Print Preview - C:DOCUME~1e3userLOCALS~1Tempe3temp 180

Citation SERVICE BULLETINSB750-76-09

REVISION TRANSMITTAL

This sheet transmits Revision 1 to SB750-76-09, which:A. Adds revision 1 of Rolls-Royce Service Bulletin AE 3007C-73-053.

B. Adds revision 1 of Rolls-Royce Service Bulletin AE 3007C-73-054.

C. Adds revision 1 of Rolls-Royce Service Bulletin AE 3007C-73-055.

NOTE: This revision replaces the original issue of SB750-76-09.

REVISION COMPLIANCE

NO EFFECT. Airplanes previously modified by this service bulletin are not effected by this revision.

LOG OF REVISIONS

Original Issue August 3, 2011

Revision 1 September 28, 2012

Original Issue - August 3, 2011 SB750-76-09Revision 1 - September 28, 2012 Page 1 of 1

Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271,Email: [email protected]

COPYRIGHT © 2011


TITLE

ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADEVERSION C9.2

EFFECTIVITY

MODEL SERIAL NUMBERS

750 (Citation X) -0001 thru -0312

The equivalent of this service bulletin has been incorporated on production airplanes -0313 and On.

NOTE: Airplanes -0001 thru -0172 must know if SB750-76-05 Engine Controls - Full Authority DigitalEngine Control (FADEC) Software Upgrade Version C9 (Enhanced) or SB750-76-08 EngineControls - Full Authority Digital Engine Control (FADEC) Software Upgrade Version C9.1 WithEnhanced Climb Performance have been accomplished before this service bulletin is started.

NOTE: Airplanes -0160 thru -0172 must know if SB750-71-10 Power Plant - 400 Pound Gross WeightAnd Five Percent Thrust Increase has been accomplished before this service bulletin is started.

REASON

C9.2 FADEC software upgrade incorporates changes that correct production and field issues related tothe current engine/FADEC software configuration. The primary changes involve solutions to:

1) Correcting ADC Revisionary Mode events on the ground during low speed takeoffs.

2) Providing additional ITT margin on eligible engines.

DESCRIPTION

This service bulletin provides parts and instructions to upgrade the FADEC to software version C9.2.

COMPLIANCE

RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period orphase inspection.

A service bulletin published by Cessna Aircraft Company may be recorded as “completed” in an aircraftlog only when the following requirements are satisfied:

1) The mechanic must complete all of the instructions in the service bulletin, including the intenttherein.

2) The mechanic must correctly use and install all applicable parts supplied with the service bulletinkit. Only with written authorization from Cessna Aircraft Company can substitute parts or rebuiltparts be used to replace new parts.

3) The mechanic or airplane owner must use the technical data in the service bulletin only asapproved and published.

4) The mechanic or airplane owner must apply the information in the service bulletin only to aircraftserial numbers identified in the “Effectivity” section of the bulletin.

5) The mechanic or airplane owner must use maintenance practices that are identified as acceptablestandard practices in the aviation industry and governmental regulations.

Original Issue - August 3, 2011 SB750-76-09Revision 1 - September 28, 2012 Page 1 of 5

Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271,Email: [email protected]

This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United Statesin accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991

COPYRIGHT © 2011

SB750-76-09Page 2 Revision 1 - September 28, 2012


No individual or corporate organization other than Cessna Aircraft Company is authorized to make orapply any changes to a Cessna-issued service bulletin, service letter, or flight manual supplement withoutprior written consent from Cessna Aircraft Company.

Cessna Aircraft Company is not responsible for the quality of maintenance performed to comply with thisdocument, unless the maintenance is accomplished at a Cessna-owned Citation Service Center.

APPROVAL

Cessna received FAA approval for the technical data in this publication that changes the airplane typedesign.

