SERVICE BULLETIN TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10

Transcription

1 Citation SB TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10 EFFECTIVITY REASON MODEL SERIAL NUMBERS 750 (Citation X) thru NOTE: Airplanes thru must know if SB Engine Controls - Full Authority Digital Engine Control (FADEC) Software Upgrade Version C9.2 or SB Engine Controls - Full Authority Digital Engine Control (FADEC) Software Upgrade Version C9.2 have been accomplished before this service bulletin is started. NOTE: Airplanes thru must know if SB Power Plant Pound Gross Weight And Five Percent Thrust Increase has been accomplished before this service bulletin is started. This service bulletin improves T2.5 initial check to fix no dispatch condition seen at cold/high airports. DESCRIPTION This service bulletin provides parts and instructions to remove the engine FADECs and send them to Textron Aviation for an upgrade. COMPLIANCE RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period or inspection. A service bulletin published by Textron Aviation may be recorded as completed in an aircraft log only when the following requirements are satisfied: 1) The mechanic must complete all of the instructions in the service bulletin, including the intent therein. 2) The mechanic must correctly use and install all applicable parts supplied with the service bulletin kit. Only with written authorization from Textron Aviation can substitute parts or rebuilt parts be used to replace new parts. 3) The mechanic or airplane owner must use the technical data in the service bulletin only as approved and published. 4) The mechanic or airplane owner must apply the information in the service bulletin only to aircraft serial numbers identified in the Effectivity section of the bulletin. 5) The mechanic or airplane owner must use maintenance practices that are identified as acceptable standard practices in the aviation industry and governmental regulations. No individual or corporate organization other than Textron Aviation is authorized to make or apply any changes to a Textron Aviation-issued service bulletin, service letter, or flight manual supplement without prior written consent from Textron Aviation. Textron Aviation is not responsible for the quality of maintenance performed to comply with this document, unless the maintenance is accomplished at a Textron Aviation-owned Service Center. SB September 12, 2016 Page 1 of 5 Textron Aviation Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2016

2 Citation SB APPROVAL Textron Aviation received FAA approval for the technical data in this publication that changes the airplane type design. Textron Aviation received EASA approval for the technical data in this publication that changes the airplane type design. FLIGHT CREW OPERATIONS No Changes WEIGHT AND BALANCE INFORMATION Negligible REFERENCES Cessna Model 750 Citation X Maintenance Manual Rolls-Royce Maintenance Manual Subtask Revision 58 or later Rolls-Royce Service Bulletin AE 3007C , Engine Fuel and Control - New FADEC with Software Version C10 for the AE 30007C1 Engine Rolls-Royce Service Bulletin AE 3007C , Engine Fuel and Control - New FADEC with Software Version C10 for the AE 30007C Enhanced Engine Rolls-Royce Service Bulletin AE 3007C , Engine Fuel and Control - New FADEC with Software Version C10 for the AE 30007C Engine PUBLICATIONS AFFECTED Cessna Model 750 Citation X Illustrated Parts Catalog ACCOMPLISHMENT INSTRUCTIONS 1. Prepare the airplane for maintenance. A. Make sure that the airplane is electrically grounded. B. Make sure that all switches are in the OFF/NORM position. C. Disconnect electrical power from the airplane. (1) Disconnect the airplane batteries. (2) Disconnect external electrical power. D. Attach maintenance warning tags to the batteries and external power receptacle that have "DO NOT CONNECT ELECTRICAL POWER - MAINTENANCE IN PROGRESS" written on them. 2. Determine the airplane configuration. If the configuration is Configuration A, go to Step 3. If the configuration is Configuration B, go to Step 4. If the configuration is Configuration C, go to Step 5. SB Page 2 September 12, 2016

3 Citation SB Configuration A Configuration B Configuration C Engine Serial Number Range SB Compliance SB Compliance AE3007C thru No Not Applicable AE3007C thru No No AE3007C Enhanced AE3007C Enhanced thru Yes Not Applicable thru Yes No AE3007C thru No Yes AE3007C thru 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 right FADEC B (UK006). (Refer to the Model 750 Maintenance Manual, Chapter 76, Full Authority Digital Engine Control (FADEC) - Maintenance Practices.) NOTE: If a Diode Adapter is installed on the FADEC, the Diode Adapter must stay installed on the FADEC. NOTE: The existing FADEC units are to be sent to either the Wichita, Sacramento, San Antonio, or Paris Citation Service Centers, for upgrade to Version C10 modification level and returned to the owner/operator for installation. Contact one of the service centers listed above for advanced scheduling instructions. B. Install four upgraded or FADEC Version C10 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 Manual Subtask Revision 58 or later.) D. Remove maintenance warning tags and connect the airplane batteries. E. Do an operational check of the FADEC units. (Refer to Rolls-Royce Service Bulletin AE 3007C , Revison 1 or later, Engine Fuel and Control - New FADEC with Software Version C10 for the AE 30007C Engine.) 4. (Configuration B) Upgrade the FADECs. A. Remove the left FADEC A (UK005), right FADEC A (UK004), left FADEC B (UK007) and right FADEC B (UK006). (Refer to the Model 750 Maintenance Manual, Chapter 76, Full Authority Digital Engine Control (FADEC) - Maintenance Practices.) NOTE: If a Diode Adapter is installed on the FADEC, the Diode Adapter must stay installed on the FADEC. NOTE: The existing FADEC units are to be sent to either the Wichita, Sacramento, San Antonio, or Paris Citation Service Centers, for upgrade to Version C10 modification level and returned to the owner/operator for installation. Contact one of the service centers listed above for advanced scheduling instructions. B. Install four upgraded or FADEC Version C10 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 Manual Subtask Revision 58 or later.) D. Remove maintenance warning tags and connect the airplane batteries. SB September 12, 2016 Page 3

4 Citation SB E. Do an operational check of the FADEC units. (Refer to Rolls-Royce Service Bulletin AE 3007C , Engine Fuel and Control - New FADEC with Software Version C10 for the AE 30007C Enhanced Engine.) 5. (Configuration C) Upgrade the FADECs. A. Remove the left FADEC A (UK005), right FADEC A (UK004), left FADEC B (UK007) and right FADEC B (UK006). (Refer to the Model 750 Maintenance Manual, Chapter 76, Full Authority Digital Engine Control (FADEC) - Maintenance Practices.) NOTE: If a Diode Adapter is installed on the FADEC, the Diode Adapter must stay installed on the FADEC. NOTE: The existing FADEC units are to be sent to either the Wichita, Sacramento, San Antonio, or Paris Citation Service Centers, for upgrade to Version C10 modification level and returned to the owner/operator for installation. Contact one of the service centers listed above for advanced scheduling instructions. B. Install four upgraded or FADEC Version C10 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 Manual Subtask Revision 58 or later.) D. Remove maintenance warning tags and connect the airplane batteries. E. Do an operational check of the FADEC units. (Refer to Rolls-Royce Service Bulletin AE 3007C , Engine Fuel and Control - New FADEC with Software Version C10 for the AE 30007C1 Engine.) 6. Make an entry in the airplane logbook that states compliance and method of compliance with this service document. NOTE: Textron Aviation recommends that compliance with all service documents is reported to Camp Systems International. Complete a record of compliance. (Maintenance Transaction Report, Log Book Entry, or other record of compliance.) Put a copy of the completed record of compliance in the airplane logbook. Send a copy of the completed record of compliance to: Camp Systems International Incorporated, 8201 East 34th Street North, Building 1100 Suite 1101 Wichita, KS SB Page 4 September 12, 2016

5 Citation SB MATERIAL INFORMATION (Configuration A) Upgrade to one of the parts that follow: NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION FADEC Version C Return for upgrade FADEC Version C Return for upgrade (Configuration B) Upgrade to one of the parts that follow: NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION FADEC Version C Return for upgrade FADEC Version C Return for upgrade (Configuration C) Upgrade to one of the parts that follow: NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION FADEC Version C Return for upgrade FADEC Version C Return for upgrade NOTE: The existing FADEC units are to be sent to either the Wichita, Sacramento, or Paris Citation Service Centers, for upgrade to Version C10 modification level and returned to the owner/operator for installation. Contact one of the service centers listed above for advanced scheduling instructions. SB September 12, 2016 Page 5

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7 Citation OWNER ADVISORY SB TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10 TO: Cessna Aircraft Owner REASON This service bulletin improves T2.5 initial check to fix no dispatch condition seen at cold/high airports. COMPLIANCE RECOMMENDED. This service bulletin should be accomplished at a scheduled maintenance period or inspection. LABOR HOURS WORK PHASE MATERIAL AVAILABILITY LABOR-HOURS Modification 6.0 PART NUMBER AVAILABILITY COST * * * * * * * * * * * * NOTE: The existing FADEC units are to be sent to either the Wichita, Sacramento, San Antonio, or Paris Citation Service Centers, for upgrade to Version C10 modification level and returned to the owner/operator for installation. Contact one of the service centers listed above for advanced scheduling instructions. WARRANTY This bulletin is recommended. Eligible airplanes may qualify for parts and labor coverage to the extent noted in the Labor Hours and Material Availability sections of this document. SB September 12, 2016 Page 1 of 2 Textron Aviation Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT 2016

