Entry Checklist - NASA · ENT–798 ENT–799 ENT–801 ENT–802 MULTI–1599 MULTI–1616 Incorporate the following: 1. Replace vii thru x 2. Replace 2–3 & 2–2 (five pages each

Lyndon B. Johnson Space CenterHouston, Texas

National Aeronautics andSpace Administration

Verify this is the correct version for the pending operation (training, simulation or flight).Electronic copies of FDF books are available. URL: http://mod.jsc.nasa.gov/fdf

JSC–48019

Entry Checklist

Mission Operations DirectorateOperations Division

Generic, Rev FApril 24, 2002

SSP Flight Data File PAGE CHANGE NOTICE JSC–48019

ENTRY C/L GENERIC Rev F (Apr 24, 2002)

PCN–1 (Oct 25, 2002) Sheet 1 of 1

List of Implemented Change Requests (482s):

ENT–798ENT–799ENT–801ENT–802

MULTI–1599MULTI–1616

Incorporate the following:

1. Replace vii thru x

2. Replace 2–3 & 2–2 (five pages each in Flt Qual only)Replace 2–3 & 2–4

3. Replace 5–1 & 5–2

4. Replace 7–3 & 7–4, 7–7 & 7–8

5. Replace CC 8–19 & CC 8–20

Prepared by:

Approved by:

Book Manager

Lead Entry GPO Chief, Ascent/Descent DynamicsBranch

Encl: 16 pages (Bond)Encl: 26 pages (Flt Qual)

File this PCN immediately behind the front cover as a permanent record

Verify this is the correct version for the pending operation (training, simulation or flight).Electronic copies of FDF books are available. URL: http://mod.jsc.nasa.gov/fdf

i ENT/ALL/GEN F

JSC–48019

MISSION OPERATIONS DIRECTORATE

ENTRY CHECKLIST

GENERIC, REVISION FApril 24, 2002

PREPARED BY:

Gwendolyn Jordan–MooreBook Manager

APPROVED BY:

Lead Entry GPO Gregory T. OliverChief, Ascent/Descent

Dynamics Branch

This document is under the configuration control of the CrewProcedures Control Board (CPCB). All proposed changes mustbe submitted on JSC Form 482 to DO3/FDF Manager.

Additional distribution of this book for official use must berequested in writing to DO3/FDF Manager. The request mustinclude justification and requester’s name, organization,position, and phone number. Contractor requests are madethrough the NASA or DOD organization supported. Deletions,reduction in quantity, or change of address may be submitted toDO3/FDF distribution manager, (713) 244–1182.

ENT/ALL/GEN F

ii ENT/ALL/GEN F

Incorporates the following:482#: ENT–794A

ENT–796

AREAS OF TECHNICAL RESPONSIBILITY

Book Manager DM43/G. Jordan–Moore 483–1261

Deorbit Burn to Entry Interface DM43/J. Patterson 483–1987

Entry Interface thru RolloutPost Landing

DM43/J. Patterson 483–1987

iii ENT/ALL/GEN F

Replace this page with page(s) from Flight Supplement

iv ENT/ALL/GEN F


v ENT/ALL/GEN F

NOTES

1. The Wheels Stop/Egress Switch List, section 7, gives thevehicle configuration at these discrete times. If switchposition difference exists between wheels stop and crewegress, egress position will be boxed beside wheels stopposition. Section 7 contains switch configuration only forpanels that are reconfigured during crew execution ofprocedures in sections 3, 4, and 5. Refer to DEORBITPREP, section 3, for egress configuration for remainingpanels.

2. This checklist is an all–vehicle book and is not complete fora specified flight without a Flight Supplement. To obtaincomplete checklist, incorporate Flight Supplement forspecific flight of interest using instructions in FlightSupplement List of Effective Pages.

3. Entry related cue cards are contained in this document.Cue cards are listed in Entry Cue Card Config section.Some cue cards are printed in the body of checklist for MSuse and also in the Entry Cue Card Config section forreference of crop marks and fabrication instructions.

4. Velcro placement, size, and shape of cue cards arecontrolled by Cue Card Book Manager.

5. Vehicle configuration or procedural steps that areapplicable to a specific vehicle are indicated by xxx .

vi ENT/ALL/GEN F

This Page Intentionally Blank

vii ENT/ALL/GEN F

ENTRY CHECKLIST

LIST OF EFFECTIVE PAGES

GENERIC 02/01/88REV F 04/24/02PCN–1 10/25/02

Sign Off * ALL/GEN F. . . . ii * ALL/GEN F. . . . . . . . . . iii *� ALL/GEN F. . . . . . . . . . iv *� ALL/GEN F. . . . . . . . . . v * ALL/GEN F. . . . . . . . . . vi * ALL/GEN F. . . . . . . . . . vii * ALL/GEN F,1. . . . . . . . . viii * ALL/GEN F,1. . . . . . . . . ix * ALL/GEN F,1. . . . . . . . . . x * ALL/GEN F,1. . . . . . . . . . xi *� ALL/GEN F. . . . . . . . . . xii *� ALL/GEN F. . . . . . . . . FS xiii * flt suppl. . . . . . FS xiv * flt suppl. . . . . . xv ALL/GEN F. . . . . . . . . xvi ALL/GEN F. . . . . . . . . 1–1 (3 pgs) � ALL/GEN F. 1–2 (3 pgs) � ALL/GEN F. 2–1 ALL/GEN F. . . . . . . . 2–2 (6 pgs) � ALL/GEN F. 2–3 (6 pgs) � ALL/GEN F,1. 2–4 ALL/GEN F. . . . . . . . 2–5 � ALL/GEN F. . . . . . . . 2–6 � ALL/GEN F. . . . . . . . 3–1 � ALL/GEN F. . . . . . . . 3–2 � ALL/GEN F. . . . . . . . FS 3–3 flt suppl. . . . . FS 3–4 flt suppl. . . . . 3–5 ALL/GEN F. . . . . . . . 3–6 ALL/GEN F. . . . . . . . 3–7 ALL/GEN F. . . . . . . . 3–8 ALL/GEN F. . . . . . . .

3–9 ALL/GEN F. . . . . . . . 3–10 ALL/GEN F. . . . . . . 3–11 ALL/GEN F. . . . . . . 3–12 ALL/GEN F. . . . . . . A3–13 MEDS/GEN F. . . . . A3–14 MEDS/GEN F. . . . . B3–13 NOM/GEN F. . . . . B3–14 NOM/GEN F. . . . . 3–15 ALL/GEN F. . . . . . . 3–16 ALL/GEN F. . . . . . . 3–17 ALL/GEN F. . . . . . . 3–18 ALL/GEN F. . . . . . . 3–19 ALL/GEN F. . . . . . . 3–20 ALL/GEN F. . . . . . . 3–21 ALL/GEN F. . . . . . . 3–22 ALL/GEN F. . . . . . . 3–23 ALL/GEN F. . . . . . . 3–24 ALL/GEN F. . . . . . . 3–25 ALL/GEN F. . . . . . . 3–26 ALL/GEN F. . . . . . . 3–27 ALL/GEN F. . . . . . . 3–28 ALL/GEN F. . . . . . . 3–29 � ALL/GEN F. . . . . . . 3–30 � ALL/GEN F. . . . . . . A3–31 MEDS/GEN F. . . . . A3–32 MEDS/GEN F. . . . . B3–31 NOM/GEN F. . . . . B3–32 NOM/GEN F. . . . . 3–33 � ALL/GEN F. . . . . . . 3–34 � ALL/GEN F. . . . . . . A3–35 MEDS/GEN F. . . . . A3–36 ALL/GEN F. . . . .

* – Omit from flight book� – Replace with page from Flight Supplement� – Extra pages in crew copy only

ENT/ALL/GEN F,1

viii ENT/ALL/GEN F

B3–35 NOM/GEN F. . . . . B3–36 ALL/GEN F. . . . . 3–37 ALL/GEN F. . . . . . . 3–38 ALL/GEN F. . . . . . . A3–39 MEDS/GEN F. . . . . A3–40 MEDS/GEN F. . . . . B3–39 NOM/GEN F. . . . . B3–40 NOM/GEN F. . . . . 3–41 ALL/GEN F. . . . . . . 3–42 ALL/GEN F. . . . . . . A3–43 MEDS/GEN F. . . . . A3–44 MEDS/GEN F. . . . . B3–43 NOM/GEN F. . . . . B3–44 NOM/GEN F. . . . . 4–1 ALL/GEN F. . . . . . . . 4–2 ALL/GEN F. . . . . . . . 4–3 ALL/GEN F. . . . . . . . 4–4 ALL/GEN F. . . . . . . . 4–5 ALL/GEN F. . . . . . . . 4–6 ALL/GEN F. . . . . . . . 4–7 � ALL/GEN F. . . . . . . . 4–8 � ALL/GEN F. . . . . . . . 4–9 ALL/GEN F. . . . . . . . 4–10 ALL/GEN F. . . . . . . 4–11 � ALL/GEN F. . . . . . . 4–12 � ALL/GEN F. . . . . . . 4–13 ALL/GEN F. . . . . . . 4–14 ALL/GEN F. . . . . . . 4–15 ALL/GEN F. . . . . . . 4–16 ALL/GEN F. . . . . . . 5–1 ALL/GEN F. . . . . . . . 5–2 ALL/GEN F,1. . . . . . . . A5–3 MEDS/GEN F. . . . . . A5–4 ALL/GEN F. . . . . . B5–3 NOM/GEN F. . . . . . B5–4 ALL/GEN F. . . . . . 5–5 ALL/GEN F. . . . . . . . 5–6 ALL/GEN F. . . . . . . . 5–7 ALL/GEN F. . . . . . . . 5–8 ALL/GEN F. . . . . . . . 5–9 ALL/GEN F. . . . . . . .

5–10 ALL/GEN F. . . . . . . 5–11 ALL/GEN F. . . . . . . 5–12 ALL/GEN F. . . . . . . A5–13 ALL/GEN F. . . . . A5–14 MEDS/GEN F. . . . . A5–15 MEDS/GEN F. . . . . A5–16 MEDS/GEN F. . . . . B5–13 ALL/GEN F. . . . . B5–14 NOM/GEN F. . . . . B5–15 NOM/GEN F. . . . . B5–16 NOM/GEN F. . . . . 5–17 ALL/GEN F. . . . . . . 5–18 ALL/GEN F. . . . . . . 5–19 � ALL/GEN F. . . . . . . 5–20 � ALL/GEN F. . . . . . . 5–21 ALL/GEN F. . . . . . . 5–22 ALL/GEN F. . . . . . . 5–23 ALL/GEN F. . . . . . . 5–24 ALL/GEN F. . . . . . . 6–1 ALL/GEN F. . . . . . . . 6–2 ALL/GEN F. . . . . . . . 6–3 ALL/GEN F. . . . . . . . 6–4 ALL/GEN F. . . . . . . . 7–1 * ALL/GEN F. . . . . . . . 7–2 * ALL/GEN F. . . . . . . . 7–3 * ALL/GEN F,1. . . . . . . . 7–4 * ALL/GEN F,1. . . . . . . . 7–5 * ALL/GEN F. . . . . . . . 7–6 * ALL/GEN F. . . . . . . . 7–7 * ALL/GEN F. . . . . . . . 7–8 * ALL/GEN F,1. . . . . . . . 7–9 * ALL/GEN F. . . . . . . . 7–10 * ALL/GEN F. . . . . . . 8–1 * ALL/GEN F. . . . . . . . CC 8–2 * ALL/GEN F. . . . CC 8–3 * ALL/GEN F. . . . CC 8–4 * ALL/GEN F. . . . CC 8–5 * ALL/GEN F. . . . CC 8–6 * ALL/GEN F. . . . CC 8–7 * ALL/GEN F. . . . CC 8–8 * ALL/GEN F. . . .

� – Replace with page from Flight Supplement* – Omit from flight book

ENT/ALL/GEN F,1

ix ENT/ALL/GEN F

CC 8–9 * ALL/GEN F. . . . CC 8–10 * ALL/GEN F. . . CC 8–11 * ALL/GEN F. . . . CC 8–12 * ALL/GEN F. . . CC 8–13 * ALL/GEN F. . . CC 8–14 * ALL/GEN F. . . CC 8–15 * ALL/GEN F. . . CC 8–16 * ALL/GEN F. . . CC 8–17 * ALL/GEN F. . . CC 8–18 * ALL/GEN F. . . CC 8–19 * ALL/GEN F,1. . . CC 8–20 * ALL/GEN F. . . CC 8–21 * ALL/GEN F. . . CC 8–22 * ALL/GEN F. . . 8–23 *� ALL/GEN F. . . . . . . 8–24 *� ALL/GEN F. . . . . . .

* – Omit from flight book� – Replace with page from Flight Supplement

ENT/ALL/GEN F,1

x ENT/ALL/GEN F

ENTRY CUE CARDSTitle Ref. Page Card No.

Deorbit Burn Flight Rules(Front) CC 8–2 ENT–1a/D/I. . . . . . . . . . . . . . . . . . . . . (Back) CC 8–3 ENT–1b/D/I. . . . . . . . . . . . . . . . . . . . .

Deorbit Burn (RCS)(Front) (Top) CC 8–4 ENT–3a/D/K. . . . . . . . . . . . . . . (Front) (Bottom) CC 8–5 ENT–3aa/D/K. . . . . . . . . . . . (Back) (Top) CC 8–6 ENT–3b/D/D. . . . . . . . . . . . . . . . (Back) (Bottom) CC 8–7 ENT–3bb/D/D. . . . . . . . . . . .

Deorbit Burn (2 Eng)(Front) (Top) CC 8–8 ENT–4a/D/K. . . . . . . . . . . . . . . (Front) (Bottom) CC 8–9 ENT–4aa/D/I. . . . . . . . . . . .

Deorbit Burn (1 Eng)(Back) (Top) CC 8–10 ENT–4b/D/I. . . . . . . . . . . . . . . . (Back) (Bottom) CC 8–11 ENT–4bb/D/J. . . . . . . . . . . .

Unbalanced Prplt Deorbit Burn(Front) (Top) CC 8–12 ENT–5a/D/L. . . . . . . . . . . . . . . (Front) (Bottom) CC 8–13 ENT–5aa/D/M. . . . . . . . . . . .

Deorbit Burn (Mixed Xfeed)(Back) (Top) CC 8–14 ENT–5b/D/I. . . . . . . . . . . . . . . . (Back) (Bottom) CC 8–15 ENT–5bb/D/I. . . . . . . . . . . .

Entry Maneuvers(Front) CC 8–16 ENT–6a/E/L. . . . . . . . . . . . . . . . . . . . . (Back) CC 8–17 ENT–6b/E/Q. . . . . . . . . . . . . . . . . . . . .

Entry NO–GO Checklist(Front) CC 8–18 ENT–7a/E/I. . . . . . . . . . . . . . . . . . . . .

ADTA Mgmt (Back) CC 8–19 ENT–7b/E/N. . . . . . . . . . . Mach �

(Front) CC 8–20 ENT–8a/A,E/C. . . . . . . . . . . . . . . . . . . . . (Back) CC 8–20 ENT–8b/A,E/B. . . . . . . . . . . . . . . . . . . . .

Deorbit Burn Monitor (Front) see flt suppl flt suppl. . . . . . . . . . . . . . . . . . . . .

OMS Failures (Back) see flt suppl flt suppl. . . . . . . . . . Entry Control (Front) CC 8–21 ENT–10a/A,E/A. . . . . . . . . . Entry Control (Back) CC 8–22 ENT–10b/A,E/A. . . . . . . . . .

ENT/ALL/GEN F,1

xi ENT/ALL/GEN F


xii ENT/ALL/GEN F


(Replace with pages FS xii thru FS xiv)

xv ENT/ALL/GEN F

CONTENTS PAGE

DEORBIT MNVR PADS 1–1. . . . . . . . . . . . . . . . . . . . . . . . . . . . .

OMS PRPLT AND DEL PADS 2–1. . . . . . . . . . . . . . . . . . . . . . . .

DEORBIT BURN 3–1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OMS BURN PREP (CIL) 3–9. . . . . . . . . . . . . . . . . . . . . . . . . . OMS/RCS POST BURN RECONFIG (CIL) 3–32. . . . . . . . .

ENTRY CUE CARDS 4–1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . h = 10K LES VISORS (HC) 4–5. . . . . . . . . . . . . . . . . . . . . . .

POST LANDING PROCEDURES 5–1. . . . . . . . . . . . . . . . . . . . .

1–ORBIT LATE DEORBIT PROCEDURES 6–1. . . . . . . . . . . .

SWITCH LIST AT WHEELS STOP EGRESS 7–1. . . . . . . . . .