FLIGHT CREW OPERATIONS

No Changes

WEIGHT AND BALANCE INFORMATION

Negligible

REFERENCES

Cessna Model 750 Citation X Maintenance Manual

Rolls-Royce Maintenance Manual Subtask 77-21-25-420-001 Revision 58 or later

Rolls-Royce Service Bulletin AE 3007C-73-053, Engine Fuel and Control - New FADEC with SoftwareVersion C9.2 for the AE 30007C1 Engine, Revision 1 or later

Rolls-Royce Service Bulletin AE 3007C-73-054, Engine Fuel and Control - New FADEC with SoftwareVersion C9.2 for the AE 30007C Enhanced Engine, Revision 1 or later

Rolls-Royce Service Bulletin AE 3007C-73-055, Engine Fuel and Control - New FADEC with SoftwareVersion C9.2 for the AE 30007C Engine, Revision 1 or later

PUBLICATIONS AFFECTED

Cessna Model 750 Citation X Illustrated Parts Catalog

ACCOMPLISHMENT INSTRUCTIONS

1. Prepare the airplane for maintenance.

A. Make sure that all switches are in the OFF/NORM position.

B. Disconnect electrical power from the airplane.

(1) Disconnect the airplane battery.

(2) Disconnect external electrical power.

C. Attach maintenance warning tags to the battery and external power receptacle that have "DO NOTCONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" written on them.

2. Determine the airplane configuration:


Engine Serial NumberRange

SB750-76-08Compliance

SB750-71-10Compliance

AE3007C -0001 thru -0159 No Not ApplicableConfiguration A

AE3007C -0160 thru -0172 No No

AE3007CEnhanced -0001 thru -0159 Yes Not Applicable

Configuration BAE3007CEnhanced -0160 thru -0172 Yes No

AE3007C1 -0160 thru -0172 No YesConfiguration C

AE3007C1 -0173 thru -0312 Not Applicable Not Applicable

3. (Configuration A) Upgrade the FADECs.

A. Remove the left FADEC A (UK005), right FADEC A (UK004), left FADEC B (UK007) and rightFADEC B (UK006). (Refer to the Model 750 Maintenance Manual, Chapter 76, Full Authority DigitalEngine Control (FADEC) - Maintenance Practices.)

NOTE: The existing FADEC units are to be sent to either the Wichita, Sacramento, or San AntonioCitation Service Centers, for upgrade to Version C9.2 modification level and returned tothe owner/operator for installation. Contact one of the service centers listed above foradvanced scheduling instructions.

NOTE: International Customers: Exchange parts may be used in cases where the required partsare available as exchange. Order the exchange part and, upon completion expedite thereturn of the removed core to avoid return penalties. Contact Citation Parts Distribution,phone at 1-800-835-4000 (Domestic) or 1-316-517-7542 (International). Send Email to:[email protected] or telefax at 1-316-517-7711.

B. Install four upgraded 23089591, 23089594, 23089593, or 23089590 FADEC Version C9.2 Units(UK005, UK004, UK007 and UK006). (Refer to the Model 750 Maintenance Manual, Chapter 76,Full Authority Digital Engine Control (FADEC) - Maintenance Practices.)

C. Make sure that the correct ITT Trim Plug is installed. (Refer to the Rolls-Royce Maintenance ManualSubtask 77-21-25-420-001 Revision 58 or later).

D. Remove maintenance warning tags and connect the airplane batteries.

E. Do an operational check of the FADEC units per the Rolls-Royce Service Bulletin AE 3007C-73-055,Revison 1 or later, Engine Fuel and Control - New FADEC with Software Version C9.2 for theAE 30007C Engine.

4. (Configuration B) Upgrade the FADECs.




SB750-76-09Revision 1 - September 28, 2012 Page 3

SB750-76-09Page 4 Revision 1 - September 28, 2012





E. Do an operational check of the FADEC units per the Rolls-Royce Service Bulletin AE 3007C-73-054,Revision 1 or later, Engine Fuel and Control - New FADEC with Software Version C9.2 for the AE30007C Enhanced Engine.)

5. (Configuration C) Upgrade the FADECs.



NOTE: International Customers: Exchange parts may be used in cases where the required partsare available as exchange. Order the exchange part and, upon completion expedite thereturn of the removed core to avoid return penalties. Contact Citation Parts Distribution,phone at 1-800-835-4000 (Domestic) or 1-316-517-7542 (International). Send Emailto:[email protected] or telefax at 1-316-517-7711.