8 Citation OWNER ADVISORY SB Eligibility: Parts Coverage: Labor Coverage: Credit Application: All airplanes identified within the serial number effectivity of this service document. Textron Aviation-owned and Textron Aviation-authorized Service Facilities, operators, or other maintenance facilities may submit a claim for the parts required to accomplish this service document as defined in the Material Availability section of this document. Textron Aviation-owned and Textron Aviation-authorized Service Facilities rated to perform maintenance on the specific model of Cessna Aircraft may submit a claim for the labor necessary to accomplish this service document as defined in the Labor Hours section of this document. After this service document has been accomplished, a claim must be submitted to Textron Aviation within 30 days of the service document completion. Claims for compliance of this service document are to be filed as a W3 type claim. Please submit your claim form online at ww2.txtav.com/parts or the completed Textron Aviation Claim Form to warranty@txtav.com. If submitted on-line a Return Authorization will be provided. If a paper claim is submitted your claim will be entered in to the system and a Return Authorization will be sent to you. The Return Authorization must accompany any required return parts (see Material Availability, to the point of purchase. Expiration: Parts to be returned to Textron Aviation Parts Distribution should be forwarded to: Textron Aviation Parts Distribution Warranty Administration 285 South Greenwich Road Bldg B89, Docks 1-4 Wichita, KS USA September 12, 2018 (after this date the owner/operator assumes the responsibility for compliance costs) Textron Aviation reserves the right to void continued airplane warranty coverage for the parts affected by this service document until the service document is accomplished. NOTE: As a convenience, service documents are now available online to all our customers through a simple, free-of-charge registration process. If you would like to sign up, please visit the "Customer Access" link at to register. SB Page 2 September 12, 2016

9 EXPORT CONTROLLED SERVICE BULLETIN ENGINE FUEL AND CONTROL - NEW FADEC WITH SOFTWARE VERSION C10 FOR THE AE 3007C ENGINE 1. PLANNING INFORMATION A. Effectivity (1) Engines All AE 3007C engines. (2) Spares This service bulletin can be applicable to FADECs with hardware P/N or NOTE: The FADEC hardware P/N is located on the small label on top of the FADEC (Ref.FIG.1). B. Reason This service bulletin introduces new FADEC hardware and software assemblies ( and ) that incorporate FADEC software version C10 ( ). FADEC software version C10 is an incremental change from the FADEC software version C9.2 used on the AE 3007C engine. FADEC software version C10 upgrade incorporates changes that correct production and field issues related to the current FADEC software configuration as well as an on--wing life improvement. The primary changes include: (1) Incorporation of Shaft Break Logic. (2) Incorporation of NDOT Starting Logic. (3) MN Reasonable Data Limit Improvement. (4) TLA Fault Accommodation Logic Improvements. (5) T2.5 to ADC Difference Check Logic Improvements. (6) ITT Software Trim and CVG Schedule Change to Increase Max Con Margin. (7) Annunciation of Inflight POWINT to Maintenance Computer. C. Description This service bulletin gives you the procedure to reprogram the FADEC hardware and software assembly (FADEC assembly) (FADECs with hardware P/N or ) to FADEC assembly ( or ) and change the FADEC identification labels. A Rolls--Royce Controls and Data Services (CDS) authorized representative will reprogram and reidentify the FADEC assemblies. This service bulletin transmits CDS service bulletins AFFU and AFFU D. Approval Technical aspects are FAA approved. March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page1of8

10 EXPORT CONTROLLED E. Manpower On Wing FADEC Spares Rolls -Royce Approximately 3.0 man--hours are necessary to remove, reprogram, reidentify, and install the two FADECs for each engine (approximately 6.0 man--hours for each aircraft). Approximately 1.0 man--hour is necessary to reprogram and reidentify the FADEC. F. Compliance This service bulletin is recommended. You can do this service bulletin at the next convenient maintenance opportunity after this FADEC software version is available. G. Interchangeability -- Not affected H. Material Availability Customers can contact Cessna or Rolls--Royce for the current price of this service bulletin and to coordinate the reprogramming of the FADEC. I. Tooling -- Not applicable J. Weight and Balance -- Not affected K. Electrical Load Data -- Not affected L. References (1) Advance Engineering Memorandum (AEM), CN NOTE: The document above is referenced for the internal use of Rolls-Royce only. (2) AE 3007C Series Fault Isolation Manual (FIM), CSP (3) AE 3007C Series Illustrated Parts Catalog (IPC), CSP (4) AE 3007C Series Maintenance Manual (MM), CSP (5) Cessna Model 750 Aircraft Maintenance Manual (AMM). (6) CDS Service Bulletin AFFU , Engine Fuel and Control -- Full Authority Digital Engine Control Type AFFU Introduction of C10 Software. S/W Identity G307CU65B. (7) CDS Service Bulletin AFFU , Engine Fuel and Control -- Full Authority Digital Engine Control Type AFFU Introduction of C10 Software. S/W Identity G307CU65B. (8) Service Bulletin AE 3007C , Engine Fuel and Control -- New FADEC Diode Adapter. M. Prerequisites (1) Service Bulletin AE 3007C N. Corequisites -- None March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page2of8

11 EXPORT CONTROLLED 2. ACCOMPLISHMENT INSTRUCTIONS Rolls -Royce 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 , MM). (a) If the FADEC has diode adapter ( ) attached to the J4 connector, then disconnect the electrical connector from the diode adapter. Do not remove the anti--tamper label and the diode adapter from the J4 connector. (3) Reprogram and reidentify the FADEC assemblies by the CDS authorized service technician in accordance with CDS Service Bulletin (SB) AFFU or AFFU (attached). (4) When CDS authorized service technician reidentifies the FADEC, do the steps that follow: (a) Make sure that the small FADEC Modification Label on the top of the FADEC shows the information that follows (Ref. TABLE 1) (Ref. FIG. 1): TABLE 1 -- FADEC Modification Label -- Hardware Part Number Information ROLLS--ROYCE HARDWARE PART NUMBER OR (b) Make sure that the large FADEC Unit Label to be placed on the top of the FADEC shows the information that follows: FOR ROLLS--ROYCE HARDWARE PART NUMBER TABLE 2 -- Large FADEC Unit Label -- Information ROLLS--ROYCE ASSEMBLY PART NUMBER GOODRICH FADEC TYPE NUMBER GOODRICH FADEC INSTALLATION NUMBER GOODRICH LUCOL SOFTWARE NUMBER AFFU AW G307CU65B AFFU AW G307CU65B NOTE: For FADEC with hardware part number (Ref. AE 3007C , SB), do not remove the diode adapter label (Ref. FIG. 2). March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page3of8

12 EXPORT CONTROLLED (c) Rolls -Royce Make sure that the small FADEC Aircraft Identification Label to be placed near the FADEC connectors shows the information that follows (Ref. TABLE 3) (Ref. FIG.1): TABLE 3 -- Small FADEC Aircraft Identification Label -- Information ROLLS--ROYCE ASSEMBLY PART NUMBER AE 3007 SERIES MODEL NUMBER AIRCRAFT MODEL APPROVED FOR FADEC INSTALLATION AIRCRAFT TYPE APPROVED FOR FADEC INSTALLATION or AE 3007C Model 750 Citation X NOTE: The attached CDS SB is for use by CDS authorized service technicians or other authorized personnel. (5) Install the four FADEC assemblies (Ref. TASK , MM). To make sure that the correct ITT trim plug is installed on the engine, use AE 3007C Maintenance Manual Revision 56 or later. (a) If necessary, connect the diode adapter to the J4 connector (Ref. TASK , MM) and put the anti--tamper label on the FADEC and the diode adapter (Ref. AE 3007C , SB). CAUTION: DO NOT OPERATE THE AIRCRAFT UNLESS ALL FOUR OF THE FADECS HAVE THE SAME SOFTWARE VERSION INSTALLED. INCORRECT ENGINE OPERATION CAN RESULT FROM USE OF FADECS WITH TWO DIFFERENT SOFTWARE 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) when you open and close the breakers three 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 (10) If one or more of the above messages are displayed on the EICAS, then do the appropriate fault isolation task for the message displayed (Ref. Introduction, FIM). CAUTION: THE ENGINES CANNOT BE OPERATED WITH ONE OR MORE OF THE DISPLAYED EICAS MESSAGES LISTED ABOVE. DAMAGE TO THE ENGINE CAN RESULT. (11) Do the engine operational check with FADEC channel A selected in control for both engines (Ref. TASK , MM). NOTE: Do not remove electrical power from the avionics bus. CAUTION: IF ONE OR MORE OF THE MESSAGES LISTED BELOW ARE DISPLAYED ON THE EICAS, THEN STOP THE ENGINE. DAMAGE TO THE ENGINE CAN RESULT. March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page4of8

13 EXPORT CONTROLLED Rolls -Royce (12) Examine the EICAS display for the messages listed below: (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 step 2.A.(12) are displayed, then go to step 2.A.(14). If one or more of the messages listed in step 2.A.(12) are displayed on the EICAS, the do the steps that follow: (a) Stop the engine (Ref. TASK , 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 maintenance messages in the aircraft maintenance test (AMT) for all four FADECs (Ref. Introduction, FIM). (15) If one or more engine--related maintenance messages are shown on the MFD, then do the appropriate fault 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 both engines. B. Record compliance with this service bulletin. (1) Remove the FADEC cards from Section 1, Part VII of the engine records. Discard the Engine 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 of the 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 Data Rolls--Royce Corporation Attention: AE Service Data Manager 450 South Meridian Street, Mail Code MC--N3--04 Indianapolis, Indiana USA cra.del.data@rolls--royce.com FAX: March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page5of8

14 EXPORT CONTROLLED Rolls -Royce FADEC Identification Labels -- Proper Location of Specific Data FIG. 1 March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page6of8

15 EXPORT CONTROLLED Rolls -Royce FADEC with Diode Adapter Label FIG. 2 March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page7of8

16 EXPORT CONTROLLED 3. MATERIAL INFORMATION Rolls -Royce A. Configuration Chart -- Not applicable NEW P/N OR QTY/ ENG NAME OLD P/N 2 FADEC Assy, Hardware and Software FADEC Assy, Hardware and Software INSTRUCTIONS/DISPOSITION NOTES 1. Program item to new software version. B. Consumable Materials -- None C. Expendable Parts -- None QTY/ ENG INSTRUCTIONS/ DISPOSITION CUSTOMER SUPPORT ROLLS-ROYCE March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page8of8

