3 of theManual Targeting display, (figure 7-6). Valid IKBinput entries for window 3 are A, B, C, D, E, F, or itmay be left blank. If it is left blank, the currentlyidentified mission group will be assumed. If no mis-sion group has been preplaned, a default missiongroup A will be assumed. The range of valid alphacharacters (A-F) is dependent on the quantity ofmission groups associated with the launch pointand missile type currently loaded.

TARGET LOCATION

The target location is the geographical position andelevation which a missile is to strike. The targetlocation data fields appear on the direct target defi-nition screen (CF-588), figure 7-7. The positionentry key fields are:

• Target point reference latitude in degrees, min-utes, and ten-thousandths of a minute.

• Target point reference longitude in degrees, min-utes, and ten-thousandths of a minute.

• Target point reference elevation ([AMI] MSL;Less [AMI] MSL or HAE) in feet.

• Less [AMI] Target point elevation reference(HAE or MSL).

BEARING TO TARGET

The bearing to target specifies the weapon’s termi-nal ground track to the target (figure 7-8). The de-sired bearing to target is entered in window 7,(figure 7-7) of the Direct Target screen (CF-588).The valid input values are from 0 to 360 degrees (0= North) and 999, the default value, which indi-cates the missile will use the angle from the aircraftto the target at point of release, as the bearing totarget.

TARGET IMPACT ANGLE

The target impact angle specifies the angle in de-grees, relative to local level plane at the target (fi-gure 7-8). The impact angle is entered in window 8of CF-588, the Direct Target screen (figure 7-7). Thevalid input values are from 0 (level) to 90 (vertical)degrees. The default impact angle is 60 degrees.

NOTE

If less than 20 is entered for an impactangle, the missile will use a built in mini-mum value of 20. If more than 70 is enteredfor an impact angle, the missile will use abuilt in maximum value of 70.

CRUISE ALTITUDE

The cruise altitude indicator, window 6, is used tospecify a cruise altitude (MSL) for the JASSM onCF-588, the JASSM Direct Targeting display (fig-ure 7-7). Valid entries for this field range from 0 to45000 feet (MSL) and 99999, the default value, dis-played prior to operator entry. Although entriesfrom 0 to 45,000 feet are permitted, the missile willnot fly above 22,000 feet. The missile uses 15,000feet as the default value (99999).

FUZE MODE

The fuze mode indicator, window 9, (figure 7-7), isused to specify a fuze mode of either soft impact ref-erenced to Crush Switch, or hard impact referencedto G-force Sensor. On CF-588, the JASSM DirectTargeting display. The operator can select a fuzemode of Soft by entering 1 or a fuze mode of Hardby entering 2. The text SOFT or HARD will be dis-played in window 10, depending on the fuze modeselected. A default value of 1 (Soft) is displayedprior to operator entry.

All data on pages 7-20C through 7-20D (Deleted).

T.O. 1B-52H-34-2-8

7-21

JASSM Target Definition

Figure 7-8

FUZE DELAY

Fuze delay in milliseconds can be specified by en-tering a corresponding delay entry number inwindow 11, of the JASSM Direct Targeting display(CF-588) figure 7-7. Valid entries are shown in thetable below. A fuze delay will delay detonation fromthe time of impact by the specified time value. A de-fault value of 0 is displayed prior to operator entry.


0 0

1 10

2 15

3 20

4 30

5 40

6 50

7 120

MISSILE SELECTION INDICATOR

The missile selection indicator, window 12, is usedwhen selecting missiles during a manual targetingor direct target definition operation. Valid entriesare E and 0 (zero), where E indicates that the corre-sponding missile is selected for targeting and 0 in-dicates the missile is not selected. Window 12 willbe blank when any of the following conditions aretrue:

• The missile is not present• The missile is not selected and is unavailable for

selection due to a permanent fatal fault prior toa CF-DD command.

• The missile is not present or is unavailable for selection due to a permanent fatal fault followinga CF-DD command and is not a selected missile.

T.O. 1B-52H-34-2-8

7-22

TARGETING TECHNIQUES

This section describes the methods and proceduresused when entering targeting data for the followingtargeting operations:

• Manual targeting.• Direct targeting.

When a targeting display is initially requested, theassociated targeting operation becomes active. Sub-sequently, the same targeting display can be re-quested on another MFD by entering the associatedtargeting display request command while that tar-geting operation is active. This capability can beused to allow the other operator to view targetingdata. Once the targeting display is requested onanother MFD, the targeting process control com-mands, CF-DD and CF-DE, can also be entered forthat MFD. By using this method, the operators willbe able to view and confirm data that is being en-tered or continue the targeting process if an IKBfailure occurs.

NOTE

If data is being entered by both operators,data input by one operator can be overwrit-ten by data input by the other operator.

Once a target data set modification or direct target-ing operation has been completed via a CF-DD com-mand, that targeting operation is no longer active.The manual targeting operation will remain activeafter a CF-DD command has been entered. Once amanual targeting or direct targeting operation hasbeen exited using a CF-DE command, that target-ing operation will no longer be active.

NOTE

An active targeting operation will also bedeactivated if the display associated withthe active targeting operation is removedfrom all MFDs or a valid Retarget All com-mand (CF-589) or Load B-52 Sortie MissionData (CF-81,n) command is entered.

If the operator enters an invalid command throughthe IKB, the command is displayed in reverse vi-deo. If an invalid value is input in more than onefield, only the first field with an invalid value isdisplayed in reverse video when the ENTER key ispressed. If a valid value is input for that window,the next window with an invalid value is displayedin reverse video on MFD command line.

NOTE

Do not initiate a manual targeting or directtargeting operation to weapons that havenot achieved a GO status (FRMT-7, JASSMStatus).

Missile/Target Assignment (Manual Targeting)Data Entry Process

To perform the manual targeting operation, theManual Targeting display (CF-586) must be dis-played on the selected MFD. The Manual Targetingdisplay is shown in figure 7-6. The detailed dataentry process is described below.

A. Enter CF-586.

NOTE

A CF-DE command can be entered to aban-don the manual targeting operation at anytime. When a CF-DE command is entered,the manual targeting operation is termi-nated, and all associated targeting displayswill remain displayed and updated. The tar-geting availability status for each location/station, window 5, figure 7-6 will continueto be statused. All remaining windows willbe blanked.

Upon entry of a valid CF-586 command:

CF-586 display will be presented on the selectedMFD as shown in figure 7-6.

The location and station of each missile that ispresent and available for selection is displayed inwindow 6. The locations are assigned from left toright across the screen in the preferred launch se-quence, figure 7-21. This status is continually up-dated while the manual targeting display is presenton the MFD.

Blanks are displayed in the column location re-served for each missile that is not present or notavailable for selection due to a permanent fatalfault.

• Targeting data loading status (window 1).• Launch Point number (window 2).• Mission group identifier (window 3).• Missile selection status indicator (window 4).• Number of missiles remaining to be selected

(window 6).• Number of missiles required (window 7).

T.O. 1B-52H-34-2-8

Change 2 7-23

B. Enter MDFY-1 to copy line 1 to the MFD com-mand line for modification.

The information contained on line 1 is copied to theMFD command line as:

1 LAUNCH POINT (1-99) nn MISSION GROUP(A-F) a

NOTE

Modifiable fields are shown in boldface forconvenience, but are highlighted as definedwhen displayed on the MFD.

C. Enter the desired launch point and missiongroup identifier.

nn is the desired launch point number, where nn isa valid JASSM launch point number from 01 to 99.

a is the desired mission group identifier, where a isany value from A to F. The mission group identifierdefault is A.

Upon entry of the launch point and mission group,the missile assignment is indicated by an E in win-dow 4. Missiles not assigned to the launch pointwill be indicated with a 0 in window 4.

D. Enter MDFY-6 to copy line 6 to the MFD com-mand line for modification


6 x x x x x x x x x x x x

The instruction ENTER E TO SELECT OR 0 TODELETE is displayed on the bottom of the MFD.

E. Key in the desired missile assignment indica-tor as follows:

x is the indicated missile assigned to the indicatedmissile launch point or launch point and missiongroup identifier. Input is either E to indicate themissile has been selected, or 0 to indicate the mis-sile is not selected.

NOTE

Only one missile is required for assignmentto the designated launch point. If more thanone missile is selected, ranging will be in-hibited for all selected missiles while manu-al targeting is active.

F. Press the ENTER key. the missile selectionstatus for the desired missile location/station willbe updated and displayed on line 6.

The remaining number of missiles to be selected, ifany, is displayed in window 6. JASSM targets re-quire only one missile.

• The value in window 6 should be 1 when noweapon is selected or 0 when one weapon isselected. If more than one missile is selected,the difference is displayed as a negative num-ber in reverse video.

NOTE

If more than one missile is selected, all se-lected missiles will have ranging inhib-ited until corrected by the operator. CF-DD, CF-DE, or leaving the CF-586 screenare sufficient to remove the inhibit.

• If no missile is selected, a 1 is displayed innormal video indicating that one missile re-mains to be selected.

The contents of window 4 will be updated to showwhich missiles are assigned.

If more than one missile is selected, the least pre-ferred missiles will be deselected by the SMO to re-duce the number of missiles selected to one missilerequired for the designated target when a CF-DDcommand is entered. The contents of window 6 willbe updated with a 0 displayed in normal video. Thecontents of window 4 will then be updated to showwhich missile is assigned.

G. Enter CF-DD to save the target data and initi-ate the downloading of the targeting data to the se-lected missiles.

NOTE

A CF-DD command will be accepted only af-ter the missile launch point number andmission group identifier have been input,one missile required has been determined,and the Less [AMI] missile mission DTC([AMI] Weapon Group Data) is accessible.

The currently selected missile and the missile cur-rently assigned will be set as untargeted.

NOTE

These missiles will no longer be targeted totheir previous missile launch point or directtarget.

T.O. 1B-52H-34-2-8

7-24

Assignment of selected missiles and the transfer oftargeting data to selected missiles is initiated.

NOTE

Missile power must be applied to a selectedmissile in order to be targeted. A selectedmissile which does not have power appliedwill not be targeted until power is appliedand the manual targeting operation is ter-minated by either entering CF-DE or by re-moving the manual targeting display fromall MFDs.

Data modification will be inhibited and associatedtargeting displays will remain displayed and up-dated as follows:

• All line 1 and line 6 modifiable variables willbe blank.

• Windows 6 and 7 will be blank.• LOADING will be displayed in window 15 in

bright blinking video while the data is beingdownloaded to the missiles.

H. The targeting process of each selected missilecan be monitored on the FRMT-7 display. TheCF-586 display will be updated as follows:

If the transfer of targeting data to all selected mis-siles completes successfully:

• COMPLT is displayed in window 1 in normalvideo.

• The location/station of assigned missiles willbe displayed in reverse video in the appropri-ate window 5.

• Data will remain displayed in all modifiablewindows and windows 6 and 7.

If the transfer of targeting data to all selected mis-siles completes unsuccessfully:

• COMPLT is displayed in window 1 in reversevideo.

• The location/station of the unsuccessfully tar-geted missile is displayed in reverse video inthe appropriate window 5.


Direct Targeting Data Entry Process

To perform the direct targeting operation, the Di-rect Target Definition Display (CF-588) (figure 7-7)must be displayed on the selected MFD. The pro-cess is described in detail below.

A. Enter CF-588,n (figure 7-7) where n (1 to 6) isthe number of the direct target to be defined.

NOTE

A CF-DE command can be entered to exitthe direct target operation without down-loading data to the missile at any time priorto entry of a CF-DD command. When a CF-DE command is entered, the direct targetoperation is terminated, data modificationis inhibited, and the specified direct targetnumber will remain displayed on the top ofthe MFD. The targeting availability statusfor each location/station will continue to bestatused. All remaining windows areblanked. The direct target data will not besaved if a CF-DE command is entered. Theprevious direct target data is maintained.

Upon entry of a valid CF-588,n command:

The CF-588 display is presented on the selectedMFD.

The identifier n (1, 2, 3, 4, 5, or 6) for the requesteddirect target is displayed on the top of the MFD,window 1. The targeting completion status, window2 will be blank.

The location and station of each missile that ispresent and does not have a permanent fatal faultis displayed on the bottom of the MFD in a reservedcolumn location (window 13). The column locationsare assigned from left to right across the screen inpreferred launch sequence. The video mode of win-dow 13 indicates each missile’s targeting availabil-ity status (figure 7-7). This status is updated whilethe Direct Target Definition display is present onthe MFD.

T.O. 1B-52H-34-2-8

Change 3 7-25

If the requested direct target data is requested forthe first time:

• The target point reference latitude (window 3),longitude (window 4), and elevation (window 5)with a default value of 0, Less [AMI] and targetelevation reference (window 6) with a defaultvalue of 1 will be displayed.

• Cruise altitude (window 6) is displayed witha default value of 99999 feet which indicatesthe missile will use the default value of 15000feet MSL.

• The Bearing to Target (window 7) will have adefault value of 999, which indicates the mis-sile will determine the BTT at the point ofrelease. Impact angle (window 8) will have adefault value of 60 degrees.

• Fuze mode (window 9) will have a default val-ue of 1, SOFT.

• Fuze delay (window 11) will have a defaultvalue of 0.

If data for the requested direct target has been pre-viously changed and saved, the targeting data forthe specified direct target n is displayed.

The following steps outline the data modificationprocess which is initiated by entering a MDFY-ncommand where n is the line number of the data tobe copied to MFD command line. The steps beloware ordered from entry of a MDFY-1 throughMDFY-6. Data can be entered in any order and se-quencing through the lines in order is not required.

B. Enter MDFY-1 to copy line 1 to the MFD com-mand line for modification.

The information contained on line 1 is copied to theMFD command line as follows:

1 TGT PT addomm.mmmm adddomm.mmmmfffff’ Less [AMI] r

NOTE

Modifiable fields are shown in boldface forconvenience, but are highlighted as definedwhen displayed on the MFD.

C. Key in the desired target latitude, longitude,elevation, and Less [AMI] elevation reference usingthe IKB.

addomm.mmmm is the target latitude (window 3) indegrees, minutes, and ten-thousandths of a minute.a = N for North and S for South. dd = degrees from 0to 90. mm.mmmm = minutes from 00 to 59 and ten-thousandths of a minute from 0000 to 9999.

adddomm.mmmm is the target longitude (window4) in degrees, minutes, and ten-thousandths of aminute. a = E for East and W for West. ddd = de-grees from West 180 to East 179. mm.mmmm =minutes from 00 to 59 and ten-thousandths of aminute from 0000 to 9999.

fffff is the target point elevation (window 5) in feet(MSL, Less [AMI] or HAE). Input ranges from–328 to 32810 feet.

Less [AMI] r is the target elevation reference (win-dow 6). Valid input is 0 or 1. 0 represents a mea-surement of MSL for the target point elevationwhile 1 indicates HAE.

D. Press the ENTER key.

The entered latitude, longitude, elevation, and Less[AMI] target elevation reference will be displayedon line 1, windows 3, 4, 5 and Less [AMI] 6.

E. Enter MDFY-2 to copy line 2 to the MFD com-mand line for modification.


2 CRUISE ALT fffff ’

F. Key in the desired cruise altitude using theIKB.

fffff ’ is the desired cruise altitude in feet MSL(window 6). Valid input range is from 0 to 45000feet, however, the missile will not fly above 22,000feet. A value of 99999 is displayed prior to operatorentry, indicating that the default value of 15,000feet is being used.

G. Press the ENTER key.H. Enter MDFY-3 to copy line 3 to the MFD com-mand line for modification.

The information contained on line 3 will be copiedto the command line of the MFD as:

3 BRNG TO TGT bbb° IMPACT ANGLE dd°I. Key in the desired Bearing to Target and Im-pact Angle using the IKB.

bbb° is the desired bearing to target in degrees(window 7). Valid input range is from 0 to 360 de-grees (0 = North) or 999. The default value of 999 isdisplayed prior to operator entry. The default valueindicates that the missile will determine it’s bear-ing to target from the aircraft to the target at timeof launch.

dd° is the desired impact angle for the missile indegrees (window 8).

The default impact angle is 60 degrees. Valid inputvalues are from 0 (level) to 90 (vertical) degrees,however, the missile will only use an impact angleranging from 20 to 70 degrees.