ENTRY CUE CARD CONFIG 8–1. . . . . . . . . . . . . . . . . . . . . . . .

xvi ENT/ALL/GEN F


EN

T/A

LL

/GE

N F

1–

1

MNVRPADS

DEORBIT MNVR PAD

1OMS BOTH

2

3

4RCS SEL

6

TRIM LOAD

5TV ROLL

( )�

7 ( )�

8 ( )�

9

10 / : :�

14

TGT PEG 4

15 ( )�

16�

17�

18 ( )

24R

25P

26Y

BURN ATT

:

L OMS � RCS

R OMS � RCS

NONE

�

XVGO ( )

YVGO ( )

ZVGO ( )

�

�

�

( )TGT

HPHA

:∆VTOT

TGO

RCS I’CNCT:

NOTES

L

R

P

LY

RY

WT

TIG

C1

C2

HT

�T

PRPLT

REI

TXX

MNVRPADS

EN

T/A

LL

/GE

N F

1–

2

DEORBIT MNVR PAD

1OMS BOTH

2

3

4RCS SEL

6

TRIM LOAD

5TV ROLL

( )�

7 ( )�

8 ( )�

9

10 / : :�

14

TGT PEG 4

15 ( )�

16�

17�

18 ( )

24R

25P

26Y

BURN ATT

:

L OMS � RCS

R OMS � RCS

NONE

�

XVGO ( )

YVGO ( )

ZVGO ( )

�

�

�

( )TGT

HPHA

:∆VTOT

TGO

RCS I’CNCT:

NOTES

L

R

P

LY

RY

WT

TIG

C1

C2

HT

�T

PRPLT

REI

TXX

PR

PLT

/D

EL

PAD

S

2–1 ENT/ALL/GEN F

OMS PRPLT AND DEL PADS

PR

PLT

/D

EL

PAD

S

2–2 ENT/ALL/GEN F

BURN CARD OMS PRPLT PADDEORBITBURN(1 ENG)

OMS XFEED RETURN at �VTOT =

or at %

DEORBITBURN(RCS)

RCS I’CNCT TK SW at �VTOT =

OMS PRPLT LOW: �VTOT =

UNBALANCEDPRPLTDEORBITBURN

INITIAL CONFIG: TK ISOLs - CL

While feeding 2 OMS from 1 POD:OMS PRPLT FAIL:

Secure OMS

Secure OMS

Interconnect OMS to RCS

THC + X for :

If (XFEED) ENG ‘↓’

When OMS QTY:

5%: OMS TK ISOL (two) - OP

4%: OMS TK ISOL (two) - CL

If (STRAIGHT FEED) ENG ‘↓’

OMS ENG FAIL:At �VTOT =

or at %

TK ISOL (two) - OP

TK ISOL (two) - CL

Return to 2 ENG, 2 POD FLOW:At �VTOT = TK ISOLs - OP

OMS ENG FAIL: (XFEED CUE)

OMS QTY %L or %R

DEORBITBURN(MIXEDXFEED)

FEED FROM GOOD POD:At �VTOT =

or at %

OMS He PRESS (two) - OPTK ISOL (two) - OPXFEED (two) - OP

Secure OMSOMS PRPLT LOW:

AFT RCS RECONFIG at �VTOT =OMS ENG FAIL:

OMS He PRESS (two) - OPTK ISOL (two) - OP

OMS XFEED (two) - CL

:

EI–5 MM303 INRTL ATT

MM304 PREBANK (ENT MNVR Cue Card)

ALTM SET

CLG INIT

EXPECTED AIL TRIM

VREL 1ST REVERSAL

XCG AT TD

LAND SITE 50K

38K

28K

20K

12K

7K

3K

1K

SURFACE

∆T MACH .9 TO HAC

TOT AFT QTY 1 (%)

TOT AFT QTY 2 (%)

PREBANK/FLIP HP

FRCS: DUMP TO % (USE TIME AS CUE)

PRE–DEORBITAPU START: SINGLE APU START, ATTEMPT

APU START SEQUENCE

DEORBITBURN CUE CARD:

OMS TIG SLIP – NO EXEC > TIG +

RCS DOWNMODING

STOP/CONTINUE CUES: L OMS FAIL HP

STOP/CONTINUE CUES: R OMS FAIL HP

S FAIL HPOMS ENG FAIL XFEED QTY CUE

ENGINE FAIL HP

SAFE HP

::

APU(s)

AFT HP B/U SITE

OX FU

P YR

RL

�

OVHDL deg

STRTR TAC

MAX Nz Nz LIMIT

AIMPOINT SPEEDBRAKE

CLOSE–IN

% @ 3K

REMARKS:

THEN

%R%L

RL �

�

RWY

MLS

�

:

�

NOM

S.F.

NOM

/

/

/

/

/

/

/

/

/

ENTRY/LANDING

:

2–3 ENT/ALL/GEN F

DEL PAD

ENT/ALL/GEN F,1

2–4 ENT/ALL/GEN F


2–5 ENT/ALL/GEN F


2–6 ENT/ALL/GEN F


3–1 ENT/ALL/GEN F


3–2 ENT/ALL/GEN F


(Replace with pages FS 3–2 thru FS 3–4)

3–5 ENT/ALL/GEN F

1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC DEORB MNVR COAST

TIG–46

B FINAL DEORB UPDATE/UPLINK

MCC UPDATE:DEL PADOMS PRPLT PAD

MCC UPLINK:PASS SVBFS SVPASS TGTBFS TGTBFS IMU GYRO/ACCEL

C G50 �LAND SITE per DEL PADSET TACAN tw

On MCC GO:C CRT1 LOAD – ITEM 22 EXEC

TIMER – ITEM 23 EXEC

CRT1,3 �PASS & BFS TGTs per MNVR PAD:BURN ATT∆VTOTTGOHA HP

G51 SEL ATMOSPHERE:incl ≤ 50° ITEM 22 EXECincl > 50° SEL ITEM NR (table)

Hemi Jan Feb Mar Apr May Jun Jul Aug Sep Oct Nov Dec

N Desc 23 23 23 23 22 24 24 24 22 23 23 23

S Asc 24 24 22 23 23 23 23 23 23 23 22 24

N Asc

S Desc22

3–6 ENT/ALL/GEN F


C OMS TVC GMBL CHECK (Perform during S–band AOS)

CRT1 SECONDARY CHECKPerform SEC L,R then PRI L,R GMBL CK

**

If down arrow(s) or Ms:Select good GMBL

**

MS LES Pressure Integrity Check

P APU PRE–START (Perform during S–band AOS)

R4 �HYD BRAKE ISOL VLV (three) tb – CL�LG EXTEND ISOL VLV tb – CL

*****

R2R4

R2

If tb not CL:(Aff) HYD CIRC PUMP – ON(Aff) ISOL VLV – CLHold 5 sec,�tb – CLHYD CIRC PUMP – OFF

*****

R2 BLR N2 SPLY (three) – ONBL �� PWR (three) – ONBL �� CNTLR/HTR (three) – B

�APU AUTO SHUTDN (three) – ENAAPU CNTLR PWR (three) – ONHYD MN PUMP PRESS (three) – LO

�APU SPEED SEL (three) – NORMAP �� OPER (three) – OFFAP �� FUEL TK VLV (three) – CL

�cb FUEL TK VLV ENABLE (six) – CL

3: BFS, SM SYS SUMM 2P R2 APU FUEL TK VLV (three) – OP

�APU/HYD RDY tb (three) – grayAPU FUEL TK VLV (three) – CL

2: GNC 50 HORIZ SIT3: BFS, GNC 50 HORIZ SIT

3–7 ENT/ALL/GEN F

1: GNC DEORB MNVR COAST 2: GNC 50 HORIZ SIT3: BFS, GNC 50 HORIZ SIT

HORIZ SIT CONFIG

ALTM – ITEM 9

PASS ITEM BFS ITEM PTI INH �1LAND SITE (DEL PAD) �41 �41RWY (DEL PAD) �3 �3

�4 �4TACAN (DEL PAD) �5 �5RA blank �46TAEM TGT

G&N OVHD �6 blankHSI blank blankXEP NEP �7 NEP �7AIM (DEL PAD) NOM

(or CLSE)�8 NOM

(or CLSE)�8

SPDBK NOM �39TAC INH �20 INH �20GPS INH �43 INH �43DRAG H AUT �22 AUT �22ADTA H INH �26 INH �26ADTA TO G&C INH �29 AUT �28DES any failed TACANs � �

TAC DELTA �35AIF G INH �48

**

If BFS engaged:Set BFS HSD ITEMs to PASS config

**

.+

3–8 ENT/ALL/GEN F

1: GNC DEORB MNVR COAST 2: GNC 50 HORIZ SIT3: GNC 51 OVERRIDE

�� ELEVON AUTO – ITEM 17 (*)�� SSME REPOS – ITEM 19 (ENA)�� WRAP MODE – ITEM 45 (ENA)

If PLB holding > 10K lb:FILTER ALT – ITEM 21 EXEC (*)

3: BFS, GNC 51 OVERRIDE

�� ELEVON AUTO – ITEM 17 (*)�� SSME REPOS – ITEM 19 (ENA)�� WRAP MODE – ITEM 45 (ENA)

If PLB holding > 10K lb:�� FILTER ALT – ITEM 21 (*)

**

DES any failed/comm faultedIMU, RGA, AA, or SURF feedback

**

2: GNC DEORB MNVR COAST

3: BFS, GNC DEORB MNVR COAST

�� BFS GMBL sel config same as PASS GMBLsel config

3–9 ENT/ALL/GEN F


P OMS BURN PREP

CRT2 OMS ENG TRIMS2 ENG BURN:

�TRIM LOAD per MNVR PAD or:L,R – ITEM 6 +0.0 –5.7 +5.7 EXEC

1 ENG BURN:�TRIM LOAD per MNVR PAD or:

P – ITEM 6 +0.0 EXECGood eng Y:

LY – ITEM 7 +5.2 EXECRY – ITEM 8 –5.2 EXEC

XFEED: Failed engine prop togood engine

RCS DEORBIT OR RCSHe/PRPLT TK FAIL

Do not terminate OMS/RCSInterconnect

O7 AFT L,R RCSHe PRESS (four) – OP (tb–OP)TK ISOL (six) – GPC (tb–OP)XFEED (four) – GPC (tb–CL)

�MSTR RCS XFEED – OFF

O8 L,R OMS�He PRESS/VAP ISOL (four) – CL�TK ISOL (four) – OP (tb–OP)�XFEED (four) – CL (tb–CL)

FWD RCSHe PRESS (two) – OP (tb–OP)

3–10 ENT/ALL/GEN F


RCS BURN PREPP O8 L,R OMS

�He PRESS/VAP ISOL (four) – CL�TK ISOL (four) – OP (tb–OP)

L OMS XFEED (two) – OP (tb–OP)�R OMS XFEED (two) – CL (tb–CL)

O7 AFT L,R RCSXFEED (four) – OP (tb–OP)TK ISOL (six) – CL (tb–CL)

MS3 Remove and stow Side Hatch UV Filterand Locking Device, and Pyro BoxSafing Pin

TIG–25 VENT DOOR CLOSE

NOTEVENT DOOR CLOSE must beperformed prior to MM302 transition

2: GNC 51 OVERRIDE

CRT2 VENT DOOR CNTL CLOSE – ITEM 44 EXEC


1: GNC DEORB MNVR COAST 2: GNC 51 OVERRIDE3: BFS, GNC DEORB MNVR COAST

2: GNC DEORB MNVR COAST

B DEORB UPDATE/UPLINK (if reqd)MCC UPDATE:

DEL PADOMS PRPLT PAD

MCC UPLINK:PASS,BFS SVPASS,BFS TGT

C G50 �LAND SITE per DEL PADSET TACAN tw

MS1/MS2 SEAT INGRESS

On MCC GO:CRT1 LOAD – ITEM 22 EXEC

TIMER – ITEM 23 EXECCRT1,3 �� PASS & BFS TGTs per MNVR PAD:

BURN ATT∆VTOTTGOHA HP

C CRT1 GNC, OPS 302 PRO

1: GNC DEORB MNVR COAST 2: GNC 51 OVERRIDE3: BFS, GNC DEORB MNVR COAST

MCC/CREW GO/NO–GO FOR DEORBITBURN

*****

P

C

R2

CRT1

IF NO–GO FOR DEORBITBURN:

HYD MN PUMP PRESS (three) –NORM

GNC, OPS 301 PRO

*****

IF 1 ORBIT DELAY:Go to section 6, 1–ORB LATE


1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC DEORB MNVR EXEC

IF 24–HR EXTENSIONP O7 AFT L,R RCS

He PRESS A (two) – GPC (tb–OP)He PRESS B (two) – CL (tb–CL)TK ISOL (six) – OP (tb–OP)XFEED (four) – CL (tb–CL)

O8 FWD RCSHe PRESS A – GPC (tb–OP)He PRESS B – CL (tb–CL)

C6 Unstow ORB PKT C/LTerminate Deorbit Procedures,go to DEORB PREP, D/O PREPBACKOUT

TIG–20> MNVR TO DEORBIT BURN ATT

C C3 �DAP: AUTOB F6/F8 �ADI ATT (two) – INRTL

A �� ERR (two) – MEDA �� RATE (two) – MED

C MNVR to BURN ATT(�ADI ATT with CRT BURN ATT)

B Copy last DEL PAD and OMS PRPLT PADdata on DEORBIT BURN Cue Cards

F6/F8 �DEORBIT BURN and DEORBIT BURNMONITOR Cue Cards installed

A14 RCS/OMS HTRFWD RCS – OFFL POD (two) – A OFF,B OFFR POD (two) – A OFF,B OFFOMS CRSFD LINES (two) –A AUTO,B AUTO

FWD RCS JET 5 (one) – OFFAFT RCS JET 5 (one) – OFF

A3–13 ENT/ALL/GEN F

1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, SM SYS SUMM 2

TIG–5> P SINGLE APU START (Attempt one APU)

R2 APU FUEL TK VLV – OPAPU OPER – START/RUN

MDU �HYD PRESS ind – LO green

***

If no start, shut down APU(ENT PKT, APU/HYD)

Do not execute Deorbit Burn

***

R2 �HYD CIRC PUMP (three) – OFF

3: BFS, GNC SYS SUMM 2

C �BURN ATT � 5°

B Go to DEORBIT BURN (Cue Card)

MEDSENT/MEDS/GEN F



TIG–5> P SINGLE APU START (Attempt two APUs)


MDU �HYD PRESS ind – LO green

************

If no start:APU OPER – OFFStart another APU

If second APU starts,shut down unstarted APU(ENT PKT, APU/HYD) >>

If neither starts,� Do not start third APU� Do not execute Deorbit Burn� Shut down unstarted APUs

(ENT PKT, APU/HYD) >>

************





MEDSENT/MEDS/GEN F

B3–13 ENT/ALL/GEN F


TIG–5> P SINGLE APU START (Attempt one APU)


F8 �HYD PRESS ind – LO green

***

If no start, shut down APU(ENT PKT, APU/HYD)

Do not execute Deorbit Burn

***





ENT/NOM/GEN FNOM



TIG–5> P SINGLE APU START (Attempt two APUs)


F8 �HYD PRESS ind – LO green

************

If no start:APU OPER – OFFStart another APU

If second APU starts,shut down unstarted APU(ENT PKT, APU/HYD) >>

If neither starts,� Do not start third APU� Do not execute Deorbit Burn� Shut down unstarted APUs

(ENT PKT, APU/HYD) >>

************





ENT/NOM/GEN FNOM

BU

RN

CA

RD

S

3–15 ENT/ALL/GEN FMS ONLY

DEORBIT BURN CARDS

BU

RN

CA

RD

S


APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

DPS3 RDNT fail, Split X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

4 1 GPC X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

6 GPC BITE (Multiple GPCs) X. . . . . . . . . . . . . . . . . . . . . . . . . . .

ECLS7 2 Av Bay Fans in Bay 3 X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

8 2 Av Bay Fans in Bay 1 or 2 X. . . . . . . . . . . . . . . . . . . . . . . . . . .

ELEC9 H2 Manf or TK leak (not in

depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . . .

10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

11 CNTL CA1 (No BFS Engage in GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

12 Multi Φ AC BUS (unshorted) X. . . . . . . . . . . . . . . . . . . . . . . . . . .

GNC13 1 MLS (if reqd), IMU, or TACAN

(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

17 3 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . . .

21 Both OMS Eng fail X 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

22 Prplt Lk after LAST LOS . . . . . . . . . . . . . . . . . . . .

AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . . .

24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

25 1 AFT RCS PROP TK fail X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

COMM26 MCC GO for DEORBIT not rcvd X. . . . . . . . . . . . . . . . . . . . .

FAILURE

PRE TIG POST TIG

Delay (max)

OneOrbit

OneDay

StopBurn,> Safe

HP

ENT–1a/D/I

perigee adjust

1 Stop Burn > OMS PRPLT FAIL HP (Ref: DEL PAD/BURN Card)2 Stop Burn > OMS ENG FAIL HP (Ref: DEL PAD/BURN Card)

HOOKVELCRO

HOOKVELCRO

DEORBIT BURN FLIGHT RULESONE–ORBIT LATE AVAILABLE


APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


4 1 GPC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


ECLS7 2 Av Bay Fans in Bay 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .



depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . .

10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

11 CNTL CA1 (No BFS Engagein GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

12 Multi ΦAC BUS (unshorted) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

17 3 ADTAs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . .



AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . .

24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

25 1 AFT RCS PROP TK FAIL X. . . . . . . . . . . . . . . . . . . . . . . . . . .


FAILURE

PRE TIG POST TIGDelay(max)OneDay

StopBurn,> Safe

HP

ENT–1b/D/I

perigee adjust


HOOKVELCRO

HOOKVELCRO

DEORBIT BURN FLIGHT RULESONE–ORBIT LATE NOT AVAILABLE


�MM302 �OMS BOTHEnter TGO + 5 sec

�TRIM per MNVR PAD or P +0.0, LY –5.7, RY +5.7L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OP

�DAP – AUTO(PASS)/DISCADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ON

TIG–2 OMS ENG (two) – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)

If no OMS ignition: APUs – SHUT DNOMS PRPLT FAIL:

Failed OMS ENG – OFFSTOP BURN:

Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS

CONTINUE BURN:

ITEM 18 +0 EXECWhen good OMS QTY:

5%: L,R OMS XFEED (four) – OP4%: Good OMS TK ISOL (two) – CL

If OMS Pc < 80 or OMS TEMP, OMS ENG – OFF

�ADI – LVLH, center needlesRCS COMPLETION

OMS ENG FAIL:Failed OMS ENG – OFFOMS XFEED at 1/2 ∆VTOT at fail

OMS Xor OMS QTY

2nd OMS FAIL (ENG or PRPLT):

Failed OMS ENG – OFFIf PRPLT FAIL:

Secure aff OMS ITEM 18 +0 EXEC

STOP BURN:

APUs – SHUT DN

CONTINUE BURN:

�ADI – LVLH, center needlesInterconnect good OMS to RCS

THC +X (�OMS% vs RCS Burn Time)RCS I’CNCT TK SW (N/A PRPLT FAIL)RCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG

RCS COMPLETION

********************************************

********************************************

DEORBIT BURN (2 ENG)

EitherPRPLT FAIL(SAFE) HP

BothENG FAIL

HP

R OMSFAIL HP

L OMSFAIL HP

ENT–4a/D/K

% R%L or

: )


RCS COMPLETION:THC +X to TGT HP or TOT AFT QTY 1

THC +X to PREBANK/FLIP HP orAt AFT QTY 1 TOT AFT QTY 2

if CUR HP: PREBANK/FRCS COMPLETION

PREBANK/FLIPHP

AFT

HP

TGTHP

FRCS COMPLETION (if applicable):MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)

CUTOFF+ :02 OMS ENG(s) – OFF (If < 3 IMU, at

* AFT RCS RECONFIG if INTERCONNECT *Trim X,Z residuals < 2 fps (< 0.5 fps if shallow)

********************

********************

THC +X to TGT HP

ENT–4aa/D/I

% then

%

):

PREBANK/FRCS COMPLETION


�MM302 �OMS L or R�OMS BURN CONFIG (L or R XFEED)

Enter TGO + 10 sec�TRIM per MNVR PAD or P +0.0, LY +5.2, RY –5.2

L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . .


TIG–2 Good OMS ENG – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)

* If no OMS ignition: APUs – SHUT DN *

OMS XFEED RETURN at ∆VTOT =

orL,R OMS TK ISOL (four) – OPL,R OMS XFEED (four) – CL

OMS PRPLT FAIL:OMS ENG – OFF

STOP BURN:APUs – SHUT DN

SAFE Secure aff OMSHP

CONTINUE BURN:Secure aff OMSITEM 18 +0 EXEC


THC +X(�OMS% vs RCS Burn Time)AFT RCS RECONFIG

RCS COMPLETIONOMS ENG FAIL:

OMS ENG – OFFSTOP BURN:

ENG APUs – SHUT DNFAILHP

CONTINUE BURN:�ADI – LVLH, center needles

Interconnect OMS to RCSTHC +X(�OMS% vs RCS Burn Time)RCS I’CNCT TK SWRCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG

RCS COMPLETIONRCS +X JET FAIL OFF:

STOP BURN:SAFE APUs – SHUT DN

HPCONTINUE BURN:

ITEM 18 +0 EXECG23 Resel jets

**************************************

**************************************

DEORBIT BURN (1 ENG)

ENT–4b/D/I

):

%at





PREBANK/FLIPHP

AFT

HP

TGTHP


CUTOFF+ :02 OMS ENG – OFF (If < 3 IMU, at


********************

********************

THC +X to TGT HP

ENT–4bb/D/J

% then

%

):



�MM302 �RCS SEL�RCS BURN CONFIG (L OMS I’CNCT)

L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . . .

�DAP – INRTL/DISCADI – LVLH(REF)/MED/MEDFLT CNTLR PWR (two) – ON

TIG THC +X (No deorbit > TIG +

Maintain PITCH ATT ERR ± 3°Monitor ∆VTOT:

RCS I’CNCT TK SW at ∆VTOT =R OMS XFEED (two) – OPL OMS XFEED (two) – CL

OMS PRPLT LOWAFT RCS RECONFIG AT ∆VTOT =RCS COMPLETION

OMS PRPLT FAIL (MULTIPLE JETS FAIL OFF):Secure aff OMS


HPCONTINUE BURN:

ITEM 18 +0 EXECG23 Resel jetsInterconnect good OMS to RCS

THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION

RCS +X JET FAIL OFF:STOP BURN:

SAFE APUs – SHUT DNHP

CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jets

********************

********************

DEORBIT BURN (RCS)

ENT–3a/D/K

: )




THC +X to PREBANK/FLIP HP or

At AFT QTY 1 TOT AFT QTY 2if CUR HP: PREBANK/FRCS COMPLETION

PREBANK/FLIP

HP

AFTHP

TGTHP

FRCS COMPLETION (if applicable):

MNVR to –X Att (pitch up at 3°/sec to VGOz = +1/4 ∆VTOT)THC –X to TGT HP or FRCS depletion (JETS FAIL OFF)

CUTOFF VGOx = 0, release THC

AFT RCS RECONFIGTrim Inplane X,Z residuals < 2 fps (< 0.5 if shallow)

********************

********************

ENT–3aa/D/K

% then

%

THC +X to TGT HP



�TRIM per MNVR PAD or P + 0.0, LY –5.7, RY +5.7�DAP – AUTO(PASS)/DISC

ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONFeed 2 ENG from 1 POD

L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OPL,R OMS TK ISOL (two) – CL (tb–CL)L,R OMS XFEED (four) – OP (tb–OP)


If no OMS ignition: APUs – SHUT DNWhile feeding 2 OMS from 1 POD:

OMS PRPLT FAIL:Failed OMS ENG(s) – OFF

STOP BURN:APUs – SHUT DNSecure OMS

SAFE HP

CONTINUE BURN:ITEM 18 +0 EXECIf Both ENGs ‘↓’:

Secure OMS�ADI – LVLH, center needles


THC +X forAFT RCS RECONFIG

RCS COMPLETION If (XFEED) ENG ‘↓’:

When OMS QTY:5%: OMS TK ISOL (two) – OP4%: OMS TK ISOL (two) – CL



If (STRAIGHT FEED) ENG ‘↓’: OMS ENG FAIL

OMS ENG FAIL (CONTINUE BURN):Failed OMS ENG – OFF

at ∆VTOT =or

TK ISOL(two) – OP

TK ISOL(two) – CL

Return to 2 ENG, 2 POD FLOW at ∆VTOT:L,R OMS TK ISOL (two) – OP (tb–OP)L,R OMS XFEED (four) – CL (tb–CL)

at %

***************************************

***************************************

UNBALANCED PRPLT DEORBIT BURN

ENT–5a/D/L

: )

:


ENT–5aa/D/M

OMS PRPLT FAIL:Failed OMS ENG – OFF

STOP BURN:Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS

CONTINUE BURN:






or OMS QTY



Secure aff OMSITEM 18 +0 EXEC


CONTINUE BURN:

�ADI – LVLH, center needlesInterconnect Good OMS to RCS


RCS COMPLETIONRCS COMPLETION:

THC +X to TGT HP or TOT AFT QTY 1

At AFT QTY 1if CUR HP:

PREBANK/FLIP

HP

AFTHP

TGT

HPFRCS COMPLETION (if applicable):




***********************************************************

***********************************************************

R OMSFAIL HP

L OMSFAIL HP


BothENG FAIL

HP


THC +X to TGT HP

THC +X to PREBANK/FLIP HP orTOT AFT QTY 2PREBANK/FRCS COMPLETION

):

% then

%

%R%L or


�MM302 �OMS L(R) or RCSEnter TGO + 10 sec

�L,R OMS TK ISOL (four) – GPCL,R OM �XFEED (four) – GPC

�tb config from table (OMS SSR–1)�DAP – AUTO(PASS)/DISC

ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONMan repress to maintain good OMS Tk Ps > 234 psi (simo)If OMS BURN INITIATION:

�TRIM per MNVR PAD or: P +0.0, LY +5.2, RY –5.2TIG–2: Good OMS ENG – ARM/PRESS

TIG–2:15 EXEC (No EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)

* If no OMS ignition, APUs – SHUT DN *If RCS BURN INITIATION:

Man repress L,R OMS > L,R RCS TK PsL,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL

TIG–2:00 THC +X (No Deorbit > TIG +Maintain PITCH ATT ERR � 3°

FEED FROM GOOD POD:

at ∆VTOT =or

OMS He PRESS/VAP ISOL (two) – OPOMS TK ISOL (two) – OP (tb–OP)OMS XFEED (two) – OP (tb–OP)SECURE OMS

OMS PRPLT LOWAFT RCS RECONFIG at ∆VTOT =RCS COMPLETION

DEORBIT BURN (MIXED XFEED)

ENT–5b/D/I

at %

: )

: )




SAFE Secure L,R OMSHP

CONTINUE BURN:Secure L,R OMSITEM 18 +0 EXEC


OMS ENG FAIL:OMS ENG – OFF

STOP BURN:ENG APUs – SHUT DN

FAILHP CONTINUE BURN:

Man repress L,R OMS > L,R RCS TK PsFEED FROM GOOD POD:

OMS HE PRESS/VAP ISOL(two) – OP

TK ISOL (two) – OP

OMS XFEED (two) – CL

L,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL

�ADI – LVLH, center needlesTHC +X (�Lowest OMS % vs

RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION



CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jet




PREBANK/FLIPHP

AFTHP

TGTHP



CUTOFF VGOx = 0, Release THC+ :02 OMS ENG(s) – OFF (If < 3 IMU, at


:

**********************************************************

**********************************************************

ENT–5bb/D/I


THC +X to TGT HP

)

%

% then







PO

ST

BU

RN


1: GNC DEORB MNVR EXEC 2: GNC DEORB MNVR EXEC3: BFS, GNC SYS SUMM 2

**********************************

C3O8

F6,F8C3

C3

O8

O7

O8

F6,F8C3

If no OMS IGNITION at TIG:OMS ENG (two) – OFF

�APU – SHUT DNMSTR MADS PWR – OFFL,R OMS

He PRESS/VAP ISOL (four) – CL�XFEED (four) – CL

GNC, OPS 301 PROFLT CNTLR PWR (two) – OFF

�DAP: AUTO�MCC at next AOS

If burn terminated with HP > SAFE HP:�OMS ENG (two) – OFF�APU – SHUT DN

MSTR MADS PWR – OFFOPS 301 PROIf I’CNCT:

DAP: INRTL/PULSEL, R OMS


AFT L,R RCSHe PRESS A (two) – GPC (tb–OP)He PRESS B (two) – CL (tb–CL)TK ISOL (six) – OP (tb–OP)XFEED (four) – CL (tb–CL)

FWD RCSHe PRESS A – GPC (tb–OP)He PRESS B – CL (tb–CL)

FLT CNTLR PWR (two) – OFF�DAP: AUTO�MCC at next AOS on DEORBIT DELAY

of 24 hr

**********************************

MEDSENT/MEDS/GEN F

PO

ST

BU

RN



MS Stow Flight Deck SpOC

B F6,F8 FLT CNTLR PWR (two) – OFFC3 �DAP: AUTO

OMS/RCS POST BURN RECONFIG

P O7 AFT L,R RCS�He PRESS (four) – OP (tb–OP)�TK ISOL (six) – GPC (tb–OP)�XFEED (four) – GPC (tb–CL)

O8 L,R OMSHe PRESS/VAP ISOL (four) – CL

�TK ISOL (four) – OP (tb–OP)

**

If OMS PRPLT FAIL,�Aff TK ISOL (two) – CL

**

XFEED (four) – CL (tb–CL)

O3 RCS/OMS PRESS sell – RCS as reqdRCS/OMS PRPLT QTY sel – RCS as reqd

MEDSENT/MEDS/GEN F

PO

ST

BU

RN



**********************************

C3O8

F7,F8C3

C3

O8

O7

O8

F7,F8C3

If no OMS IGNITION at TIG:OMS ENG (two) – OFF

�APU – SHUT DNMSTR MADS PWR – OFFL,R OMS


GNC, OPS 301 PROFLT CNTLR PWR (two) – OFF

�DAP: AUTO�MCC at next AOS

If burn terminated with HP > SAFE HP:�OMS ENG (two) – OFF�APU – SHUT DN

MSTR MADS PWR – OFFOPS 301 PROIf I’CNCT:

DAP: INRTL/PULSEL, R OMS


AFT L,R RCSHe PRESS A (two) – GPC (tb–OP)He PRESS B (two) – CL (tb–CL)TK ISOL (six) – OP (tb–OP)XFEED (four) – CL (tb–CL)

FWD RCSHe PRESS A – GPC (tb–OP)He PRESS B – CL (tb–CL)

FLT CNTLR PWR (two) – OFF�DAP: AUTO�MCC at next AOS on DEORBIT DELAY

of 24 hr

**********************************

ENT/NOM/GEN FNOM

PO

ST

BU

RN



MS Stow Flight Deck SpOC

B F7,F8 FLT CNTLR PWR (two) – OFFC3 �DAP: AUTO

OMS/RCS POST BURN RECONFIG

P O7 AFT L,R RCS�He PRESS (four) – OP (tb–OP)�TK ISOL (six) – GPC (tb–OP)�XFEED (four) – GPC (tb–CL)

O8 L,R OMSHe PRESS/VAP ISOL (four) – CL

�TK ISOL (four) – OP (tb–OP)

**

If OMS PRPLT FAIL,�Aff TK ISOL (two) – CL

**

XFEED (four) – CL (tb–CL)

O3 RCS/OMS PRESS sell – RCS as reqdRCS/OMS PRPLT QTY sel – RCS as reqd

ENT/NOM/GEN FNOM






1: GNC 53 ENTRY CONTROLS 2: BFS, GNC SYS SUMM 23: GNC DEORB MNVR COAST

EI–20 C SECONDARY ACTUATOR CHECK(if not previously performed and time permits)

NOTEIf port does not bypass during check, bypassaffected port after check:

SEC ACT BYPASS – ITEM 8 +X X EXECIf affected port still does not bypass:

SEC ACT RESET – ITEM 9 +X X EXEC

R2 1. HYD MN PUMP PRESS (one) – NORM

CRT3 2. SURF DRIVE ON, ITEM 39 EXEC (*)Wait at least 5 sec

MDU �SPI: Stop drive test when elevon posnswithin +12° to –27°

SURF DRIVE OFF, ITEM 40 EXEC (*)

CRT1 3. �POS STIM ENA, ITEM 7 – (no *)

C3 4. �FCS CH 1,2,3,4 – AUTO

CRT1 5. SEC ACT CK, CH 1 – ITEM 1 EXEC (*)SEC ACT CK, START – ITEM 5 EXEC (*)

6. �All CH 1 PORTS BYPASS, ‘↓’STOP – ITEM 6 EXEC (*)

C3 7. FCS CH 1 – ORIDECRT1 �All CH 1 PORTS RESET, no ‘↓’

FCS CH 1 – AUTO

8. Repeat steps 5 thru 7 for CH 2,3,4

MEDSENT/MEDS/GEN F


1: GNC 23 RCS 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2

EI–18 P FORWARD RCS DUMP(Use for off–nominal X cg entry)

Determine FWD RCS ‘DUMP TO %’ using lowestof Ox or Fu qty (calculator or DEL PAD)

FOUR JET DUMP:

F RCS PRPLT TO BE DUMPED (%)

0 605040302010

10090807060

0:000:09

0:180:27

0:360:45

0:541:03

1:121:21

1:301:39

1:48

1:481:57

2:062:15

2:242:33

2:422:52

3:00

TIME FROM DUMP INITIATION (M:S)

NOTEDuring dump disregard FRCS qty

MEDS


1: GNC 53 ENTRY CONTROLS 2: BFS, GNC SYS SUMM 23: GNC DEORB MNVR COAST

EI–20 C SECONDARY ACTUATOR CHECK(if not previously performed and time permits)

NOTEIf port does not bypass during check, bypassaffected port after check:

SEC ACT BYPASS – ITEM 8 +X X EXECIf affected port still does not bypass:

SEC ACT RESET – ITEM 9 +X X EXEC

R2 1. HYD MN PUMP PRESS (one) – NORM

CRT3 2. SURF DRIVE ON, ITEM 39 EXEC (*)Wait at least 5 sec

F7 �SPI: Stop drive test when elevon posnswithin +12° to –27°

SURF DRIVE OFF, ITEM 40 EXEC (*)

CRT1 3. �POS STIM ENA, ITEM 7 – (no *)

C3 4. �FCS CH 1,2,3,4 – AUTO

CRT1 5. SEC ACT CK, CH 1 – ITEM 1 EXEC (*)SEC ACT CK, START – ITEM 5 EXEC (*)

6. �All CH 1 PORTS BYPASS, ‘↓’STOP – ITEM 6 EXEC (*)

C3 7. FCS CH 1 – ORIDECRT1 �All CH 1 PORTS RESET, no ‘↓’

FCS CH 1 – AUTO

8. Repeat steps 5 thru 7 for CH 2,3,4

ENT/NOM/GEN FNOM



EI–18 P FORWARD RCS DUMP(Use for off–nominal X cg entry)

Determine FWD RCS ‘DUMP TO %’ using lowestof Ox or Fu qty (calculator or DEL PAD)

FOUR JET DUMP:


0 605040302010

10090807060

0:000:09

0:180:27

0:360:45

0:541:03

1:121:21

1:301:39

1:48

1:481:57

2:062:15

2:242:33

2:422:52

3:00



NOM



TWO JET DUMP:


0 605040302010

10090807060

0:000:18

0:350:53

1:111:28

1:462:04

2:212:39

2:563:15

3:32

3:323:50

4:084:25

4:435:01

5:185:36

5:54



CRT2 FWD RCS ARM – ITEM 36 EXECFWD RCS DUMP – ITEM 37 EXEC

(Start watch)When dump time achieved:

FWD RCS OFF – ITEM 38 EXEC


1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, GNC SYS SUMM 2

ENTRY SW CHECK

C L2 �CAB RELIEF A,B – ENA (tb–ENA)�ANTISKID – ON�NWS – 1�ENTRY MODE – AUTO

3: GNC 51 OVERRIDE

�ROLL MODE – AUTO

B L2/C3 �SPD BK – Full Fwd

P C3 �SRB SEP – AUTO�ET SEP – AUTO

B F6/F8 �AIR DATA – NAVADI ERR – MEDADI RATE – MED

�HSI SEL MODE – ENTRYC F6 HSI SE �� SOURCE (two) – NAV, 1P F8 HSI SE �� SOURCE (two) – NAV, 2

B F3 �TRIM RHC/PNL (two) – INH�PNL (two) – ON

Exercise BRAKE PEDALS



NOTEIf NAVAIDS OFF due to PKT C/LPWRDN, switch ON per PWRDNprocedure

C F6 �RADAR ALTM – 1P F8 RADAR ALTM – 2

O8 �RADAR ALTM (two) – ON�MLS (three) – ON (PASS)�MLS CH (three), FS 3–2

O7 �TACAN MODE (three) – GPCRACA �� ANT SEL (three) – AUTO

�TACAN CH (three), FS 3–2

MEDSENT/MEDS/GEN F



EI–13 REMAINING APUs START

**

If an APU failed to start at TIG–5,start remaining good APU only

**

R2 APU FUEL TK VLV (two) – OP�APU/HYD RDY tb (two) – gray

* If tb – bp, attempt normal start *

APU OPER (two) – START/RUNMDU �HYD PRESS ind (two) – LO green

R2 �RDY tb (two) – bp

*****

If OIL OUT P < 25 and OIL OUTTEMP not increasing after APUstart or no start:

Shut down APU (ENT PKT,APU/HYD)