E. Do an operational check of the FADEC units per the Rolls-Royce Service Bulletin AE 3007C-73-053,Revision 1 or later, Engine Fuel and Control - New FADEC with Software Version C9.2 for theAE 30007C1 Engine.

6. Record that this service bulletin has been completed.

A. Complete a Maintenance Transaction Report.

B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook.

C. Send a copy of the completed Maintenance Transaction Report to: CESCOM C/O Camp SystemsInternational, 8200 East 34th Street North, Building 1600 Suite 1607 Wichita, KS 67226.

MATERIAL INFORMATION

(Configuration A) Upgrade to one of the parts that follow:


NEW P/N QUAN-TITY

KEY WORD OLD P/N INSTRUCTIONS/DISPOSITION

23089591 4 FADEC Version C9.2 23087358 Return to Cessna forupgrade




(Configuration B) Upgrade to one of the parts that follow:

NEW P/N QUAN-TITY






(Configuration C) Upgrade to one of the parts that follow:

NEW P/N QUAN-TITY






NOTE: The existing FADEC units are to be sent to either the Wichita, Sacramento, or San Antonio CitationService Centers, for upgrade to Version C9.2 modification level and returned to the owner/operator forinstallation. Contact one of the service centers listed above for advanced scheduling instructions.

NOTE: International Customers: Exchange parts may be used in cases where the required parts are availableas exchange. Order the exchange part and, upon completion expedite the return of the removed coreto avoid return penalties. Contact Citation Parts Distribution, phone at 1-800-835-4000 (Domestic)or 1-316-517-7542 (International). Send Email to: [email protected] or telefax at1-316-517-7711.

SB750-76-09Revision 1 - September 28, 2012 Page 5

Citation OWNER ADVISORYSB750-76-09

TITLEENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADEVERSION C9.2

TO:Cessna Aircraft Owner

REASONC9.2 FADEC software upgrade incorporates changes that correct production and field issues related tothe current engine/FADEC software configuration. The primary changes involve solutions to:

1) Correcting ADC Revisionary Mode events on the ground during low speed takeoffs

2) Providing additional ITT margin on eligible engines

COMPLIANCERECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period orphase inspection.

LABOR HOURS

WORK PHASE MAN-HOURS

Modification 6.0

Original Issue - September 28, 2012 SB750-76-09Revision 1 - August 22, 2014 Page 1 of 3

Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800

This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United Statesin accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991

COPYRIGHT © 2012

SB750-76-09Page 2 Revision 1 - August 22, 2014


MATERIAL AVAILABILITY

PART NUMBER AVAILABILITY COST23089591 * *

23089594 * *

23089593 * *

23089590 * *

23089602 * *

23089601 * *

23089600 * *

23089599 * *

23089598 * *

23089597 * *

23089596 * *

23089595 * *

NOTE: Owner/Operators: The existing FADEC units are to be sent to either the Wichita, Sacramento,or San Antonio Citation Service Centers, for upgrade to Version C9.2 modification level andreturned to the owner/operator for installation. Contact one of the service centers listed above foradvanced scheduling instructions.


* Please contact Cessna Service Parts & Programs for current cost and availability of parts listed in thisservice bulletin. Phone at 1-800-835-4000 (Domestic) or 1-316-517-7542 (International). Send emailto: [email protected] or telefax at 1-316-517-7711.

Based on availability and lead times, parts may require advanced scheduling.

In cases where the required part(s) are available as exchange, order the exchange part and, uponcompletion, expedite the return of the removed core to avoid return penalties. Contact the CessnaService Parts & Programs Sales Desk for availability of exchange parts.


WARRANTYThis bulletin is recommended. Eligible airplanes may qualify for parts and labor coverage, as describedbelow.

Eligibility: All Citations identified within the serial number effectivity of this service bulletin..

Parts Coverage: Cessna-owned and Cessna-authorized Citation Service Facilities, operators, or othermaintenance facilities may submit a Citation Credit Claim Form for the parts required toaccomplish this bulletin.

Labor Coverage: Cessna-owned and Cessna-authorized Citation Service Facilities may submit a CitationCredit Claim Form for the labor necessary to accomplish this service bulletin. Please noteManpower Requirements for coverage guidelines.