J. Press the ENTER key.

T.O. 1B-52H-34-2-8

7-26

K. Enter MDFY-4 to copy line 4 to the MFD com-mand line for modification.


4 FUZE MODE n XXXX

L. Key in the desired Fuze Mode Identifier usingthe IKB.

n is the missile’s fuze impact setting. Valid inputsfor fuze mode are 1 (Soft Impact) and 2 (Hard Im-pact). The default value of 1 is displayed prior tooperator entry.

M. Press the ENTER key.

The entered fuze mode is displayed on line 4, win-dow 9. The corresponding fuze mode of SOFT orHARD is displayed in window 10.

N. Enter MDFY-5 to copy line 5 to the MFD com-mand line for modification.


5 FUZE DELAY n (0-7)

O. Key in the desired Fuze Delay Identifier usingthe IKB.

n is a single digit entry that identifies the millisec-ond fuze delay of the missile. Valid input entries forfuze delay are 0 through 7.

P. Press the ENTER key.

The entered fuze delay identifier is displayed inwindow 11.

Select/deselect missile(s) to be assigned to the des-ignated target as follows:

Q, Enter MDFY-6 to copy line 6 to the MFD com-mand line for modification.

The instruction ENTER ‘E’ TO SELECT OR ‘0’ TODELETE is displayed on the MFD.

NOTE

Only one missile is required for assignmentto the designated direct target. If more thanone missile is selected, ranging will be in-hibited for all selected missiles while directtargeting is active.

R. Press the ENTER key.

The remaining number of missiles to be selected, ifany, is displayed in window 14. JASSM targets re-quire only one missile.

• The value in window 6 should be 1 when noweapon is selected or 0 when one weapon isselected. If more than one missile is selectedthe difference is displayed as a negative num-ber in reverse video.

NOTE

If more than one missile is selected, all se-lected missiles will have ranging inhib-ited until corrected by the operator. CF-DD, CF-DE, or leaving the CF-586 screenare sufficient to remove the inhibit.

• If no missile is selected, a 1 is displayed innormal video indicating that one missile re-mains to be selected.

The contents of window 12 will be updated to showwhich missiles are selected.

If more than one missile is selected, the least pre-ferred missiles will be deselected by the SMO to re-duce the number of missiles selected to one missilerequired for the designated target when a CF-DDcommand is entered. The contents of window 6 willbe updated with a 0 displayed in normal video. Thecontents of window 4 will then be updated to showwhich missile is assigned.

S. If no other missiles are to be selected, enterCF-DD to save the direct target data and initiatethe downloading of the targeting data to the se-lected missiles.

NOTE

If no missile is selected and a CF-DD com-mand is entered, the data for the desig-nated direct target will be saved.

Currently selected missiles and missiles currentlyassigned will be set as untargeted.

NOTE

These missiles will no longer be targeted totheir previous launch point or direct target.

T.O. 1B-52H-34-2-8

7-27/(7-28 blank)

The SMO will compute the targeting data for eachselected missile and initiate the transfer of thatdata to the missiles.

• A selected missile that does not have powerapplied will be assigned but not targeted.

Data modification will be inhibited and associatedtargeting displays will remain displayed and up-dated as follows:

• LOADING is displayed in window 2 in brightblinking video while the data is being down-loaded to the missiles.

• The specified direct target number will re-main displayed in window 1.

• The targeting availability status for each loca-tion/station, window 13, will continue to bestatused.

• All remaining windows will be blanked.

T. The targeting process of the selected missilecan be monitored on the FRMT-7 display.The CF-588 display will be updated as follows:

1. If the transfer of targeting data to the selectedmissile completes successfully:

• COMPLT is displayed in window 2 in normalvideo.

• The location/station of assigned missiles isdisplayed in bright underline video in the ap-propriate window 13.

• All modifiable windows and windows 14 and15 will be blank.

2. If the transfer of targeting data to the selectedmissiles completes unsuccessfully:

• COMPLT is displayed in window 2 in reversevideo.

• The location/station of each missile that wasnot successfully targeted is displayed in re-verse video in the appropriate window 13.


BLA

T.O. 1B-52H-34-2-8

7-29

TARGET RANGING

The SMO will perform Safe Launch advisories andLAR achievability/timing calculations for the asso-ciated target if any of the following conditions exist:

• A direct target mission has been downloaded intoa missile and that direct target has been selectedas the current weapon event with a PRGM-Dn com-mand.• The current B-52 mission destination has alaunch point associated with it and an associatedtarget mission has been downloaded into a missile.

NOTE

Ranging will be inhibited for all selectedmissiles on which Manual or Direct Target-ing is in progress.

JASSM uses a preplanned Static Launch Accept-ability Region (LAR) to determine when a target is

In-Zone for launch. This LAR is determined duringmissile mission planning, and used to determinethe B-52 route planning. Figure 7-9 illustrates anIn-Range and static In-Zone LAR.

There are two type of LARs, In-Range and In-Zone.The In-Range LAR is the larger of the two. Launchwhile In-Range, but not In-Zone will command themissile to fly to the target, omitting all waypoints.The missile will approach the target from the direc-tion of the waypoint immediately prior to the tar-get. As a result, an In-Range launch does not followthe preplanned route of flight, and therefore cannotfulfill a TOT requirement. The In-Zone LAR issmaller than the In-Range LAR with tighter toler-ances on location and heading, allowing a launchthat will follow the preplanned route. The automat-ic launch point, at the closest point of approach, isexplained further in the In-Zone LAR subsectionand in figure 7-13. If launched at the preplannedtime, the missile will arrive at the target within ±5seconds of the planned TOT.

JASSM Static LAR

Figure 7-9

T.O. 1B-52H-34-2-8

7-30

The JASSM SMO computes In-Range and In-Zoneachievability, Time to Go (TTG) to the In-Range/In-Zone LARs, and Time to Go (TTG) out of In-Range/In-Zone LARs for the ranging event. The SAIR pa-rameters are computed as a function of the LARdata provided by the missiles, mission data, and thecurrent aircraft flight conditions. The JASSM SMOwill establish a ranging cycle for polling a missile’sranging message and determine the current rang-ing event in order to provide ranging informationfor operator display and launch processing.

The JASSM SMO polls the missile associated withthe current ranging event a minimum of once persecond. For missiles associated with other targets/launch points (Direct Targets, Next RangingEvent), the JASSM SMO polls at least one (1) mis-sile every two (2) seconds. However, the JASSMSMO will attempt a ranging cycle rate of one (1)missile per pylon per major frame to accommodateboth of these requirements. The JASSM SMO pro-vides the capability to interrupt the ranging cyclewith a higher priority (Current, next, and other di-rect targets) ranging request for its data.

The JASSM SMO only polls operational missilesand starts the ranging cycle when the aircraft isairborne and at least one missile is present andpowered on with Min TXA, Min TDS, and has beentargeted by the JASSM SMO.

All missile stations will be included in the rangingcycle. If missile ranging cannot be performed be-cause it failed to satisfy the above criteria, theJASSM SMO marks the missile as not In-Range,unachievable (clear any steering cues), and ensuresthe In-Range TTG values are marked as invalid.The cycle will continue with the next major framewith the next missile in the cycle for the respectivepylon.

The JASSM SMO provides In-Range/In-Zone statusindications as follows:

• FRMT-7 Missile Status and Inventory for allpresent missiles.

• PRGM Display (Launch and Ranging data) forthe current ranging event and all direct tar-gets.

• Missile event recording when there is achange of status.

Current Ranging Event

The current ranging event will be determined fromthe B-52 Mission data as it is flown by the aircraftexcept when pre-empted by operator action. Thecurrent ranging event will be one of the followingmissile event types:

• Preplanned JASSM Launch Point.• Operator created Direct Target.

The current ranging event is defined as the nextplanned missile event on the Carrier Mission databased on the current destination of the aircraft(current mission leg only) when not pre-empted byan operator selected missile event. The JASSMSMO allows the operator to select the current rang-ing event for direct targets. The JASSM SMO alsoallows the operator to select the current rangingevent when the selected destination is a JASSMlaunch point. An operator selected ranging eventtakes precedence over the next missile event indi-cated in the carrier mission data. The launch pointmust have missiles assigned. Achievability, TTG toEnter In-Range/In-Zone, TTG to Exit In-Range/In-Zone and safe launch verification is performed forthe current ranging event. The missile associatedwith the current ranging event and the missile en-tered into launch countdown must be the same mis-sile. During launch countdown, the JASSM SMOcontinues the ranging calculations for the currentlaunch point using the last valid data from the mis-sile prior to commanding Commit To Separate Store(CTS).

The JASSM SMO terminates the current rangingevent when one of the following occurs:

• The missile event is disabled (missiles per tar-get is less than 1).

• The missile is in the process of being poweredoff, or has a power-off fault.

• For direct targets, the operator changes thesystem to Automatic Launch mode.

• The current ranging event (non-operator se-lected ranging event) is not the current (In-Range or In-Zone LAR) destination identifiedin the Carrier Mission data. (This may occurdue to destination sequencing.)

• Operator deselection.• The mission data preplanned launch point is

behind the aircraft and the aircraft has exitedthe In-Range LAR.

T.O. 1B-52H-34-2-8

7-31

The missile event following the terminated currentranging event in the Carrier Mission data will be-come the current ranging event.

The JASSM SMO shall not range on a missile eventif any of the following conditions exist:

• The missile event is disabled (missiles per tar-get is less than 1).

• The missile is not targeted, powered off, is inthe process of being powered off, or has a pow-er-off fault.

• The missile event (non-operator selected rang-ing event) is not the current (In-Range or In-Zone LAR) destination identified in the B-52Mission data (This may occur due to destina-tion sequencing).

• Any preplanned launch point occurring priorto the current destination of the aircraft.

IN-RANGE LAR

The missile provides the characteristics of the In-Range LAR and the In-Range status to the JASSMSMO. The JASSM SMO uses valid In-Range datafrom the missile and aircraft prime data to deter-mine In-Range Achievability, TTG to enter and exitthe In-Range LAR. The In-Range calculations areonly performed for the launch points and direct tar-gets identified as the current/next ranging events.

In-Range Achievability

The JASSM SMO sets In-Range Achievable, if thecurrent aircraft ground track will intersect the In-Range circle for the current ranging event. Figure7-10 illustrates when JASSM is In-Range achiev-able.

The JASSM SMO processes data to determine if In-Range is achievable (value of In-Range circle radiusis greater than the absolute value of Target cross-range) for a JASSM launch by computing the fol-lowing:

• Range from aircraft prime position to Targetusing the aircraft prime latitude and longi-tude from FMS and In-Range LAR latitudeand longitude.

• Azimuth of Target with respect to aircraftprime position relative to North, using the air-craft prime latitude and longitude from FMSand In-Range LAR latitude and longitude.

• Azimuth of Target with respect to aircraftprime position relative to the ground trackline through aircraft prime position, using theaircraft prime ground track from FMS andazimuth of Target with respect to aircraftprime position relative to True North.

• Target downrange and crossrange distancefrom aircraft prime position with respect toaircraft ground track, using the range fromaircraft to Target, azimuth of Target with re-spect to aircraft position relative to theground track line through aircraft position.

JASSM In-Range Unachievable

The geometry defining an unachievable In-RangeLAR is illustrated in figure 7-11. For direct targetsonly, the JASSM SMO provides a directional arrowthat points to the target and blanks the TTG In-Range, if unachievable, until passing the point ofclosest point of approach (CPOA) to the direct tar-get. After passing CPOA for a direct target, theJASSM SMO will remove the directional arrow,blank the TTG, and display the In-Range LAR labelin reverse video.

Time to Go to Enter/Exit In-Range

The JASSM SMO computes the TTG to the entry/exit points of the In-Range LAR when the aircraftis outside the In-Range circle and In-Range isachievable. The JASSM SMO computes TTG usingdistance to enter/exit In-Range (current prime air-craft position, closest intersection point of aircraftground track line with In-Range LAR circle, far-thest intersection point of aircraft ground track linewith In-Range LAR circle) and current prime air-craft ground speed from FMS. The TTG displayedmay have an error of up to �5 seconds, however,when In-Range, 0:00 will be displayed for TTG-Rentry time.

Once the aircraft is inside LAR, the TTG to exitcounts down to zero as the aircraft approaches theexit point. The In-Range LAR exit point is the pointat which In-Range Achievable transitions fromachievable to unachievable. If TTG to exit is equalor greater than one hour, the time displayed will be59:59. The JASSM SMO blanks the TTG when In-Range becomes unachievable.

T.O. 1B-52H-34-2-8

7-32

JASSM Achievable In-Range LAR


PMD

B40823

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

D 1

NAV

0 : :L 10 : :

MAN LNCH REQ

0 : 1 :1 1 : :

: : 5

1 5 0 0

B. IN-RANGE

D2

2 −

1 5 2 33 0 5 3

3 3 7

1 4 : 1 5TOT5 9 : 5 90 : 0 0RANGEL 7D 1

72

1 0 9 5 6 5 13 9 1 4

3 J ASSML P

D 1

: 2 5

PMD

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

D 1

1 NAV

0 : 0 0 : 0 0L 10 : 0 4 : 2 2

NAV

MAN LNCH REQ

4 9 3

0 : 1 5 : 2 01 1 : 16 : 0 0

1 : 2 6 : 5 8

21 5 0 0

3 5 51

4 5 : 2 0 5 9 : 5 9 TOTTTG−RR2D 1

A. PRIOR TO ENTERING IN-RANGE

D 1

B40822

T.O. 1B-52H-34-2-8

7-33


PMD

B40824

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

0 : 1 :: :

: :

1 5 0 0

1

0 6 5 1

2

A. IN-RANGE UNACHIEVABLE ON LEFT

3 3 6

2 NAV

5 2 010 7 4 8D2

TOTR7

NCHL REQMAN

0 8 02

D 1 D2

1 9 0 61 1 3 6 2 7

3 J ASSML P

TTG−R

D2

T.O. 1B-52H-34-2-8

7-34

JASSM Unachievable In-Range LAR


PMD

B40825

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

0 : 1 :: :

: :

1 5 0 0

1

TOT

NCHL REQMAN

1 5 4

0

D 1

0

D2

NAV

5 3 01 0 1 4 3 5D 1

L 7 TTG−R

2 −

7 05 4 3 6 6 5 1

1 1 0 6 1 2

2 3 J ASSML P

B. IN-RANGE UNACHIEVABLE ON RIGHT

D 1

T.O. 1B-52H-34-2-8

7-35


T.O. 1B-52H-34-2-8

7-36

IN-ZONE LAR

The definition of the In-Zone LAR is illustrated in fig-ure 7-12. The missile provides the characteristics ofthe In-Zone LAR and the In-Zone status to theJASSM SMO. The JASSM SMO uses In-Zone datafrom the missile which is marked valid by the missileand aircraft prime data to determine In-Zone Achiev-ability, TTG to enter and exit the In-Zone LAR. TheIn-Zone parameters are displayed on the MFD. WhenIn-Zone data is invalid, the TTG for the current rang-ing event missile is displayed in reverse video.

To achieve In-Zone LAR, the aircraft must be with-in tolerance of preplanned release conditions. Alti-tude must be within ± 3000 feet of the planned

HAE altitude. Speed must be within ± 0.1 TrueMach of preplanned release speed. Heading toler-ance is selectable in the AFMSS setup, but is nor-mally ± 20°. Releases should always be at level con-ditions. Release advisories are provided to theRN/N in the Program Display to guide the crew tothe correct release conditions.

Weapon release advisories do not inhibitlaunch. Possible collision between weaponsand between weapon and aircraft can occur ifweapon is launched with a release advisorydisplayed.

JASSM In-Zone LAR

Figure 7-12

T.O. 1B-52H-34-2-8

7-37

In-Zone Achievability

The JASSM SMO sets In-Zone Achievable to logicone if the current aircraft ground track will inter-sect the In-Zone LAR area for the current event. Fi-gure 7-13 illustrates an achievable In-Zone LAR.

The JASSM SMO processes data supplied by themissile to determine if In-Zone is achievable for aJASSM launch by computing the following:

• Latitude and longitude for the point of inter-section of In-Zone Start Angle and In-ZoneArc Min Radius, using In-Zone Arc Center lat-itude and longitude, In-Zone Arc Min Radius,as the distance d, and In-Zone Start Angle.