*****

MEDSENT/MEDS/GEN F



NOTEIf NAVAIDS OFF due to PKT C/LPWRDN, switch ON per PWRDNprocedure

C F7 �RADAR ALTM – 1P F8 RADAR ALTM – 2

O8 �RADAR ALTM (two) – ON�MLS (three) – ON (PASS)�MLS CH (three), FS 3–2

O7 �TACAN MODE (three) – GPCRACA �� ANT SEL (three) – AUTO

�TACAN CH (three), FS 3–2

NOMENT/NOM/GEN F



EI–13 REMAINING APUs START

**

If an APU failed to start at TIG–5,start remaining good APU only

**

R2 APU FUEL TK VLV (two) – OP�APU/HYD RDY tb (two) – gray

* If tb – bp, attempt normal start *

APU OPER (two) – START/RUNF8 �HYD PRESS ind (two) – LO greenR2 �RDY tb (two) – bp

*****

If OIL OUT P < 25 and OIL OUTTEMP not increasing after APUstart or no start:

Shut down APU (ENT PKT,APU/HYD)

*****

NOMENT/NOM/GEN F


1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, SM SYS SUMM 2

*******************

If two APUs operating:�Good HYD MN PUMP PRESS

(two) – LO until EI–6, thenperform SSME HYD REPRESS atEI–6, and delete HYD FLUIDTHERMAL CONDITIONING

If only one APU operating:(Good) APU AUTO SHUTDN (one) – INH

�APU HYD MN PUMP PRESS (one) – LO

Delete SSME HYD REPRESS andHYD FLUID THERMALCONDITIONING

Delay MM304 trans until EI–2Immediately prior to MM304 trans:

(Good) HYD MN PUMP PRESS(one) – NORM

APU SPEED SEL (one) – HI

*******************

HYD MN PUMP PRESS (three) – NORMHYD PRESS ind (three) – HI green

P SSME HYD REPRESS

R2 �HYD MN PUMP PRESS (three) – NORM

**

If HYD SYS 2 or SYS 1 failed,cycle SYS 3

**

R4 HYD MPS/TVC ISOL VLV SYS 2 – OP(MA possible)

Hold 5 sec,�tb – OPWait 10 sec – CLHold 5 sec,�tb – CL

HYD MPS/TVC ISOL VLV SYS 1 – OP(MA possible)

Hold 5 sec,�tb – OPWait 10 sec – CLHold 5 sec,�tb – CL


1: GNC DEORB MNVR COAST 2: GNC DEORB MNVR COAST3: BFS, SM 0 THERMAL

**************

EI–11>P HYD FLUID THERMAL CONDITIONING (MCC CALL)

CRT2 SURF DRIVE ON – ITEM 39 EXECStart TIMER

SPI Observe AEROSURFACES CYCLINGELEV U33 to D18 degRUD R5 to L5 degSPDBK 15 to 10%BDY FLP 93.6 to 3.5%

When SURF DRIVE ON (5 min),CRT2 SURF DRIVE OFF – ITEM 40 EXEC

**************

BURN REPORT (from FS 3–33)

B Stow DEORBIT BURN and DEORBITBURN MONITOR Cue Cards

�ENTRY Cue Cards installed

** ALL

If 8 psi cabin entry, �Tabs/Visor – CL/LES O2 – ON

**

*******************

*******************



G SUIT INFLATION

ALL Load – 1.5 (three turns cw if reqd)

FCS CH CONFIG

If less than four PASS GPCs, config FCSCHs so that each GPC cmds equalnumber of CHs (see table)

GNC 53 CONTROLSConfig SURF FBK (see table)

AVAILABLE FCH CH CONFIG SURF FDBK

GPCs FCS CHs AUTO ORIDE OFF SEL DESEL

3 432

33

2

112

332

1 �1 �2 *

2 432

422

22

422

2 *2 *

� If CH 4 – OFF, do not desel PASS SURF FDBK

MEDSENT/MEDS/GEN F



B F6,F8 FLT CNTLR PWR (two) – ON

EI–7 If Mini–Cam Entry video reqd:MS2 O19 TV PWR – ON

V10 PWR – ONDISPLAY pb – Toggle to display tapecount

REC pb (two) – Press to beginrecording

�LCD displays RED DOT

EI–6 Go to ENTRY MANEUVERS (Cue Card)

MEDSENT/MEDS/GEN F

*******************

*******************



G SUIT INFLATION

ALL Load – 1.5 (three turns cw if reqd)

FCS CH CONFIG

If less than four PASS GPCs, config FCSCHs so that each GPC cmds equalnumber of CHs (see table)

GNC 53 CONTROLSConfig SURF FBK (see table)

AVAILABLE FCH CH CONFIG SURF FDBK

GPCs FCS CHs AUTO ORIDE OFF SEL DESEL

3 432

33

2

112

332

1 �1 �2 *

2 432

422

22

422

2 *2 *

� If CH 4 – OFF, do not desel PASS SURF FDBK

NOMENT/NOM/GEN F



B F7,F8 FLT CNTLR PWR (two) – ON

EI–7 If Mini–Cam Entry video reqd:MS2 O19 TV PWR – ON

V10 PWR – ONDISPLAY pb – Toggle to display tapecount

REC pb (two) – Press to beginrecording

�LCD displays RED DOT

EI–6 Go to ENTRY MANEUVERS (Cue Card)

ENT/NOM/GEN FNOM

EN

T C

UE

CA

RD

S

4–1 ENT/ALL/GEN F MS ONLY

ENTRY CUE CARDS

EN

T C

UE

CA

RD

S




ENTRY NO–GO CHECKLIST

ENT–7a/E/I

AERO AUTO XWINDFAILURE OF: PTI DTO FCS DTO

MODE 1APU/HYD: 1 APU X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

2 APUs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISPLAYS: 2 ADIs X. . . . . . . . . . . . . . . . . . . .

CDR HUD X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTROLLERS:

RHC: 1L X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RHC: 2L & 2R X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RPTA: 2L or 2R X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

GNC: 2 AAs (LAT) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 AAs (NORM) X(M < 2.5) X. . . . . . . . . . . . . . . . . . 2 RGAs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 R DDU PWR SPLY X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 IMU (or 1 IMU + BITE) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADTA NOT INCORP

OR DLMA X (M < 2). . . . . . . . . . . . . . . . . . . . . . . . . . . . MLS NOT INCORP X(< 6K ft). . . . . . . . . . . . . . . . . . . . . 2 FCS CH (same surface) X X. . . . . . . . . . . . . . . . . . . . . . . . . .

DPS: 1 GPC (not restrung) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 GPC (restrung) X. . . . . . . . . . . . . . . . 2 GPC (not restrung) X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 FF X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FF X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

RCS: LEAK (AFT – during ENT) X. . . . . . . 2 YAW JETs (same side) X. . . . . . . . . MIN RCS QTY X. . . . . . . . . . . . . . . . . .

TRIM: Ail > ± 2.0 deg X. . . . . . . . . . . . . . . . . . DOWNMODE:

FCS problem X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AOA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

PLB: PLBD Latch Gang X. . . . . . . . . . . . . . . LDG/DECEL:

Tire Leak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HYD BRAKE ISOL VLV X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . < 100% Brakes X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NWS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

ENERGY – OFF NOMINAL:Roll Ref Alert X. . . . . . . . . . . . . . . . . . . Above Upper Traj Line X. . . . . . . . . . . . MCC GCA, or VEL & PSN

update X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No A/L by 6K ft X. . . . . . . . . . . . . . . . . . . . . . . . . . . . .

DATA: OPS RECORDERS X(LOS). . . . . . . . . . . . XWIND:

< 10 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 15 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 10 Knots Gust X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

GROUND SYSTEMS:No Runway Aim Point X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

NOTES

1 Consider runway redesignation (M > 6) to avoid Xwind landing2 GO if PAPI and BALL BAR available3 Pitch AUTO mode NO–GO for M < 2.54 GO if only string 4 affected

4

4

2

3

3

3


ENTRY MANEUVERS

FLIGHTCONDITIONS MANEUVER

EI–5�LVLH ATT

GNC, OPS 304 PROIf PREBANK, R/Y – CSSRoll at 1°/sec toMaintain PREBANK ± 5°

If previous OMS OX TK or He TK or RCS OX TKleak: G51 VENT DOORS – OP

PTI – ENA at EI–5 when applicable

***

***

q = 1– (AOA) HYD MN PUMP PRESS (three) – NORM

‘GuidanceBox’ @

q ∼8or

D ∼3

–

CLOSED LOOP GUIDANCE ____:____:____If PREBANK: P,R/Y – AUTO

Begin AIL trim monitoring* *

D = 11 �DRAG H (FORCE if editing)V = 19K �MPS/TVC ISOL VLV – CLV = 15K �NAVAIDS (I/O RESET if reqd)

If ELS: UHF MODE – G T/R* *

V = 12K RAD BYP VLV MODE (two) – AUTOCNTLR LOOP (two) – AUTO B(A)

V = 10K �SPDBK to 81%

∆Az = 10.5° FIRST ROLL REVERSAL

ENT–6a/E/L


ENT–6b/E/Q(Partial)


V = 7K �TACAN status

V = 5K ADTA PROBES – DEPLOY (�HEAT)Begin AIL and RUD trim monitoring

M = 2.7�APUs

HUD PWR (two) – ON

* If M < 2.5; P CSS for ADTA to G&C incorp *

M = 2.0 Ensure ADTA to G&C else �Theta limits

M = 0.9 P, R/Y – CSS as reqd�SPDBK CMD vs POS�R FLT CNTLR – ON�NWS – 1

Lock Inertia Reels

.MAX Nz

M = 0.7 �LG EXTEND ISOL VLV – OP

h = 15K �MLS

h = 10K �A/L, TABS/VISORS – CL/LES O2 – ON (KSC)

h = 2K LANDING GEAR ARM pb – ARM

h = 300 LANDING GEAR DN pb – DN

MAIN GEAR TD �SPDBK – 100%

V = 195 KEAS DRAG CHUTE pb (two) – ARM, DPY (simo)

V = 185 KEAS DEROTATE

NOSE GEAR TDSRB SEP – MAN/AUTO and depress pb

�Auto Load Relief�HYD BRAKE ISOL VLV (three) – OP

MIDFIELD andV < 140 KGS BRAKE as required (8–10 fps2, –0.25 to –0.3G)

* If 5K’ remaining and V > 140 KGS – MAX BRAKING *

V = 60 KGS DRAG CHUTE JETT pb – JETT

V = 40 KGS BRAKE < 6 fps2 (–0.2G) (Antiskid cutout)

WHEEL STOP Go to ENT C/L, POST LANDING PROCEDURES



4–7 ENT/ALL/GEN F


4–8 ENT/ALL/GEN F


EN

TR

YM

ISC


50K

38K

28K

20K

12K

7K

/

/

/

/

/

/

/

ENT–6b/E/Q

SURF /

3K

/1K

DRAG CHUTE DEPLOYMCC Call Flight ConditionEarly Main Gear TDNOMINAL 195 KEAS

If leaking/flat tiredelay derot 10 kts

Late Post–Nose Gear TDXwind DTO

EmergencyOnly

No DeployExcept CDR call

NO DEPLOYprior to MGTD> 230 KEAS< 80 KGSXwind > 15 kts

(Partial)

EN

TR

YM

ISC








ENTRY CONTROLARCS QTY (L + R) < 10%ARCS QTY = 0 & JETSFAIL OFF

1. ENTRY MODE – NO Y JET(R/Y CSS; expect sluggish control)

q ≥ 20 & M > 6 2. G51 ELEVON FIXED – ITEM 18 EXEC (*)

CONTROLPROBLEMS* &ARCS QTY > 0

3. ENTRY MODE – AUTOWhen control regained:

4. ENTRY MODE – NO Y JET5. �AIL trim

M < 6 & ARCS QTY > 0 6. ENTRY MODE – AUTOM < 5 7. TRIM/RHC PNL – ENA

8. TRIM ROLL – away from AIL trim (to < 1)*Region of least margin: M 12–8

AIL TRIM ≥ 3°TAL 1. G51 WRAP MODE – ITEM 45 EXEC (ACT)AIL trim = 5 2. BF – MAN

3. BF – UP (to 0%)NO Y JET 4. Perform roll reversals at 3°/s (expect sluggish control)M < 13 &AIL trim = 5

5. P – CSS6. Fly α per schedule:

M 12 11 10 9 8–6 5α 37 36 35 33 30 26

M < 5 7. TRIM/RHC PNL – ENA8. TRIM ROLL – away from AIL trim (to < 1)9. P – AUTO

M < 2 10. BF – AUTOENT–10a/A,E/A

HIGH–FREQ OSC OR SURF/JET CYCLEReturning PL> 10K lbs

1. G51 �FILTER ALT – ITEM 21 (*)

2. P, R/Y – CSSOsc/Cycle continues 3. ENTRY MODE – LO GAIN

Osc/Cyclestops

4. ENTRY MODE – AUTO5. P, R/Y – AUTO

ENT–10b/A,E/A




RATIO < 1

MCC: AUTOor INH*

COMMOK

NOCOMM

IF BADADTA

RATIO > 1

G&CNAV

AUTO

TACANOK

MCC: INH

IF BAD NAVSTATE

MCC:FORCE

NO TACANADTA

ERRATICADTA

STEADYINH AUTO FORCE

Two or moregood ADTAs

Evaluate h,�,MMCC:

AUTO (G&C)

Evaluate h,�,MIf reasonable:

AUTO (G&C)

*(If ADTA H will degrade NAV state)

ADTA MGMT

V = 6K NO COMM TACAN MGMT

If 1st acq –FORCE

IF NOT –ZERO �STATE

RATIO< 1 RATIO > 1 ONE TACAN

LOCKED NO LOCK

AUTO TROUBLESHOOT BELOW V =5.5K

DESELECTMISSINGTACANS,then –AUTO

BELOW V =5.5K

TOGGLETACAN

IF BADTACAN

IF BAD NAVSTATE

AUTO

For � STATE UPDATES (on MCC call):P, R/Y – CSSDRAG H, TACAN, ADTA – INHOn MCC call, back to AUTO

NAV DELTA PAD

�Z 15 ( )

( )

( )

( )

( )

( )�X 10

�Y 11

�Z 12

�X 13

�Y 14



PO

ST

LD

G

5–1 ENT/ALL/GEN F

POST LANDING PROCEDURES

PO

ST

LD

G

5–2 ENT/ALL/GEN F

********************************************

LOSS OF COMMIn event of loss of comm (day or night), the following signalswill be utilized to indicate onboard status to convoy:

Crew should continue signals until acknowleged by convoyFrom Crew (with Mini Mag light stowed in ACES orSpotlight stowed in volume 3b)Crew OK Circular motionOMS/RCS & Hatch safed Circular motionAPU shutdn Circular motionCrew needs assistance;will open/blow hatch Vertical motion

Crew needs assistance;will not open/blow hatch Horizontal motion

From ConvoyConvoy will acknowledge crew signals with sequence ofthree flashes of headlights on convoy vehicle

Continuous flashing – Emer pwrdn and egress

*************************************************EXPEDITED PWRDNAccomplish for:

� Loss of all comm, including hand signals, withconvoy elements

� Loss of telemetry and onboard systems monitoringvisibility

� Fuel leak (OMS, RCS, or APU) if:– Nonisolatable, or– Leak occurs during RTLS, TAL, AOA, or

POST D/O TIG� Fire Suppression Bottle discharged during entry for

confirmed or suspected fireIf APU, OMS, RCS Fuel Leak:

APUs OFF ASAPAs time permits:

RCS,OMS SAFING (RJDs), 5–4GPC DEACT

O6 GPC MODE 1,2,3,4,5 (five) – STBY (tb–bp)O6 GPC MODE 1,2,3,4,5 (five) – HALT

ET UMBILICAL DOOR OPENING, 5–5 (RTLS/TAL only)‘MODE 5’ POST LANDING EGRESS Cue Card (CDR orMCC call) then EMER PWRDN Cue Card

NOTEBefore declaring loss of comm, attempt to contactconvoy on 259.7 using PRC–112 radio channel A

********************************************

ENT/ALL/GEN F,1


1: GNC VERT SIT 2 2: GNC SYS SUMM 13: BFS, GNC VERT SIT 2

POST LANDING

WARNINGAPUs OFF ASAP for APUHydrazine, OMS, RCS (FWD orAFT), or MPS propellant leak

00:00 After orbiter stops:C Report, “WHEELS STOP”

Establish COMM with NCC

L2 SPD BK – MAN, full fwdNWS – OFF

P If RTLS or TAL abort:Perform ET UMBILICAL DOOROPENING, 5–5

R2 �APU AUTO SHUTDN (three) – ENAAP �� SPEED SEL (three) – NORM

R1 �AC BUS SNSR (three) – AUTO

C F6 FLT CNTLR PWR – OFF

B F3 HUD PWR (two) – OFF

If ELS:P C3 MSTR MADS(OEX) PWR – OFF

(OEX for OV102)DoD ELS, MCC call DoD OSC onNCC

NOTEMCC will report “GO/NO–GOTO DOFF SUITS” (post safetyassessment)

ENT/MEDS/GEN FMEDS



CDRNOTE

CDR activities are now on evennumbered pages and PLTactivities on odd numbered pages

RCS, OMS SAFING (RJDs)C3 �OMS ENG (two) – OFFO14:F RJD DRIVER (nine) – OFFO15:F RJD LOGIC (eight) – OFFO16:F OMS ENG VLV (two) – OFF

C,P,MS DRAG CHUTE SAFING(Not performed if ELS)

O15:E cb MNB DRAG CHUTE SYS 2 – opO16:E cb MNC DRAG CHUTE SYS 1 – opF2,F3, �DRAG CHUTE PBI lts (six) – off F4

DEACT AIR DATA PROBE HTRSC3 �AIR DATA PROBE (two) – DPY

C,P,MS LANDING GEAR SAFING(Not performed if ELS)

R14:F cb ESS 1BC LDG GEAR ARM/DNRESET – cl

NOTESM0 TIRE PRESS msgs occurwhen LG ARM/DN RESETperformed

A12 LG ARM/DN RESET – RESETF6,F8 �LDG GEAR pb (four) – lt offA12 LG ARM/DN RESET – dnR14:F cb ESS 1BC LDG GEAR ARM/DN