CreditApplication:

All work must be completed and the Citation Credit Claim Form submitted before the dateshown below. Send the Citation Credit Claim, along with any required parts (see MaterialInformation), to the point of purchase.Parts to be returned to Cessna Service Parts & Programs should be forwarded to:

Citation Warranty Administration7121 Southwest BoulevardWichita, KSUSA 67215

Expiration: December 31, 2015

NOTE: As a convenience, service documents are now available online to all our customers through asimple, free-of-charge registration process. If you would like to sign up, please visit the "CustomerAccess" link at www.cessnasupport.com to register.

SB750-76-09Revision 1 - August 22, 2014 Page 3

July 22, 2011

TO: Recipients of AE 3007C Series Service Bulletins

SUBJECT: Service Bulletin AE 3007C--73--053, Engine Fuel and Control --New FADEC with Software Version C9.2 for the AE 3007C1 Engine

This letter transmits Revision 1 to the subject service bulletin. Replace the originalissue with this Revision 1.

This is a complete revision.

Revision 1 transmits revision 1 of Goodrich Service Bulletin AFFU100--73--7764.

If you have complied with the previous issue of this bulletin, no additional work isrequired.

The following list includes the original issue date and all revisions to this bulletin:

Original issue May 2, 2011Revision 1 July 22, 2011

CUSTOMER SUPPORTROLLS--ROYCE

Rolls--Royce CorporationP.O. BOX 420Indianapolis, IN 46206 USAPhone: 317--230--3774Fax: 317--230--6084email: [email protected]

CHECK THAT ALL PREVIOUS TRANSMITTALS HAVE BEEN INCORPORATED -- if any have not been received please adviseRolls--Royce Corporation Publication Services, Indianapolis, Indiana, USA

P U B L I C A T I O N T R A N S M I T T A L

May 2, 2011

Page 1 of 8

AE 3007C--73--053Revision 1July 22, 2011

ENGINE FUEL AND CONTROL -- NEW FADEC WITH SOFTWAREVERSION C9.2 FOR THE AE 3007C1 ENGINE

1. PLANNING INFORMATION

A. Effectivity

(1) Engines

All AE 3007C1 engines.

(2) Spares

This service bulletin can be applicable to any FADEC with hardware P/N 23073177,23074372 or 23085791.

NOTE: The FADEC hardware P/N is located on the small label on top of the FADEC(Ref. FIG. 1).

B. Reason

This bulletin introduces new FADEC hardware and software assemblies (23089595 and23089598) that incorporates FADEC software version C9.2 (23089589).

FADEC Software version C9.2 is an incremental change from the FADEC software version C9.1used on the AE 3007C1 engine.

FADEC Software version C9.2 upgrade incorporates changes that correct production and fieldissues related to the current FADEC software configuration. The primary changes include:-- Correcting ADC Reversionary Mode events on ground during low speed Takeoff-- Providing additional ITT margin on eligible engines.

C. Description

This service bulletin gives you the procedure to reprogram the FADEC hardware and softwareassembly (FADEC assembly) (any FADEC with hardware P/N 23074372 or 23085791) toFADEC assembly (23089595 or 23089598) and change the FADEC identification labels.

A Goodrich Engine Control Systems authorized representative will reprogram and reidentify theFADEC assemblies.

This service bulletin transmits Goodrich service bulletins AFFU100--73--7764 revision 1 andAFFU101--73--7764.

D. Approval

Technical aspects are FAA approved.

SERVICEBULLETIN

EXPORT CONTROLLED

Rolls--RoyceSERVICE BULLETIN

EXPORT CONTROLLED

May 2, 2011

Page 2 of 8


E. Manpower

On Wing Approximately 3.0 man--hours are necessary to remove, reprogram,reidentify and install the two FADECs for each engine (approximately6.0 man--hours per aircraft).

FADEC spares Approximately 1.0 man--hour is necessary to reprogram and reidentifythe FADEC.

Required labor will be reimbursed by Rolls-Royce when accomplished for eligible engines underthe stated effectivity and compliance at Cessna Service Centers.