17 EXPORT CONTROLLED SERVICE BULLETIN COMPLIANCE ENGINE FUEL AND CONTROL - NEW FADEC WITH SOFTWARE VERSION C10 FOR THE AE 3007C 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 Data Rolls--Royce Corporation Attn: AE Service Data Manager 450 South Meridian Street, Speed Code MC--N3--04 Indianapolis, Indiana USA cra.rel.data@rolls-royce.com FAX: March 14, 2016 AE 3007C Page1of3

18 EXPORT CONTROLLED Rolls -Royce March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page9of8

19 ROLLS-ROYCE CONTROLS AND DATA SERVICES SHAFTMOOR LANE HALL GREEN BIRMINGHAM B28 8SW ENGLAND TELEPHONE: FAX: TRANSMITTAL FULL AUTHORITY DIGITAL ENGINE CONTROL, TYPE: AFFU100 ATA REF THIS PAGE TRANSMITS THE INITIAL ISSUE OF AFFU Reason for issue Introduction of C10 Software. S/W Identity G307CU65B. Action Keep this SB with the Component Maintenance Manual. Put in this SB Transmittal page and the SB pages 1 thru 10 dated. APPROVED FOR CONTROLS AND DATA SERVICES Signed: Date:22nd January 2016 TRANSMITTAL AFFU Page 1 of 2

20 Controls and Data Services BLANK PAGE TRANSMITTAL AFFU Page 2 of 2

21 Controls and Data Services ENGINE FUEL AND CONTROL - CONTROL - FULL AUTHORITY DIGITAL ENGINE CONTROL TYPE AFFU100 - INTRODUCTION OF C10 SOFTWARE. S/W IDENTITY G307CU65B 1. Planning Information A. Effectivity AFFU100, Full Authority Digital Engine Control (FADEC), unit type numbers given below: AFFU AH-1 AFFU AH-1 AFFU AH-1 AFFU AK-01 AFFU AK-01 AFFU AK-01 AFFU AK-02 AFFU AK-02 AFFU AK-02 AFFU AL-01 AFFU AL-01 AFFU AL-01 AFFU AL-02 AFFU AL-02 AFFU AL-02 AFFU AL-03 AFFU AL-03 AFFU AL-03 AFFU100-01AM01 AFFU100-02AM01 AFFU100-03AM01 AFFU100-01AM02 AFFU100-02AM02 AFFU100-03AM02 AFFU100-01AM03 AFFU100-02AM03 AFFU100-03AM03 AFFU100-01AN01 AFFU100-02AN01 AFFU100-03AN01 AFFU100-01AN02 AFFU100-02AN02 AFFU100-03AN02 AFFU100-01AN03 AFFU100-02AN03 AFFU100-03AN03 NOTE: This Service Bulletin can also be applicable to any other FADEC types with the Rolls-Royce Hardware Part Numbers , or B. Concurrent Requirements Not applicable. C. Reason A number of improvements were identified to correct production and field issues related to the current FADEC software and on-wing life improvement, the main changes in C10 software include: Incorporation of Shaft Break Logic Incorporation of Ndot Starting Logic MN Reasonable Data Limit Improvement TLA Fault Accommodation Logic Improvements T2.5 to ADC Difference Check Logic Improvements ITT Software Trim and CVG Schedule Change to Increase Max Con Margin Annunciation of Inflight POWINT to Maintenance Computer. D. Description This Service Bulletin introduces a new version of FADEC software (C10 Identity G307CU65B) to introduce the improvements identified in para 1.C. AFFU Page 1 of 10

22 Controls and Data Services When the accomplishment instructions (Para. 3) have been done the FADEC type number changes as follows: (1) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-01AW01 or AFFU100-01AW02 or AFFU100-01AW03. (2) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-02AW01 or AFFU100-02AW02 or AFFU100-02AW03. (3) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-03AW01 or AFFU100-03AW02 or AFFU100-03AW03. E. Compliance Controlled Service Introduction To be only fitted on New Production / Overhaul and Repair, in accordance with Rolls- Royce purchase order or other authoritative method as agreed with Rolls-Royce Corporation. F. Approval This Service Bulletin have been technically agreed by Rolls-Royce Corporation. G. Manpower Program and identify one FADEC - one hour. H. Weight and Balance None. I. Electrical Load Data Not Changed. J. Software Accomplishment Summary Refer to the Aero Engine Controls, Software Accomplishment Summary document No. J408/0080 issue 1. K. References Controls and Data Services modification CP7831 AFFU100 Component Maintenance Manual (CMM) L. Other Publications Affected AFFU100 Component Maintenance Manual (CMM) M. Interchangeability or Intermix-ability of Parts Not applicable. AFFU Page 2 of 10

23 2. Material Information A. Material - Price and Availability Controls and Data Services This modification is chargeable to the operator or requesting party. B. Industry Support Information Not applicable. C. Material Necessary for Each Component NOTE: If necessary, use the equivalent alternatives for the items given in the table below: New P/N Description Old P/N Qty Instruction Note or Unit Label (preferred) or Unit Label (alternative) Aircraft Identification Label Modification Label Instruction Note(s): 1. Discard and install new item. 2. Replace with new item if necessary. D. Reidentified Parts (1) When the FADEC is programmed with the new software, the unit type number changes as follows: AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-01AW01 AFFU100-01AM01 AFFU100-01AN01 AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-02AW01 AFFU100-02AM01 AFFU100-02AN01 AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-03AW01 AFFU100-03AM01 AFFU100-03AN01 AFFU Page 3 of 10

24 Controls and Data Services AFFU AK-02 AFFU AL-02 AFFU100-01AM02 AFFU100-01AN02 become AFFU100-01AW02 AFFU AK-02 AFFU AL-02 AFFU100-02AM02 AFFU100-02AN02 AFFU AK-02 AFFU AL-02 AFFU100-03AM02 AFFU100-03AN02 AFFU AL-03 AFFU100-01AM03 AFFU100-01AN03 AFFU AL-03 AFFU100-02AM03 AFFU100-02AN03 AFFU AL-03 AFFU100-03AM03 AFFU100-03AN03 become become become become become AFFU100-02AW02 AFFU100-03AW02 AFFU100-01AW03 AFFU100-02AW03 AFFU100-03AW03 3. Accomplishment Instructions The accomplishment instructions must be done by an authorised Maintenance, Repair and Overhaul facility. The FADEC is programmed with the new software through a connector on the front of the FADEC. A. Procedure (Refer to the CMM, ) (1) Make sure that the new control software is installed in the FADEC Programming Facility. (2) Install the new control software into the FADEC (refer to the Testing and Fault Isolation section in the CMM). (3) Carefully remove the FADEC unit label (refer to Repair No.3 in the CMM). AFFU Page 4 of 10

25 Controls and Data Services (4) Make sure that the new unit label, either ( ) or ( ), is marked with the applicable data that follows: (a) Unit Label ( ) marking: Type NO. AFFU100-01AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A INST. NO SW STD G307CU65B Type NO AFFU100-03AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B Type NO AFFU100-01AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A AFFU Page 5 of 10

26 Controls and Data Services INST. NO SW STD G307CU65B Type NO AFFU100-03AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B Type NO AFFU100-01AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A INST. NO SW STD G307CU65B Type NO AFFU100-03AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B AFFU Page 6 of 10

27 Controls and Data Services (b) Unit Label ( ) marking (refer to Figure 1) REV A Unit Label ( ) marking areas Figure 1 TP29382 NOTE: The new unit label ( ) will be marked by hand or machine with the data that follows: The character size for Allison (RRC) part number must be 7,11 to 8,13 mm (0.28 to 0.32 in). REV A must be marked in character size 1,98 to 2,69 mm (0.078 to in) on the new label outside of the label data blocks in the approximate location as shown in Figure 1. Additional human readable data on the unit label is acceptable and the order of this data can vary to fit into the label data blocks: AFFU100-01AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW01 Allison Part No AFFU Page 7 of 10

28 Controls and Data Services Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-01AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-01AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU Page 8 of 10

29 Controls and Data Services (5) Install the new unit label (marked at step 3.A.(4)) to the FADEC (refer to Repair No.3 in the CMM). (6) Carefully remove the Aircraft Identification Label (refer to Repair No.3 in the CMM). (7) Make sure that the new Aircraft Identification Label is marked with the necessary data as follows: AFFU100-01AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-02AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-01AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-02AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-01AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 AFFU Page 9 of 10

30 BOX 4 Controls and Data Services CITATION X AFFU100-02AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 BOX 4 CITATION X (8) Install the new Aircraft Identification Label (marked at step 3.A.(7)) to the FADEC (refer to Repair No.3 in the CMM). (9) If it is necessary to replace the modification label ( ) then do the procedure that follows: (a) (b) Carefully remove the modification label (refer to Repair No.3 in the CMM). Make sure the new modification label is marked with the data that follows: serial number of the FADEC, related hardware part number (refer to Para. 1.D.), applicable modification number(s). (c) Install the new modification label (marked at step 3.A.(9)(b)) to the FADEC (refer to Repair No.3 in the CMM). (10) If it is necessary to do the test procedure on the new FADEC types (refer to the Testing and Fault Isolation section in the CMM) use the software files identified in the latest PAT Schedule: LUCOL Software Test Files G307C65B Refer to the latest PAT Schedule AFFU Page 10 of 10

31

32 ROLLS-ROYCE CONTROLS AND DATA SERVICES SHAFTMOOR LANE HALL GREEN BIRMINGHAM B28 8SW ENGLAND TELEPHONE: FAX: TRANSMITTAL FULL AUTHORITY DIGITAL ENGINE CONTROL, TYPE: AFFU101 ATA REF THIS PAGE TRANSMITS THE INITIAL ISSUE OF AFFU Reason for issue Introduction of C10 Software. S/W Identity G307CU65B. Action Keep this SB with the Component Maintenance Manual. Put in this SB Transmittal page and the SB pages 1 thru 5 dated. APPROVED FOR CONTROLS AND DATA SERVICES Signed: Date:22nd January 2016 TRANSMITTAL AFFU Page 1 of 2