RESET – op

Check with MS3. Report to MCC: “RJDsOFF, SIDE HATCH, DRAG CHUTE,AND LANDING GEAR SAFED” (MCCreport to NCC) MEDS



POST LANDING

WARNINGAPUs OFF ASAP for APUHydrazine, OMS, RCS (FWD orAFT), or MPS propellant leak

00:00 After orbiter stops:C Report, “WHEELS STOP”

Establish COMM with NCC

L2 SPD BK – MAN, full fwdNWS – OFF

P If RTLS or TAL abort:Perform ET UMBILICAL DOOROPENING, 5–5

R2 �APU AUTO SHUTDN (three) – ENAAP �� SPEED SEL (three) – NORM

R1 �AC BUS SNSR (three) – AUTO

C F7 FLT CNTLR PWR – OFF

B F3 HUD PWR (two) – OFF

If ELS:P C3 MSTR MADS(OEX) PWR – OFF

(OEX for OV102)DoD ELS, MCC call DoD OSC onNCC

NOTEMCC will report “GO/NO–GOTO DOFF SUITS” (post safetyassessment)

NOMENT/NOM/GEN F



CDRNOTE

CDR activities are now on evennumbered pages and PLTactivities on odd numbered pages

RCS, OMS SAFING (RJDs)C3 �OMS ENG (two) – OFFO14:F RJD DRIVER (nine) – OFFO15:F RJD LOGIC (eight) – OFFO16:F OMS ENG VLV (two) – OFF

C,P,MS DRAG CHUTE SAFING(Not performed if ELS)

O15:E cb MNB DRAG CHUTE SYS 2 – opO16:E cb MNC DRAG CHUTE SYS 1 – opF2,F3, �DRAG CHUTE PBI lts (six) – off F4

DEACT AIR DATA PROBE HTRSC3 �AIR DATA PROBE (two) – DPY

C,P,MS LANDING GEAR SAFING(Not performed if ELS)

R14:F cb ESS 1BC LDG GEAR ARM/DNRESET – cl

NOTESM0 TIRE PRESS msgs occur whenLG ARM/DN RESET performed

A12 LG ARM/DN RESET – RESETF6,F8 �LDG GEAR pb (four) – lt offA12 LG ARM/DN RESET – dnR14:F cb ESS 1BC LDG GEAR ARM/DN

RESET – op

Check with MS3. Report to MCC:“RJDs OFF, SIDE HATCH, DRAGCHUTE, AND LANDING GEARSAFED” (MCC report to NCC)NOM

SETUP:

BF

LOAD TEST:

RELEASE:

R

BF�

�BF

�R

R�

>

�

�

��

�>

>

5–5 ENT/ALL/GEN F


PLT ET UMBILICAL DOOR OPENING

Report to MCC, “ET UMBILICALDOORS ARE COMING OPEN”

R2 ET UMB DRMODE – GPC/MANR LAT – REL (tb–bp, REL ∼6 sec)R LAT – OFFR DR – OP (tb–bp)Wait 12 sec, R DR – OFF (tb–bp)L LAT – REL (tb–bp, REL ∼6 sec)L LAT – OFFL DR – OP (tb–bp)Wait 12 sec, L DR – OFF (tb–bp)MODE – GPC

HYDRAULIC LOAD TEST (ON MCC CALL)NOTE

Minimum of two operating hydsystems is reqd for this test

F4 BDY FLP pb – MANF8 �FLT CNTLR PWR – ON

NOTEIf only two systems are operating, donot depressurize either hyd pump

R2 HYD MN PUMP PRESS 1 – LO (MA)C3 Run Full Load Test:

BDY FLP – TRAILRHC – Forward ctrRudder full left

When set, do following simo:BDY FLP – UP (to � 6%)RHC – move to aft ctrRudder full right

RHC – releaseRudder – neutralBDY FLP – reset to TRAIL

R2 HYD MN PUMPPRESS 1 – NORMPRESS 3 – LO (MA)

C3 Repeat Load TestR2 HYD MN PUMP PRESS 3 – NORM

5–6 ENT/ALL/GEN F


CDRMCC Report GO/NO–GO for DPS transition

DPS TRANSITION – GNC 9 (If PASS)

NOTEDo not perform any keyboard itementries or switch throws 10 sec beforeand after moding PASS GPCs to RUNor making OPS transition requests.

MCC will call for BFS to be taken fromRUN to STBY for OPS Recorderdumping and PL monitoring as reqd

�BFC CRT DISP – ON

CRT3 BFS, GNC, OPS 000 PRO

3: BFS, GNC BFS MEMORY

1: GNC 0 GPC MEMORY

Verify:

STR 1 12 23 34 4

PL 1/2 1CRT 1 1

2 23 34 0

L 1 12 2

MM 1 12 2

912340

CONFIGGPC

CRT1 GNC, OPS 901 PRO

5–7 ENT/ALL/GEN F


PLT SET BODY FLAP (Prior to OPS 9)F4 BODY FLAP pb – MANC3 BODY FLAP – DOWN (100%)

PLT SSME REPOSITIONING (If PASS, OPS 9,and GO from MCC)

2: GNC 105 TCS CONTROL

R4 HYD MPS/TVC ISOL VLV SYS (three) – OPHold 5 sec, �tb – OP

**

If less than two HYD MPS/TVCISOL VLVs open, �MCC

**

CRT2 CLEAR MSG – ITEM 8 EXECSELECT ID – ITEM 1 +0 2 EXEC

�NAME VFB 84 (∼60 sec)MM READ – ITEM 2 EXEC

�‘AI MODE 1(0,3) COMPLETE’ msg (∼2.5 min)�‘VFB 84 – COMPLETE’ msg

***

If any ‘AI MODE X FAILED RETEST’ msg:�MCC, report ECP ERROR

To terminate: CANCEL – ITEM 5 EXEC

***

Go to APU/HYD SHUTDN >>

PLT SPDBK REPOSITIONING (KSC only, ON MCC GO)

R4 �HYD MPS/TVC ISOL VLV SYS (three) – CL

2: GNC 113 ACTUATOR CONTROL

CRT2 Al MODE 1 MDM – ITEM 23 EXEC (*)I �ACTUATOR GIMBALING STATUS – RUN, CPLTSB – ITEM 1 EXEC (*)RATE – ITEM 29 +1 EXECFIN POS – ITEM 30 +8 EXEC

�START 31 – → ←START – ITEM 31 EXEC (*→ ←)

�STATUS – RUN, CPLT (∼30 sec)

**

If STATUS – STOP or BUSY:�MCC, (To terminate: ITEM 32 EXEC)

**

Go to APU/HYD SHUTDN >>

5–8 ENT/ALL/GEN F

1: AS DESIRED 2: AS DESIRED3: AS DESIRED

CDR RAD RECONFIG(On MCC call, unless no COMM)

O1 When FREON EVAP OUT TEMP > 40degF:

L1 RAD OUT TEMP – HIO1 When FREON EVAP OUT TEMP > 55

degF, proceed to NH3 ACT

NH3 ACTO1 When FREON EVAP OUT TEMP > 55

degF, select one of the following asspecified by MCC:

L1 NH3 CNTLR A – PRI/GPC ( )NH3 CNTLR A – SEC/ON ( )NH3 CNTLR B – PRI/GPC ( )NH3 CNTLR B – SEC/ON ( )

*******************

O1L1

O1

During NH3 ops:If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP < 32 degF:

1. FREON PUMP LOOP 1,2(two) – OFF (ASAP)

2. H2O PUMP LOOP 1 – ON3. NH3 CNTLR A(B) – OFFIf no PL H2O Loop present:

4. FLOW PROP VLV LOOP 1,2(two) – PL HX (tb–PL)

If PL H2O Loop present:5. Activate PL H2O Loop

6. FREON PUMP LOOP 1 – BWait 3 min, then:

7. FREON PUMP LOOP 2 – B8. Go to NH3 RECONFIG, 5–22 >>

If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP > 65 degF:

9. Go to NH3 RECONFIG, 5–22

*******************

5–9 ENT/ALL/GEN F

1: AS DESIRED 2: AS DESIRED3: BFS, SM SYS SUM 2

PLT APU/HYD SHUTDN

�SSME REPOS complete (if PASS)

R4 HYD MPS/TVC ISOL VLVS (1,2,3; 5 secinterval) – CL (hold each 5 sec) �tb – cl

R2 BLR PWR (three) – OFFBLR N2 SPLY (three) – OFFAPU OPER (1,2,3; 5 sec interval) – OFF (MA)

APU FUEL TK VLV (three) – CLAP �� Shutdn (Hyd Press)APU CNTLR PWR (three) – OFF

Report to MCC, “APU/HYD SHUTDOWN”MCC Report to Convoy 1, “SSME

REPOSITIONING COMPLETE ANDAPU/HYD SHUTDOWN”

Report, “GO/NO–GO FOR VENT DOORPURGE POSITIONING”

POST LANDING MPS RECONFIG(After APU/HYD shutdn + 1 min)

R2 MPS He ISOL (six) – CL

MPS He I’CNCT L – OUT OPMPS PNEU L ENG He XOVR – CL

NOTEExpect multiple MAs for MPSHe P as regs bleed down


1: AS DESIRED 2: AS DESIRED3: AS DESIRED

C,MSC PCS DEACTIVATION

L2 O2 SYS 1,2 SPLY (two) – CL (tb–CL)O �� EMER tb – bp

MS GPS PWDNA13 (A12 for OV102)

****

If landing not at KSC, EDW, or NOR:GPS ENCRYPT – ZEROIZEWait 1 secGPS ENCRYPT – NORMAL

****

GPS PWR – OFFGPS PRE AMPL UPPER – OFFGPS PRE AMPL LOWER – OFF

MCC Report, “GO/NO–GO FOR EXTENDEDPWR UP”

NOTEIf GO for EXTENDED PWR UP, goto SYS DEACT FOR EXTENDEDPWR UP, 5–14.

If NO–GO for EXTENDED PWR UP,go to GPC DEACT (below)

C GPC DEACT(Perform after RCS/OMS VALVE TESTcompleted by PLT)

O6 GPC MODE 1,2,3,4,5 (five) – STBY (tb–bp)

GPC MODE 1,2,3,4,5 (five) – HALTInform MS to proceed with POSTLANDING PAYLOAD ACTIVITIES(if reqd), FS 5–19


1: AS DESIRED 2: GNC 105 TCS CONTROL3: AS DESIRED

PLT VENT DOOR PURGE POSITIONING (PASS)(on MCC GO, not performed if ELS)

CRT2 CLEAR MSG – ITEM 8 EXECSELECT ID – ITEM 1 +0 3 EXEC

�NAME ‘VFB89’ (∼60 sec)MM READ – ITEM 2 EXECAfter ‘VFB89 – ENTERING 30 MINDELAY’ msg, CANCEL – ITEM 5 EXEC

RCS, OMS VALVE TESTPause 1 sec between each line

O7 �MSTR RCS XFEED – OFFO8 L,R OMS He PRESS/VAP ISOL (four) –

CL,GPCL OMS XFEED (two) – OP (tb–OP),then – CL (tb–CL)

R OMS XFEED (two) – OP (tb–OP),then – CL (tb–CL),GPC

L,R OMS TK ISOL(four) – CL (tb–CL),then – OP (tb–OP),GPC

L OMS XFEED (two) – OP (tb–OP),GPCFWD RCS

He PRESS (two) – CL (tb–CL),GPCTK ISOL (two) – CL (tb–CL),then – OP (tb–OP),GPC

MANF ISOL (five) – CL (tb–CL)then – OP(tb–OP),GPC

O7 L,R RCSHe PRESS (four) – CL (tb–CL),GPCMANF ISOL (ten) – CL (tb–CL),then – OP (tb–OP),GPC

TK ISOL (six) – CL (tb–CL)XFEED (four) – OP (tb–OP),then – CL (tb–CL),GPC

TK ISOL (six) – OP (tb–OP),GPC


1: OFF 2: OFF3: OFF

C,MS,PS HATCH OPENING (Convoy)

SEAT EGRESS

C,MS,PS Pull G SUIT controller clip (if inflated)Lap Belt and Chute – ReleaseEgress seat (Helmet reqd if ELS)

MS,PS Unstow ‘Return to Houston’ Bags (exceptELS)

HATCH OPENING (ELS)

ALL �Tabs/Visor – CLGreen Apple – PULL

MS Open Hatch/Deploy Slide per decal

C Give PLT GO for VEHICLE PWRDN

C,MS,PS ORBITER UNAIDED EGRESS

Egress orbiterHand carry Landing Site Data book(if ELS) (reference ELS POSTLANDING procedures)

EX

TE

ND

PW

R U

P


1: OFF 2: OFF3: OFF

PLTNOTE

If GO for EXTENDED PWR UP,go to SYS DEACT FOREXTENDED PWR UP, 5–15.

If NO–GO for EXTENDED PWRUP, continue ops

HATCH OPENING (ELS)

Before hatch opening:�Tabs/Visor – CL

Green Apple – PULL

VEHICLE PWRDN (on GO from CDR)

NOTEAll vehicle lighting andorbiter O2 will be lost atpwrdn

R1 MN BUS TIE (three) – OFFFC/MN BUS (three) – OFFESS BUS SOURCE FC (three) – OFF

EGRESS

Pull G SUIT controller clip (if inflated)Egress seat, orbiter(Helmet reqd if ELS)

MCC TO KSC HANDOVER (at crew egress)

MEDS

EX

TE

ND

PW

R U

P


1: GNC 0 GPC MEMORY 2: AS DESIRED3: AS DESIRED

CDR SYS DEACT FOR EXTENDED PWR UP(Perform after Vent Door Purge Positioncompleted by PLT)

1: GNC 0 GPC MEMORY

STR 1 12 13 14 1

PL 1/2 1CRT 1 1

2 13 14 0

L 1 12 1

MM 1 12 1

910000

CONFIGGPC


GPC PWRDN

O6 GPC MODE 2,3,4 (three) – STBYGPC MODE 2,3,4 (three) – (tb–bp)GPC MODE 2,3,4 (three) – HALT

CRT1 If no GPC failure,ERR LOG RESET – ITEM 48 EXEC

O6 GPC PWR 2,3,4 (three) – OFFLTG (five) – OFF

C2 IDP/CRT 2 PWR – OFF

Inform MS2 to proceed with MS SysDeact activities, 5–18

ENT/MEDS/GEN FMEDS



PLT SYS DEACT FOR EXTENDED PWR UP

F8 FLT CNTLR PWR – OFFF3 TRIM PNL – OFF

TRI �RHC – INHR4 HYD BRAKE HTR (three) – OFFO8 LTG (five) – OFFO17:A ATVC (four) – OFF

MEDSENT/MEDS/GEN F


1: AS DESIRED 2: OFF3: AS DESIRED

C,MS,PS

C L2 ANTISKID – OFF�NWS – OFF

C3 �FCS CH (four) – AUTOF3 TRIM PNL – OFF

TRI �RHC – INHMS If reqd, install and lock PL Bay Window

Shades

IDP/CRT 4 PWRDN

MS R12 IDP/CRT 4 PWR – OFF

EGRESS(After MS Sys Deact complete)

L1 H2O PUMP LOOP 1 – ON

C L5 L COMM PWR – OFF

C,MS,PS PULL G SUIT controller clip (if inflated)Egress seat

MS A11,A15, COMM CCU PWR – OFFMS,PS MO39M

Unstow ‘Return to Houston’ Bags

C,MS,PS Egress orbiter

MEDSENT/MEDS/GEN F

EX

TE

ND

PW

R U

P


1: OFF 2: OFF3: OFF

PLTNOTE

If GO for EXTENDED PWR UP,go to SYS DEACT FOREXTENDED PWR UP, 5–15.