• Latitude and longitude for the point of inter-section of In-Zone Start Angle and In-ZoneArc Max Radius, using In-Zone Arc Centerlatitude and longitude, In-Zone Arc Min Ra-dius, as the distance d, and In-Zone StartAngle.

• Latitude and longitude for the point of inter-section of In-Zone Stop Angle and In-Zone ArcMin Radius, using In-Zone Arc Center lati-

tude and longitude, In-Zone Arc Max Radius,as the distance d, and In-Zone Stop Angle.

• Latitude and longitude for the point of inter-section of In-Zone Stop Angle and In-Zone ArcMax Radius, using In-Zone Arc Center lati-tude and longitude, In-Zone Arc Max Radius,as the distance d, and In-Zone Stop Angle.

• In-Zone approach azimuth with respect to thepoint of intersection of In-Zone Stop Angleand In-Zone Arc Min Radius relative to North.

• Range from aircraft position to Waypoint #1position, using the current aircraft prime lati-tude and longitude from FMS and In-Zone ArcCenter latitude and longitude.

• Azimuth of Waypoint #1 with respect to air-craft position relative to aircraft ground trackline, using the current aircraft prime latitudeand longitude from FMS and In-Zone ArcCenter latitude and longitude.

JASSM In-Zone Unachievable

The geometry defining an unachievable In-ZoneLAR is illustrated in figure 7-14.

JASSM Achievable In-Zone LAR


PMD

B40826

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

0 : 1 :: :

: :

1 5 0 0

1

0

2 8TOT

NCHL REQMAN

0 8 02

2

TTG− Z

1 5 4

3 J ASSML P

5 169 4 1

L 2 TTG−R

ROL L

L P 0 3:4 3 2 2

4 −NAV

0 2 4 9 9 3 09 2 4 5

A. RANGE CALCULATED, ZONE NOT CALCULATED

PMD

B40827

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

NAV

0 : 1 :: :

: :

1 5 0 0

53

: 5 : TOTL P 0

0

3 J ASSML P

16 5 1

04

TTG− Z9

0 0 2

:

−

6 5 19

: 1 2

4 9

1 4 7

3 93

TTG−RL 2

0

2 2 5 89 5

6

9 2 4 2 0

2 4 3 0

B. RANGE AND ZONE CALCULATED

T.O. 1B-52H-34-2-8

7-38

JASSM Achievable In-Zone LAR (Cont)


PMD

B40828

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

MAN LNCH REQ

0 : 1 :: :

1 5 0 0

1

1 :TOT5 9 : 5 90 : 0 0L

6 5 1

3 3D 1

3 J ASSML P

6 3 19 2 4 2 1

4 1 52 RANGEL P 0 3

TTG− Z 1 3 : 16 1 : 5 9

0 5 13

0 : 0 2 : 4 9

4 −NAV

9 2 4 2 2

C. IN-RANGE, NOT IN-ZONE

: 3 3

PMD

B40829

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

D 1 0 : :L : :

NAV

0 : 1 :: 1 :

1 : 2 6 : 5 8

1 5 0 0

53

: 5 : OT

D. IN-RANGE AND IN-ZONE

D2

L 2 RANGEL P 0 3

ZONE0 00 1 5

0 : 0 0 1 2 2

2

3 J ASSML P

16 5 19 1 9 16

0 24

6 5 19 9 2 6

:ROL L

3 T 1 :4 15 2 0:

T.O. 1B-52H-34-2-8

7-39


T.O. 1B-52H-34-2-8

7-40

JASSM Unachievable In-Zone LAR

PMD

B40830

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

0 : 1 :: :

: :

1 5 0 0

1

0

TOT

NCHL REQMAN

TTG− Z

1 5 4

3 J ASSML P

5 16

LP 0 3

4 −NAV

0 2 4 9 9 3 0

D 1

1 4 : 1 58 4 3 0 3

95:950 : 0 02L

RANGE

0 5 2

4 3 1 98

3

: 2 0

Figure 7-14

T.O. 1B-52H-34-2-8

7-41

Time to Go to Enter/Exit In-Zone

The JASSM SMO computes the TTG to the entry/exit point of the In-Zone LAR area when the air-craft is outside the In-Zone LAR area and In-ZoneAchievable is achievable. The TTG displayed mayhave an error up to �5 seconds with TTG-Z entrytime displayed as 0:00, once In-Zone. When In-Zoneis achievable for a JASSM launch, the JASSM SMOprocesses data to determine Time to Go to enter/exit In-Zone by using the following parameters:

• Distance to go to In-Zone entry point (currentprime aircraft position, intersection point ofaircraft ground track line with In-Zone ArcMax Radius) and current prime aircraftground speed.

• Distance to go to In-Zone exit point (currentprime aircraft position, intersection point ofaircraft ground track line with In-Zone ArcMin Radius) and current prime aircraftground speed.

Once the aircraft is inside In-Zone LAR, the time toexit counts down to zero. The JASSM SMO blanksTTG when In-Zone in unachievable.

Time on Target

The JASSM SMO displays the current Time on Tar-get (TOT) on PRGM screen any time the missile in-

dicates an In-Range or In-Zone status for the cur-rent ranging event.

In-Zone Advisories

When In-Zone is achievable for a JASSM launch,the JASSM SMO shall compute In-Zone advisoriesfor Altitude, Mach and Heading.

Preplanned Launch Point (Mission Data PreplannedMissions Only)

The preplanned Launch Point latitude and longi-tude are identified in the missile Mission data. Fora JASSM Launch Point within the In-Zone LAR,the JASSM SMO determines the closest point of ap-proach (CPOA) for the preplanned launch point(JASSM LP). If the closest point of approach iswithin the In-Zone LAR, the JASSM SMO will al-low an automatic launch at this point. If the closestpoint of approach is not within the In-Zone LAR,but In-Range LAR is achievable, the JASSM SMOrequires a manual launch. Figure 7-15 illustratesCPOA geometry for a CPOA outside the In-ZoneLAR, but within the In-Range LAR.

For preplanned JASSM launch points which do nothave an In-Zone LAR defined, the JASSM SMO re-quires a manual launch.

JASSM Closest Point of Approach Outside In-Zone LAR


PMD

B40832

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

NAV

0 : 1 :: :

: :

1 5 0 0

53

: 5 : TOTL 2 RANGEL P 0 3

0 00

3 J ASSML P

16 5 1

0 24

D 13

TTG− Z9

0 0 23

D2

:5 1

9 5 3 6:1

−

6 5 19 5

4 1 50 : 0 0 1 2 3

TRN L EF T

4 91 1

B. IN-ZONE, OUT OF HEADING TOLERANCE

5

: 1 2

PMD

B40831

1 CPA

D

PTA

D

− −PRGM -L

PTA

D

ETE

8 0 0 ’1 5 0 0

0 : :L : :

NAV

0 : 1 :: :

: :

1 5 0 0

53

: 5 : TOTL 2 RANGEL P 0 3

0 00

3 J ASSML P

16 5 1

0 24

D 13

TTG− Z9

MAN LNCH REQ

0 0 23

D2

HDG TOL1 : 5 9 0 : 1 2

5 19 5 3 6

51:41

−

5 0 6 5 19 5 4 3

A. PRIOR TO IN-ZONE

16

: 71

T.O. 1B-52H-34-2-8

7-42

JASSM Closest Point of Approach OutsideIn-Zone LAR (Cont)


T.O. 1B-52H-34-2-8

7-43

TARGET RANGING INDICATIONS

Operator entry of PRGM displays the PRGM screen(figure 7-16) that will contain ranging data if any ofthe preceding conditions exist. Operator entry ofPRGM-Dn displays the PRGM screen with rangingdata for the defined direct target (n = 1 - 6). The fol-lowing is a summary of the windows which provideranging data displayed on the PRGM screen.

• Window 3 displays the JASSM launch pointnumber or direct target identifier for which rangingdata is being provided.• Window 4 displays the location/station of the mis-sile assigned to the target. The launch ability andranging status of the missile is displayed in thiswindow.• The In-Range status is displayed in window 5.• Window 6 indicates the time to go (mm:ss) in or-der to achieve In-Range. If the time displayed is00:00, the aircraft is already In-Range.• Window 7 indicates the remaining In-Range timein minutes and seconds if the aircraft continues flyingat the current ground speed, altitude, and groundtrack.• Window 8 displays TOT (Time on Target) label ifthe missile is calculating the Time of Flight.• Window 9 indicates the Weapon TOT which iscalculated by adding the Current Time of Flight(CTOF) plus UTC when CTOF is returned from aweapon ranging on a target. CTOF is the time fromrelease (Umbilical separation) to target impactbased on current aircraft position and heading. Ifthe aircraft is In-Zone, CTOF represents the esti-mated flight time from the current aircraft positionto the target along the preplanned flight path. Ifthe aircraft is In-Range and not In-Zone, CTOF rep-resents the estimated flight time from the currentaircraft position to the target along the In-Rangeflight path. TOT is accurate within ±5 seconds onlyif the aircraft is In-Zone and the mission is plannedas Time on Target required.• Window 10 displays an arrow as a steering cuewhen the aircraft is not on track and needs to steereither left ( ← ) or right ( → ) in order to achieveIn-Range. Preplaned targets will not use arrowsteering cues. Direct targets will have arrow steer-ing cues for In-Range only. A blank in window 10indicates the aircraft is on track to intersect In-Range or the target is a preplaned target.• The In-Zone status is displayed in window 11.• Window 12 indicates the time to go (mm:ss) inorder to achieve In-Zone. If the time displayed is00:00, the aircraft is already In-Zone.

• Window 13 indicates the remaining In-Zone timefor a launch point in minutes and seconds if theaircraft continues flying at the current groundspeed, altitude, and ground track.• Window 15 indicates seeker guidance capability.A blank indicates missile has seeker guidance capa-bility, the reverse video text SKR indicates the mis-sile mission requires a seeker and either a terminalguidance fault exists or a seeker is not available.• Window 16 indicates launch method require-ments. If a manual launch is required, MAN LNCHREQ will be displayed in bold. If the window isblank, an automatic launch is permitted.

IN-RANGE/IN-ZONE INDICATION

The In-Range/In-Zone status for missile launches isprovided in windows 5 (Range) and 11 (Zone) of thePRGM Screen display, see figure 7-16. This statusis displayed in different video modes to indicatewhether the aircraft is approaching In-Range/In-Zone or is currently In-Range/In-Zone.

NOTE

Once the missile is launched, it will flywaypoints, if it is In-Zone or was In-Zone inthe last 8 seconds. If the missile was launchedwithin 8 seconds of exiting In-Zone, In-Rangewill be displayed upon launch, but the missilewill fly an In-Zone profile.

WEAPON LAUNCH ADVISORIES

Weapon launch advisories appear on the PRGMscreen display (figure 7-16, window 14) to alert theaircrew that an action is required to ensure weaponlaunch parameters are met. When multiple weaponlaunch advisories exist, the highest applicable advi-sory message will be displayed on the PRGM dis-play. The defined JASSM weapon launch advisoriesand the corrective action are contained at the end ofthis section in figure 7-23.

NOTE

Weapon launch advisories are calculated bythe aircraft. In-Range and In-Zone indica-tions are independently calculated by theweapon. Due to differences in these calcula-tions, such as computing method and datalatency, it is possible there may be a differ-ence in the timing of these indications. TheIn-Range and In-Zone indications describethe status of the weapon, and will be hon-ored by the weapon when launched.

T.O. 1B-52H-34-2-8

7-44

SAFE RELEASE ADVISORIES

The JASSM SMO does not have any safe launch re-strictions which would prevent missile launch. Thesafe release advisories, displayed on the PRGMscreen, inform the operators of a potentially unsafelaunch condition, however, launch can still be per-formed.

When multiple safe release advisories exist, thehighest applicable advisory message will be dis-played on the PRGM Display. The defined JASSM

safe release advisories and the corrective action arecontained at the end of this section in figure 7-22.

Safe release advisories do not inhibit launch.Possible collision between weapons and be-tween weapon and aircraft can occur if weap-on is launched with a safe release advisorydisplayed.

PRGM Display In-Range/In-Zone Indications

PMD

1 CPA

PTA

D 1

2 2 2 2 2 2

4

10

3511

612

713

1416

D D

PTAETE

− −PRGM−

A75619

1

8

15

9

WINDOW DISPLAY TEXT VIDEO INDICATION

TTG-R Normal Aircraft is approaching In-Range.

5 TTG-R ReverseAircraft is not In-Range and In-Range is unachievable or

missile is not targeted.

RANGE Bright Underline Aircraft is currently In-Range.

TTG-Z Normal Aircraft is approaching In-Zone.

11 TTG-Z ReverseAircraft is not In-Zone and In-Zone is unachievable or

missile is not targeted.

ZONE Bright Underline Aircraft is currently In-Zone.

NOTE

In-Range LAR is determined by the missile and retrieved by the SMO In-Rangestatus and Range distance messages.

Figure 7-16

T.O. 1B-52H-34-2-8

7-45

MISSILE LAUNCH

The missile launch process, including the means forcontrolling, suspending, and stopping a missilelaunch, as well as launch command restrictions aredescribed in the following paragraphs. Figure 7-17shows a Launch Sequence Timeline.

If launch is commanded while either unlock consentswitch is in the lock position, the advisory messageNO CONSENT will be displayed on each MFD.

NOTE

Once the missile is launched, it will flywaypoints, if it is In-Zone or was In-Zone inthe last 8 seconds. If the missile was launchedwithin 8 seconds of exiting In-Zone, In-Rangewill be displayed upon launch, but the missilewill fly an In-Zone profile.

MISSILE LAUNCH PROCESS

The following provides a summary of the activitieswhich the SMO will command or control to launch amissile:

• Apply 28-volt dc #2 power to the missile station.If unsuccessful, a dc #2 power discrepancy masterfault will be declared as indicated by the textxy:ACFT PWR displayed as a master fault.• Issue a Preset-Verify-Execute (PVE) commandsequence to apply Release Consent to the missile.If the PVE command sequence fails after twosuccessive issue attempts, a double critical verifymaster fault will be issued and indicated by thetext X:CRIT VRFY displayed as a master fault andWIU power will be removed. A release consent driv-er failure will be indicated by the master fault textX:RC DRVR. If the selected station fails to verify ontwo consecutive attempts, a double critical functionejector master fault will be issued and indicated bythe text X:UNCMD PVE displayed as a masterfault and WIU power will be removed.• Command a Commit to Separate (CTS) com-mand.• Remove the release consent.• Verify that missile status indicates the missilehas Committed to Separate Store (CTSS). If unsuc-cessful, the master fault xy:ABORT will be dis-played, the SMO will perform a normal shutdownof the missile and inhibit reapplication of power tothe missile.• Remove 28-volt dc #1 and 28-volt dc #2 power. Ifunsuccessful in removing either power, WIU status

will indicate a dc power discrepancy master faultwhich will be displayed as xy:ACFT PWR orxy:28-volt dc #2 respectively. If missile communica-tion fails after removal of 28-volt dc #1 and 28-voltdc #2 power, indicating a battery failure, xy:CTSSwill be displayed as a permanent fatal master fault.Reapplication of power to the missile is inhibited.• Apply unregulated 38-volt dc EED power to theselected location. If unsuccessful, a 38-volt dc EEDuncommanded low fault will be declared as indi-cated by the text X:EED PWR displayed as a mas-ter fault.• Perform the Ejector Squib Fire PVE sequence. Ifa failure exists after two attempts, a double criticalverify fault will be indicated by the text X:CRITVRFY displayed as a master fault. An ejector squibfire driver failure will be indicated by the textX:SQF DRVR displayed as a master fault. Two sub-sequent failures to verify the preset will result ina double critical function ejector selection masterfault being issued as indicated by the textX:UNCMD PVE being displayed as a master faultand power being removed from the missile.• Remove unregulated 38-volt dc EED power fromthe selected location. If unsuccessful after two at-tempts, a 38-volt dc EED uncommanded high faultwill be declared, power will be removed from theWIU and all missiles associated with the WIU, andthe text X:EED PWR will be displayed as a masterfault.• Command Critical Terminate to the location.• Perform missile scoring recording.• The missile launch advisory will be displayed onall MFDs. The missile launch advisory will remaindisplayed for 5 seconds, then the missile launch ad-visory will be blanked. The SMO displays appropri-ate xy (x = L (left pylon) or R (right pylon), y = 1,2, 3, 6, 7, or 8) for each launched missile in succes-sive launch advisory locations from left to right onthe bottom of the MFD. The SMO determines if themissile was successfully launched, aborted, or ishung and will display either AWAY, ABORT, orHUNG in normal video in the location immediatelyfollowing the launch advisory location for that mis-sile.• If the missile has become hung, HUNG will bedisplayed in reverse video in window 9 of theFRMT-7 display. xy:HUNG will be displayed as amaster fault. An unsuccessful launch sequence willbe indicated by the text xy:ABORT displayed as amaster fault.• Power application to the missile will be inhibited.