33 Controls and Data Services BLANK PAGE TRANSMITTAL AFFU Page 2 of 2

34 Controls and Data Services ENGINE FUEL AND CONTROL - CONTROL - FULL AUTHORITY DIGITAL ENGINE CONTROL TYPE AFFU101 - INTRODUCTION OF C10 SOFTWARE. S/W IDENTITY G307CU65B 1. Planning Information A. Effectivity AFFU101, Full Authority Digital Engine Control (FADEC), unit type numbers given below: AFFU101-02AL01 AFFU101-02AL02 AFFU101-02AL03 AFFU101-02AM01 AFFU101-02AM02 AFFU101-02AM03 AFFU101-02AN01 AFFU101-02AN02 AFFU101-02AN03 B. Concurrent Requirements Not applicable. C. Reason A number of improvements were identified to correct production and field issues related to the current FADEC software and on-wing life improvement, the main changes in C10 software include: Incorporation of Shaft Break Logic Incorporation of Ndot Starting Logic MN Reasonable Data Limit Improvement TLA Fault Accommodation Logic Improvements T2.5 to ADC Difference Check Logic Improvements ITT Software Trim and CVG Schedule Change to Increase Max Con Margin Annunciation of Inflight POWINT to Maintenance Computer. D. Description This Service Bulletin introduces a new version of software (C10 Identity G307CU65B) to introduce the improvements identified in para 1.C. When the accomplishment instructions (Para. 3) have been done the FADEC type number changes as follows: AFFU Page 1 of 5

35 Controls and Data Services (1) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU101-02AW01 or AFFU101-02AW02 or AFFU101-02AW03. E. Compliance Controlled Service Introduction To be only fitted on New Production / Overhaul and Repair, in accordance with Rolls- Royce purchase order or other authoritative method as agreed with Rolls-Royce Corporation. F. Approval This Service Bulletin have been technically agreed by Rolls-Royce Corporation. G. Manpower Program and identify one FADEC - one hour. H. Weight and Balance None. I. Electrical Load Data Not Changed. J. Software Accomplishment Summary Refer to the Aero Engine Controls, Software Accomplishment Summary document No. J408/0080 issue 1. K. References Controls and Data Services modification CP7831 AFFU101 Component Maintenance Manual (CMM) L. Other Publications Affected AFFU101 Component Maintenance Manual (CMM) M. Interchangeability or Intermix-ability of Parts Not applicable. 2. Material Information A. Material - Price and Availability This modification is chargeable to the operator or requesting party. B. Industry Support Information Not applicable AFFU Page 2 of 5

36 Controls and Data Services C. Material Necessary for Each Component NOTE: If necessary, use the equivalent alternatives for the items given in the table below: New P/N Description Old P/N Qty Instruction Note Unit Label Modification Label Instruction Note(s): 1. Discard and install new item. 2. Replace with new item if necessary. D. Reidentified Parts (1) When the FADEC is programmed with the new software, the unit type number changes as follows: AFFU101-02AL01 AFFU101-02AM01 become AFFU101-02AW01 AFFU101-02AN01 AFFU101-02AL02 AFFU101-02AM02 become AFFU101-02AW02 AFFU101-02AN02 AFFU101-02AL03 AFFU101-02AM03 become AFFU101-02AW03 AFFU101-02AN03 3. Accomplishment Instructions The accomplishment instructions must be done by an authorised Maintenance, Repair and Overhaul facility. The FADEC is programmed with the new software through a connector on the front of the FADEC. A. Procedure (Refer to the CMM, ) (1) Make sure that the new control software is installed in the FADEC Programming Facility. (2) Install the new control software into the FADEC (refer to the Testing and Fault Isolation section in the CMM). (3) Carefully remove the FADEC unit label (refer to Repair No.3 in the CMM). AFFU Page 3 of 5

37 Controls and Data Services (4) Make sure that the new unit label ( ) is marked with the applicable data given below (refer to Figure 1): REV A Unit Label ( ) marking areas Figure 1 TP29382 NOTE: The new unit label ( ) will be marked by hand or machine with the data that follows: The character size for Allison (RRC) part number must be 7,11 to 8,13 mm (0.28 to 0.32 in). REV A must be marked in character size 1,98 to 2,69 mm (0.078 to in) on the new label outside of the label data blocks in the approximate location as shown in Figure 1. Additional human readable data on the unit label is acceptable and the order of this data can vary to fit into the label data blocks: AFFU101-02AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU Page 4 of 5

38 Controls and Data Services AFFU101-02AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU101-02AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B (5) Install the new unit label (marked at step 3.A.(4)) to the FADEC (refer to Repair No.3 in the CMM). (6) If it is necessary to replace the modification label ( ) then do the procedure that follows: (a) (b) Carefully remove the modification label (refer to Repair No.3 in the CMM). Make sure the new modification label is marked with the data that follows: serial number of the FADEC, related hardware part number (refer to Para. 1.D.), applicable modification number(s). (c) Install the new modification label (marked at step 3.A.(6)(b)) to the FADEC (refer to Repair No.3 in the CMM). (7) If it is necessary to do the test procedure on the new FADEC types (refer to the Testing and Fault Isolation section in the CMM) use the software files identified in the latest PAT Schedule. LUCOL Software Test Files G307C65B Refer to latest PAT Schedule AFFU Page 5 of 5

39 EXPORT CONTROLLED SERVICE BULLETIN ENGINE FUEL AND CONTROL - NEW FADEC WITH SOFTWARE VERSION C10 FOR THE AE 3007C ENHANCED ENGINE 1. PLANNING INFORMATION A. Effectivity (1) Engines All AE 3007C Enhanced engines. (2) Spares This service bulletin can be applicable to FADECs with hardware P/N or NOTE: The FADEC hardware P/N is located on the small label on top of the FADEC (Ref.FIG.1). B. Reason This service bulletin introduces new FADEC hardware and software assemblies ( and ) that incorporate FADEC software version C10 ( ). FADEC software version C10 is an incremental change from the FADEC software version C9.2 used on the AE 3007C engine. FADEC software version C10 upgrade incorporates changes that correct production and field issues related to the current FADEC software configuration as well as an on--wing life improvement. The primary changes include: (1) Incorporation of Shaft Break Logic. (2) Incorporation of NDOT Starting Logic. (3) MN Reasonable Data Limit Improvement. (4) TLA Fault Accommodation Logic Improvements. (5) T2.5 to ADC Difference Check Logic Improvements. (6) ITT Software Trim and CVG Schedule Change to Increase Max Con Margin. (7) Annunciation of Inflight POWINT to Maintenance Computer. C. Description This service bulletin gives you the procedure to reprogram the FADEC hardware and software assembly (FADEC assembly) (FADECs with hardware P/N or ) to FADEC assembly ( or ) and change the FADEC identification labels. A Rolls--Royce Controls and Data Services (CDS) authorized representative will reprogram and reidentify the FADEC assemblies. This service bulletin transmits CDS service bulletins AFFU and AFFU D. Approval Technical aspects are FAA approved. March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page1of8

40 EXPORT CONTROLLED E. Manpower On Wing FADEC Spares Rolls -Royce Approximately 3.0 man--hours are necessary to remove, reprogram, reidentify, and install the two FADECs for each engine (approximately Approximately 1.0 man--hour is necessary to reprogram and reidentify the FADEC. F. Compliance This service bulletin is optional. G. Interchangeability -- Not affected H. Material Availability Customers can contact Cessna or Rolls--Royce for the current price of this service bulletin and to coordinate the reprogramming of the FADECs. I. Tooling -- Not applicable J. Weight and Balance -- Not affected K. Electrical Load Data -- Not affected L. References (1) Advance Engineering Memorandum (AEM), CN NOTE: The document above is referenced for the internal use of Rolls-Royce only. (2) AE 3007C Series Fault Isolation Manual (FIM), CSP (3) AE 3007C Series Illustrated Parts Catalog (IPC), CSP (4) AE 3007C Series Maintenance Manual (MM), CSP (5) Cessna Model 750 Aircraft Maintenance Manual (AMM). (6) CDS Service Bulletin AFFU , Engine Fuel and Control -- Full Authority Digital Engine Control Type AFFU Introduction of C10 Software. S/W Identity G307CU65B. (7) CDS Service Bulletin AFFU , Engine Fuel and Control -- Full Authority Digital Engine Control Type AFFU Introduction of C10 Software. S/W Identity G307CU65B. (8) Service Bulletin AE 3007C , Engine Fuel and Control -- New FADEC Diode Adapter. M. Prerequisites (1) Service Bulletin AE 3007C N. Corequisites -- None March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page2of8

41 EXPORT CONTROLLED 2. ACCOMPLISHMENT INSTRUCTIONS Rolls -Royce 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 , MM). (a) If the FADEC has diode adapter ( ) attached to the J4 connector, then disconnect the electrical connector from the diode adapter. Do not remove the anti--tamper label and the diode adapter from the J4 connector. (3) Reprogram and reidentify the FADEC assemblies by the CDS authorized service technician in accordance with CDS Service Bulletin (SB) AFFU or AFFU (attached). (4) When CDS authorized service technician reidentifies the FADEC, do the steps that follow: (a) Make sure that the small FADEC Modification Label on the top of the FADEC shows the information that follows (Ref. TABLE 1) (Ref. FIG. 1): TABLE 1 -- FADEC Modification Label -- Hardware Part Number Information ROLLS--ROYCE HARDWARE PART NUMBER OR (b) Make sure that the large FADEC Unit Label to be placed on the top of the FADEC shows the information that follows: FOR ROLLS--ROYCE HARDWARE PART NUMBER TABLE 2 -- Large FADEC Unit Label -- Information ROLLS--ROYCE ASSEMBLY PART NUMBER GOODRICH FADEC TYPE NUMBER GOODRICH FADEC INSTALLATION NUMBER GOODRICH LUCOL SOFTWARE NUMBER AFFU AW G307CU65B AFFU AW G307CU65B NOTE: For FADEC with hardware part number (Ref. AE 3007C , SB), do not remove the diode adapter label (Ref. FIG. 2). March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page3of8