If NO–GO for EXTENDED PWRUP, continue ops

HATCH OPENING (ELS)

Before hatch opening:�Tabs/Visor – CL

Green Apple – PULL

VEHICLE PWRDN (on GO from CDR)

NOTEAll vehicle lighting andorbiter O2 will be lost atpwrdn

R1 MN BUS TIE (three) – OFFFC/MN BUS (three) – OFFESS BUS SOURCE FC (three) – OFF

EGRESS

Pull G SUIT controller clip (if inflated)Egress seat, orbiter(Helmet reqd if ELS)

MCC TO KSC HANDOVER (at crew egress)

NOM

EX

TE

ND

PW

R U

P



CDR SYS DEACT FOR EXTENDED PWR UP(Perform after Vent Door Purge Position completedby PLT)

1: GNC 0 GPC MEMORY

STR 1 12 13 14 1

PL 1/2 1CRT 1 1

2 13 14 0

L 1 12 1

MM 1 12 1

910000

CONFIGGPC


GPC PWRDN

O6 GPC MODE 2,3,4 (three) – STBYGPC MODE 2,3,4 (three) – (tb–bp)GPC MODE 2,3,4 (three) – HALT

CRT1 If no GPC failure,ERR LOG RESET – ITEM 48 EXEC

O6 GPC PWR 2,3,4 (three) – OFFLTG (five) – OFF

C2 CRT 2 PWR – OFF

Inform MS2 to proceed with MS SysDeact activities, 5–18

ENT/NOM/GEN FNOM



PLT SYS DEACT FOR EXTENDED PWR UP

F8 INST PWR – OFFFLT CNTLR PWR – OFF

F3 TRIM PNL – OFFTRI �RHC – INH

R4 HYD BRAKE HTR (three) – OFFO8 LTG (five) – OFFO17:A ATVC (four) – OFF

NOMENT/NOM/GEN F



C,MS,PS

C L2 ANTISKID – OFF�NWS – OFF

C3 �FCS CH (four) – AUTOF6 INST PWR – OFFF3 TRIM PNL – OFF

TRI �RHC – INHMS If reqd, install and lock PL Bay Window

Shades

EGRESS(After MS Sys Deact complete)

L1 H2O PUMP LOOP 1 – ON

C L5 L COMM PWR – OFF

C,MS,PS PULL G SUIT controller clip (if inflated)Egress seat

MS A11,A15, COMM CCU PWR – OFFMS,PS MO39M

Unstow ‘Return to Houston’ Bags

C,MS,PS Egress orbiter

NOMENT/NOM/GEN F

MS

EX

TP

WR

UP



PLT EGRESS(When desired after ground support personnelestablishes comm at PS station)

R6 R COMM PWR – OFFPull G SUIT controller clip (if inflated)Egress seat, orbiter

MCC TO KSC HANDOVER(At crew egress or GSE cooling activation,whichever occurs later)

MS

EX

TP

WR

UP



MS MS SYS DEACT FOR EXTENDED PWR UP

MS1 Perform POST LANDING PAYLOAD ACTIVITIES (if reqd), FS 5–19

MS2 LRU DEACTIVATION(After APU/HYD SHUTDN)

O14,O15, O16 BRAKES (three) – OFF

cb GPS PRE AMPL (four) – OP(OV103,105 only)

GPS 2 PRE AMPL UPPER – opGPS 2 PRE AMPL LOWER – op(OV104 only)

RGA (four) – OFFIMU (three) – OFFASA (four) – OFFcb ADTA (four) – opcb/sw ACCEL (four) – op/OFFcb DDU (six) – opcb MNA NWS – opcb MNB NWS – op

O7 TACAN MODE (three) – OFFO8 RADAR ALTM (two) – OFF

MLS (three) – OFFC L1 IMU FAN (three) – OFF

APU HEATER DEACTIVATION(After APU/HYD SHUTDN)

A12 APU HTRTK/FU LINE H2O SYS (six) – OFFGAS GEN/FUEL PUMP (three) – OFFLUBE OIL LINE (three) – OFF

RCS/OMS HEATERS PWRDN

A14 OMS CRSFD LINE A,B (two) – OFFIf reqd, install and lock PL Bay WindowShades

MS2 Inform CDR, “POST LANDINGPROCEDURE COMPLETE”





AS

P E

XT

PW

R U

P



ASP INTEGRATED POST LANDING PROCEDURESFOR EXTENDED PWR UP

ASP 1 A15 Connect Comm (PS)PS Comm CCU PWR – ON

ASP 1 Comm ck with MCC

ASP to Report when “CREW READY TO MCC EGRESS”

ASP to Report “POST LANDING PROCEDURE MCC COMPLETE”

AS

P E

XT

PW

R U

P



CDR SYS DEACT FOR EXTENDED PWR UP

NH3 RECONFIG(On MCC call; Cooling Cart not ready)

L1 1. NH3 CNTLR A(B) – OFFO1 When FREON EVAP OUT TEMP

> 55 degF, select one of the following asspecified by MCC:

L1 2. NH3 CNTLR A – PRI/GPC ( )NH3 CNTLR A – SEC/ON ( )NH3 CNTLR B – PRI/GPC ( )NH3 CNTLR B – SEC/ON ( )

******************

O1L1

O1

During NH3 ops:If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP < 32 degF:


2. H2O PUMP LOOP 1 – ON3. NH3 CNTLR A(B) – OFF4. If present, activate PL H2O

LOOP�MCC for steps

If no comm:5. Go to VEHICLE PWRDN,

5–13 >>6. �MCC

If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP > 65 degF:

7. Go to POST LANDING LOSSOF COOLING, 5–24

******************



CDR NH3 DEACT(On MCC call if Cooling Cart ready)

L1 1. NH3 CNTLR A(B) – OFF

2. RAD OUT TEMP – NORM

******************

O1L1

O1

After NH3 TERMINATION:If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP < 32 degF:


2. H2O PUMP LOOP 1 – ON3. If present, activate PL H2O

LOOP�MCC for steps

If no comm:4. Go to VEHICLE PWRDN,

5–13 >>5. �MCC

If EVAP OUT TEMP alarm andFREON EVAP OUT TEMP > 65 degFfor 5 min:

6. Go to POST LANDING LOSSOF COOLING, 5–24

******************



POST LANDING LOSS OF COOLING (NH3FAILED OR DEPLETED)

C L1 1. NH3 CNTLR A,B (two) – OFF

2. �RAD BYP VLV MAN SEL (two) – RADFLOW (tb–RAD, 3 sec)

3. �RAD CNTLR OUT TEMP – NORMC,P,MS 4. �Complete post landing procedures thru

ENT C/L, 5–18 & FS 5–19 ASAPAssume GO for EXTENDED PWR UP

B C3 5. �BFC CRT SEL – 3+1BFC CRT DISP – ON

3: BFS, SM SYS SUMM 2

Terminate monitoring if ground coolingestablished (Convoy commandercall) >>

CRT3 6. Monitor AV BAY TEMP (three)When AV BAY TEMP 1 or 2 > 113 orAV BAY TEMP 3 > 107 or notemperature insight:

P 7. Go to VEHICLE PWRDN,5–13 >>

A 8. Crew egress if not already complete

1–O

RB

LA

TE

6–1 ENT/ALL/GEN F

1–ORBIT LATE DEORBIT PROCEDURES

Refer to DEORBIT BURN FLIGHT RULESCue Card for failures that require 1–orbitdelay

1–O

RB

LA

TE

6–2 ENT/ALL/GEN F


1–ORBIT LATE DEORBIT PROCEDURES

TRANS B These procedures assume:DAP 1. All DEORB PREP completed

2. DEORBIT BURN completed up tobut not including SINGLE APUSTART, 3–13. If activities are notcomplete, then do them duringtroubleshooting time

C CRT1 GNC, OPS 301 PRO

R2 �HYD MN PUMP PRESS (three) – NORM

B A14 RCS/OMS HTRFWD RCS – A AUTOL POD (two) – A AUTO,B OFFR POD (two) – A AUTO,B OFFOMS CRSFD LINES (two) –A AUTO,B OFF

FWD RCS JET 5 (one) – AUTOAFT RCS JET 5 (one) – AUTO

H2O TANK CONFIG

R11L SPLY H2O TKC INLET – OP (tb–OP)SPLY H2O TKC OUTLET – OP (tb–OP)

TIG–1:10> IMU/IMU ALIGN

Perform IMU/IMU alignment using best IMU asreference. �MCC for reference IMU

1: GNC 21 IMU ALIGN

C CRT1 IMU/IMU – ITEM 14 + __ EXECALIGN IMU 1(2,3) –ITEM 10(11,12) EXEC (*)

If no comm, EXEC – ITEM 16 EXEC (*)Rcd MET ___/___:___

�EXEC, ITEM 16 – (no *) (4–6 min)

6–3 ENT/ALL/GEN F


C MCC UPDATE:DEL PADPRPLT PAD

MCC UPLINK:PASS TGTBFS TGT


ALL FLUID LOADING: 1–ORBIT LATE

Approx 1 hr prior to new TIG, drink 8 fluidoz water plus take 2 salt tablets every15 min for total of 16 fluid oz water and4 salt tablets per crewmember

FINAL DEORB UPDATE/UPLINK

C MCC UPDATE:DEL PADPRPLT PAD

MCC UPLINK:PASS SVBFS SVPASS TGTBFS TGTBFS IMU GYRO/ACCEL

G50 �LAND SITE as reqdSET TACAN tw

On MCC GO:CRT1 LOAD – ITEM 22 EXEC

TIMER – ITEM 23 EXECCRT1,3 �PASS & BFS TGTS per MNVR PAD:

BURN ATT∆VTOTTGOHA HP

6–4 ENT/ALL/GEN F


IF WAVEOFFGo to IF NO–GO FORDEORBIT BURN, 3–11

TIG–15>B A14 RCS/OMS HTRFWD RCS – OFFL POD (two) – A OFF,B OFFR POD (two) – A OFF,B OFFOMS CRSFD LINES (two) –A AUTO,B AUTO

FWD RCS JET 5 (one) – OFFAFT RCS JET 5 (one) – OFF

TIG–10> MNVR TO 1–ORBIT LATE DEORBIT ATT

C3 �DAP: AUTOB F6,F8 �ADI ATT (two) – INRTL

A �� ERR (two) – MEDA �� RATE (two) – MED

C MNVR to BURN ATT(�ADI ATT with CRT BURN ATT)

B Copy last DEL PAD and OMS PRPLT PADdata on DEORBIT BURN Cue Cards

F6/F8 �DEORBIT BURN and DEORBIT BURNMONITIOR Cue Cards installed

3: BFS, SM SYS SUMM 2

R2 HYD MN PUMP PRESS (three) – LO

Return to DEORBIT BURN Cue Cards andSINGLE APU START, 3–13

SW

LIS

T

7–1 ENT/ALL/GEN F NOT FLOWN

SWITCH LIST AT WHEELS STOP EGRESS

LEFT SEAT

L5 7–2. . . . . . . . . . . . . . L1 7–2. . . . . . . . . . . . . . L2 7–2. . . . . . . . . . . . . .

F2 7–2. . . . . . . . . . . . . . F3 7–2. . . . . . . . . . . . . . F6 7–2. . . . . . . . . . . . . . F7 7–3. . . . . . . . . . . . . .

C2 7–3. . . . . . . . . . . . . C3 7–3. . . . . . . . . . . . .

O6 7–4. . . . . . . . . . . . . O7 7–4. . . . . . . . . . . . . O14 7–4. . . . . . . . . . . . O15 7–5. . . . . . . . . . . .

RIGHT SEAT

O16 7–6. . . . . . . . . . . . O17 7–6. . . . . . . . . . . . O8 7–6. . . . . . . . . . . . .

RIGHT SEAT

F4 7–6. . . . . . . . . . . . . . F8 7–6. . . . . . . . . . . . . .

R1 7–7. . . . . . . . . . . . . R2 7–7. . . . . . . . . . . . . R4 7–7. . . . . . . . . . . . . R6 7–8. . . . . . . . . . . . .

R7 7–8. . . . . . . . . . . . . R10 7–8. . . . . . . . . . . . R12 7–8. . . . . . . . . . . . R14 7–8. . . . . . . . . . . .

AFT

A11 7–9. . . . . . . . . . . . A12 7–9. . . . . . . . . . . . A13 7–9. . . . . . . . . . . . A14 7–9. . . . . . . . . . . . A15 7–9. . . . . . . . . . . .

MIDDECK – FWD

MO39M 7–10. . . . . . . . . MO42F 7–10. . . . . . . . .

NOTES

� This section contains switch configuration at egress forpanels that are reconfigured in this checklist for EXTENDPWR UP option. Refer to DEORBIT PREP, section 3, foregress configuration of remaining panels subsequent toscheduled Deorbit Prep switch verification checks.

� denotes physical break in panel structure.

� Switch list at WHEELS STOP EGRESS

SW LIST

NOT FLOWN 7–2 ENT/ALL/GEN F

LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESS

L5 L COMM PWR – ON OFF

All switches per DEORB PREP except:L1 IMU FAN B – ON OFF

H2O PUMP LOOP 1 (two) – OFF,B ON,BRAD CNTLR LOOP 1,2 (two) – AUTO BRAD BYP VLV MAN SEL 1 – ctr (tb–RAD)RAD BYP VLV MAN SEL 2 – ctr (tb–RAD or BYP)H2O BYP VLV MODE 1 – AUTOH2O BYP VLV MODE 2 – AUTO or MANNH3 CNTLR A(B) – OFF PRI/GPC or SEC/ON or OFF

L2 ANTISKID – ON OFFNWS – 1 OFFBDY FLP – AUTO/OFFENTRY MODE – AUTOTRIM R,P,Y (three) – ctrSBTC – as reqd full forwardO2 SYS 1,2 SPLY (two) – ctr (tb–OP)

ctr (tb–CL)N2 SYS 1,2 (four) – ctr (tb–OP)

F2 All pb lts – as reqd lt off

F3 L HUD PWR – ON OFFL TRIM RHC/PNL – as reqd INHL TRIM PNL – as reqd OFFR HUD PWR – ON OFFR TRIM RHC/PNL – as reqd INH

F3 R TRIM PNL – as reqd OFFDRAG CHUTE ARM 1/ARM 2 pb – as reqd lt offDRAG CHUTE DPY 1/DPY 2 pb – as reqd lt offDRAG CHUTE JETT 1/JETT 2 pb – as reqd lt off

(OV103,5)F6 INST PWR – FLT/MPS OFF

DATA BUS – 3AIR DATA – NAVADI ATT – LVLHADI ERR – as reqdADI RATE – as reqdLDG GEAR ARM pb – ARM/lt on lt offLDG GEAR DN pb – DN/lt on lt offLDG GEAR tb (three) – DNHSI SEL MODE – ENTRYHSI SEL SOURCE (two) – NAV,1BFC DISENGAGE – dnABORT MODE – OFFABORT pb – lt off(OV102,4)HUD DATA BUS – 1AIR DATA – NAVADI ATT – LVLHADI ERR – as reqdADI RATE – as reqdLDG GEAR ARM pb – ARM/lt on lt offLDG GEAR DN pb – DN/lt on lt offLDG GEAR tb (three) – DNHSI SEL MODE – ENTRY


LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESSF6 HSI SEL SOURCE (two) – NAV,1

BFC DISENGAGE – rtABORT MODE – OFFABORT pb – lt offFLT CNTLR POWER – ON OFFRADAR ALTM – 1

(OV103,5)F7 FLT CNTLR PWR – ON OFF

RADAR ALTM – 1

(OV103,5)C2 CRT PWR (1,3) – ON

CRT 2 PWR – ON OFFL CRT SEL – as reqdR CRT SEL – as reqd(OV102,4)IDP/CRT PWR (1,3) – ONIDP/CRT 2 PWR – ON OFFL IDP/CRT SEL – as reqdR IDP/CRT SEL – as reqd(all)1,2,3 MAJ FUNC (three) – GNCEVENT TIMER MODE – as reqdEVENT TIMER CNTL – ctrTIMER SET tw (four) – as reqdTIMER – ctr

C3 OMS ENG (two) – OFFBFC CRT DISP – ONBFC CRT SEL – 3+1FCS CH (four) – AUTOBDY FLP – AUTO/OFFAIR DATA PROBE STOW (two) – INHOV102 MN ENG VIB SHUTDN – INHMN ENG LIMIT SHUTDN – AUTOTRIM R,P,Y (three) – ctrSBTC – full forwardDAP – lts offSRB SEP – MAN/AUTOET SEP – MANAUD CTR – 1OI PCMMU PWR – 1OI PCMMU FORMAT – GPCS–BD PM CNTL – CMDS–BD PM ANT – GPCAIR DATA PROBE (two) – DPYUPLK – ENAOV103,4,5 MSTR MADS PWR – ON OFFOV102 MSTR OEX PWR – ON OFFC/W MEM – ctrC/W MODE – NORMOV102 PL SAFING (five) – SAFEOV103,4 RTG PUMP – PRIOV103 PL SAFING (2,3,4,5) – SAFEOV104 RTG SHORT PRI(SEC) ENA – DSBLOV104 RTG SHORT PRI(SEC) SHORT – OFFEMER LTG – FF/ON (as reqd)

ENT/ALL/GEN F,1


LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESSO6 LTG PNL (two) – BRT, as reqd OFF

LTG INST (two) – BRT, as reqd OFFLTG L GLRSHLD FLOOD (two) – BRT, as reqd OFFL SEAT/CTR CNSL FLOOD (two) – BRT, as reqd OFFSTAR TRK DR CNTL (two) – OFF (tb–CL)STAR TRR PWR (two) – OFFUHF SPLX/EVA XMIT FREQ – 259.7/414.2UHF SPLX/EVA PWR AMPL – ONUHF SPLX SQUELCH – ONUHF EVA STRING – 1UHF ENCRYPT – OFFUHF MODE – SPLXANNUN LAMP TEST – ctrANNUN BUS SEL ACA 1 – MNAANNUN BUS SEL ACA 2/3 – MNBANNUN INTEN (two) – VAR, as reqdMTU – AUTOOV103,5 DEU (four) – dnOV102,4 IDP (four) – dnMDM PL1,PL2 (two) – ONMDM PL3 – OFFMDM FA1,2,3,4 (four) – ONMDM FF1,2,3,4 (four) – ONGPC PWR 1,5 – ONGPC PWR 2,3,4 – ON OFFGPC OUTPUT 1 – NORM (tb–gray)GPC OUTPUT 2,3,4 – NORM (tb–gray) bpGPC OUTPUT 5 – BACKUP (tb–bp)IPL SOURCE – OFFGPC MODE 1,5 – RUN (tb–RUN)GPC MODE 2,3,4 – RUN (tb–RUN)

O6 GPC MODE 2,3,4 – HALT (tb–bp)

O7 TACAN 1,2,3 MODE (three) – GPC OFFTACAN 1,2,3 ANT SEL (three) – AUTOTACAN 1,2,3 CH tw (three) – 111XTACAN 1,2,3 (if Edw landing)AFT L RCS He PRESS (two) – OP (tb–OP)AFT L RCS He PRESS (two) – GPC (tb–CL)AFT L RCS TK ISOL (three) – GPC (tb–OP)AFT L RCS MANF ISOL 1,2,3,4 (four) – OPAFT L RCS MANF ISOL 1,2,3,4 (four) – (tb–OP)AFT L RCS MANF ISOL 1,2,3,4 (four) GPC (tb–OP)AFT L RCS MANF ISOL 5 – GPC (tb–OP)AFT L RCS XFEED (two) – GPC (tb–CL)MSTR RCS XFEED – OFFAFT R RCS He PRESS (two) – OP (tb–OP)AFT R RCS He PRESS (two) – GPC (tb–CL)AFT R RCS TK ISOL (three) – GPC (tb–OP)AFT R RCS MANF ISOL 1,2,3,4 (four) – OPAFT R RCS MANF ISOL 1,2,3,4 (four) – (tb–OP)AFT R RCS MANF ISOL 1,2,3,4 (four) GPC (tb–OP)AFT R RCS MANF ISOL 5 – GPC (tb–OP)AFT R RCS XFEED (two) – GPC (tb–CL)

O14:A BRAKES MNA – ON OFFRGA 1 – ON OFFIMU 1 – ON OFFFC1 CNTLR – ONAll cbs closed except:

O14:C OV102,3,5 cb MNA TACAN 1 – op

ENT/ALL/GEN F,1


LEFT SEAT SWITCH LIST AT WHEELS STOP EGRESS

O14:D OV104 GPS 1 PRE AMPL UPPER – opOV104 GPS 1 PRE AMPL LOWER – opcb MNA GPS PRE AMPL (two) – op

O14 cb MNA CAB VENT – opcb MNA CAB VENT ISOL – op op

O14:E cb MNA ADTA 1 – cl opcb MNA ACCEL 1 – cl opcb MNA DDU L – cl opcb MNA CAB AFT – op opcb MNA NWS – cl