T.O. 1B-52H-34-2-8

7-46 Change 2

JASSM Launch Sequence Timeline (Typical)

Figure 7-17

AUTOMATIC LAUNCH DETERMINATION

The SMO will initiate automatic launch of a missilewhen all the following conditions are true for thatmissile:

• Automatic launch mode has been selected by theoperator.

Do not switch from automatic to manuallaunch mode while the missile is in launchcountdown. This will abort the missile witha permanent fatal fault.

NOTE

Selection of Automatic Launch mode is limi-ted to missions where the preplanned JASSMLaunch Point (JASSM LP) is located at a dis-tance of at least three seconds of flight insidethe planned In-Zone area. The reason for thislimitation is that, for auto launches, the SMOcalculates the start of the launch countdown(LCD) to occur three seconds before the air-craft achieves the closest point of approach tothe preplanned JASSM LP. This allows re-lease of the missile precisely at the JASSMLP, or at the aircraft’s closest point of ap-proach to the JASSM LP if the aircraft is de-viating from the preplanned route. If at thestart of LCD the aircraft is not within the In-Zone area, the SMO displays an LCD ENTRY

([AMI] JASSM LCD ENTRY) advisory andwaits until the aircraft is within the In-Zonearea to begin LCD. If the first In-Zone indica-tion received from the missile occurs after theaircraft has passed the closest point of ap-proach to the JASSM LP, the SMO will inhibitautomatic launch and indicate manuallaunch is required in addition to the LCDENTRY ([AMI] JASSM LCD ENTRY) advi-sory.

• The missile has power applied and is in an AllUp Round (AUR) Ready state:

• Weapon is Safe to Launch:• There is no critical weapon hardware failure.• Weapon has received minimum TXA data.• Weapon has minimum targeting data.• Timeline aborted has not been issued.• Weapon is not in IBIT.

• TXA is good.• Last BIT passed.• Warm-up is complete.

• The pilot’s munitions consent switch and the nav-igator’s unlock consent switch are in the unlockposition.• No missile jettison request is present and no jet-tison is in progress for any missile.• No WIU faults are detected which would preventthe launch of the missile.• LAR conditions have been met for the missile.The missile status must indicate In-Zone. TheJASSM will launch at the point of closest approachto the JASSM launch point.

T.O. 1B-52H-34-2-8

7-47

MANUAL LAUNCH DETERMINATION

Manual launch mode is selected at the time theSMO is loaded. The selection of manual launchmode, either by the operator or default, will be indi-cated on the WCP launch select switch and on theCF-E display. The following conditions must be truein order for the operator to manually launch a mis-sile:

• Manual launch mode is the current mode of op-eration.• The missile has had power applied.• The pilot’s munitions consent switch and the nav-igator’s unlock consent switch are in the unlockposition.• No missile jettison request is present and no jet-tison is in progress for any missile.• No WIU faults are detected which would preventthe launch of the missile.• LAR conditions have been met for the missile.Missile status indicates In-Range.• Missile status indicates Safe to Launch:

• There is no critical weapon hardware failure.• Weapon has received minimum TXA data.• Weapon has minimum targeting data.• Timeline aborted has not been issued.• Weapon is not in IBIT.

Manual launch is required for the following:• The missile is targeted to a direct target.• The missile has a fault requiring manual launch.• The point of closest approach is outside of thezone.• The seeker is required, but not functional.• Invalid zone data.

• Target data set contains no valid waypoints.

Use care not to deselect (press again) themanual launch switch while the weapon isin launch countdown. This will abort theweapon with a permanent fatal fault.

MISSILE LAUNCH TERMINATION

The missile launch process will be terminated be-fore the selected missile has been launched if any ofthe following conditions occur:• Any WIU or missile fault occurs which requiresthat power be removed from the WIU or missile.• The WIU or missile has power removed.• The missile is no longer targeted to the currentranging event.• An ACU reconfiguration occurs.• A jettison is in progress for any missile on thesame pylon as the launch missile.• Operator deselects the manual launch command.• Operator switches from automatic to manuallaunch mode.• If either unlock consent is removed.• CLR-D or PRGM-Dn is entered during a directlaunch.

NOTE

Prior to CTS, the SMO will declare a non-fatal LCD Abort fault. If the abort conditionoccurs, past CTS and the carrier mission isnot captive carry, the SMO will issue a mes-sage to abort the missile and declare a per-manent fatal LCD Abort fault.

T.O. 1B-52H-34-2-8

7-48

PREFERRED LAUNCH/JETTISON SEQUENCE

The JASSM preferred launch/jettison sequence isshown in the figure 7-18 and the following table.

If there is a retained/HUNG center stationstore, launching/jettisoning an adjacentshoulder station may result in a Store-to-Store contact. When a center station storeis retained/HUNG, operators will retain theadjacent shoulder station stores.

LAUNCHSEQUENCE

PYLON POSITION

POSITION

1 LP - 2 LP Forward Center

2 RP - 2 RP Forward Center

3 LP - 7 LP Aft Center

4 RP - 7 RP Aft Center

5 LP - 1 LP Forward Outboard

6 RP - 3 RP Forward Outboard

7 LP - 3 LP Forward Inboard

8 RP - 1 RP Forward Inboard

9 LP - 6 LP Aft Outboard

10 RP - 8 RP Aft Outboard

11 LP - 8 LP Aft Inboard

12 RP - 6 RP Aft Inboard

MISSILE LAUNCH RESTRICTIONS

Currently there are no SMO launch inhibits to mis-sile launch due to aircraft flight conditions. Safe re-lease advisories and the corrective action are con-tained in figure 7-22.

Safe release advisories do not inhibitlaunch. Possible collision between weaponsand between weapon and aircraft can occurif weapon is launched with a release adviso-ry displayed.

JASSM FREE FLIGHT SEQUENCE

Following separation from the aircraft, the JASSM:• Detects separation.• Deploys its wings to 75 degrees to aid pitch sta-bility and separation from the aircraft.• Deploys its tail to add yaw control and the lugsretract.• Deploys its wings to 45 degrees, when initialpitch stability is achieved.• Releases elevon brakes to make pitch and controlactive.• Activates fuel control and engine squib (3.0 secafter separation), if in engine start envelope.• Releases wedges on underside of stakes to insureclean separation from the aircraft.• Switches to alternator power, FUZE ARM (RPMsatisfied), FUZE safe separation timer – On.• Engine achieves max thrust when at proper alti-tude.• FUZE firing mode/delay time is set by missionprocessor.• GPS satellite acquisition occurs 90 seconds afterseparation from the aircraft.

T.O. 1B-52H-34-2-8

7-49

JASSM Preferred Launch/Jettison Sequence


Figure 7-18

T.O. 1B-52H-34-2-8

7-50 Change 2

MISSILE JETTISON

The operator can command the SMO to jettisonmissiles using either the WPN JETTISON switchon the WCP or the pilots’ Bomb Bay & Missile jetti-son switch. The OAS must be operational with theJASSM SMO loaded ([AMI] as primary SMO) andWIU power must be on for jettison of JASSMs us-ing the WCP or the Pilots’ switch. With OAS orWIU off, or a SMO other than the JASSM SMOloaded, jettison of JASSMs can only be accom-plished using the Alternate Jettison Control Panel(AJCP). All methods require unlock consent. ThePilot Bomb Bay and Missile jettison switch has thesame effect as if all locations and all stations wereselected on the WCP and then the WPN JETTISONswitch was selected.

NOTE

The radar navigator’s jettison switch wasexcluded from operation with the JASSMSMO, however, a malfunction in the jettisonsystem (failed blocking diode) could enablethe switch, making it function in the samemanner as the pilots’ Jettison Control BombBay & Missile switch.

If the WCP JETTISON switch or Pilot Jettison ALLswitch is used, the jettison is controlled by the SMOand the process is as follows:• Operator selects Location and Station of mis-sile(s) to be jettisoned on the WCP.• Operator moves JETT switch to the JETT posi-tion.1. Classified data erase will be commanded if mis-

sile power is on, but will not be statused for comple-tion.2. Missile power will be removed if missile power

is on.3. The SMO commands ejector squib fire to the

ejector of the missile in the most preferred releasesequence order.4. The SMO performs a scoring recording on the

flight DTUC/DTC for jettisoned missile.5. The missile launch advisory is requested on all

MFDs. The missile launch advisory will remain dis-played for 5 seconds. The advisory area of eachMFD where the missile launch advisory is dis-played will be blanked. The SMO displays appropri-ate xy (x = L (left pylon) or R (right pylon); y = 1, 2,3, 6, 7, or 8) for each jettisoned missile in successive

launch advisory locations from left to right on thebottom of the MFD.6. The SMO determines if the missile has been

successfully jettisoned, is hung, or jettison isaborted and displays either JETT, HUNG orABORT for the jettisoned missile in normal video inthe location immediately following the launch advi-sory location for that missile.7. If the missile has become hung, HUNG will be

displayed in reverse video in window 9 of theFRMT-7 display. The text xy:HUNG will be dis-played as a master fault when the missile is hung.8. If the jettison has been aborted, ABORT will be

displayed in reverse video in window 9 of theFRMT-7 display. The text xy:ABORT will be dis-played as a non-fatal master fault.9. The SMO requests a video recording of the

launch advisory.10. The SMO then inhibits power reapplication to

the selected station. (Power application is allowed ifjettison of missiles was aborted.)11. The SMO repeats all steps 1 through 10 above

until all the desired missiles have been jettisoned.

When missiles are jettisoned using the Alternate Jet-tison Control Panel (AJCP) hard-wired switches,EED power is applied independent of the WIU. How-ever, if the WIU has power applied, the WIU will con-tinue to monitor the state of the EED power.

NOTE

If missiles are jettisoned using the AJCPhard-wired switches while the SMO is loadedand the WIU is powered on, there is the prob-ability that the WIU status retrieved by theSMO will show that the EED power is onwhen it has not been commanded on by theSMO. If this occurs, WIU master fault will bedeclared, x:EED PWR (x = L or R to indicateleft or right WIU) will be displayed, and theWIU will be powered off by the SMO.

Also, a missile Present Discrepancy master faultwill be declared for each missile jettisoned via theAJCP. This results in the display of xy:WPNPRSNT for each missile. The text WPN PRSNT willalso be displayed in window 9 of the FRMT-7 dis-play for each missile jettisoned via the AJCP.

If jettison is commanded while either unlock consentswitch is in the lock position, the advisory messageNO CONSENT will be displayed on each MFD.

T.O. 1B-52H-34-2-8

Change 2 7-51

SIMULATION CAPABILITIES

Less [AMI] This paragraph describes any differ-ences in the SMO capabilities while in SIM mode.SIM mode is commanded by entering CF-52. Theoperator can verify the currently active SMO mode,whether STRIKE or SIM, by observing window 1 oneither the CF- menu, the CF-5 menu or the CF-57menu.

[AMI] This section describes any differences in theSMO capabilities while in the FULL or PART SIMmode. PART SIM mode is commanded by enteringCF-51. FULL SIM mode is commanded by enteringCF-52. The operator can verify the currently activeSMO mode, whether STRIKE, FULL SIM or PARTSIM, by observing either the CF- menu, the CF-5menu or the CF-57 menu.

NOTE

[AMI] For JASSM there is no difference be-tween the FULL and PART SIM modes.

SIMULATED MISSILE LOADOUT

Each time a SIM mode is commanded, only the mis-siles shown as present in the stores table will beshown present. Subsequent to releases (launches orjettisons) in a SIM mode, commanding STRIKE andreentering SIM will reset only the missiles identi-fied in the stores table as present.

On SIM mode entry, the assignments set while inSTRIKE mode are maintained. However, the mis-siles are marked as untargeted. FRMT-7 will dis-play the target assignments in normal video. Less[AMI] To prevent assignment carry over fromstrike mode reload mission.

Less [AMI] On SIM mode exit, all missiles aremarked as unassigned and untargeted. FRMT-7will display blanks (i.e. no targets assigned) for thetargeting status. The operator must either reloadthe B-52 mission, accomplish a retarget all opera-tion (CF-589), or accomplish a manual targeting op-eration (CF-586).

[AMI] On SIM mode exit, all missile assignmentsthat were set in STRIKE mode will be retained.FRMT-7 will display target assignments as theywere before entry into a SIM mode.

SIMULATED TARGETING OPERATIONS

Manual Targeting can be commanded while a SIMmode is active by operator entry of CF-586. ManualTargeting while a SIM mode is active will operateas described in Section I.

Direct Targeting can be commanded while a SIMmode is active by operator entry of CF-588,n. DirectTargeting while a SIM mode is active will operateas described in Section I.

SIMULATED WCE RESPONSES

While in a SIM mode, WCE and missile I/O is nottransmitted and actual WCE and missile statusand responses to commands are not available.Therefore, while in a SIM mode, the following con-cepts are implemented by the SMO:

• No faults are declared for any WCE or mis-siles.

• WCE and missile responses are simulatedusing the response times are shown below.

SIM Mode Response TimesDESIRED WCE/MISSILE

STATUSRESPONSE TIME

(SECONDS)

WIU initialization 15.625Missile IBIT completion 180.0Missile battery activation 1.27

Power is not applied to the pilot’s munitions consentswitch when the SMO is operating in SIM mode and,therefore, the switch position is not known to theSMO. The pilot’s munitions consent switch input issimulated as being the same as the navigator’s unlockconsent switch. Therefore, providing ejector unlockconsent from the navigator’s unlock consent switch isthe only ejector unlock consent that is necessary to al-low the simulated release of missiles.

NOTE

After a SIM mode is exited by commandingSTRIKE mode, the B-52 mission data andthe SMO must be reloaded to guaranteeproper operation of the system.

SIMULATED RANGING

While in SIM mode, ranging is accomplished in thesame manner as in STRIKE. The SMO performsranging by using the TDS data from the missile mis-sion data DTUC ([AMI] selected weapon group) foreach missile. The data along with the aircraft posi-tion and headings is used to estimate the parame-ters in the missile LAR message.

T.O. 1B-52H-34-2-8

7-52 Change 2

SMO TERMINATION

SMO execution can be terminated in two ways:• Less [AMI] Another SMO can be loaded into

the ACUs, using a SMO load and initialization pro-cess similar to that used for initial SMO loading.This process terminates execution of and overwritesthe SMO which is already loaded. With thismethod, FMS will continue to be executed. TheSMO will delay compliance with the command toterminate execution until the SMO has removedpower from the WIUs and until all outstandingSMO faults have been recorded (if a Flight DataRecord tape is installed).

• Less [AMI] Also, CF-67 can be entered by theoperator. This command halts execution of all soft-ware loaded into the ACUs (FMS and any loadedSMO). The SMO will delay compliance with theshutdown request until all outstanding SMO faultshave been recorded and for as long as it takes theSMO to remove power from all WCE and missilesthat have powered applied.

• [AMI] Loading another SMO or entering zeroat the location the JASSM SMO is loaded, termi-nates execution and unloads the SMO. With thismethod, the FMS and CSP will continue to operate.

• [AMI] Alternatively, the operator can enterCF-67 which halts execution of all software loadedinto the ACUs (FMS, CSP, and any loaded SMO).

SMO RESTART

The method of restarting the SMO is dependentupon the method which terminated SMO execution.The two methods are described below.

• Less [AMI] If SMO execution was terminatedby loading another SMO into the ACUs, or ACUmemory has been erased, the SMO must be re-loaded into the ACUs.

• Less [AMI] If SMO execution was terminatedby entering CF-67, and ACU memory has not beenerased, FMS and the SMO can be restarted by de-pressing the PROC SYNC button on the computercontrol panel.

• [AMI] If the SMO execution was terminatedby loading another SMO into the ACU, the SMOmust be reloaded into the ACUs.