F. Compliance

This service bulletin is recommended. You should do this service bulletin at the next convenientmaintenance opportunity after this FADEC software version is available.

G. Interchangeability -- Not affected

H. Material Availability

Customers should contact Cessna or Rolls--Royce to coordinate the reprogramming of theFADECs.

I. Tooling -- Not applicable

J. Weight and Balance -- Not affected

K. Electrical Load Data -- Not affected

L. References

(1) Advance Engineering Memorandum (AEM), CN500012715295.

NOTE: The document above is referenced for the internal use of Rolls-Royce only.

(2) AE 3007C Fault Isolation Manual (FIM), CSP34065.

(3) AE 3007C Illustrated Parts Catalog (IPC), CSP33001.

(4) AE 3007C Maintenance Manual (MM), CSP34012.

(5) Cessna Model 750 Aircraft Maintenance Manual (AMM).

(6) Goodrich Service Bulletin AFFU100--73--7764, Engine Fuel and Control -- Full AuthorityDigital Engine Control Type AFFU100 -- Introduction of C9.2 Software. S/W IdentityG307CU64D.


(8) Service Bulletin AE 3007C--72--301, Engine -- Find the Hot Section Configuration forUpdated Maximum Continuous Interstage Turbine Temperature (ITT) Limits.

(9) Service Bulletin AE 3007C--73--046, Engine Fuel and Control -- New FADEC DiodeAdapter.

M. Prerequisites

(1) Service Bulletin AE 3007C--73--046.

N. Corequisites -- None


EXPORT CONTROLLED

May 2, 2011

Page 3 of 8


2. ACCOMPLISHMENT INSTRUCTIONS

A. Reprogram the FADEC assemblies.

REF. FIG. 1

REF. FIG. 2

REF. TABLE 1

REF. TABLE 2

REF. TABLE 3

(1) Remove electrical power from the FADEC assemblies (Ref. Cessna Model 750 AMM).

(2) Remove the four FADECs from the aircraft (Ref. TASK 73--25--10--000--801, MM).

(a) If the FADEC has diode adapter (86632307) attached to the J4 connector, thendisconnect the electrical connector from the diode adapter. Do not remove theanti--tamper label and the diode adapter from the J4 connector.

(3) Reprogram and reidentify the FADEC assemblies by the Goodrich authorized servicetechnician in accordance with Goodrich Service Bulletin AFFU100--73--7764 orAFFU101--73--7764.

(4) When the Goodrich authorized service technician reidentifies the FADEC, do the steps thatfollow:

(a) Make sure that the small FADEC Modification Label on the top of the FADEC, showsthe following information (Ref. TABLE 1) (Ref. FIG. 1):

Rolls-Royce HardwarePart Number

23074372OR

23085791

FADEC Modification Label -- Hardware Part Number InformationTABLE 1


EXPORT CONTROLLED

May 2, 2011

Page 4 of 8


(b) Make sure that the large FADEC Unit Label to be placed on the top of the FADEC,shows the following information (Ref. TABLE 2) (Ref. FIG. 1):

ForRolls-RoyceHardware

Part Number

Rolls-RoycePart Number

Goodrich FADECType Number

Goodrich FADECInstallationNumber

Goodrich LUCOLSoftware Number

23074372 23089598 AFFU100--03AN02 86625446 G307CU64D

23085791 23089595 AFFU101--02AN02 86634559

Large FADEC Unit Label -- InformationTABLE 2

NOTE: For FADEC with hardware part number 23085791 (see service bulletin AE3007C--73--046) do not remove the diode adapter label (Ref. FIG. 2).

(c) Make sure that the small FADEC Aircraft Identification Label to be placed near theFADEC connectors shows the following information (Ref. TABLE 3) (Ref. FIG. 1):

Rolls-Royce PartNumber

AE 3007 Series ModelNumber

Aircraft Model Approvedfor FADEC Installation

Aircraft Type Approvedfor FADEC Installation

23089598 AE 3007C1 Model 750 Citation X

Small FADEC Aircraft Identification Label -- InformationTABLE 3

NOTE: The attached Goodrich service bulletin is for use by Goodrich authorizedservice technicians or other authorized personnel.