42 EXPORT CONTROLLED (c) Rolls -Royce Make sure that the small FADEC Aircraft Identification Label to be placed near the FADEC connectors shows the information that follows (Ref. TABLE 3) (Ref. FIG.1): TABLE 3 -- Small FADEC Aircraft Identification Label -- Information ROLLS--ROYCE ASSEMBLY PART NUMBER AE 3007 SERIES MODEL NUMBER AIRCRAFT MODEL APPROVED FOR FADEC INSTALLATION AIRCRAFT TYPE APPROVED FOR FADEC INSTALLATION or AE 3007C Enhanced Model 750 Citation X NOTE: The attached CDS SB is for use by CDS authorized service technicians or other authorized personnel. (5) Install the four FADEC assemblies (Ref. TASK , MM). To make sure that the correct ITT trim plug is installed on the engine, use AE 3007C Maintenance Manual Revision 56 or later. (a) If necessary, connect the diode adapter to the J4 connector (Ref. TASK , MM) and put the anti--tamper label on the FADEC and the diode adapter (Ref. AE 3007C , SB). CAUTION: DO NOT OPERATE THE AIRCRAFT UNLESS ALL FOUR OF THE FADECS HAVE THE SAME SOFTWARE VERSION INSTALLED. INCORRECT ENGINE OPERATION CAN RESULT FROM USE OF FADECS WITH TWO DIFFERENT SOFTWARE 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) when you open and close the breakers three 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 (10) If one or more of the above messages are displayed on the EICAS, then do the appropriate fault isolation task for the message displayed (Ref. Introduction, FIM). CAUTION: THE ENGINES CANNOT BE OPERATED WITH ONE OR MORE OF THE DISPLAYED EICAS MESSAGES LISTED ABOVE. DAMAGE TO THE ENGINE CAN RESULT. (11) Do the engine operational check with FADEC channel A selected in control for both engines (Ref. TASK , MM). NOTE: Do not remove electrical power from the avionics bus. CAUTION: IF ONE OR MORE OF THE MESSAGES LISTED BELOW ARE DISPLAYED ON THE EICAS, THEN STOP THE ENGINE. DAMAGE TO THE ENGINE CAN RESULT. March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page4of8

43 EXPORT CONTROLLED Rolls -Royce (12) Examine the EICAS display for the messages listed below: (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 step 2.A.(12) are displayed, then go to step 2.A.(14). If one or more of the messages listed in step 2.A.(12) are displayed on the EICAS, then do the steps that follow: (a) Stop the engine (Ref. TASK , 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 maintenance messages in the aircraft maintenance test (AMT) for all four FADECs (Ref. Introduction, FIM). (15) If one or more engine--related maintenance messages are shown on the MFD, then do the appropriate fault 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 both engines. B. Record compliance with this service bulletin. (1) Remove the FADEC cards from Section 1, Part VII of the engine records. Discard the Engine 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 of the 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 Data Rolls--Royce Corporation Attention: AE Service Data Manager 450 South Meridian Street, Mail Code MC--N3--04 Indianapolis, Indiana USA cra.del.data@rolls--royce.com FAX: March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page5of8

44 EXPORT CONTROLLED Rolls -Royce FADEC Identification Labels -- Proper Location of Specific Data FIG. 1 March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page6of8

45 EXPORT CONTROLLED Rolls -Royce FADEC with Diode Adapter Label FIG. 2 March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page7of8

46 EXPORT CONTROLLED 3. MATERIAL INFORMATION Rolls -Royce A. Configuration Chart -- Not applicable NEW P/N OR QTY/ ENG NAME OLD P/N 2 FADEC Assy, Hardware and Software FADEC Assy, Hardware and Software INSTRUCTIONS/DISPOSITION NOTES 1. Program item to new software version. B. Consumable Materials -- None C. Expendable Parts -- None QTY/ ENG INSTRUCTIONS/ DISPOSITION CUSTOMER SUPPORT ROLLS-ROYCE March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page8of8

47 EXPORT CONTROLLED SERVICE BULLETIN COMPLIANCE ENGINE FUEL AND CONTROL - NEW FADEC WITH SOFTWARE VERSION C10 FOR THE AE 3007C 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 Data Rolls--Royce Corporation Attn: AE Service Data Manager 450 South Meridian Street, Speed Code MC--N3--04 Indianapolis, Indiana USA cra.rel.data@rolls-royce.com FAX: March 14, 2016 AE 3007C Page1of3

48 EXPORT CONTROLLED Rolls -Royce March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page9of8

49 ROLLS-ROYCE CONTROLS AND DATA SERVICES SHAFTMOOR LANE HALL GREEN BIRMINGHAM B28 8SW ENGLAND TELEPHONE: FAX: TRANSMITTAL FULL AUTHORITY DIGITAL ENGINE CONTROL, TYPE: AFFU100 ATA REF THIS PAGE TRANSMITS THE INITIAL ISSUE OF AFFU Reason for issue Introduction of C10 Software. S/W Identity G307CU65B. Action Keep this SB with the Component Maintenance Manual. Put in this SB Transmittal page and the SB pages 1 thru 10 dated. APPROVED FOR CONTROLS AND DATA SERVICES Signed: Date:22nd January 2016 TRANSMITTAL AFFU Page 1 of 2

50 Controls and Data Services BLANK PAGE TRANSMITTAL AFFU Page 2 of 2

51 Controls and Data Services ENGINE FUEL AND CONTROL - CONTROL - FULL AUTHORITY DIGITAL ENGINE CONTROL TYPE AFFU100 - INTRODUCTION OF C10 SOFTWARE. S/W IDENTITY G307CU65B 1. Planning Information A. Effectivity AFFU100, Full Authority Digital Engine Control (FADEC), unit type numbers given below: AFFU AH-1 AFFU AH-1 AFFU AH-1 AFFU AK-01 AFFU AK-01 AFFU AK-01 AFFU AK-02 AFFU AK-02 AFFU AK-02 AFFU AL-01 AFFU AL-01 AFFU AL-01 AFFU AL-02 AFFU AL-02 AFFU AL-02 AFFU AL-03 AFFU AL-03 AFFU AL-03 AFFU100-01AM01 AFFU100-02AM01 AFFU100-03AM01 AFFU100-01AM02 AFFU100-02AM02 AFFU100-03AM02 AFFU100-01AM03 AFFU100-02AM03 AFFU100-03AM03 AFFU100-01AN01 AFFU100-02AN01 AFFU100-03AN01 AFFU100-01AN02 AFFU100-02AN02 AFFU100-03AN02 AFFU100-01AN03 AFFU100-02AN03 AFFU100-03AN03 NOTE: This Service Bulletin can also be applicable to any other FADEC types with the Rolls-Royce Hardware Part Numbers , or B. Concurrent Requirements Not applicable. C. Reason A number of improvements were identified to correct production and field issues related to the current FADEC software and on-wing life improvement, the main changes in C10 software include: Incorporation of Shaft Break Logic Incorporation of Ndot Starting Logic MN Reasonable Data Limit Improvement TLA Fault Accommodation Logic Improvements T2.5 to ADC Difference Check Logic Improvements ITT Software Trim and CVG Schedule Change to Increase Max Con Margin Annunciation of Inflight POWINT to Maintenance Computer. D. Description This Service Bulletin introduces a new version of FADEC software (C10 Identity G307CU65B) to introduce the improvements identified in para 1.C. AFFU Page 1 of 10

52 Controls and Data Services When the accomplishment instructions (Para. 3) have been done the FADEC type number changes as follows: (1) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-01AW01 or AFFU100-01AW02 or AFFU100-01AW03. (2) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-02AW01 or AFFU100-02AW02 or AFFU100-02AW03. (3) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-03AW01 or AFFU100-03AW02 or AFFU100-03AW03. E. Compliance Controlled Service Introduction To be only fitted on New Production / Overhaul and Repair, in accordance with Rolls- Royce purchase order or other authoritative method as agreed with Rolls-Royce Corporation. F. Approval This Service Bulletin have been technically agreed by Rolls-Royce Corporation. G. Manpower Program and identify one FADEC - one hour. H. Weight and Balance None. I. Electrical Load Data Not Changed. J. Software Accomplishment Summary Refer to the Aero Engine Controls, Software Accomplishment Summary document No. J408/0080 issue 1. K. References Controls and Data Services modification CP7831 AFFU100 Component Maintenance Manual (CMM) L. Other Publications Affected AFFU100 Component Maintenance Manual (CMM) M. Interchangeability or Intermix-ability of Parts Not applicable. AFFU Page 2 of 10

53 2. Material Information A. Material - Price and Availability Controls and Data Services This modification is chargeable to the operator or requesting party. B. Industry Support Information Not applicable. C. Material Necessary for Each Component NOTE: If necessary, use the equivalent alternatives for the items given in the table below: New P/N Description Old P/N Qty Instruction Note or Unit Label (preferred) or Unit Label (alternative) Aircraft Identification Label Modification Label Instruction Note(s): 1. Discard and install new item. 2. Replace with new item if necessary. D. Reidentified Parts (1) When the FADEC is programmed with the new software, the unit type number changes as follows: AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-01AW01 AFFU100-01AM01 AFFU100-01AN01 AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-02AW01 AFFU100-02AM01 AFFU100-02AN01 AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-03AW01 AFFU100-03AM01 AFFU100-03AN01 AFFU Page 3 of 10