• [AMI] If the SMO execution is terminated bya CF-67 command, the FMS and the SMO can berestarted by pressing the PROC SYNC button onthe computer control panel and logging on to theOAS using the CF-61 command, then the SMOmust be reloaded.

T.O. 1B-52H-34-2-8

Change 2 7-52A/(7-52B blank)

MESSAGES

This paragraph defines all SMO messages, their indi-cations and lists any corrective action which can betaken by the operator to resolve the anomaly whenapplicable.

MASTER FAULTS

The JASSM Master Faults are identified in figure7-19. Master faults are an indication of WCE ormissile failures, or conditions which will precludethe launch of missiles. Master faults are displayedin reverse video at the bottom left hand end of theMFD. When the faulted device is a WIU or a mis-sile, the text that is displayed will be preceded by alocation or location and station identifier. The textfor WIU faults that are not associated with a spe-cific station will be preceded by L or R. L will bedisplayed to identify the faulted device location asthe left pylon and R will be displayed to identify thefaulted device location as the right pylon. Missilefaults and WIU faults that are associated with aspecific location will be preceded by a location andstation identifier of the form xy, where x will be Lor R to identify the left or right pylon, respectively,and y will be the station number, 1, 2, 3, 6, 7 or 8.Faults which are not applicable to this SMO areidentified with the text N/A in the correspondingfault text and fault type columns of figure 7-19.

No corrective action can be taken by the operator forWIU or missile faults, although power re-applicationcan be commanded by the operator when power isremoved from a faulted device. If the SMO has deter-mined that power should not be re-applied because ofthe failure, the SMO will not respond to the commandto apply power. The operator can override an ECUNO-GO fault and an ECU AC POWER fault with aCF-68 command to allow WIU power application.

Permanent fatal faults will initiate a CDE, leavingthe weapon assigned, but untargeted.

With an ECU fault present, damage to equip-ment may occur if WIU power remains on asa result of selecting ECU power override.

The SMO expects the ejectors to be pinned in theunlock position. If they are not pinned in the unlockposition at one or more stations, an uncommandedejector locked non-fatal master fault xy:UNCMDLK will be generated for each of those stations.

When both ejector unlock enable monitors for a WIUindicate that ejector unlock enable is not present, thetext x:NO UE is displayed as a master fault for thatWIU. Unlock enable power is provided to each WIUwhen the pilot’s munitions consent switch and the

navigator’s unlock consent switch are in the unlockposition. Even if the ejectors are pinned in the unlockposition, this fault will still prevent a normal releasesequence because this power is also used to fire thesquibs which eject the missile.

The types of master faults identified in figure 7-19,the associated abbreviations and the actions takenby the SMO as a result of the fault are as follows.

Safety Critical (SC)

Safety critical faults present a safety threat to per-sonnel or to the aircraft. The SMO will removepower from the faulted device and inhibit re-ap-plication of power by the operator. Power will beremoved from the affected missile when a missile orstation safety critical fault is detected. There are noidentified safety critical faults for the JASSM SMO.

Permanent Fatal (PF)

The SMO will perform a normal shutdown of thefaulted device and inhibit re-application of power bythe operator. Any weapon or station permanent fatalfault that occurs after CTS has been commanded tothat weapon will be treated as a safety critical fault.

Transient Fatal (TF)

The SMO will perform a normal shutdown of thefaulted device. Re-application of power by the oper-ator is allowed. Any missile or station transientfatal fault which occurs after CTS has been com-manded to that missile will be treated as a perma-nent fatal fault.

Non Fatal (NF)

The SMO will not remove power from the faulteddevice.

ADVISORIES AND STATUS MESSAGES

The SMO Advisories are identified in figure 7-20. TheSMO Status Messages are identified in figure 7-21.Advisories and Status Messages are displayed inreverse video at the bottom right hand end of theMFD.

SAFE RELEASE AND WEAPON LAUNCH ADVISORIES

The safe release advisories are identified in figure7-22. The weapon launch advisories are identifiedin figure 7-23. Safe release and launch advisoriesare displayed, approximately, in the center ofPRGM display. See figures 7-22 and 7-23.

FRMT-7 WEAPON FAULTS

The weapon faults displayed as part of the missilestatus block on FRMT-7 and FRMT-7xy, and also atthe bottom of the FRMT-7xy display, are listed infigure 7-24.

BLA

T.O. 1B-52H-34-2-8

Change 2 7-53

JASSM Master FaultsFault Indication Coding:

• NF = NON-FATAL Fault• PF = PERMANENT FATAL Fault• SC = SAFETY CRITICAL Fault• TF = TRANSIENT FATAL Fault• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER

FAULTINDICATION

FAULTTYPE POSSIBLE CAUSE SYSTEM RESPONSE OPERATOR ACTION

ARMAMENT INTERFACE UNIT MASTER FAULTS

AIU COMMLess [AMI] orAIU [AMI]

NF 1. Armament Interface Unit(AIU) communications failure.2. AIU terminal failure.3. Interruptible Direct Current(IDC) power enable discrepan-cy (uncommanded power on oroff).

NOTEFault displayed and re-corded every 30 minutes,as long as the fault ispresent.

This master fault may result inany or all of the following:1. Loss of Environmental Con-trol Unit (ECU) power control.2. Loss of WIU power control.3. Weapons cannot be pow-ered or launched.4. Less [AMI] SMO controlledjettison is not available.5. RBS tone cutoff will not oc-cur.6. [AMI] Loss of Pylon jettisoncapability.7. [AMI] Loss of OAS control ofbay door operation.

1. Acknowledge message2. Check Circuit Breakerson the AUX BNS S/V FIL-TER BOX Circuit BreakerPanel. Pull and reset, if re-quired.3. Verify status of weaponand WIU power.

AIU 28 VDC NF STORE 28 VDC T/R power discrepancy.


This master fault may result inany or all of the following:1. May not be able to applyWIU essential (ESS) power.2. May not be able to applystore 28 VDC #1 power.

1. Acknowledge message.2. Check Circuit Breakerson the AUX BNS S/V FIL-TER BOX Circuit BreakerPanel. Pull and reset, if re-quired.3. [AMI] Check AIU circuitbreaker on the RIGHT S/VFILTER BOX CIRCUITBREAKER PANEL. Pulland reset, if required.4. Verify status of weaponand WIU power.


T.O. 1B-52H-34-2-8

7-54 Change 3

JASSM Master Faults (Cont)FAULT

INDICATIONFAULTTYPE POSSIBLE CAUSE SYSTEM RESPONSE OPERATOR ACTION

ENVIRONMENTAL CONTROL UNIT MASTER FAULTS

ECU TF ECU NO-GO and ECU orrideis off. NOTE

1. Environmental conditionsare out of limits.2. Insufficient Airflow.3. Low engine power settings.4. Transient failure duringclimb or descent.5. ECU failure.

• If an environment No-Gofault is detected from theECU after power has beenapplied for at least twominutes, power will be re-moved from all weaponsand both WIUs one minutefrom the time that the faultis displayed.

•Fault displayed and re-corded every 30 minutes,as long as the fault is pres-ent.

This master fault may result inany or all of the following:1. Cooling air to the WIU is un-available or inadequate.2. Weapon temperature or air-flow out of limits could causedegraded weapon perfor-mance and weapon malfunc-tions.3. If the fault remains for morethan 1 minute, weapon powerand WIU power are removed.

With an ECU fault pres-ent, damage to equip-ment may occur if WIUpower remains on con-tinuously as a result ofselecting ECU poweroverride. While in ECUpower override, the WIUmay be operated using a30 minute on, 15 minuteoff, 30 minute on cycle.

1. Acknowledge message.2. If the cause is low air-flow, increase power on en-gines 3 and 4.3. Close air outlet knobsand decrease cabin tem-perature.4. Verify pilot’s cabin mas-ter pressure switch is inECS.5. In potential icing condi-tions check pilot’s anti-icingis on.6. Remove weapon powerand recycle WIU power.7. If override is warranted,operator entry of CF-68commands the SMO to ac-tivate ECU power override.

NOTE

• If the CF-68 commandis entered within 1 min-ute of the fault indica-tion, weapon and WIUpower will remain on,otherwise, weapon andWIU power are auto-matically removed.

• If WIU and/or weaponpower is removed be-cause of a fault, theCF-68 command mustbe entered prior to re-applying WIU power.


T.O. 1B-52H-34-2-8

Change 3 7-55



ENVIRONMENTAL CONTROL UNIT MASTER FAULTS (Cont)

ECU PWR TF ECU AC power discrepancy(uncommanded on or off) andECU orride is off. NOTE

Loss of conditioned air to theWIU.

• If an environment No-Gofault is detected from theECU after power has beenapplied for at least twominutes, power will be re-moved from all weaponsand both WIUs one minutefrom the time that the faultis displayed.

•Displayed and recordedevery 30 minutes, as longas the fault is present.

1. Before WIU power on – un-able to power up WIU or weap-ons.2. After WIU power on – WIUand weapon power is re-moved.

With an ECU fault pres-ent, damage to equip-ment may occur if WIUpower remains on con-tinuously as a result ofselecting ECU poweroverride. While in ECUpower override, theWIU may be operatedusing a 30 minute on, 15minute off, 30 minute oncycle.

1. Acknowledge message.2. Remove weapon powerand recycle WIU power.3. If override is warranted,operator entry of CF-68commands the SMO to ac-tivate ECU power override.

NOTE

• If the CF-68 commandis entered within 1 min-ute of the fault indica-tion, weapon and WIUpower will remain on,otherwise, weapon andWIU power are auto-matically removed.

• If WIU and/or weaponpower is removed be-cause of a fault, theCF-68 command mustbe entered prior to re-applying WIU power.


T.O. 1B-52H-34-2-8

7-56 Change 2



WEAPON INTERFACE UNIT MASTER FAULTS

x:CRIT VRFY TF Double critical verify Fault.1. [AMI] Preset commandedbut response not verified.2. [AMI] WIU CRITICAL COM-MAND status not valid.3 [AMI] Weapon address se-lected with no critical functionactive.

1. WIU and weapon power areremoved.2. JASSM heater power notavailable.3. Jettison or launch sequencemay be aborted.

1. Acknowledge message.2. Re-apply WIU power.3. If Fault persists, verifyWIU power is removed.4. If Fault occurred postCTS, accomplish POSTSTRIKE/ABORT checklist.

x:EED PWR TF 1. 38 VDC Electro-explosiveDevise (EED) power on whennot commanded on.

1. Weapon power and WIUpower will be removed.2. Weapon heater power notavailable.

1. Acknowledge message.2. Re-apply WIU power.3. If Fault occurred postCTS, accomplish POSTSTRIKE/ABORT checklist.4. [AMI] If fault resultedfrom AJCP jettison, contin-ue.

NF 2. 38 VDC Electro-explosiveDevise (EED) off when notcommanded off.

1. If EED power is not presentwhen requested (i.e. during alaunch or jettison), a non-fatalmaster fault will occur and theWIU will remain on.2. Jettison or launch sequencemay be aborted.3. Weapon heater power notavailable, if WIU powered off.

1. Acknowledge message.2. Less [AMI] Removeweapon and WIU power.3. Less [AMI] Accom-plish POST STRIKE/ABORT checklist.4. [AMI] If Fault occurredpost CTS, accomplishPOST STRIKE/ABORTchecklist.5. [AMI] If fault resultedfrom AJCP jettison, contin-ue.


T.O. 1B-52H-34-2-8

Change 2 7-57



WEAPON INTERFACE UNIT MASTER FAULTS

x:ESS PWR TF 1. 28 VDC Essential (ESS)power off when not command-ed off.

1. Essential power is not pres-ent when desired.2. Weapon and WIU power willbe removed3. JASSM heater power notavailable.

1. Acknowledge message.2. Check AIU circuit break-er on S/V FILTER BOX Cir-cuit Breaker panels.3. If WIU and weapon pow-er are removed, re-applyWIU power.4. If fault persists, verifyWIU power is removed.5. If Fault occurred postCTS, accomplish POSTSTRIKE/ABORT checklist.

NF 2. 28 VDC ESS power onwhen not commanded on.

1. Less [AMI] Essential poweris present when not desired.2. [AMI] If power is on whencommanded off, a non-fatalmaster fault will occur and WIUpower will remain on.3. JASSM heater power notavailable, if WIU powered off.

1. Acknowledge message.2. Check S/V FILTER BOXCircuit Breaker panels.3. If WIU and weapon pow-er are removed, re-applyWIU power.4. If fault persists, verifyWIU power is removed.5. If Fault occurred postCTS, accomplish POSTSTRIKE/ABORT checklist.

x:NO UE NF Unlock enable not presentwhen commanded.


Launch or SMO controlled jetti-son unavailable.

1. Acknowledge message.2. Set Pilot’s and WCPconsent switches to theLOCK position.3. Set Pilot’s and WCPconsent switches to theUNLOCK position.4. If Fault remains:

A. Set Pilot’s and WCPconsent switches to theLOCK position.

B. Remove weaponpower and cycle WIU power.

C. Set Pilot’s and WCPconsent switches to the UN-LOCK position.5. If fault persists, accom-plish POST STRIKE/ABORT checklist, if appli-cable.


T.O. 1B-52H-34-2-8

7-58 Change 2



WEAPON INTERFACE UNIT MASTER FAULTS (Cont)

x:RC DRVRLess [AMI]

NF Release consent driveruncommanded off.

NOTEA CTSS PF Fault will fol-low and the SMO will shutdown weapon power.

May result in an aborted launchor jettison sequence.

1. Acknowledge message.2. Accomplish POSTSTRIKE/ ABORT checklist,if applicable.

x:RC DRVR [AMI] NF Release consent driveruncommanded off.

1. A pre-CTSS LCD abort andrelease consent Fault will oc-cur if the weapon is unable toverify receipt of Release Con-sent. In this case, the SMO willnot remove weapon power.2. May result in an abortedlaunch or jettison sequence.

1. Acknowledge message.2. Re-apply WIU power.3. If fault persists, verifyWIU power is removed.4. If fault occurred postCTS, accomplish POSTSTRIKE/ ABORT checklist.

x:UNCMD DRVR TF 1. Double release consentdriver uncommanded on fault.2. Less [AMI] Double ejectorsquib fire driver status of truewhen not commanded.

1. Weapon and WIU power willbe removed.2. Jettison or launch sequencemay be aborted.3. JASSM heater power notavailable.

1. Acknowledge message.2. Attempt re-applyingWIU and weapon power.3. If fault persists, verifyWIU power is removed andaccomplish POSTSTRIKE/ABORT checklist,if applicable.

x:UNCMD PVE TF 1. Double critical commandregister status fault.2. Double critical function ejec-tor selection station fault.

1. WIU and weapon power areremoved.2. JASSM heater power notavailable.

1. Acknowledge message.2. Attempt re-applyingWIU and weapon power.3. If fault persists, verifyWIU, and weapon, power isremoved and accom-plish POST STRIKE/ABORT checklist, if appli-cable.

x:UNCMD UE NF Unlock enable (UE) poweravailable without Pilot’s andWCP UNLOCK switches in theUNLOCK position (i.e., systemhas consent without switchesset for consent).

Hardware safeguard providedby Pilot’s and WCP unlock con-sent circuit is negated.

1. Acknowledge message.2. Cycle the Pilot’s andWCP UNLOCK switches toLOCK.3. If fault remains, poweroff weapons and cycle WIUpower.2. Cycle the Pilot’s andWCP UNLOCK switches toLOCK.4. Continue normal proce-dures, however, ejectorrack unlock enable is pres-ent. For non-combat mis-sions leave WIU power off.For combat missions do notpower WIUs over friendlyterritory.


T.O. 1B-52H-34-2-8

Change 2 7-59



WEAPON INTERFACE UNIT MASTER FAULTS (Cont)

x:WIU TF WIU end around communica-tion test fault – data transmittedto the WIU does not match datareceived from the WIU duringpower on sequence.

1. WIU power is removed.2. JASSM heater power notavailable.

1. Acknowledge message.2. Cycle WIU power.3. If fault persists, verifyWIU power is removed.

x:WIU COMM TF Double WIU communicationfailure.

1. WIU and weapon power areremoved.2. JASSM heater power notavailable.


x:WIU RESET TF 1 WIU not reset.2. WIU reset monitor activefault.