(5) Install the four FADEC assemblies (Ref. TASK 73--25--10--400--801, MM). To make surethat the correct ITT trim plug is installed on the engine, use AE 3007C MaintenanceManual Revision 56 or later.

(a) If necessary, connect the diode adapter to the J4 connector (Ref. TASK70--00--00--910--804, MM) and put the anti--tamper label on the FADEC and the diodeadapter (Ref. AE 3007C--73--046, SB).

CAUTION: DO NOT OPERATE THE AIRCRAFT UNLESS ALL FOUR OF THE FADECSHAVE THE SAME SOFTWARE VERSION INSTALLED. INCORRECT ENGINEOPERATION CAN RESULT FROM USING FADECS WITH TWO DIFFERENTSOFTWARE VERSIONS.

(6) Supply electrical power to the FADECs (Ref. Cessna Model 750 AMM).

(7) Put the avionics power switch to the ON position (Ref. Cessna Model 750 AMM).

(8) Cycle all of the FADEC circuit breakers (breakers) by opening and closing the breakersthree times.

(9) Examine the EICAS display for the messages listed below:

(a) FADEC BUS FAIL L/R -- A/B

(b) FADEC FAIL L/R -- A/B

(c) FADEC FAULT L/R -- A/B

(d) FADEC REV ADC -- L/R

(e) FADEC REV N1 L/R


EXPORT CONTROLLED

May 2, 2011

Page 5 of 8


(10) If any of the above messages are displayed on the EICAS, do the appropriate faultisolation task for the message displayed (Ref. FIM).

CAUTION: THE ENGINES SHOULD NOT BE OPERATED WITH ANY OF THE ABOVELISTED EICAS MESSAGES DISPLAYED. DAMAGE TO THE ENGINE CANRESULT.

(11) Do the engine operational check with FADEC channel A selected in control for bothengines (Ref. TASK 72--00--00--700--801, MM).

NOTE: Do not remove electrical power from the avionics bus.

CAUTION: IF ANY OF THE MESSAGES LISTED BELOW ARE DISPLAYED ON THEEICAS, STOP THE ENGINE. ENGINE DAMAGE CAN RESULT.


(a) ENG TLA FAILED L/R

(b) FADEC BUS FAIL L/R -- A/B

(c) FADEC FAIL L/R -- A/B

(d) FADEC FAULT L/R -- A/B

(e) FADEC REV ADC -- L/R

(f) FADEC REV N1 L/R

(13) If none of the messages in 2.A.(12) are displayed, go to step 2.A.(14).

If any of the messages listed in 2.A.(12) are displayed on the EICAS, do the following:

(a) Stop the engine (Ref. TASK 72--00--00--700--801, MM).

(b) Do the appropriate fault isolation task for the message displayed (Ref. FIM).

(c) Do steps 2.A.(11) thru 2.A.(13) again.

(14) Use the right--hand multi--function display (MFD) to access the engine maintenancemessages in the aircraft maintenance test (AMT) for all four FADECs(Ref. Introduction, FIM).

(15) If any engine--related maintenance messages are shown on the MFD, do the appropriatefault isolation task for the message displayed (Ref. FIM).

(16) Do steps 2.A.(11) thru 2.A.(13) again with FADEC channel B selected in control for bothengines.

B. Record compliance with this service bulletin.

(1) Remove the FADEC cards from Section1 Part VII of the engine records. Discard theEngine Equipment Record cards. This record card will no longer be issued for the FADEC.

(2) Record the part number and serial number of each installed FADEC in Section 1 Part II ofthe engine records.

(3) Record compliance with this service bulletin in Section 1 Part III of the engine records.