54 Controls and Data Services AFFU AK-02 AFFU AL-02 AFFU100-01AM02 AFFU100-01AN02 become AFFU100-01AW02 AFFU AK-02 AFFU AL-02 AFFU100-02AM02 AFFU100-02AN02 AFFU AK-02 AFFU AL-02 AFFU100-03AM02 AFFU100-03AN02 AFFU AL-03 AFFU100-01AM03 AFFU100-01AN03 AFFU AL-03 AFFU100-02AM03 AFFU100-02AN03 AFFU AL-03 AFFU100-03AM03 AFFU100-03AN03 become become become become become AFFU100-02AW02 AFFU100-03AW02 AFFU100-01AW03 AFFU100-02AW03 AFFU100-03AW03 3. Accomplishment Instructions The accomplishment instructions must be done by an authorised Maintenance, Repair and Overhaul facility. The FADEC is programmed with the new software through a connector on the front of the FADEC. A. Procedure (Refer to the CMM, ) (1) Make sure that the new control software is installed in the FADEC Programming Facility. (2) Install the new control software into the FADEC (refer to the Testing and Fault Isolation section in the CMM). (3) Carefully remove the FADEC unit label (refer to Repair No.3 in the CMM). AFFU Page 4 of 10

55 Controls and Data Services (4) Make sure that the new unit label, either ( ) or ( ), is marked with the applicable data that follows: (a) Unit Label ( ) marking: Type NO. AFFU100-01AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A INST. NO SW STD G307CU65B Type NO AFFU100-03AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B Type NO AFFU100-01AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A AFFU Page 5 of 10

56 Controls and Data Services INST. NO SW STD G307CU65B Type NO AFFU100-03AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B Type NO AFFU100-01AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A INST. NO SW STD G307CU65B Type NO AFFU100-03AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B AFFU Page 6 of 10

57 Controls and Data Services (b) Unit Label ( ) marking (refer to Figure 1) REV A Unit Label ( ) marking areas Figure 1 TP29382 NOTE: The new unit label ( ) will be marked by hand or machine with the data that follows: The character size for Allison (RRC) part number must be 7,11 to 8,13 mm (0.28 to 0.32 in). REV A must be marked in character size 1,98 to 2,69 mm (0.078 to in) on the new label outside of the label data blocks in the approximate location as shown in Figure 1. Additional human readable data on the unit label is acceptable and the order of this data can vary to fit into the label data blocks: AFFU100-01AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW01 Allison Part No AFFU Page 7 of 10

58 Controls and Data Services Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-01AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-01AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU Page 8 of 10

59 Controls and Data Services (5) Install the new unit label (marked at step 3.A.(4)) to the FADEC (refer to Repair No.3 in the CMM). (6) Carefully remove the Aircraft Identification Label (refer to Repair No.3 in the CMM). (7) Make sure that the new Aircraft Identification Label is marked with the necessary data as follows: AFFU100-01AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-02AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-01AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-02AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-01AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 AFFU Page 9 of 10

60 BOX 4 Controls and Data Services CITATION X AFFU100-02AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 BOX 4 CITATION X (8) Install the new Aircraft Identification Label (marked at step 3.A.(7)) to the FADEC (refer to Repair No.3 in the CMM). (9) If it is necessary to replace the modification label ( ) then do the procedure that follows: (a) (b) Carefully remove the modification label (refer to Repair No.3 in the CMM). Make sure the new modification label is marked with the data that follows: serial number of the FADEC, related hardware part number (refer to Para. 1.D.), applicable modification number(s). (c) Install the new modification label (marked at step 3.A.(9)(b)) to the FADEC (refer to Repair No.3 in the CMM). (10) If it is necessary to do the test procedure on the new FADEC types (refer to the Testing and Fault Isolation section in the CMM) use the software files identified in the latest PAT Schedule: LUCOL Software Test Files G307C65B Refer to the latest PAT Schedule AFFU Page 10 of 10

61

62 ROLLS-ROYCE CONTROLS AND DATA SERVICES SHAFTMOOR LANE HALL GREEN BIRMINGHAM B28 8SW ENGLAND TELEPHONE: FAX: TRANSMITTAL FULL AUTHORITY DIGITAL ENGINE CONTROL, TYPE: AFFU101 ATA REF THIS PAGE TRANSMITS THE INITIAL ISSUE OF AFFU Reason for issue Introduction of C10 Software. S/W Identity G307CU65B. Action Keep this SB with the Component Maintenance Manual. Put in this SB Transmittal page and the SB pages 1 thru 5 dated. APPROVED FOR CONTROLS AND DATA SERVICES Signed: Date:22nd January 2016 TRANSMITTAL AFFU Page 1 of 2

63 Controls and Data Services BLANK PAGE TRANSMITTAL AFFU Page 2 of 2

64 Controls and Data Services ENGINE FUEL AND CONTROL - CONTROL - FULL AUTHORITY DIGITAL ENGINE CONTROL TYPE AFFU101 - INTRODUCTION OF C10 SOFTWARE. S/W IDENTITY G307CU65B 1. Planning Information A. Effectivity AFFU101, Full Authority Digital Engine Control (FADEC), unit type numbers given below: AFFU101-02AL01 AFFU101-02AL02 AFFU101-02AL03 AFFU101-02AM01 AFFU101-02AM02 AFFU101-02AM03 AFFU101-02AN01 AFFU101-02AN02 AFFU101-02AN03 B. Concurrent Requirements Not applicable. C. Reason A number of improvements were identified to correct production and field issues related to the current FADEC software and on-wing life improvement, the main changes in C10 software include: Incorporation of Shaft Break Logic Incorporation of Ndot Starting Logic MN Reasonable Data Limit Improvement TLA Fault Accommodation Logic Improvements T2.5 to ADC Difference Check Logic Improvements ITT Software Trim and CVG Schedule Change to Increase Max Con Margin Annunciation of Inflight POWINT to Maintenance Computer. D. Description This Service Bulletin introduces a new version of software (C10 Identity G307CU65B) to introduce the improvements identified in para 1.C. When the accomplishment instructions (Para. 3) have been done the FADEC type number changes as follows: AFFU Page 1 of 5

65 Controls and Data Services (1) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU101-02AW01 or AFFU101-02AW02 or AFFU101-02AW03. E. Compliance Controlled Service Introduction To be only fitted on New Production / Overhaul and Repair, in accordance with Rolls- Royce purchase order or other authoritative method as agreed with Rolls-Royce Corporation. F. Approval This Service Bulletin have been technically agreed by Rolls-Royce Corporation. G. Manpower Program and identify one FADEC - one hour. H. Weight and Balance None. I. Electrical Load Data Not Changed. J. Software Accomplishment Summary Refer to the Aero Engine Controls, Software Accomplishment Summary document No. J408/0080 issue 1. K. References Controls and Data Services modification CP7831 AFFU101 Component Maintenance Manual (CMM) L. Other Publications Affected AFFU101 Component Maintenance Manual (CMM) M. Interchangeability or Intermix-ability of Parts Not applicable. 2. Material Information A. Material - Price and Availability This modification is chargeable to the operator or requesting party. B. Industry Support Information Not applicable AFFU Page 2 of 5

66 Controls and Data Services C. Material Necessary for Each Component NOTE: If necessary, use the equivalent alternatives for the items given in the table below: New P/N Description Old P/N Qty Instruction Note Unit Label Modification Label Instruction Note(s): 1. Discard and install new item. 2. Replace with new item if necessary. D. Reidentified Parts (1) When the FADEC is programmed with the new software, the unit type number changes as follows: AFFU101-02AL01 AFFU101-02AM01 become AFFU101-02AW01 AFFU101-02AN01 AFFU101-02AL02 AFFU101-02AM02 become AFFU101-02AW02 AFFU101-02AN02 AFFU101-02AL03 AFFU101-02AM03 become AFFU101-02AW03 AFFU101-02AN03 3. Accomplishment Instructions The accomplishment instructions must be done by an authorised Maintenance, Repair and Overhaul facility. The FADEC is programmed with the new software through a connector on the front of the FADEC. A. Procedure (Refer to the CMM, ) (1) Make sure that the new control software is installed in the FADEC Programming Facility. (2) Install the new control software into the FADEC (refer to the Testing and Fault Isolation section in the CMM). (3) Carefully remove the FADEC unit label (refer to Repair No.3 in the CMM). AFFU Page 3 of 5

67 Controls and Data Services (4) Make sure that the new unit label ( ) is marked with the applicable data given below (refer to Figure 1): REV A Unit Label ( ) marking areas Figure 1 TP29382 NOTE: The new unit label ( ) will be marked by hand or machine with the data that follows: The character size for Allison (RRC) part number must be 7,11 to 8,13 mm (0.28 to 0.32 in). REV A must be marked in character size 1,98 to 2,69 mm (0.078 to in) on the new label outside of the label data blocks in the approximate location as shown in Figure 1. Additional human readable data on the unit label is acceptable and the order of this data can vary to fit into the label data blocks: AFFU101-02AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU Page 4 of 5

68 Controls and Data Services AFFU101-02AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU101-02AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B (5) Install the new unit label (marked at step 3.A.(4)) to the FADEC (refer to Repair No.3 in the CMM). (6) If it is necessary to replace the modification label ( ) then do the procedure that follows: (a) (b) Carefully remove the modification label (refer to Repair No.3 in the CMM). Make sure the new modification label is marked with the data that follows: serial number of the FADEC, related hardware part number (refer to Para. 1.D.), applicable modification number(s). (c) Install the new modification label (marked at step 3.A.(6)(b)) to the FADEC (refer to Repair No.3 in the CMM). (7) If it is necessary to do the test procedure on the new FADEC types (refer to the Testing and Fault Isolation section in the CMM) use the software files identified in the latest PAT Schedule. LUCOL Software Test Files G307C65B Refer to latest PAT Schedule AFFU Page 5 of 5