1. WIU power is removed.2. JASSM heater power notavailable.



T.O. 1B-52H-34-2-8

7-60 Change 2



STATION MASTER FAULTS

xy:28VDC2 TF WIU status indicates 28 VDC#2 uncommanded on.

1. Weapon batteries may besquibbed inadvertently.2. Weapon may be launchedor jettisoned with power still atthe umbilical.3. [AMI] Weapon COMM NO-GO and weapon power remov-al may follow failure.

1. Acknowledge message.2. If weapon power is notremoved:

A. Remove weaponpower.

B. Cycle WIU power.C. Re-apply weapon

power.D. If fault persists, shut

down weapons and WIU,and accomplish POSTSTRIKE/ABORT checklist.3. If weapon power was re-moved, shut down WIU andaccomplish POSTSTRIKE/ABORT checklist.

xy:ABORT PF 1. Launch countdown abortfault after CTS.2. CTSS Battery Failure.(Non-Captive Carry missions).

1. Weapon power is removed.2. SMO inhibits weapon powerre-application.3. Weapon batteries may havebeen squibbed.

1. Acknowledge message.2. Verify weapon power re-moved.3. Accomplish POSTSTRIKE/ABORT checklist.4. If fault occurred duringCaptive Carry launch, re-move weapon power anddo not attempt furtherlaunches at that station.

xy:ACFT PWR NF 1. 28 VDC #1 Power Fault (Uncommanded on or off).2. 28 VDC #2 Power Fault (Uncommanded off). May oc-cur due to the loss of AIU 28VDC T/R power or WIU 28VDC ESS power.3. 3-Phase 115V AC PowerFault (Uncommanded on).

1. Manual launch required.2. Weapon may be jettisoned/released, with power still ap-plied at the umbilical.

1. Acknowledge message.2. Remove weapon power.3. Cycle WIU power.4. Re-apply weapon power.5. If the fault persists, re-move weapon power.

xy:BIA Fail NF Bomb Impact Assessment(BIA) Fault.

1.Manual launch required.2. Weapon power not re-moved.3. [AMI] Weapon will not trans-mit terminal targeting data.4. [AMI] MDT may be cor-rupted.

1. Acknowledge message.2. Cycle weapon power.3. If BIA is required andthe fault persists, re-move weapon power.

xy:BUS TEST NF MIL-STD-1553B Weapon BusTest Fault.

Loss of dual redundant 1553weapon bus. Communicationretry will occur on second bus.

1. Acknowledge message.2. Monitor for additionalbus faults.


T.O. 1B-52H-34-2-8

Change 2 7-61



STATION MASTER FAULTS (Cont)

xy:COMM NOGO TF 1. Aircraft ID fault.2. Weapon comm fault.3. Almanac received fault.4. GPS keys transfer fault.5.Timeline abort fault.6. Surface/Fin delay fault. Findeployment delay is less thancommanded.7 Timeline integration fault.8. Mass data transfer fault.Weapon functions dependanton data transferred by the SMOmay not have received the cor-rect data.9. Uncommanded timelineabort fault.10.Simulated launch count-down fault. (Captive Carry only)11. Minimum TXA fault.12. INS/INU no longer desig-nated as prime OAS navigationsource with JASSMs powered.13. [AMI] Possible hardwareproblem located at the aircraftstation interface.

Weapon power is removed. 1. Acknowledge message.2. If the fault occurred be-fore CTS:

A. Ensure an INS/INU isdesignated as the primenavigation model.

B. Re-apply weapon power. C. If the fault persists,verify weapon power is re-moved.3. If the fault occurred afterCTS, accomplish POSTSTRIKE/ABORT checklist.

xy:CTSS PF 1. Uncommanded Commit toSeparate (CTSS) fault.2. Uncommanded CTS fault.

1. LCD is terminated.2. Weapon power is removed.3. CDE is commanded.4. Weapon batteries may beactive.5. SMO inhibits weapon powerreapplication.

1. Acknowledge message.2. Accomplish POSTSTRIKE/ABORT checklist.3. Verify weapon power isremoved.

xy:EJECTOR NF 1. Ejector status discrepancyfault.2. Uncommanded ejector lockfault.

NOTE

If pylon is improperly config-ured, there should also be aWPN PRSNT fault and allweapons on that pylonshould show the same pylonrelated faults.

1. Ejector status indicates:A. Both locked and un-

locked.B. Neither locked nor un-

locked.C. Locked

2. This fault may occur if:A. The ejectors are not

physically pinned in the un-locked position.

B. The ICSMS pylon as-sembly is not correctly figured.3. [AMI] Manual launch re-quired.

1. Remove weapon andWIU power.2. Ensure the ejector in-flight safety lock is in theunlock position and thelockout bolt is installed.3. Ensure pylon is properlyconfigured.4. Re-apply WIU power.5. If fault persists, do notattempt launch or jettison atthis station.


T.O. 1B-52H-34-2-8

7-62 Change 2




xy:ERASE FAIL NF 1. Data erase fault.2. Less [AMI] CDE fault.

Mission classified data erasewas not successful per weap-on CDE.

1. Acknowledge message.2. Recommand weaponCDE (CF-575).3. If Fault persists:

A. Verify weapon poweris removed. B. Weapon must be han-dled as if it contains classi-fied data.

xy:FTS(Flight Test Only)

NF Flight Termination System(FTS) is not active when com-manded or is active when notcommanded.

1. FTS may not be available.2. Manual launch is required.Test launch may not be achiev-able.3. FTS battery may be activeand battery life is limited to 15minutes.

1. Acknowledge message.2. [AMI] If mission is anOTL, perform POSTSTRIKE/ABORT checklist.3. If mission is captivecarry, cycle weapon power.4. If fault persists, accom-plish POST STRIKE/ABORT checklist.

xy:GPS DATA NF 1. Ephemeris received fault.2. Time received fault.

1. Loss of Ephemeris data.2. Loss of ability to accuratelyacquire GPS satellites forweapons.3. May cause weapon failureto validate crypto keys.4. Manual launch required.

1. Acknowledge message.2. Verify the Interface Unit(IU) and GPS receiver arepowered on.3. Verify INU is poweredand navigating.4. Check the GPS DATAvalidity on the PKB.5. Check GPS system faulton FRMT-6.6. Determine weapon GPSinitialization status.7. Perform weapon CDE.8. Recycle weapon power.

NOTE

Auto retargeting is re-quired, if targeting is de-sired.

9. If the fault persists, verifyweapon power is removed.


T.O. 1B-52H-34-2-8

Change 2 7-63




xy:GPS INIT NF AS Status/SV Configurationfault.

1. Weapon may not track GPS.2. Manual launch required.3. GPS accuracy may be im-paired.

NOTE

The B-52 GPS 3A re-ceiver requires approxi-mately 15 minutes to de-cipher the new daily keyafter a Zulu day rollover.A NO KEYS may be dis-played for weapons thathave power cycled dur-ing this period.

1. Acknowledge message.2. Verify the IU and GPSreceiver are on and track-ing satellites.3. Verify current date onCF-61.4. Verify KEY PRESENTis displayed on the IUPKB.5. Verify initialization data,including date, is sent viathe PKB.6. Verify FLY-TO has beencommanded and the B-52is navigating.7. Command a weaponCDE.8. Zeroize GPS receiver.9. If keys are available onthe B-52 mission DTUC/DTC:

A. Ensure B-52 mis-sion DTUC/DTC isinstalled.

B. Cycle IU power.10. If keys are not avail-able on the B-52 missionDTUC/DTC, manually in-put GPS keys data via theIU IKB.11. Cycle weapon power.12. If the fault persists,verify weapon power is re-moved.


T.O. 1B-52H-34-2-8

7-64 Change 2




xy:HTR PWR NF 3 Phase 115 VAC Power Fault(Uncommanded off)

1. Weapon power is removedor not applied.2. Weapon communicationNo-Go may follow failure.3. JASSM heater power notavailable at that station.4. Manual launch required.5. [AMI] Launch or jettison se-quence may be aborted.

1. Acknowledge message.2. Remove weapon power.3. Cycle WIU power.4. Re-apply weapon power.5. If fault persists, removeweapon power.

xy:HUNG PF Hung store following a launchor jettison attempt.

NOTE

A JASSM should only beconsidered to be a HUNGstore, if the xy:HUNG mes-sage is received.

1. Weapon is hung at ejector.2. Weapon battery may be ac-tive.3. Weapon present status indi-cates a weapon is present afterejectors squib fire commandhas been issued.4. Weapon power is removed.5. SMO inhibits re-applicationof weapon power.6. [AMI] SMO issues an abortcommand to the weapon.

1. Acknowledge message.2. Obtain visual confirma-tion of hung store, if pos-sible.3. Accomplish POSTSTRIKE/ABORT checklist.

xy:LCD FAIL NF LCD abort prior to CTS.Less [AMI] CTSS battery fail-ure (Captive Carry missionsonly).

1. Weapon will not launch.2, LCD is terminated.3. [AMI] If abort occurs beforeCTS weapon power will not beremoved nor re-application in-hibited. Weapon batteries willnot have been squibbed.

1. Verify LAR, weapon andunlock consent status.2. Cycle missile power.3. If fault persists, verifyweapon power is removed.4. Accomplish POSTSTRIKE/ABORT checklist,if applicable.

xy:OVERTEMP NF 1. Overtemp caution fault. The missile will set an Over-temperature Caution based onthe probability of the missileoverheating before completingits mission, if the missile is notlaunched in approximately tenminutes.2. Overtemp warning fault The missile will set an Over-temperature Warning based onthe probability of the missileoverheating before completingits mission, if the missile is notlaunched in approximately oneminute.

1. For overheat caution fault,the weapon is in danger ofoverheating in not less than tenminutes. FRMT-7xy displaysHOT in reverse video.

2. For overheat warning fault,the weapon is in danger ofoverheating in not less thanone minute. FRMT-7xy dis-plays HOT in blinking, reversevideo.3. [AMI] Manual launch is re-quired.

1. Acknowledge message.2. If launch is not imminent,remove missile power andallow missile to cool forapproximately 45 minutes.3. Cycle weapon power.4. If fault persists, removeweapon power.


T.O. 1B-52H-34-2-8

Change 2 7-65




xy:SEEKER NF Terminal Guidance fault. 1. Terminal guidance hasfailed. Weapon may not hit tar-get.2. Manual launch required.

1. Acknowledge message.2. If the seeker mission canbe accomplished without aseeker, proceed withlaunch. Otherwise, assignthe mission to weapon witha good seeker.3. Cycle weapon power.4. If fault persists, removeweapon power.

xy:SQUIB NOGO PF Squibs fault. 1. Weapon power is removed.2. SMO inhibits re-applicationof weapon power.

1. Acknowledge message.2. Accomplish POSTSTRIKE/ABORT checklist.

xy:STORE ID TF Weapon store descriptiontransmitted from the weapondoes not match B-52 missiondata.

Weapon power is removed. 1. Acknowledge message.2. Verify correct B-52 mis-sion is loaded.3. Re-apply weapon power.4. If fault persists, verifyweapon power is removed.

xy:TGT NOGO TF Target data not loaded/invalid. 1. Weapon power removed.2. Weapon not targeted withplanned mission.

1. Acknowledge message.2. Verify correct weaponmission DTUC/DTC isinstalled.3. Power off the WIUs.4. Reload the SMO andB-52 mission.5. Re-apply WIU power.6. Re-apply weapon powerand perform a weapon CDEprior to completion of IBIT(Within 20 seconds ofweapon power application).7. Re-apply weapon power.8. If fault persists, verifyweapon power is removed.

xy:TIK FAILLess [AMI] (Flight Test Only)

NF Test Instrumentation Kit (TIK)fault.

1. Weapon telemetry not avail-able.2. Manual launch required.

1. Acknowledge message.2. Verify correct weaponmission is loaded.3. Cycle weapon power.4. Verify telemetry re-sponse with ground.5. Cycle telemetry power,as required, to matchFRMT-7 to telemetry signal.6. If fault persists and func-tional TIK is required, abortmission objective.


T.O. 1B-52H-34-2-8

7-66 Change 2



STATION MASTER FAULTS (CONT)

xy:TLMY(Flight Test Only)

NF Telemetry fault. 1. Telemetry may not be onor off as requested.2. Manual launch required.

1. Acknowledge message.2. Verify telemetry responsewith ground.3. Cycle telemetry power, asrequired, to match FRMT-7 totelemetry signal.4. Remove weapon and WIUpower.5. Reload SMO and re-applyWIU and weapon power.6. Command weapon telem-etry on.7. If fault persists and func-tional telemetry is required,abort mission objective.

xy:WARM UP NF Weapon thermal conditioningand testing is not complete tenminutes after standby power isapplied.

1. Weapon will not enter IBITand therefore, will not align.2. Manual launch is required.

1. Acknowledge message.2. Cycle weapon power.3. If fault persists, verifyweapon power is removed.

xy:WPN DATA NF Weapon mission data fault.Approximate waypoint data,release data, target engage-ment data, or target data is notvalid after mass data transferor completion of primary targetmessage.

Weapon may not have re-ceived correct targeting data.

1. Acknowledge message.2. Less [AMI] Verify the cor-rect weapon mission DTUCis installed.2. [AMI] Verify DTC is cor-rectly installed and cycleweapon power.3. Command auto targeting.4. Power off the WIUs andreload the SMO and B-52mission.5. Re-apply WIU power.6. Re-apply weapon powerand perform a weaponCDE.7. ]Re-attempt auto-target-ing.8. Attempt manual target-ing.9. If fault persists, removeweapon power.


T.O. 1B-52H-34-2-8

Change 2 7-67



STATION MASTER FAULTS (CONT)

xy:WPN NOGO TF 1. Weapon BIT report No-Go(CS fault, Processor fault, GPSBIT fault, PS Fault, Engine Con-trols fault, PF fault, IMU fault).2. Critical hardware fault.3. Uncommanded data erasefault.4. Activate IBIT fault.5. Release consent uncom-manded fault.6. Uncommanded weapon testfault.7. Reset power dropout fault.8. [AMI] Uncommanded IBITfault.

1. Weapon power is removed.2. LCD is terminated (if active).

1. Acknowledge message.2. If fault occurred postCTS, accomplish POSTSTRIKE/ABORT checklist.3. If fault occurred pre CTScycle weapon power.4. If fault persists, removeweapon power.

NOTELess [AMI] If this fault oc-curs in conjunction with aWPN DTUC?? masterfault, the operator mustcycle DTUC mount poweror remove and re-insertthe weapon missionDTUC in order to recoveruse of the weapon missionDTUC.

xy:WPN PRSNT NF 1. Ejector Weapon presentmonitor status and umbilicalweapon present status disagreeon weapon presence.2. Stores table disagrees withejector weapon present monitorstatus and umbilical weaponpresent status.3. ICSMS pylon assembly is notconfigured correctly.4. [AMI] Ejector weapon pres-ent monitor or umbilical weaponpresent monitor changes statusafter a hung store fault.

NOTE

If pylon is improperly config-ured, there should also be anEJECTOR fault and all weap-ons on that pylon should showthe same pylon related faults.

1. No weapon present or at in-correct station.2. Weapon presence cannotbe determined.3. Incorrect mission load.4. Manual launch required.

1. Acknowledge message.2. Verify correct weaponmission is loaded (CF-81).3. Less [AMI] Verify correctmission DTUC is installedand the DTUC retainer knobis in the proper position.4. Cycle WIU power.5. If on the ground, ensurethe pylon is properly config-ured.


T.O. 1B-52H-34-2-8

7-68 Change 2



OTHER MASTER FAULTSJASSM EVENT[AMI]

NF JASSM SMO is secondary andmission planned JASSM launchpoint is within 25 minutes.

Weapon for mission plannedlaunch is not targeted.

1. Acknowledge message.2. Make JASSM SMO pri-mary, then power missiles.

JASSM MSNDATA?? [AMI]

NF 1. Mission data discrepancy.2. Invalid or no Classified Param-eters loaded.3. Launch commanded while inStrike Mode with a Ferry missionloaded.

Carrier mission data notavailable or incorrect.

1. Acknowledge message.2. Verify DTC correctlyinstalled, then reload mis-sion data.

JASSM WPNDATA?? [AMI]

NF 1. The JASSM SMO has de-tected a discrepancy with theavailability of Weapon Groupdata on the DTC.2. GPS Crypto Keys or or Alma-nac Data are unavailable fromthe DTC and the IU upon weap-on power on or after processorreconfiguration prior to JASSMweapon power on.