O14:F MMU 1 – ONRJD (six) – ON OFFL OMS ENG VLV – ON OFFASA 1 – ON

O15:A BRAKES MNB – ON OFFRGA (two) – ON OFFIMU 2 – ON OFFFC2 CNTLR – ON

O15:D cb MNB NWS – cl opAll cbs closed except:

O15:C OV104 GPS 2 PRE AMPL UPPER – opO15:D OV104 GPS 2 PRE AMPL LOWER – opO15:C OV102,3 cb MNB TACAN 2 – opO15:E cb MNB ADTA 2 – cl op

cb MNB ACCEL 2 – cl opcb MNB DRAG CHUTE SYS 2 – cl opDDU (two) – cl op

O15:F MMU 2 – ONRJD (four) – ON OFF

O15:F ASA 2 – ON OFFACCEL 4 – ON OFF


RIGHT SEAT SWITCH LIST AT WHEELS STOP EGRESSO16:A BRAKES MNC – ON OFF

RGA 3 – ON OFFIMU 3 – ON OFFFC3 CNTLR – ONAll cbs closed except:

O16:C OV102 cb MNC TACAN 3 – opO16:D OV104 GPS 3 PRE AMPL UPPER – op

OV104 GPS 3 PRE AMPL LOWER – opcb MNC GPS PRE AMPL (two) – opcb MNC GPS O2 EMER – op

O16:E cb MNC ADTA (two) – cl opcb MNC DDU R – cl opcb MNC DDU AFT – opcb MNC DRAG CHUTE SYS 1 – cl op

O16:F RJD (six) – ON OFFR OMS ENG VLV – ON OFFASA 3,4 (two) – ON OFFACCEL 3 – ON OFFRJD L5/F5/R5 DRIVER – OFF

O17:A ATVC (four) – ON OFFO17:B EIU (three) – OFFO17:C SIG CONDR FREON A – AC2

SIG CONDR FREON B – AC3SIG CONDR OL 1/2 – ONSIG CONDR OR 1/2 – ON

O17:D SIG CONDR OA 1/2/3 – ONMDM OA 1/2/3 – ONMEC (two) – OFF

O8 RADAR ALTM (two) – ON OFFO8 MLS (three) – ON OFF

O8 MLS CH tw (three) – as reqdR SEAT/CTR CNSL FLOOD (two) – as reqdLTG PNL R – BRT OFFLTG PNL R OVHD – BRT OFFLTG PNL R INST – BRT OFFLTG PNL NUMERIC – BRT OFFLT G R GLRSHLD FLOOD – OFFOMS KIT He PRESS/VAP ISOL (two) – CLOMS KIT TK ISOL (two) – CL (tb–bp)L OMS He PRESS/VAP ISOL (two) – CL GPCL OMS TK ISOL (two) – OP (tb–OP) GPC (tb–OP)L OMS XFEED (two) – CL (tb–CL) GPC (tb–OP)R OMS He PRESS/VAP ISOL (two) – CL GPCR OMS TK ISOL (two) – OP (tb–OP) GPC (tb–OP)R OMS XFEED (two) – CL (tb–CL) GPC (tb–CL)FWD RCS He PRESS (two) – OP (tb–OP)FWD RCS He PRESS (two) – GPC (tb–CL)FWD RCS TK ISOL (two) – OP (tb–OP)FWD RCS TK ISOL (two) GPC (tb–OP)FWD RCS MANF ISOL 1,2,3,4 – OP (tb–OP)FWD RCS MANF ISOL 1,2,3,4 – GPC (tb–OP)FWD RCS MANF ISOL 5 – GPC (tb–OP)ANNUN LAMP TEST – ctr

F4 All pb lts – as reqd

F8 OV103,5 INST PWR – ON OFFOV103,5 DATA BUS – 4OV102,4 HUD DATA BUS – 4AIR DATA – NAVADI ATT – LVLHADI ERR – as reqd


RIGHT SEAT SWITCH LIST AT WHEELS STOP EGRESS

F8 ADI RATE – as reqdLDG GEAR ARM pb – ARM/lt ON lt OFFLDG GEAR DN pb – DN/lt ON lt OFFLDG GEAR tb (three) – DNHSI SEL MODE – ENTRYHSI SEL SOURCE (two) – NAV, 2FLT CNTLR PWR – ON OFFRADAR ALTM – 2

R1 All switches and cbs per DEORB PREP except:PL PRI MNC – as reqd per FS 5–19

R2 MPS PRPLT DUMP SEQ (two) – GPCMPS ENG PWR (six) – OFFMPS He ISOL (six) – GPCMPS PNEU L ENG He XOVR – GPCMPS PNEU He ISOL – GPCMPS He I’CNECT (three) – GPCMPS LH2 ULL PRESS – AUTOAPU/HYD RDY tb (three) – bpAPU OPER (three) – START/RUN OFFAPU SPEED SEL (three) – NORMHYD MN PUMP PRESS (three) – NORMAPU CNTLR PWR (three) – ON OFFAPU AUTO SHUTDN (three) – ENABLR CNTLR/HTR (three) – BBLR PWR (three) – ON OFFBLR N2 SPLY (three) – ON OFF

R2 HYD CIRC PUMP (three) – OFFAPU FUEL TK VLV (three) – OP CLcb APU FU TK VLV ENA (six) – clET UMB DR MODE – GPCET UMB DR CTRLINE LAT – GND (tb–STO)ET UMB L DR – OFF (tb–CL)– tb–bpET UMB L LAT – OFF (tb–LAT)– tb–RELET UMB R DR – OFF (tb–CL)– tb–bpET UMB R LAT – OFF (tb–LAT)– tb–REL

R4 HYD BRAKE HTR (three) – AUTO OFFHYD BRAKE ISOL VLV 1,2,3 – GPC (tb–OP)HYD MPS/TVC ISOL VLV (three) – ctr (tb–CL)HYD MPS/TVC ISOL VLV (three) – ctr (tb–OP)LG/NWS HYD SYS – AUTO 1/2LG/EXTEND ISOL VLV – GPC (tb–op)MPS ENG CNTLR HTR (three) – OFFMPS MANF PRESS (two) – GPCMPS FILL/DRAIN LO2 OUTBD – GNDMPS FILL/DRAIN LO2 INBD – GNDMPS FILL/DRAIN LH2 OUTBD – GNDMPS FILL/DRAIN LH2 INBD – GNDMPS H2 PRESS LINE VENT – GNDMPS LO2 PREVLV (three) – GPCMPS LH2 PREVLV (three) – GPCMPS FDLN RLF ISOL (two) – GPC


RIGHT SEAT SWITCH LIST AT WHEELS STOP EGRESS

R6 R COMM PWR – ON

R7 (NOTE: Pnl may be deleted if spacelab not flown)All switches per DEORB PREP exceptpowered spacelab config:SS INV – ctr (lt on)SS AC/DC PWR – ctr (lt on)AV FAN ON 1 – ctr (lt on)H2O LOOP PUMP 1 – ctr (lt on)Unpowered spacelab config same as above except lts

off:

R10 MS AUD PWR – AUD/TONEMS AUD A/G (two) – T/RMS AUD A/A – T/RMS AUD ICOM (two) A – T/RMS AUD ICOM (two) B – T/RMS AUD VOX SENS – as reqdMS AUD PAGE – dnMS AUD VOL tw (five) – as reqdMS AUD XMIT/ICOM MODE – PTT/PTT

R12 OV103,5 CRT 4 PWR – ON OFFOV102,4 IDP/CRT 4 PWR – ON OFFMAJ FUNC – SM

All cbs closed except:R14:B OV102,4,5 cb MNA PALLET DSC 1A/2B – op*

OV104,5 cb MNA PALLET DSC 3A – opOV102,4,5 cb MNB PALLET DSC 1B – op*

R14:B OV104,5 cb MNB PALLET DSC 4B – opOV102,4,5 cb MNC PALLET DSC 2A – op*OV104,5 cb MNC PALLET DSC 3B/4A – op

R14:C cb MNA UHF EVA – opcb MNB KU ELEC – opcb MNB ANT HTR – opcb MNB CABLE HTR – opcb MNC KU SIG PROC – opcb MNC UHF EVA – op

R15:F cb ESS 1BC LDG GEAR ARM/DN RESET – op cl

* Closed if EDO

ENT/ALL/GEN F,1


AFT FLIGHT DECK SWITCH LIST AT WHEELS STOP EGRESS

A11 MS COMM CCU PWR – ON OFF

A12 APU HTR GAS GEN/FUEL PUMP (three) – B AUTOAPU HTR GAS GEN/FUEL PUMP (three) – OFFAPU HTR LUBE OIL LINE (three) – B AUTO OFFAPU HTR TK/FU LINE H2O SYS 1A,2A,3A – OFFAPU HTR TK/FU LINE H2O SYS 1B,2B,3B – AUTOAPU HTR TK/FU LINE H2O SYS 1B,2B,3B – OFFLG ARM/DN RESET – dnFC3 STRUCT RTN – ctr (tb–ON)HYD HTR (eight) – OFFHYD CIRC PUMP PWR 1 – MNAHYD CIRC PUMP PWR 2 – MNBHYD CIRC PUMP PWR 3 – MNC

A13 OS AUD MSTR SPKR VOL – as reqdSPKR PWR – OFF

A14 RCS/OMS HTR FWD RCS – OFFRCS/OMS HTR L POD (two) – OFFRCS/OMS HTR R POD (two) – OFFRCS/OMS HTR OMS KIT – OFFRCS/OMS HTR OMS CRSFD LINES (two) – A AUTORCS/OMS HTR OMS CRSFD LINES (two) – OFFRCS/OMS HTR OMS CRSFD LINES (two) – B AUTORCS/OMS HTR OMS CRSFD LINES (two) – OFFRCS/OMS HTR FWD RCS JET 1,2,3,4 (four) – AUTORCS/OMS HTR FWD RCS JET 5 – OFFRCS/OMS HTR AFT RCS JET 1,2,3,4 (four) – AUTORCS/OMS HTR AFT RCS JET 5 – OFF

A14 PYRO (twelve) – SAFERMS LAT – SAFE

A15 PS COMM CCU PWR – ON OFFDC UTIL PWR MNC – as reqdAC UTIL PWR AC3 – OFF


MIDDECK – FORWARD SWITCH LIST AT WHEELS STOP EGRESS

MO39M MIDDECK COMM CCU PWR – ON OFF

MO42F MIDDECK SPKR AUD PWR – OFFMIDDECK SPKR AUD A/G (two) – T/RMIDDECK SPKR AUD A/A – T/RMIDDECK SPKR AUD ICOM (two) – T/RMIDDECK SPKR AUD VOX SENS – as reqdMIDDECK SPKR AUD MSTR SPKR VOL – as reqdMIDDECK SPKR AUD PAGE – dnMIDDECK SPKR AUD VOL tw (five) – as reqdMIDDECK SPKR AUD XMIT/ICOM MOD – PTT/VOXMIDDECK SPKR AUD TONES – ACCU/BYPMIDDECK SPKR AUD SPKR PWR – OFFGPC MEM DUMP – OFFBYP TONE VOL – as reqd

CU

E C

AR

DC

ON

FIG

8–1 ENT/ALL/GEN F FAB USE ONLY

ENTRY CUE CARD CONFIG

CU

E C

AR

DC

ON

FIG

CC 8–2 ENT/ALL/GEN F FAB USE ONLY

APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


4 1 GPC X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


ECLS7 2 Av Bay Fans in Bay 3 X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .



depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . . .

10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

11 CNTL CA1 (No BFS Engage in GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

12 Multi Φ AC BUS (unshorted) X. . . . . . . . . . . . . . . . . . . . . . . . . . .


(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

17 3 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . . .



AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . . .

24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

25 1 AFT RCS PROP TK fail X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


FAILURE

PRE TIG POST TIG

Delay (max)

OneOrbit

OneDay

StopBurn,> Safe

HP

TOP

ENT–1a/D/I

perigee adjust


HOOKVELCRO

HOOKVELCRO

DEORBIT BURN FLIGHT RULESONE–ORBIT LATE AVAILABLE

(reduced copy)


TOPBACK OF ‘DEORBIT BURN FLIGHT RULES’

APU/HYD1 No APU operating X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

LDG/DECEL2 NWS (KSC) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


4 1 GPC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

5 BFS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


ECLS7 2 Av Bay Fans in Bay 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .



depleted tk(s) ) X. . . . . . . . . . . . . . . . . . . . . . .

10 2 MN Buses X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

11 CNTL CA1 (No BFS Engagein GPC 3/5) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

12 Multi ΦAC BUS (unshorted) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .


(C–band not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

14 IMU Dilemma X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

15 RHC Dilemma X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

16 2 IMUs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

17 3 ADTAs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

18 2 ADTAs, AAs, RGAs, FCS (LKBD not avail) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

OMS19 Prplt Tank X X 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

20 Ignition (neither eng ignites) X. . . . . . . . . . . . . . . . . . . . . . . . . .



AFT RCS23 2 jets, same direction, same pod X. . . . . . . . . . . . . . . . . . . .

24 Prplt Lk after LAST LOS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

25 1 AFT RCS PROP TK FAIL X. . . . . . . . . . . . . . . . . . . . . . . . . . .


FAILURE

PRE TIG POST TIGDelay(max)OneDay

StopBurn,> Safe

HP

ENT–1b/D/I

perigee adjust


HOOKVELCRO

HOOKVELCRO

DEORBIT BURN FLIGHT RULESONE–ORBIT LATE NOT AVAILABLE

(reduced copy)


HOOKVELCRO

HOOKVELCRO

�MM302 �RCS SEL�RCS BURN CONFIG (L OMS I’CNCT)

L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . . .

�DAP – INRTL/DISCADI – LVLH(REF)/MED/MEDFLT CNTLR PWR (two) – ON

TIG THC +X (No deorbit > TIG +

Maintain PITCH ATT ERR ± 3°Monitor ∆VTOT:

RCS I’CNCT TK SW at ∆VTOT =R OMS XFEED (two) – OPL OMS XFEED (two) – CL

OMS PRPLT LOWAFT RCS RECONFIG AT ∆VTOT =RCS COMPLETION

OMS PRPLT FAIL (MULTIPLE JETS FAIL OFF):Secure aff OMS


HPCONTINUE BURN:

ITEM 18 +0 EXECG23 Resel jetsInterconnect good OMS to RCS

THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION



CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jets

********************

********************

DEORBITBURN(RCS)

HINGE

ENT–3a/D/K

TOP

: )

(reduced copy)




THC +X to PREBANK/FLIP HP or

At AFT QTY 1 TOT AFT QTY 2if CUR HP: PREBANK/FRCS COMPLETION

PREBANK/FLIP

HP

AFTHP

TGTHP



CUTOFF VGOx = 0, release THC

AFT RCS RECONFIGTrim Inplane X,Z residuals < 2 fps (< 0.5 if shallow)

********************

********************

TOPHINGED AT BOTTOM OF‘DEORBIT BURN (RCS)’

HINGE

ENT–3aa/D/K

% then

%

THC +X to TGT HP

(reduced copy)


HOOKVELCRO

HOOKVELCRO

HINGE

ENT–3b/D/D

TOPBACK OF ‘DEORBIT BURN (RCS)’

(reduced copy)


TOPHINGED AT BOTTOM OF

BACK OF ‘DEORBIT BURN (RCS)’

HINGE

ENT–3bb/D/D

(reduced copy)



�TRIM per MNVR PAD or P +0.0, LY –5.7, RY +5.7L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OP



If no OMS ignition: APUs – SHUT DNOMS PRPLT FAIL:

Failed OMS ENG – OFFSTOP BURN:

Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS

CONTINUE BURN:






OMS Xor OMS QTY



Secure aff OMS ITEM 18 +0 EXEC

STOP BURN:

APUs – SHUT DN

CONTINUE BURN:



RCS COMPLETION

HOOKVELCRO

HOOKVELCRO

********************************************

********************************************

DEORBITBURN (2 ENG)

TOP


BothENG FAIL

HP

R OMSFAIL HP

L OMSFAIL HP

ENT–4a/D/KHINGE

% R%L or

: )

(reduced copy)





PREBANK/FLIPHP

AFT

HP

TGTHP




********************

********************

TOPHINGED AT BOTTOM OF‘DEORBIT BURN (2 ENG)’

HINGE

THC +X to TGT HP

ENT–4aa/D/I

% then

%

):


(reduced copy)


�MM302 �OMS L or R�OMS BURN CONFIG (L or R XFEED)

Enter TGO + 10 sec�TRIM per MNVR PAD or P +0.0, LY +5.2, RY –5.2

L,R OMS He PRESS/VAP ISOL A (two) – OPWait 2 sec B (two) – OP. . . . . . . . . . . . . . . . . .