69 EXPORT CONTROLLED SERVICE BULLETIN ENGINE FUEL AND CONTROL - NEW FADEC WITH SOFTWARE VERSION C10 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 FADECs with hardware P/N or NOTE: The FADEC hardware P/N is located on the small label on top of the FADEC (Ref.FIG.1). B. Reason This service bulletin introduces new FADEC hardware and software assemblies ( and ) that incorporate FADEC software version C10 ( ). FADEC software version C10 is an incremental change from the FADEC software version C9.2 used on the AE 3007C1 engine. FADEC software version C10 upgrade incorporates changes that correct production and field issues related to the current FADEC software configuration as well as an on--wing life improvement. The primary changes include: (1) Incorporation of Shaft Break Logic. (2) Incorporation of NDOT Starting Logic. (3) MN Reasonable Data Limit Improvement. (4) TLA Fault Accommodation Logic Improvements. (5) T2.5 to ADC Difference Check Logic Improvements. (6) ITT Software Trim and CVG Schedule Change to Increase Max Con Margin. (7) Annunciation of Inflight POWINT to Maintenance Computer. C. Description This service bulletin gives you the procedure to reprogram the FADEC hardware and software assembly (FADEC assembly) (FADECs with hardware P/N or ) to FADEC assembly ( or ) and change the FADEC identification labels. A Rolls--Royce Controls and Data Services (CDS) authorized representative will reprogram and reidentify the FADEC assemblies. This service bulletin transmits CDS service bulletins AFFU and AFFU D. Approval Technical aspects are FAA approved. March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page1of8

70 EXPORT CONTROLLED E. Manpower Rolls -Royce On Wing Approximately 3.0 man--hours are necessary to remove, reprogram, reidentify, and install the two FADECs for each engine (approximately 6.0 man--hours for each aircraft). FADEC Spares Approximately 1.0 man--hour is necessary to reprogram and reidentify the FADEC. Required labor will be reimbursed by Rolls--Royce when accomplished for eligible engines under the stated effectivity and compliance at Cessna Service Centers. F. Compliance This service bulletin is recommended. You can do this service bulletin at the next convenient maintenance opportunity after this FADEC software version is available. G. Interchangeability -- Not affected H. Material Availability Customers can contact Cessna or Rolls--Royce to coordinate the reprogramming of the FADECs. I. Tooling -- Not applicable J. Weight and Balance -- Not affected K. Electrical Load Data -- Not affected L. References (1) Advance Engineering Memorandum (AEM), CN NOTE: The document above is referenced for the internal use of Rolls-Royce only. (2) AE 3007C Series Fault Isolation Manual (FIM), CSP (3) AE 3007C Series Illustrated Parts Catalog (IPC), CSP (4) AE 3007C Series Maintenance Manual (MM), CSP (5) Cessna Model 750 Aircraft Maintenance Manual (AMM). (6) CDS Service Bulletin AFFU , Engine Fuel and Control -- Full Authority Digital Engine Control Type AFFU Introduction of C10 Software. S/W Identity G307CU65B. (7) CDS Service Bulletin AFFU , Engine Fuel and Control -- Full Authority Digital Engine Control Type AFFU Introduction of C10 Software. S/W Identity G307CU65B. (8) Service Bulletin AE 3007C , Engine Fuel and Control -- New FADEC Diode Adapter. M. Prerequisites (1) Service Bulletin AE 3007C N. Corequisites -- None March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page2of8

71 EXPORT CONTROLLED 2. ACCOMPLISHMENT INSTRUCTIONS Rolls -Royce 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 , MM). (a) If the FADEC has diode adapter ( ) attached to the J4 connector, then disconnect the electrical connector from the diode adapter. Do not remove the anti--tamper label and the diode adapter from the J4 connector. (3) Reprogram and reidentify the FADEC assemblies by the CDS authorized service technician in accordance with CDS Service Bulletin (SB) AFFU or AFFU (attached). (4) When the CDS authorized service technician reidentifies the FADEC, do the steps that follow: (a) Make sure that the small FADEC Modification Label on the top of the FADEC shows the information that follows (Ref. TABLE 1) (Ref. FIG. 1): TABLE 1 -- FADEC Modification Label -- Hardware Part Number Information ROLLS--ROYCE HARDWARE PART NUMBER OR (b) Make sure that the large FADEC Unit Label to be placed on the top of the FADEC shows the information that follows: FOR ROLLS--ROYCE HARDWARE PART NUMBER TABLE 2 -- Large FADEC Unit Label -- Information ROLLS--ROYCE ASSEMBLY PART NUMBER GOODRICH FADEC TYPE NUMBER GOODRICH FADEC INSTALLATION NUMBER GOODRICH LUCOL SOFTWARE NUMBER AFFU AW G307CU65B AFFU AW G307CU65B NOTE: For FADEC with hardware part number (Ref. AE 3007C , SB), do not remove the diode adapter label (Ref. FIG. 2). March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page3of8

72 EXPORT CONTROLLED (c) Rolls -Royce Make sure that the small FADEC Aircraft Identification Label to be placed near the FADEC connectors shows the information that follows (Ref. TABLE 3) (Ref. FIG.1): TABLE 3 -- Small FADEC Aircraft Identification Label -- Information ROLLS--ROYCE ASSEMBLY PART NUMBER AE 3007 SERIES MODEL NUMBER AIRCRAFT MODEL APPROVED FOR FADEC INSTALLATION AIRCRAFT TYPE APPROVED FOR FADEC INSTALLATION or AE 3007C1 Model 750 Citation X NOTE: The attached CDS SB is for use by CDS authorized service technicians or other authorized personnel. (5) Install the four FADEC assemblies (Ref. TASK , MM). To make sure that the correct ITT trim plug is installed on the engine, use AE 3007C Maintenance Manual Revision 56 or later. (a) If necessary, connect the diode adapter to the J4 connector (Ref. TASK , MM) and put the anti--tamper label on the FADEC and the diode adapter (Ref. AE 3007C , SB). CAUTION: DO NOT OPERATE THE AIRCRAFT UNLESS ALL FOUR OF THE FADECS HAVE THE SAME SOFTWARE VERSION INSTALLED. INCORRECT ENGINE OPERATION CAN RESULT FROM USE OF FADECS WITH TWO DIFFERENT SOFTWARE 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) when you open and close the breakers three 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 (10) If one or more of the above messages are displayed on the EICAS, then do the appropriate fault isolation task for the message displayed (Ref. Introduction, FIM). CAUTION: THE ENGINES CANNOT BE OPERATED WITH ONE OR MORE OF THE DISPLAYED EICAS MESSAGES LISTED ABOVE. DAMAGE TO THE ENGINE CAN RESULT. (11) Do the engine operational check with FADEC channel A selected in control for both engines (Ref. TASK , MM). NOTE: Do not remove electrical power from the avionics bus. CAUTION: IF ONE OR MORE OF THE MESSAGES LISTED BELOW ARE DISPLAYED ON THE EICAS, THEN STOP THE ENGINE. DAMAGE TO THE ENGINE CAN RESULT. March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page4of8

73 EXPORT CONTROLLED Rolls -Royce (12) Examine the EICAS display for the messages listed below: (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 step 2.A.(12) are displayed, then go to step 2.A.(14). If one or more of the messages listed in step 2.A.(12) are displayed on the EICAS, then do the steps that follow: (a) Stop the engine (Ref. TASK , 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 maintenance messages in the aircraft maintenance test (AMT) for all four FADECs (Ref. Introduction, FIM). (15) If one or more engine--related maintenance messages are shown on the MFD, then do the appropriate fault 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 both engines. B. Record compliance with this service bulletin. (1) Remove the FADEC cards from Section 1, Part VII of the engine records. Discard the Engine 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 of the 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 Data Rolls--Royce Corporation Attention: AE Service Data Manager 450 South Meridian Street, Mail Code MC--N3--04 Indianapolis, Indiana USA cra.del.data@rolls--royce.com FAX: March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page5of8

74 EXPORT CONTROLLED Rolls -Royce FADEC Identification Labels -- Proper Location of Specific Data FIG. 1 March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page6of8

75 EXPORT CONTROLLED Rolls -Royce FADEC with Diode Adapter Label FIG. 2 March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page7of8

76 EXPORT CONTROLLED 3. MATERIAL INFORMATION Rolls -Royce A. Configuration Chart -- Not applicable NEW P/N OR QTY/ ENG NAME OLD P/N 2 FADEC Assy, Hardware and Software FADEC Assy, Hardware and Software INSTRUCTIONS/DISPOSITION NOTES 1. Program item to new software version. B. Consumable Materials -- None C. Expendable Parts -- None QTY/ ENG INSTRUCTIONS/ DISPOSITION CUSTOMER SUPPORT ROLLS-ROYCE March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page8of8

77 EXPORT CONTROLLED SERVICE BULLETIN COMPLIANCE ENGINE FUEL AND CONTROL - NEW FADEC WITH SOFTWARE VERSION C10 FOR THE AE 3007C 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 Data Rolls--Royce Corporation Attn: AE Service Data Manager 450 South Meridian Street, Speed Code MC--N3--04 Indianapolis, Indiana USA cra.rel.data@rolls-royce.com FAX: March 14, 2016 AE 3007C Page1of3

78 EXPORT CONTROLLED Rolls -Royce March 14, 2016 AE 3007C E COPYRIGHT 2016 Rolls--Royce Corporation (unpublished) Page9of8

79 ROLLS-ROYCE CONTROLS AND DATA SERVICES SHAFTMOOR LANE HALL GREEN BIRMINGHAM B28 8SW ENGLAND TELEPHONE: FAX: TRANSMITTAL FULL AUTHORITY DIGITAL ENGINE CONTROL, TYPE: AFFU100 ATA REF THIS PAGE TRANSMITS THE INITIAL ISSUE OF AFFU Reason for issue Introduction of C10 Software. S/W Identity G307CU65B. Action Keep this SB with the Component Maintenance Manual. Put in this SB Transmittal page and the SB pages 1 thru 10 dated. APPROVED FOR CONTROLS AND DATA SERVICES Signed: Date:22nd January 2016 TRANSMITTAL AFFU Page 1 of 2