1. Weapon mission data notavailable or incorrect foravailable weapon.2. Improper crypto keysloaded. Crypto keys not validfor current date.3. SIM mode ranging is notavailable without CLAPARdata.

NOTEThe GPS receiver requiresapproximately 15 minutesto decipher the new dailykey after a Zulu day rol-lover. a NO KEYS or KEYRECV may be displayedwhile this condition exists.

1. Acknowledge message.2. Verify DTC installed cor-rectly.3. Verify GPS/IU is on andtracking satellites.4. Verify Key Present isdisplayed on the IU PKB.5. Verify FLY-TO has beencommanded and B-52 isnavigating.6. If keys available on theDTC, verify current date onCF-61.7. Verify/deselect keyoverride in IU PKB.8. Command a weaponCDE.9. Zeroize GPS receiver.10. Cycle GPS/IU power.11. If keys are not availableon the mission DTC, inputGPS keys via the IU PKB orCrypto Fill port.12. Cycle weapon power.13. If fault persists, removeweapon power.

MSN DATA??Less [AMI]

NF 1. Mission data discrepancy. Carrier mission data notavailable or incorrect.

1. Acknowledge message.2. Reload B-52 mission.3. Determine DTUC statusfrom FRMT-6 and if neces-sary, re-install DTUC into adifferent DTU cavity.

NO CONSENT NF Launch or jettison was com-manded and either the pilot’s ornavigator’s unlock consentswitch or both are not in the un-lock position.

Weapon will not launch/jetti-son.

1. Acknowledge message.2. Ensure both unlock con-sent switches are in the un-lock position.3. Re-attempt release.


T.O. 1B-52H-34-2-8

Change 2 7-68A



OTHER MASTER FAULTS

UNLOCK CONSENT NF The Navigator’s unlock consentswitch and the Pilot’s weaponconsent switch are in oppositepositions.

No unlock consent enableand ejector squib fire is notpossible.

NOTE[AMI] PMCP Unlock Con-sent Switch position moni-tor is not available to theSMO unless WIU power isapplied. Default is LOCK.

1. Acknowledge message.2. Place both unlock con-sent switches in the unlockposition.3. If the fault persists, setboth switches to the lockposition.4. If fault persists, removeweapon power and cycleWIU power.

WPN DTUC??Less [AMI]

NF 1. Weapon DTUC access failurehas occurred. The JASSM SMOhas detected a discrepancy withthe availability of data on theweapon mission DTUC.2. Weapon mission DTUC is notavailable when access is needed.3. Improper crypto keys loadedor crypto keys are not valid forthe current date.

1. SIM mode ranging is notavailable without CLAPARdata.

1. Acknowledge message.2. Verify correct missionDTUC is installed and theDTUC retainer knob is inthe proper position.3. Confirm DTU status onFRMT-6.4. Remove/reseat weaponmission DTUC.5. Re-install the missionDTUC into a different DTUcavity.6. Verify the correct datewas entered on CF-61.7. If available, input currentcrypto keys through the IUPKB.

NOTEIf this fault occurs in con-junction with a xy:WPNNOGO master fault, re-move and re-insert theweapon mission DTUC.


T.O. 1B-52H-34-2-8

7-68B Change 2

JASSM AdvisoriesLess [AMI]

Fault Indication Coding:

• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER

FAULTINDICATION POSSIBLE CAUSE OPERATOR ACTION

ALIGN FAIL(Reverse Video)

Missile alignment failure. Check OAS Nav Mode is INS AIDEDNAV. Recycle missile power.

B: LOCATION(Reverse Video)

The BAY location select switch was selected. B (bay) is not a selectable location,do not select bay location switch,and verify selection.

LCD ENTRY(Reverse Video)

No JASSM launch point/direct target is selected or no weapon isready to be launched when the manual launch switch is momentarilydepressed while in manual launch mode.

1. Ensure current destination is aJASSM launch point/direct target.

2. Ensure the associated weapon isoperational and targeted.

LOCATION??(Reverse Video)

A station switch was selected with no location selected or an op-eration was attempted without designating a Location on theWCP.

Select a location before selecting astation.

LOC/STA??(Reverse Video)

1. A weapon is not present at one or more of the selected stationswhen weapon power on, jettison, CDE, or TM on/off is command-ed.

Select only stations that have aweapon present.

2. No location/station is selected when weapon power on/off, jetti-son, CDE, or TM on/off is commanded.

Select location(s) and station(s) priorto placing weapon jettison switch inSEL position.

3. A weapon, which has a permanent fatal Fault, was selected indi-vidually when weapon power on/off, CDE, or TM on/off was com-manded.

Select only stations that do not havea weapon with a permanent fatalFault.

4. An unpowered weapon was selected when CDE was commanded. Select only weapons that have pow-er applied.

5. A weapon, where CTS has been commanded, was selected whenCDE, TM on/off, FTS enable, jettison, weapon power on was com-manded.

Do not command power off to aweapon that has received the CTScommand.

STATION??(Reverse Video)

An invalid station select switch (4 or 5) was selected. Select a valid station (1-3, 6-8).

WPN GPS DATA(Reverse Video)

Input/Output with the Interface Unit (IU) failed (GPS Almanac,Ephermeris, AS/SV Configuration data, or Time Mark Data accessattempt).

Verify the correct weapon DTUC isinstalled and powered, and the IUand aircraft GPS receiver are opera-tional.

xy:LCD ENTRY(Reverse Video)

Entry into Launch Countdown (LCD) was attempted but was unsuc-cessful due to LCD entry check failure.

Review FRMT-7 and Master Faultsdisplayed and re-attempt launch.


T.O. 1B-52H-34-2-8

Change 2 7-68C

JASSM Advisories (Cont)[AMI]

Fault Indication Coding:• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER


B: LOCATION(Reverse Video)

The BAY location select switch was selected. B (bay) is not a selectable JASSMlocation, do not select bay locationswitch, and verify selection.

JASSM ALIGN FAIL(Reverse Video)

Missile alignment failure. 1. Check OAS Nav Mode is INSAIDED NAV.2. Recycle missile power.

JASSM EVENT(Reverse Video)

The JASSM SMO is secondary and a mission plannedJASSM launch point is within 30 minutes.

1. Proceed with mission profile.2. If required, make JASSM SMOprime, then power and align missiles.

JASSM GPS DATA(Reverse Video)

I/O with the IU failed. 1. Verify that the GPS Initializationfile exists on the DTC and the aircraftIU and GPS receiver are operational.

JASSM LCD ENTRY(Reverse Video)

No JASSM launch point/direct target is selected or no weap-on is ready to be launched when the manual switch is mo-mentarily depressed while in manual launch mode.1. Entry into LCD was expected but unsuccessful.2. LCD is not initiated for the current release event.3. A weapon is not selected for launch and:

A. If in automatic launch mode, aircraft is within the In-Zone LAR and will be at the point of closest approach whenLCD is complete.

B. If in manual launch mode, a manual launch commandis present. SMO will reset the manual launch command iflaunch entry requirements are not met.

1. Ensure current destination is aJASSM launch point/direct target.2. Ensure the associated weapon isoperational and targeted beforepressing the manual launch switchwhile in manual launch mode.

JASSM LOC/STA??(Reverse Video)

1. A weapon is not present at one or more of the selected sta-tions when weapon power on, jettison, CDE, or TM on/off iscommanded.

1. Select appropriate location(s) andstation(s) with weapon(s) present.

2. No location/station is selected when weapon power on/off, jettison, CDE, or TM on/off is commanded.

2. Select location(s) and station(s)prior to entering the command.

3. A weapon with a permanent fatal fault was selected indi-vidually when weapon power on/off, CDE, or TM on/off com-manded.

3. Do not select a station having aweapon with a permanent fatal fault.

4. A weapon, which is not powered and not permanently fatalfaulted, was selected when CDE was commanded.

4. Select only weapons that havepower applied.

5. A weapon, where CTS has been commanded, was selec-ted when CDE, TM on/off, FTS enable, jettison, weaponpower on was commanded.

5. Do not enter a command to aweapon that has received the CTScommand.

L: LOCATION??(Reverse Video)

1. PCP Left Pylon switch was selected but there is no SMOassigned to the LP location.2. WCP LOCATION L PYLON switch was selected but thereis no SMO assigned to the LP location.3. WCP LOCATION LEFT PYLON switch was selected sub-sequent to selection of the Bay location and/or the Right Py-lon location and the SMO assigned to the LP location is notthe same as the SMO assigned to the previously selectedlocation.

1. Deselect the PCP LP switch andassign a SMO to the Left Pylon loca-tion, if required.2. Assign a SMO to the Left Pylonlocation before selecting the WCPLOCATION L PYLON switch, if re-quired.


T.O. 1B-52H-34-2-8

7-68D Change 2

JASSM Advisories (Cont)[AMI]

Fault Indication Coding:• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER


LOCATION??(Reverse Video)

WCP station switch was selected with no location selected. Select a location on the WCP.

LOC/STA??(Reverse Video)

No location and station selected when weapon power on/offor jettison is commanded.

Select location(s) and station(s) priorto entering the command.

R: LOCATION??(Reverse Video)

1. PCP Right Pylon switch was selected but there is no SMOassigned to the RP location.2. WCP LOCATION R PYLON switch was selected but thereis no SMO assigned to the RP location.3. WCP LOCATION RIGHT PYLON switch was selectedsubsequent to selection of the Bay location and/or the LeftPylon location and the SMO assigned to the RP location isnot the same as the SMO assigned to the previously selectedlocation.

1. Deselect the PCP RP switch andassign a SMO to the Right Pylonlocation, if required.2. Assign a SMO to the Right Pylonlocation before selecting the WCPLOCATION R PYLON switch, if re-quired.

STATION??(Reverse Video)

1. An invalid station select switch (4 or 5) was selected.2. Individual WCP station switch was selected with multiplelocations selected and the SMO has inhibited such.

1. Select a valid station (1-3, 6-8).2. Select the ALL station switch orhave only one location selected.

STORES DATA FAIL(Reverse Video)

A failure occurred during stores data loading from the DTC. 1. Ensure the DTC is properly in-serted.2. Reattempt mission data load.3. Determine DTR status fromFRMT-6.4. Reinstall DTC to different DTRand reload mission.

x:JETT INHIB(Reverse Video)

Either a WCP selective jettison or a BMJCP Jettison All hasbeen commanded for a location for which there is no SMOassigned.

1. For a WCP selective jettison, se-lect the location(s) for which the pri-mary SMO is assigned.2. For a BMJCP Jettison All, changethe primary SMO and reissue the Jet-tison All request.

xy:LCD ENTRY(Reverse Video)

Entry into Launch Countdown (LCD) was attempted but wasunsuccessful due to LCD entry check failure.

Review FRMT-7 and Master Faultsdisplayed and re-attempt launch.


T.O. 1B-52H-34-2-8

Change 2 7-69

JASSM Status Messages

MESSAGE TEXT STATUS INDICATED

GO/NOGO COMPLT (Normal Video) The Go/No-Go Test has been completed for all weapons thathave had power applied.

SIT COMPLT (Normal Video) The System Integrity Test has been completed for all weaponsthat have had power applied.

CDE COMPLT (Normal Video)Less [AMI]JASSM CDE COMPLT (Normal Video)[AMI]

Classified data erase has been completed for all selectedweapons.

Figure 7-21

Safe Release Advisories

Safe release advisories do not inhibit launch. Possible collision between weap-ons and between weapon and aircraft can occur if weapon is launched with arelease advisory displayed.

NOTE

In order of priority, safe release advisories follow weapon launch advisories inthe following order:

RELEASE ADVISORY INDICATION CORRECTIVE ACTION

ROLL Maximum roll angle (10°) or maximumroll rate (5°/second) violated.

Decrease aircraft roll angle or maximum roll rate.

PITCH Maximum pitch angle (10°) or maxi-mum pitch rate (5°/second) violated.

Decrease aircraft pitch angle ormaximum pitch rate.

LEVL_OFF Vertical velocity or vertical acceleration(< –0.5 G or >2.0 G) is too high.

Decrease altitude rate of change.

YAW Maximum yaw rate (1°/second) vio-lated.

Decrease aircraft yaw rate.

(blank) No release advisory exists. None.

Figure 7-22

T.O. 1B-52H-34-2-8

7-70

Weapon Launch AdvisoriesNOTE

• Weapon launch advisories are displayed when crew actions are required, toobtain an effective JASSM launch.

• The weapon launch advisories are shown below in the order of highest prior-ity.

LAUNCH ADVISORY INDICATION CORRECTIVE ACTION

CLIMB (Blinking, BrightUnderlined Video)

Aircraft altitude is at, below or within 500feet of the minimum altitude for release.Applicable when the aircraft is In-Zoneor In-Zone is achievable.

Increase aircraft altitude rate ofchange.

ACCEL (Blinking, BrightUnderlined Video)

Aircraft speed is at, below or within 0.02Mach of the minimum Mach for release.Applicable when the aircraft is In-Zoneor In-Zone is achievable.

Increase aircraft airspeed.

DIVE (Blinking, BrightUnderlined Video)

Aircraft altitude is at, above or within 500feet of the maximum altitude for release.Applicable when the aircraft is In-Zoneor In-Zone is achievable.

Decrease altitude rate of change.

DECEL (Blinking, BrightUnderlined Video)

Aircraft speed is at, above, or within 0.02Mach of the maximum Mach for release.Applicable when the aircraft is In-Zoneor In-Zone is achievable.

Decrease aircraft airspeed.

HDG TOL(Blinking Video)

Current aircraft heading is within 6° to 9°of heading tolerance limits. Applicable when the aircraft is not In-Zone, but In-Zone is achievable.

Put the aircraft back on preplannedpath or wait until the aircraft is In-Zone for the TRN LEFT or TRNRIGHT indication.

HDG TOL(Blinking, Bright Video)

Current aircraft heading is within 3° to 6°of heading tolerance limits. Applicable when the aircraft is not In-Zone, but In-Zone is achievable.


HDG TOL (Blinking,Bright Underlined Video)

Current aircraft heading is within 3° oroutside of heading tolerance limits.Applicable when the aircraft is not In-Zone, but In-Zone is achievable.



T.O. 1B-52H-34-2-8

7-71

LAUNCH ADVISORY INDICATION CORRECTIVE ACTION

TRN LEFT(Blinking Video)

Aircraft heading is within 6° to 9° of theright heading tolerance limit for release.(Turn LEFT to correct.) Applicable whenthe aircraft is In-Zone only.

Turn aircraft to the left until withintolerance for release.

TRN LEFT(Blinking, Bright Video)

Aircraft heading is within 3° to 6° of theright heading tolerance limit for release.(Turn LEFT to correct.) Applicable whenthe aircraft is In-Zone only.


TRN LEFT (Blinking,Bright Underlined Video)

Aircraft heading is within 3° or outside ofthe right heading tolerance limit for re-lease. (Turn LEFT to correct.) Applica-ble when the aircraft is In-Zone only.


TRN RIGHT(Blinking Video)

Aircraft heading is within 6° to 9° of theleft heading tolerance limit for release.(Turn RIGHT to correct.) Applicablewhen the aircraft is In-Zone only.

Turn aircraft to the right until withintolerance for release.

TRN RIGHT(Blinking, Bright Video)

Aircraft heading is within 3° to 6° of theleft heading tolerance limit for release.(Turn RIGHT to correct.) Applicablewhen the aircraft is In-Zone only.


TRN RIGHT (Blinking,Bright Underlined Video)

Aircraft heading is within 3° or outside ofthe left heading tolerance limit for re-lease. (Turn RIGHT to correct.) Applica-ble when the aircraft is In-Zone only.


(blank) No launch advisory exists. None.


T.O. 1B-52H-34-2-8

7-72

FRMT-7 Weapon Faults

FRMT-7 MESSAGEVIDEO

HIGHLIGHT CAUSE

ABORT R LCD abort after CTS.CTSS Battery Failure.

ACFT PWR R 3-Phase 115V AC power Fault (uncommanded on).28 VDC #1 Power Fault.28 VDC #2 Power Fault (uncommanded off).

BIA FAIL R BIA Fault.

BUS TEST R Weapon Bus Test Fault.