C. Complete the Service Bulletin Compliance form and return it to:

AE Service DataRolls--Royce CorporationAttn: AE Service Data ManagerP.O. Box 420, Speed Code U17Indianapolis, Indiana 46206--0420USA

E--mail [email protected] 317--230--4010


EXPORT CONTROLLED

May 2, 2011

Page 6 of 8


FADEC Identification Labels -- Proper Location of Specific DataFIG. 1


EXPORT CONTROLLED

May 2, 2011

Page 7 of 8


FADEC with Diode Adapter LabelFIG. 2


EXPORT CONTROLLED

May 2, 2011

Page 8 of 8


3. MATERIAL INFORMATION

A. Configuration Chart

NEW ROLLS-ROYCE P/N

QTY/ENG NAME

ROLLS-ROYCE

HARDWAREOLD P/N

QTY/ENG

INSTRUCTIONS/DISPOSITION

23089598OR

2 FADEC Assy, Hardwareand Software

23074372 2 1

23089595 2 FADEC Assy, Hardwareand Software

23085791 2 1

INSTRUCTIONS/DISPOSITION NOTES

1. Program item to new software version.

B. Consumable Materials -- None

C. Expendable Parts -- None

CUSTOMER SUPPORTROLLS-ROYCE

May 2, 2011

Page 1 of 3

Revision 1July 22, 2011

AE 3007C--73--053

SERVICE BULLETIN COMPLIANCE

ENGINE FUEL AND CONTROL -- NEW FADEC WITH SOFTWAREVERSION C9.2 FOR THE AE 3007C1 ENGINE

LEFT ENGINE:Engine Serial Number: ________________Engine Hours: ________________Engine Cycles: ________________

RIGHT ENGINE:Engine Serial Number: ________________Engine Hours: ________________Engine Cycles: ________________

AIRCRAFT:Aircraft Serial Number: ________________Aircraft Tail Number: ________________

Operator: ________________Name of person completing form: ________________Phone: ________________Fax: ________________Date: ________________

FADEC A Serial Numbers: ________________________________

FADEC B Serial Numbers: ________________________________

Return this Service Bulletin Compliance Form to:AE Service DataRolls--Royce CorporationAttn: AE Service Data ManagerP.O. Box 420, Speed Code U17Indianapolis, Indiana 46206--0420USA

Email: [email protected]: 317--230--4010

SERVICEBULLETIN

EXPORT CONTROLLED


EXPORT CONTROLLED

ALERT

May 2, 2011

Page 2 of 3


AE 3007C--73--053

July 22, 2011


SUBJECT: Service Bulletin AE 3007C--73--054, Engine Fuel and Control --New FADEC with Software Version C9.2 for the AE 3007C1Enhanced Engine











May 2, 2011

Page 1 of 8


ENGINE FUEL AND CONTROL -- NEW FADEC WITH SOFTWAREVERSION C9.2 FOR THE AE 3007C ENHANCED ENGINE


A. Effectivity

(1) Engines

All AE 3007C engines.

(2) Spares



B. Reason


FADEC Software version C9.2 is an incremental change from the FADEC software version C9.1used on the AE 3007C engine.

FADEC Software version C9.2 upgrade incorporates changes that correct production and fieldissues related to the current FADEC software configuration as well as an on wing lifeimprovement. The primary changes include:-- Correcting ADC Reversionary Mode events on ground during low speed Takeoff-- Providing additional ITT margin on eligible engines.

C. Description




D. Approval


SERVICEBULLETIN

EXPORT CONTROLLED


EXPORT CONTROLLED

May 2, 2011

Page 2 of 8


E. Manpower



F. Compliance

This service bulletin is optional.



Customers should contact Cessna or Rolls--Royce for the current price of this service bulletinand to coordinate the reprogramming of the FADECs.




L. References



(2) AE 3007C Series Fault Isolation Manual (FIM), CSP34065.

(3) AE 3007C Series Illustrated Parts Catalog (IPC), CSP33001.

(4) AE 3007C Series Maintenance Manual (MM), CSP34012.