80 Controls and Data Services BLANK PAGE TRANSMITTAL AFFU Page 2 of 2

81 Controls and Data Services ENGINE FUEL AND CONTROL - CONTROL - FULL AUTHORITY DIGITAL ENGINE CONTROL TYPE AFFU100 - INTRODUCTION OF C10 SOFTWARE. S/W IDENTITY G307CU65B 1. Planning Information A. Effectivity AFFU100, Full Authority Digital Engine Control (FADEC), unit type numbers given below: AFFU AH-1 AFFU AH-1 AFFU AH-1 AFFU AK-01 AFFU AK-01 AFFU AK-01 AFFU AK-02 AFFU AK-02 AFFU AK-02 AFFU AL-01 AFFU AL-01 AFFU AL-01 AFFU AL-02 AFFU AL-02 AFFU AL-02 AFFU AL-03 AFFU AL-03 AFFU AL-03 AFFU100-01AM01 AFFU100-02AM01 AFFU100-03AM01 AFFU100-01AM02 AFFU100-02AM02 AFFU100-03AM02 AFFU100-01AM03 AFFU100-02AM03 AFFU100-03AM03 AFFU100-01AN01 AFFU100-02AN01 AFFU100-03AN01 AFFU100-01AN02 AFFU100-02AN02 AFFU100-03AN02 AFFU100-01AN03 AFFU100-02AN03 AFFU100-03AN03 NOTE: This Service Bulletin can also be applicable to any other FADEC types with the Rolls-Royce Hardware Part Numbers , or B. Concurrent Requirements Not applicable. C. Reason A number of improvements were identified to correct production and field issues related to the current FADEC software and on-wing life improvement, the main changes in C10 software include: Incorporation of Shaft Break Logic Incorporation of Ndot Starting Logic MN Reasonable Data Limit Improvement TLA Fault Accommodation Logic Improvements T2.5 to ADC Difference Check Logic Improvements ITT Software Trim and CVG Schedule Change to Increase Max Con Margin Annunciation of Inflight POWINT to Maintenance Computer. D. Description This Service Bulletin introduces a new version of FADEC software (C10 Identity G307CU65B) to introduce the improvements identified in para 1.C. AFFU Page 1 of 10

82 Controls and Data Services When the accomplishment instructions (Para. 3) have been done the FADEC type number changes as follows: (1) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-01AW01 or AFFU100-01AW02 or AFFU100-01AW03. (2) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-02AW01 or AFFU100-02AW02 or AFFU100-02AW03. (3) The FADEC with Rolls-Royce Hardware Part Number becomes FADEC unit type AFFU100-03AW01 or AFFU100-03AW02 or AFFU100-03AW03. E. Compliance Controlled Service Introduction To be only fitted on New Production / Overhaul and Repair, in accordance with Rolls- Royce purchase order or other authoritative method as agreed with Rolls-Royce Corporation. F. Approval This Service Bulletin have been technically agreed by Rolls-Royce Corporation. G. Manpower Program and identify one FADEC - one hour. H. Weight and Balance None. I. Electrical Load Data Not Changed. J. Software Accomplishment Summary Refer to the Aero Engine Controls, Software Accomplishment Summary document No. J408/0080 issue 1. K. References Controls and Data Services modification CP7831 AFFU100 Component Maintenance Manual (CMM) L. Other Publications Affected AFFU100 Component Maintenance Manual (CMM) M. Interchangeability or Intermix-ability of Parts Not applicable. AFFU Page 2 of 10

83 2. Material Information A. Material - Price and Availability Controls and Data Services This modification is chargeable to the operator or requesting party. B. Industry Support Information Not applicable. C. Material Necessary for Each Component NOTE: If necessary, use the equivalent alternatives for the items given in the table below: New P/N Description Old P/N Qty Instruction Note or Unit Label (preferred) or Unit Label (alternative) Aircraft Identification Label Modification Label Instruction Note(s): 1. Discard and install new item. 2. Replace with new item if necessary. D. Reidentified Parts (1) When the FADEC is programmed with the new software, the unit type number changes as follows: AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-01AW01 AFFU100-01AM01 AFFU100-01AN01 AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-02AW01 AFFU100-02AM01 AFFU100-02AN01 AFFU AH-1 AFFU AK-01 AFFU AL-01 become AFFU100-03AW01 AFFU100-03AM01 AFFU100-03AN01 AFFU Page 3 of 10

84 Controls and Data Services AFFU AK-02 AFFU AL-02 AFFU100-01AM02 AFFU100-01AN02 become AFFU100-01AW02 AFFU AK-02 AFFU AL-02 AFFU100-02AM02 AFFU100-02AN02 AFFU AK-02 AFFU AL-02 AFFU100-03AM02 AFFU100-03AN02 AFFU AL-03 AFFU100-01AM03 AFFU100-01AN03 AFFU AL-03 AFFU100-02AM03 AFFU100-02AN03 AFFU AL-03 AFFU100-03AM03 AFFU100-03AN03 become become become become become AFFU100-02AW02 AFFU100-03AW02 AFFU100-01AW03 AFFU100-02AW03 AFFU100-03AW03 3. Accomplishment Instructions The accomplishment instructions must be done by an authorised Maintenance, Repair and Overhaul facility. The FADEC is programmed with the new software through a connector on the front of the FADEC. A. Procedure (Refer to the CMM, ) (1) Make sure that the new control software is installed in the FADEC Programming Facility. (2) Install the new control software into the FADEC (refer to the Testing and Fault Isolation section in the CMM). (3) Carefully remove the FADEC unit label (refer to Repair No.3 in the CMM). AFFU Page 4 of 10

85 Controls and Data Services (4) Make sure that the new unit label, either ( ) or ( ), is marked with the applicable data that follows: (a) Unit Label ( ) marking: Type NO. AFFU100-01AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A INST. NO SW STD G307CU65B Type NO AFFU100-03AW01 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B Type NO AFFU100-01AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A AFFU Page 5 of 10

86 Controls and Data Services INST. NO SW STD G307CU65B Type NO AFFU100-03AW02 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B Type NO AFFU100-01AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV E INST. NO SW STD G307CU65B Type NO AFFU100-02AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV A INST. NO SW STD G307CU65B Type NO AFFU100-03AW03 ASSY PNR ASSY REV A SER SERIAL NUMBER HDW PNR HDW REV D INST. NO SW STD G307CU65B AFFU Page 6 of 10

87 Controls and Data Services (b) Unit Label ( ) marking (refer to Figure 1) REV A Unit Label ( ) marking areas Figure 1 TP29382 NOTE: The new unit label ( ) will be marked by hand or machine with the data that follows: The character size for Allison (RRC) part number must be 7,11 to 8,13 mm (0.28 to 0.32 in). REV A must be marked in character size 1,98 to 2,69 mm (0.078 to in) on the new label outside of the label data blocks in the approximate location as shown in Figure 1. Additional human readable data on the unit label is acceptable and the order of this data can vary to fit into the label data blocks: AFFU100-01AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW01 Allison Part No AFFU Page 7 of 10

88 Controls and Data Services Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW01 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-01AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW02 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-01AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-02AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU100-03AW03 Allison Part No Assembly Rev Letter A Lucas Inst. No LUCOL Software G307CU65B AFFU Page 8 of 10

89 Controls and Data Services (5) Install the new unit label (marked at step 3.A.(4)) to the FADEC (refer to Repair No.3 in the CMM). (6) Carefully remove the Aircraft Identification Label (refer to Repair No.3 in the CMM). (7) Make sure that the new Aircraft Identification Label is marked with the necessary data as follows: AFFU100-01AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-02AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW01 Allison Part No BOX 2 AE3007C BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-01AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-02AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW02 Allison Part No BOX 2 AE3007C1 BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-01AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 AFFU Page 9 of 10

90 BOX 4 Controls and Data Services CITATION X AFFU100-02AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 BOX 4 CITATION X AFFU100-03AW03 Allison Part No BOX 2 AE3007C ENHANCED BOX 3 MODEL 750 BOX 4 CITATION X (8) Install the new Aircraft Identification Label (marked at step 3.A.(7)) to the FADEC (refer to Repair No.3 in the CMM). (9) If it is necessary to replace the modification label ( ) then do the procedure that follows: (a) (b) Carefully remove the modification label (refer to Repair No.3 in the CMM). Make sure the new modification label is marked with the data that follows: serial number of the FADEC, related hardware part number (refer to Para. 1.D.), applicable modification number(s). (c) Install the new modification label (marked at step 3.A.(9)(b)) to the FADEC (refer to Repair No.3 in the CMM). (10) If it is necessary to do the test procedure on the new FADEC types (refer to the Testing and Fault Isolation section in the CMM) use the software files identified in the latest PAT Schedule: LUCOL Software Test Files G307C65B Refer to the latest PAT Schedule AFFU Page 10 of 10

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92 ROLLS-ROYCE CONTROLS AND DATA SERVICES SHAFTMOOR LANE HALL GREEN BIRMINGHAM B28 8SW ENGLAND TELEPHONE: FAX: TRANSMITTAL FULL AUTHORITY DIGITAL ENGINE CONTROL, TYPE: AFFU101 ATA REF THIS PAGE TRANSMITS THE INITIAL ISSUE OF AFFU Reason for issue Introduction of C10 Software. S/W Identity G307CU65B. Action Keep this SB with the Component Maintenance Manual. Put in this SB Transmittal page and the SB pages 1 thru 5 dated. APPROVED FOR CONTROLS AND DATA SERVICES Signed: Date:22nd January 2016 TRANSMITTAL AFFU Page 1 of 2