COMM NOGO R Weapon communication Fault.Aircraft ID Fault.Surface/Fin Delay Fault.Almanac Received Fault.GPS Keys Transfer Fault.Mass Data Transfer Protocol Fault.Simulated Launch Fault.Timeline Abort Fault.Timeline Integration Fault.Uncommanded Timeline Abort.Min TXA Received Fault.

CTSS R Uncommanded CTS Fault.Uncommanded CTSS Fault.

EJECTOR R Ejector status discrepancy Fault.Uncommanded Ejector Lock.

ERASE FAIL R Data Erase Failure Fault.

FTS R Activate FTS Fault.

GPS DATA R Ephemeris Received Fault.Time Received Fault.

GPS INIT R AS/SV Received Failure.

HTR PWR R 3-Phase 115 VAC Power Fault (uncommanded off).

HUNG R Hung store.

LCD FAIL R LCD abort prior to CTS.CTSS Battery Failure.

OVERTEMP R Over Temperature Caution Fault.

R/Blinking Over Temperature Warning Fault.

SEEKER R Terminal Guidance Fault.


T.O. 1B-52H-34-2-8

7-73/(7-74 blank)

FRMT-7 MESSAGEVIDEO

HIGHLIGHT CAUSE

SQUIB NOGO R Squibs Fault.

STORE ID R Store description Fault.

TGT NOGO R Targeting Fault.

TIK FAIL R TIK Fault.

TLMY R Telemetry Fault.

WARM-UP R Warm-up Complete Fault.

WPN DATA R Weapon Mission Data Fault.

WPN NOGO R Reset Power Dropout Fault.Current Weapon State Fault.BIT report Fault. (CS Fault, Engine Control Fault, GPS Fault, IMU Fault,PF Fault, Processor Fault, PS Fault).Critical hardware Fault.Uncommanded Data Erase Fault.Activate IBIT Fault.Uncommanded IBIT Fault.Release Consent Uncommanded High Fault.Reset Power Dropout Fault.Uncommanded Weapon Test Fault.

WPN PRSNT R Weapon present status discrepancy.

XXX-YYYZ N Store ID when Go/NoGo Test or SIT is active and noweapon Faults exist.

28VDC2 R 28 VDC #2 Power Fault (uncommanded on).LCD Abort after CTS.

(blank) N Weapon is not present or no Fault exists for this weap-on or WIU power for this pylon is off.


BLA

T.O. 1B-52H-34-2-8

Glossary 1

Glossary

ACU Avionics Control Units

ADP Air Data Probe

AFMSS Air Force Mission Support System

AIU Armament Interface Unit

AJCP Alternate Jettison Control Panel

AOC Air Operations Center

AS/SV Anti-Spoofing/Satellite Vehicle

ATC Automatic Target Correlator

ATL Above Target Level

ATO Air Tasking Order

AUR All Upround Ready

A/W/E Aircraft/Weapon/Electronic software

BIA Bomb Impact Assesment

BIT Built In Test

BTT Bearing To Target

C&D Controls and Displays

CAD Controls And Displays processor

CCA Circuit Card Assembly

CDE Classified Data Erase

CEM Conventional Enhancement Modification

CEP Circular Error Probable

CPOA Closest Point of Approach

CTOF Current Time Of Flight

CTS Commit to Separate (synonymous to ITL)

CTSS Commit to Store Separation

CWI Conventional Weapons Integration

DMPI Desired Mean Point of Impact

DPPDB Digital Point Position Database

DTC Data Transfer Cartridge

DTCU Data Transfer Controller Unit

DTD Digital Transfer Device

DTED Digital Terrain Elevation Data

DTG Distance To Go

DTU Data Transfer Unit

DTUC Data Transfer Unit Cartridge

E East

ECU Environmental Control Unit

EED Electroexplosive Device

EMI Electromagnetic Interference

FCP Flight Computer Program

FDRC Fault Data Recorder Cartridge

FMS Flight Management System

FSP Flush Static Port

FTS Flight Termination System

GMCP Ground Maintenance Computer Program

GPI Global Position Indicator

GPS Global Positioning System

GWD Gravity Weapon Delivery

HSAB Heavy Stores Adapter Beam

IBIT Initiated Built-in-Test

ICSMS Integrated Conventional Stores Management System

IKB Integrated Keyboard

IMU Inertial Measurement Unit

IMV Instrumented Measurement Vehicle

INS Inertial Navigation System

IR Infrared

IIR Imaging and Infrared

ITL Intent to Launch (synonymous to CTS)

IUS Interface Unit Software

IZ In-Zone

JAGR JASSM Anti-Jam GPS Receiver

JASSM Joint Air-to-Surface Standoff Missile

LAR Launch Acceptability Region

LCD Launch Countdown

LOS Line of Sight

LP Launch Point

LRU Line Replaceable Unit

MCU Missile Control Unit

MF Master Fault

MFD Multifunction Display

MIDB Modern Integrated Intelligence Database

MIU Missile Interface Unit

MPS Mission Planning System

T.O. 1B-52H-34-2-8

Glossary 2

MSG Advisory message acknowledgment switch

N North

NAWD Navigation and Weapon Delivery Processor

NEW Net Explosive Weight

NF Non Fatal

NTM National Technical Means

N/A Not Applicable

OAS Offensive Avionics System

OCP Operational Computer Program

OML Outer Mold Line

PCP Power Control Panel

PDU Power Distribution Unit

PMD Prime Mission Data

PF Permanent Fatal

PGMTDB Precision Guided Munition Target Database

PME Prime Mission Equipment

PTM Precision Targeting Module

PTOF Planned Time Of Flight

PVE Preset–Verify–Execute

REPF Rear Echelon Production Facility

RF Radio Frequency

ROB Range On Bearing

S South

SC Safety Critical

SAASM Selective Availability Anti-Spoofing Module

SA Situation Awareness

SAU Splitter Amplifer Unit

SAIR Safe and In–Range

SIT System Integrity Test

SMIU Stores Management Interface Unit

SMO Stores Management Overlay

TACT Ferry Tactical Ferry Flight

TAM Target Area Module

TBMCS Theater Battle Management Core System

TF Transient Fatal

T/R Transformer/Rectifier

TAL Transfer Alignment Maneuver

TDS Target Data Set

TIK Test Instrumentation Kit

TLI Timeline Integration

TM Telemetry

TOF Time of Flight

TOT Time on Target

TTG Time to Go

TXA Transfer Alignment

UC Upper Corner

UTC Universal Time Coordinated

VAC Volts Alternating Current

VDC Volts Direct Current

W West

WCE Weapon Control Equipment

WCP Weapon Control Panel

WF Wire Frame

WGS-84 World Geodetic System 1984

WIU Weapon Interface Unit

WPM Weapon Planning Module

T.O. 1B-52H-34-2-8

Change 2 Index-1

Alphabetical Index

*DENOTES ILLUSTRATION

Page Page

AAdvisories and Status Messages 7-52AAfter Engine Start (Aircraft Power and Cooling

Air Available) 2-7After Landing Procedures 2-23After Takeoff (RN/N) 2-9Aircraft Commander’s Responsibilities 3-6Air Data System 1-6Alternate Jettison Control Panel 1-24*Automatic Launch Determination 7-46Automatic Missile Launch Checklist (RN-N) 2-19Avionics 1-6

BB-52 Carrier Equipment 1-3B-52/JASSM Weapon System 1-3B-52 Mission Data Load Display (CF-81 1-52C*Backup Notification Procedures 3-6Before Exterior Inspection (Power Off) (RN/N) 2-3Before Launch Check (RN) 2-18Blow Off Wedges 1-5

CCircuit Breaker Panels 1-23*Circuit Protection 1-23*Commands for OAS Power Control Panel

and Missile Control Panel (CF-E) 1-55*Control Function (CF) Displays 1-30Control Function (CF) Menu 1-30C*

DDefinition of Terms 3-6Destination Table Display (FRMT-10,nn) 1-69*Direct Target Copy Command (CF-Dn) 1-52GDirect Targeting Data Entry Procedures 2-13Direct Target Definition

Display (CF-588,n) 1-42*,7-20A*

EEmergency Aircrew Procedures 3-1Emergency Jettison 3-5Engine 1-6Exterior Inspection (Power Off) (RN/N) 2-3

FFCP Supervision Menu (CF-6) 1-46, 1-48*Firefighting and Evacuation Criteria 3-7, 3-7*Format (FRMT) Displays 1-56FRMT-7 Missile Faults 7-52AFRMT-7 Weapon Faults 7-52A, 7-72*FTS Enable/Disable Command (CF-57C,xy)

(OTL Only) 4-3FTS Power Source Command (CF-57D)

(OTL Only) 4-3Fuselage 1-5Fuel System 1-5

GGeneral Procedures 2-3Ground Safeing Procedures (RN-N) 2-23

HHeavy Stores Adapter Beam JASSM

Configuration 1-8*

IInflight Emergency Notification Procedures

(World Wide) 3-7Inflight Notification Procedures 3-6Inflight Procedures 2-9In-Range LAR 7-31In-Range/In-Zone Indication 7-43Integrated Keyboard (IKB) 1-18*In-Zone LAR 7-36

T.O. 1B-52H-34-2-8

Index-2 Change 2

Page Page

J, KJASSM Achievable In-Range LAR 7-32*JASSM Achievable In-Zone LAR 7-37*JASSM Advisories 7-68B*JASSM Anti-Ice Operation 5-1JASSM Closest Point of Approach Outside

In-Zone LAR 7-41*JASSM Control Function (CF) Commands 1-30B*JASSM Control Switches 1-25*JASSM Cover 1-7JASSM Employment Overview 7-3JASSM Flight Profile Summary 7-4*JASSM Flight Profiles 7-5*JASSM Format Commands 1-57*JASSM Free Flight Sequence 7-48JASSM FRMT (Format) Menu 1-58*JASSM IKB Commands 1-19*JASSM Initialization Timeline 7-9*JASSM In-Zone LAR 7-36*JASSM Jettison and Launch Envelopes 5-1, 5-3*JASSM Launch Or Jettison

With Open Bomb Bay Doors 5-1JASSM Launch Sequence Timeline (Typical) 7-46*JASSM Master Faults 7-53*JASSM Preferred Launch/Jettison Sequence 7-49*JASSM Program Commands 1-74*JASSM Safe Separation and Deconfliction 5-2JASSM SMO Flight Test Software Commands 4-1JASSM SMO Software 1-27JASSM Static LAR 7-29*JASSM Status and Inventory

Display (FRMT-7) 1-62*, 7-14*JASSM Status and Inventory Display with

Selected Station (FRMT-7xy) 1-64*, 7-15*JASSM Status Messages 7-69*JASSM Supervision Menu (CF-57) 1-32*, 4-1JASSM Suspension System 1-7JASSM Target Assignment (Manual Targeting)

Display (CF-586) 7-19*JASSM Target Definition 7-21*JASSM Targeting Menu (CF-58) 1-34*JASSM Telemetry Antenna 4-2*JASSM Unachievable In-Range LAR 7-34*JASSM Unachievable In-Zone LAR 7-40*Jettison Control Switches 1-25*Joint Air-to-Surface Standoff Missile

(JASSM) 1-3, 1-4*

LLaunch Procedures 2-17

MManual Launch Determination 7-47Manual Missile Launch Checklist (RN-N) 2-20Master Faults 7-52AMAU-12 Ejector Rack With Extension 1-9*Messages 7-52AMFD Display Figures 1-12Missile and Ejector Status 7-10Missile Check (RN/N) 2-7Missile Control Panel Backup

Display (CF-E) 1-52G, 1-53*Missile Data Flow (Typical) 1-13*Missile Jettison 3-2, 7-50Missile Launch 7-45Missile Launch Procedures 2-18Missile Launch Process 7-45Missile Launch Restrictions 7-48Missile Launch Termination 7-47Missile Mission Data and Targeting 7-17Missile Mission Types 7-3Missile Power Application 7-8Missile Power Application (N) 2-9Missile Power Removal 7-15Missile Preferred Launch Sequence 2-12*Missile Preferred Jettison Sequence 3-2*Missile Preparation For Launch (RN-N) 2-17Missile/Target Assignment Display (CF-586) 1-36*Missile/Target Assignment (Manual

Targeting Procedures 2-10Missile Targeting Methods 7-17Missile Targeting Procedures (RN-N) 2-10Mission Data Load Display (CF-81) 1-52C*Mission Planning 6-1Mission Planning Flow and Partitioning 6-3*Mission Planning Functional Flow 6-5*Mission Planning Modules 6-3Mission Planning Considerations 6-7Mission Planning Timelines 6-4Mission Supervision Menu (CF-8) 1-51, 1-52A*Multifunction Displays 1-12, 1-21*

T.O. 1B-52H-34-2-8

Change 2 Index-3/(Index-4 blank)

Page Page

NNotification Procedures – Dangerous Materials 3-6Normal Notification Procedures 3-6

OOAS Power Control Panel 1-17*OAS/Joint Air to Surface Standoff

Missile Operation 7-3OAS/Weapon System Related Controls and

Displays 1-11Offensive Avionics System (OAS)

Interface 1-11Operating Limitations 5-1

P, QPilots’ Bomb Bay & Missile Jettison Control

Switch Commanded Jettison 1-25Pilot’s Munition Consent Panel 1-16*PME Status Display (FRMT-6) 1-60*Post Strike/Abort Procedures 2-22Post Strike/Abort (RN/N) 2-22Preferred Launch/Jettison Sequence 7-48Preflight Procedures 2-3PRGM Display In-Range/In-Zone Indications 7-44*Prime Mission Data 1-28Program Displays (PRGM) 1-74, 1-75*PTM Timeline Definition 6-6*

RRelease Advisory Display 1-28, 1-29*REPF Mission Planning 6-4

SSafe Release Advisories 7-44, 7-69*Safe Release and Weapon Launch Advisories 7-52ASelective Jettison Using the AJCP 3-4Selective Jettison Using the WCP/SMO 3-3Selected Direct Target Deselection

Command (CLR-D) 1-52GSIM Mode Response Times 7-51*Simulated Missile Loadout 7-51Simulated Ranging 7-51Simulated Targeting Operations 7-51Simulated WCE Responses 7-51Simulation Capabilities 7-51SMO Control Function (CF) Commands 1-30*SMO Format Commands 1-57*SMO FRMT (Format) Menu 1-58*

SMO Load Menu (CF-62) 1-50*SMO MFD Displays 1-27SMO Restart 7-52SMO Termination 7-52Stores Inventory Summary

Display (FRMT-77) 7-68B*Supplementary Data 4-1

TTargeting Process Control (CF-DD and

CF-DE) 1-52GTarget Ranging 7-29Target Ranging Indications 7-43Targeting Techniques 7-22Telemetry Power OFF Command (CF-57B)

(Test Only) 4-3Telemetry Power ON Command (CF-57A)

(Test Only) 4-1Test Instrumentation Kit (TIK) 4-1Transfer Alignment (TXA) Halt Command

(CF-57E,xy) (Captive Carry Only) 4-4Transfer Alignment (TXA) Re-Init Command

(CF-57F,xy) (Captive Carry Only) 4-4

UUnit Mission Planning Integration 6-4USAF JASSM Mission Planning Module 6-2

VVertical Tail 1-5

W, X, Y, ZWarhead 1-5WCE Power Application 7-7WCE Power Removal 7-8Weapon Assignment Data Display (CF-DF or

CF-DB from FRMT-7, 7A, 7C or 7xy) 1-68A*Weapon Control Equipment (WCE) Status 7-7Weapon Control Panel 1-14*Weapon Group Load Menu

(CF-82A, CF-82C) 1-52E*Weapon Jettison 1-22Weapon Launch Advisories 7-43, 7-70*Weapon Monitor and Power Control 7-7Weapon Summary Display

(FRMT-12,nn/FRMT-12,Dn) 1-71*Weapon Supervision Menu (CF-5) 1-30, 1-30E*Wing Flutter Airspeed Limitations 5-1Wings 1-5WPM Timeline Definition 6-6*

BLA

Documents

AIRCREW WEAPONS DELIVERY MANUAL (NONNUCLEAR) B … 1B-52H-34-2-8 1-Jun-06 Scrib… · t.o. 1b-52h-34-2-8 1 december 2003 change 3 – 1 june 2006 aircrew weapons delivery manual (nonnuclear)