M. Prerequisites




EXPORT CONTROLLED

May 2, 2011

Page 3 of 8




REF. FIG. 1

REF. FIG. 2

REF. TABLE 1

REF. TABLE 2

REF. TABLE 3








23074372OR

23085791



EXPORT CONTROLLED

May 2, 2011

Page 4 of 8




Part Number





23074372 23089602 AFFU100--03AN03 -- --

23085791 23089599 AFFU101--02AN03 --








23089602 AE 3007C Enhanced Model 750 Citation X
















EXPORT CONTROLLED

May 2, 2011

Page 5 of 8






























EXPORT CONTROLLED

May 2, 2011

Page 6 of 8




EXPORT CONTROLLED

May 2, 2011

Page 7 of 8




EXPORT CONTROLLED

May 2, 2011

Page 8 of 8




NEW ROLLS-ROYCE P/N

QTY/ENG NAME

ROLLS-ROYCE

HARDWAREOLD P/N

QTY/ENG


23089602OR


23074372 2 1


23085791 2 1






May 2, 2011

Page 1 of 3


AE 3007C--73--054


ENGINE FUEL AND CONTROL -- NEW FADEC WITH SOFTWAREVERSION C9.2 FOR THE AE 3007C ENHANCED ENGINE









SERVICEBULLETIN

EXPORT CONTROLLED


EXPORT CONTROLLED

ALERT

May 2, 2011

Page 2 of 3


AE 3007C--73--054

July 22, 2011


SUBJECT: Service Bulletin AE 3007C--73--055, Engine Fuel and Control --New FADEC with Software Version C9.2 for the AE 3007C Engine











May 2, 2011

Page 1 of 8


ENGINE FUEL AND CONTROL -- NEW FADEC WITH SOFTWAREVERSION C9.2 FOR THE AE 3007C ENGINE


A. Effectivity

(1) Engines

All AE 3007C engines.

(2) Spares



B. Reason


FADEC Software version C9.2 is an incremental change from the FADEC software version C9.1used on the AE 3007C engine.

FADEC Software version C9.2 upgrade incorporates changes that correct production and fieldissues related to the current FADEC software configuration as well as an on wing lifeimprovement. The primary changes include:-- Correcting ADC Reversionary Mode events on ground during low speed Takeoff-- Providing additional ITT margin on eligible engines.

C. Description




D. Approval


SERVICEBULLETIN

EXPORT CONTROLLED


EXPORT CONTROLLED

May 2, 2011

Page 2 of 8


E. Manpower



Required labor will be reimbursed by Rolls-Royce when accomplished for eligible engines underthe stated effectivity and compliance at Cessna Service Centers.

F. Compliance

This service bulletin is recommended. You should do this service bulletin at the next convenientmaintenance opportunity after this FADEC software version is available.



Customers should contact Cessna or Rolls--Royce to coordinate the reprogramming of theFADECs.




L. References



(2) AE 3007C Series Fault Isolation Manual (FIM), CSP34065.

(3) AE 3007C Series Illustrated Parts Catalog (IPC), CSP33001.

(4) AE 3007C Series Maintenance Manual (MM), CSP34012.






M. Prerequisites




EXPORT CONTROLLED

May 2, 2011

Page 3 of 8




REF. FIG. 1

REF. FIG. 2

REF. TABLE 1

REF. TABLE 2

REF. TABLE 3








23074372OR

23085791



EXPORT CONTROLLED

May 2, 2011

Page 4 of 8




Part Number





23074372 23089594 AFFU100--03AN01 -- G307CU64D

23085791 23089590 AFFU101--02AN01 --








23089594 AE 3007C Model 750 Citation X
















EXPORT CONTROLLED

May 2, 2011

Page 5 of 8






























EXPORT CONTROLLED

May 2, 2011

Page 6 of 8




EXPORT CONTROLLED

May 2, 2011

Page 7 of 8




EXPORT CONTROLLED

May 2, 2011

Page 8 of 8




NEW ROLLS-ROYCE P/N

QTY/ENG NAME

ROLLS-ROYCE

HARDWAREOLD P/N

QTY/ENG


23089594OR


23074372 2 1


23085791 2 1






May 2, 2011

Page 1 of 3


AE 3007C--73--055


ENGINE FUEL AND CONTROL -- NEW FADEC WITH SOFTWAREVERSION C9.2 FOR THE AE 3007C ENGINE









SERVICEBULLETIN

EXPORT CONTROLLED


EXPORT CONTROLLED

ALERT

May 2, 2011

Page 2 of 3


AE 3007C--73--055

Documents

Print Preview - C:DOCUME~1e3userLOCALS~1Tempe3temp 180