TIG–2 Good OMS ENG – ARM/PRESSTIG–2:15 EXEC (NO EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)

* If no OMS ignition: APUs – SHUT DN *

OMS XFEED RETURN at ∆VTOT =

orL,R OMS TK ISOL (four) – OPL,R OMS XFEED (four) – CL



SAFE Secure aff OMSHP

CONTINUE BURN:Secure aff OMSITEM 18 +0 EXEC


THC +X(�OMS% vs RCS Burn Time)AFT RCS RECONFIG

RCS COMPLETIONOMS ENG FAIL:

OMS ENG – OFFSTOP BURN:

ENG APUs – SHUT DNFAILHP

CONTINUE BURN:�ADI – LVLH, center needles

Interconnect OMS to RCSTHC +X(�OMS% vs RCS Burn Time)RCS I’CNCT TK SWRCS THC +X (�OMS% vs RCS Burn Time)AFT RCS RECONFIG

RCS COMPLETIONRCS +X JET FAIL OFF:


HPCONTINUE BURN:

ITEM 18 +0 EXECG23 Resel jets

HOOKVELCRO

HOOKVELCRO

**************************************

**************************************

DEORBITBURN (1 ENG)

TOPBACK OF ‘DEORBIT BURN (2 ENG)’

ENT–4b/D/IHINGE

):

%at

(reduced copy)





PREBANK/FLIPHP

AFT

HP

TGTHP


CUTOFF+ :02 OMS ENG – OFF (If < 3 IMU, at


********************

********************

TOPHINGED AT BOTTOM OF‘DEORBIT BURN (1 ENG)’

HINGE

THC +X to TGT HP

ENT–4bb/D/J

% then

%

):


(reduced copy)



�TRIM per MNVR PAD or P + 0.0, LY –5.7, RY +5.7�DAP – AUTO(PASS)/DISC

ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONFeed 2 ENG from 1 POD

L,R OMS He PRESS/VAP ISOL A (two) – GPCL,R OMS He PRESS/VAP ISOL B (two) – OPL,R OMS TK ISOL (two) – CL (tb–CL)L,R OMS XFEED (four) – OP (tb–OP)


If no OMS ignition: APUs – SHUT DNWhile feeding 2 OMS from 1 POD:

OMS PRPLT FAIL:Failed OMS ENG(s) – OFF

STOP BURN:APUs – SHUT DNSecure OMS

SAFE HP

CONTINUE BURN:ITEM 18 +0 EXECIf Both ENGs ‘↓’:

Secure OMS�ADI – LVLH, center needles


THC +X forAFT RCS RECONFIG

RCS COMPLETION If (XFEED) ENG ‘↓’:

When OMS QTY:5%: OMS TK ISOL (two) – OP4%: OMS TK ISOL (two) – CL



If (STRAIGHT FEED) ENG ‘↓’: OMS ENG FAIL

OMS ENG FAIL (CONTINUE BURN):Failed OMS ENG – OFF

at ∆VTOT =or

TK ISOL(two) – OP

TK ISOL(two) – CL

Return to 2 ENG, 2 POD FLOW at ∆VTOT:L,R OMS TK ISOL (two) – OP (tb–OP)L,R OMS XFEED (four) – CL (tb–CL)

at %

HOOK VELCRO

***************************************

***************************************

UNBALANCEDPRPLT

DEORBITBURN

HINGE

TOP

ENT–5a/D/L

: )

:

HOOK VELCRO

(reduced copy)


TOPHINGED AT BOTTOM OF ‘UNBALANCED PRPLT DEORBIT BURN’

HINGE

ENT–5aa/D/M

OMS PRPLT FAIL:Failed OMS ENG – OFF

STOP BURN:Good OMS ENG – OFFAPUs – SHUT DNSecure aff OMS

CONTINUE BURN:






or OMS QTY



Secure aff OMSITEM 18 +0 EXEC


CONTINUE BURN:

�ADI – LVLH, center needlesInterconnect Good OMS to RCS


RCS COMPLETIONRCS COMPLETION:

THC +X to TGT HP or TOT AFT QTY 1

At AFT QTY 1if CUR HP:

PREBANK/FLIP

HP

AFTHP

TGT

HPFRCS COMPLETION (if applicable):




***********************************************************

***********************************************************

R OMSFAIL HP

L OMSFAIL HP


BothENG FAIL

HP


THC +X to TGT HP

THC +X to PREBANK/FLIP HP orTOT AFT QTY 2PREBANK/FRCS COMPLETION

):

% then

%

%R%L or

(reduced copy)


HOOK VELCRO HOOK VELCRO

�MM302 �OMS L(R) or RCSEnter TGO + 10 sec

�L,R OMS TK ISOL (four) – GPCL,R OM �XFEED (four) – GPC

�tb config from table (OMS SSR–1)�DAP – AUTO(PASS)/DISC

ADI – LVLH(REF)/HI/MEDFLT CNTLR PWR (two) – ONMan repress to maintain good OMS Tk Ps > 234 psi (simo)If OMS BURN INITIATION:

�TRIM per MNVR PAD or: P +0.0, LY +5.2, RY –5.2TIG–2: Good OMS ENG – ARM/PRESS

TIG–2:15 EXEC (No EXEC > TIG +TIG–2:15 If OMS AFT QTY < 11%, THC +X to OMS IGN + 1 secTIG–2:00 TIG Start watch (�Pc, ∆VTOT, ENG VLVs)

* If no OMS ignition, APUs – SHUT DN *If RCS BURN INITIATION:

Man repress L,R OMS > L,R RCS TK PsL,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL

TIG–2:00 THC +X (No Deorbit > TIG +Maintain PITCH ATT ERR � 3°

FEED FROM GOOD POD:

at ∆VTOT =or

OMS He PRESS/VAP ISOL (two) – OPOMS TK ISOL (two) – OP (tb–OP)OMS XFEED (two) – OP (tb–OP)SECURE OMS

OMS PRPLT LOWAFT RCS RECONFIG at ∆VTOT =RCS COMPLETION

DEORBITBURN

(MIXEDXFEED)

HINGE

TOPBACK OF ‘UNBALANCED PRPLT DEORBIT BURN’

ENT–5b/D/I

at %

: )

: )

(reduced copy)




SAFE Secure L,R OMSHP

CONTINUE BURN:Secure L,R OMSITEM 18 +0 EXEC


OMS ENG FAIL:OMS ENG – OFF

STOP BURN:ENG APUs – SHUT DN

FAILHP CONTINUE BURN:

Man repress L,R OMS > L,R RCS TK PsFEED FROM GOOD POD:

OMS HE PRESS/VAP ISOL(two) – OP

TK ISOL (two) – OP

OMS XFEED (two) – CL

L,R RCS XFEED (four) – OPL,R RCS TK ISOL (six) – CL

�ADI – LVLH, center needlesTHC +X (�Lowest OMS % vs

RCS Burn Time)AFT RCS RECONFIGRCS COMPLETION



CONTINUE BURN:ITEM 18 +0 EXECG23 Resel jet




PREBANK/FLIPHP

AFTHP

TGTHP



CUTOFF VGOx = 0, Release THC+ :02 OMS ENG(s) – OFF (If < 3 IMU, at


:

**********************************************************

**********************************************************

TOPHinged at bottom of ‘DEORBIT BURN (MIXED XFEED)’

HINGE

ENT–5bb/D/I


THC +X to TGT HP

)

%

% then

(reduced copy)


TOP

ENTRY MANEUVERS

ENT–6a/E/LPILEVELCRO

PILEVELCRO

PILEVELCRO

PILEVELCRO


EI–5�LVLH ATT

GNC, OPS 304 PROIf PREBANK, R/Y – CSSRoll at 1°/sec toMaintain PREBANK ± 5°

If previous OMS OX TK or He TK or RCS OX TKleak: G51 VENT DOORS – OP

PTI – ENA at EI–5 when applicable

***

***

q = 1– (AOA) HYD MN PUMP PRESS (three) – NORM

‘GuidanceBox’ @

q ∼8or

D ∼3

–

CLOSED LOOP GUIDANCE ____:____:____If PREBANK: P,R/Y – AUTO

Begin AIL trim monitoring* *

D = 11 �DRAG H (FORCE if editing)V = 19K �MPS/TVC ISOL VLV – CLV = 15K �NAVAIDS (I/O RESET if reqd)

If ELS: UHF MODE – G T/R* *

V = 12K RAD BYP VLV MODE (two) – AUTOCNTLR LOOP (two) – AUTO B(A)

V = 10K �SPDBK to 81%

∆Az = 10.5° FIRST ROLL REVERSAL

(reduced copy)


50K

38K

28K

20K

12K

7K

/

/

/

/

/

/

/

ENT–6b/E/Q

TOPBACK OF ‘ENTRY MANEUVERS’

HOOKVELCRO

HOOKVELCRO

HOOKVELCRO

HOOKVELCRO

SURF /

3K

/1K

DRAG CHUTE DEPLOYMCC Call Flight ConditionEarly Main Gear TDNOMINAL 195 KEAS

If leaking/flat tiredelay derot 10 kts

Late Post–Nose Gear TDXwind DTO

EmergencyOnly

No DeployExcept CDR call

NO DEPLOYprior to MGTD> 230 KEAS< 80 KGSXwind > 15 kts


V = 7K �TACAN status

V = 5K ADTA PROBES – DEPLOY (�HEAT)Begin AIL and RUD trim monitoring

M = 2.7�APUs

HUD PWR (two) – ON

* If M < 2.5; P CSS for ADTA to G&C incorp *

M = 2.0 Ensure ADTA to G&C else �Theta limits

M = 0.9 P, R/Y – CSS as reqd�SPDBK CMD vs POS�R FLT CNTLR – ON�NWS – 1

Lock Inertia Reels

.MAX Nz

M = 0.7 �LG EXTEND ISOL VLV – OP

h = 15K �MLS

h = 10K �A/L, TABS/VISORS – CL/LES O2 – ON (KSC)

h = 2K LANDING GEAR ARM pb – ARM

h = 300 LANDING GEAR DN pb – DN

MAIN GEAR TD �SPDBK – 100%

V = 195 KEAS DRAG CHUTE pb (two) – ARM, DPY (simo)

V = 185 KEAS DEROTATE

NOSE GEAR TDSRB SEP – MAN/AUTO and depress pb

�Auto Load Relief�HYD BRAKE ISOL VLV (three) – OP

MIDFIELD andV < 140 KGS BRAKE as required (8–10 fps2, –0.25 to –0.3G)

* If 5K’ remaining and V > 140 KGS – MAX BRAKING *

V = 60 KGS DRAG CHUTE JETT pb – JETT

V = 40 KGS BRAKE < 6 fps2 (–0.2G) (Antiskid cutout)

WHEEL STOP Go to ENT C/L, POST LANDING PROCEDURES

(reduced copy)

CC

8–

18

EN

T/A

LL

/GE

N F

FAB

US

E O

NLY

TOP

HOOKVELCRO

ENTRY NO–GO CHECKLIST

HOOKVELCRO

ENT–7a/E/I

339

343

347

351

355

359

3

7

11

15

19

23

27

31

35

39

LVLHPITCH(deg)

20

15

10

5

TIMEto EI(min)

AERO AUTO XWINDFAILURE OF: PTI DTO FCS DTO

MODE 1APU/HYD: 1 APU X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

2 APUs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISPLAYS: 2 ADIs X. . . . . . . . . . . . . . . . . . . .

CDR HUD X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONTROLLERS:

RHC: 1L X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RHC: 2L & 2R X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RPTA: 2L or 2R X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

GNC: 2 AAs (LAT) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 AAs (NORM) X(M < 2.5) X. . . . . . . . . . . . . . . . . . 2 RGAs X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 R DDU PWR SPLY X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 IMU (or 1 IMU + BITE) X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 ADTAs X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADTA NOT INCORP

OR DLMA X (M < 2). . . . . . . . . . . . . . . . . . . . . . . . . . . . MLS NOT INCORP X(< 6K ft). . . . . . . . . . . . . . . . . . . . . 2 FCS CH (same surface) X X. . . . . . . . . . . . . . . . . . . . . . . . . .

DPS: 1 GPC (not restrung) X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 GPC (restrung) X. . . . . . . . . . . . . . . . 2 GPC (not restrung) X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 FF X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FF X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 FA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

RCS: LEAK (AFT – during ENT) X. . . . . . . 2 YAW JETs (same side) X. . . . . . . . . MIN RCS QTY X. . . . . . . . . . . . . . . . . .

TRIM: Ail > ± 2.0 deg X. . . . . . . . . . . . . . . . . . DOWNMODE:

FCS problem X X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AOA X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

PLB: PLBD Latch Gang X. . . . . . . . . . . . . . . LDG/DECEL:

Tire Leak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HYD BRAKE ISOL VLV X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . < 100% Brakes X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NWS X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

ENERGY – OFF NOMINAL:Roll Ref Alert X. . . . . . . . . . . . . . . . . . . Above Upper Traj Line X. . . . . . . . . . . . MCC GCA, or VEL & PSN

update X X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No A/L by 6K ft X. . . . . . . . . . . . . . . . . . . . . . . . . . . . .

DATA: OPS RECORDERS X(LOS). . . . . . . . . . . . XWIND:

< 10 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 15 Knots Peak X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . > 10 Knots Gust X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

GROUND SYSTEMS:No Runway Aim Point X. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

HOOKVELCRO

HOOKVELCRO

HOOKVELCRO

HOOKVELCRO

NOTES

1 Consider runway redesignation (M > 6) to avoid Xwind landing2 GO if PAPI and BALL BAR available3 Pitch AUTO mode NO–GO for M < 2.54 GO if only string 4 affected

HOOKVELCRO

HOOKVELCRO

4

4

2

3

3

3

(red

uce

d cop

y)

CC

8–

19

EN

T/A

LL

/GE

N F

FAB

US

E O

NLY

POST LANDINGMODE 5

TABS – RELEASEVISOR – CLOSE/LOCKLES O2 – ONGREEN APPLE – PULLKNEEBOARDS – REMOVECOOLING – DISCONNECTRESTRAINT – RELEASEPARACHUTE (four) – RELEASE

COMM – DISCONNECT(G–SUIT CLIP – PULL)LES O2 – DISCONNECTPLT – EMER PWR DOWNEGRESS SEATSLIDE/ESCAPE PANEL

HOOKVELCRO

HOOKVELCRO

RATIO < 1

MCC: AUTOor INH*

COMMOK

NOCOMM

IF BADADTA

RATIO > 1

G&CNAV

AUTO

TACANOK

MCC: INH

IF BAD NAVSTATE

MCC:FORCE

NO TACANADTA

ERRATICADTA

STEADYINH AUTO FORCE

Two or moregood ADTAs

Evaluate h,�,MMCC:

AUTO (G&C)

Evaluate h,�,MIf reasonable:

AUTO (G&C)

*(If ADTA H will degrade NAV state)

ADTA MGMT

HOOKVELCRO

HOOKVELCRO ENT–7b/E/N

TOPBACK OF ‘ENTRY NO–GO CHECKLIST’

V = 6K NO COMM TACAN MGMT

If 1st acq –FORCE

IF NOT –ZERO �STATE

RATIO< 1 RATIO > 1 ONE TACAN

LOCKED NO LOCK

AUTO TROUBLESHOOT BELOW V =5.5K

DESELECTMISSINGTACANS,then –AUTO

BELOW V =5.5K

TOGGLETACAN

IF BADTACAN

IF BAD NAVSTATE

AUTO

For � STATE UPDATES (on MCC call):P, R/Y – CSSDRAG H, TACAN, ADTA – INHOn MCC call, back to AUTO

NAV DELTA PAD

�Z 15 ( )

( )

( )

( )

( )

( )�X 10

�Y 11

�Z 12

�X 13

�Y 14

BAILOUTMODE 8

REPORT POSITION�MACH < .95

P, R/Y – CSS

OPS 305/603 PRO (if reqd)

SB – AUTO; BF – AUTO

FLY 185–195 KEAS, Φ = 0°ABORT MODE – ATO

ABORT PBI – PUSH

P,R/Y – AUTO

FLT CNTLR PWR (two) – OFF

∼50K FT

TABS – RELEASE

VISOR – CLOSE / LOCK

LES O2 – ON

GREEN APPLE – PULL

∼40K FT

MS3 – VENT CABIN

CDR,PLT SEATS – LOWER

KNEEBOARDS – REMOVE

COOLING – DISCONNECT

RESTRAINT – RELEASE

D–RING – UNCOVER

∼30K FT

MS3 – JETTISON HATCH

COMM – DISCONNECT

(G–SUIT CLIP – PULL)

LES O2 – DISCONNECT

EGRESS SEAT

POLE – DEPLOY

D–RING – HOOK UP

BAILOUT

(red

uce

d cop

y)

EN

T/A

LL

/GE

N F,1


�

�

�

��

TOP

��

��

�� MACH/�

��

ENT/8a/A,E/C

TOP BACK

HOOKVELCRO

ENT/8b/A,E/B

HOOKVELCRO

�

��

��

CC

8–

21

EN

T/A

LL

/GE

N F

FAB

US

E O

NLY

HOOKVELCRO

TOP

HOOKVELCRO

HOOKVELCRO

HOOKVELCRO

ENT–10a/A,E/A

ENTRY CONTROL

(Continued on back for ‘HIGH–FREQ OSC OR SURF/JET CYCLE’)

ARCS QTY (L + R) < 10%ARCS QTY = 0 & JETSFAIL OFF

1. ENTRY MODE – NO Y JET(R/Y CSS; expect sluggish control)

q ≥ 20 & M > 6 2. G51 ELEVON FIXED – ITEM 18 EXEC (*)

CONTROLPROBLEMS* &ARCS QTY > 0

3. ENTRY MODE – AUTOWhen control regained:

4. ENTRY MODE – NO Y JET5. �AIL trim

M < 6 & ARCS QTY > 0 6. ENTRY MODE – AUTOM < 5 7. TRIM/RHC PNL – ENA

8. TRIM ROLL – away from AIL trim (to < 1)*Region of least margin: M 12–8

AIL TRIM ≥ 3°TAL 1. G51 WRAP MODE – ITEM 45 EXEC (ACT)AIL trim = 5 2. BF – MAN

3. BF – UP (to 0%)NO Y JET 4. Perform roll reversals at 3°/s (expect sluggish control)M < 13 &AIL trim = 5

5. P – CSS6. Fly α per schedule:

M 12 11 10 9 8–6 5α 37 36 35 33 30 26

M < 5 7. TRIM/RHC PNL – ENA8. TRIM ROLL – away from AIL trim (to < 1)9. P – AUTO

M < 2 10. BF – AUTO

(red

uce

d cop

y)

CC

8–

22

EN

T/A

LL

/GE

N F

FAB

US

E O

NLY

HOOKVELCRO

TOPBACK OF ‘ENTRY CONTROL’

HOOKVELCRO

HOOKVELCRO

HOOKVELCRO

ENT–10b/A,E/A

HIGH–FREQ OSC OR SURF/JET CYCLEReturning PL> 10K lbs

1. G51 �FILTER ALT – ITEM 21 (*)

2. P, R/Y – CSSOsc/Cycle continues 3. ENTRY MODE – LO GAIN

Osc/Cyclestops

4. ENTRY MODE – AUTO5. P, R/Y – AUTO

(red

uce

d cop

y)





ENTRYCHECKLIST

JSC–48019GENERIC, REV F

Flight Cover (trim bottom to expose tabs)

ALL

Documents

Entry Checklist - NASA · ENT–798 ENT–799 ENT–801 ENT–802 MULTI–1599 MULTI–1616 Incorporate the following: 1. Replace vii thru x 2. Replace 2–3 & 2–2 (five pages each