# GE CF6-80C2A5F

- Type: Engine model (FAA registry)
- Registry code: 30113
- Manufacturer (registry): GE
- Model: CF6-80C2A5F
- Engine type: Turbo-fan
- Power: 60,100 lb thrust
- Data sheet: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 6 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-80c2a5f

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022
- [AD 2022-02-18](https://openairdocs.org/ad/2022-02-18): Engine Mount Section · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 3 more. Effective Feb 25, 2022
- [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021
- [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021
- [AD 2020-22-02](https://openairdocs.org/ad/2020-22-02): Engine Fuel and Control · General Electric CF6-80C2A5F, CF6-80C2B1F, CF6-80C2B2F and 13 more. Effective Dec 3, 2020
- [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016
- [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014
- [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013
- [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012
- [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009
- [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009
- [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009
- [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008
- [AD 2008-02-17](https://openairdocs.org/ad/2008-02-17): Thrust reverser actuation systems · General Electric CF6-50A, CF6-50C, CF6-50C1 and 16 more. Effective Feb 28, 2008
- [AD 2007-21-06](https://openairdocs.org/ad/2007-21-06): Electronic control unit (ECU) · General Electric CF6-80C2A5F. Effective Nov 15, 2007
- [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007
- [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007
- [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006
- [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005
- [AD 2005-06-07](https://openairdocs.org/ad/2005-06-07): Directional pilot valve (DPV) assembly · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Apr 25, 2005
- [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004
- [AD 2004-07-13](https://openairdocs.org/ad/2004-07-13): High pressure turbine (HPT) stage 1 disks · General Electric CF6-80C2A5F, CF6-80C2B5F, CF6-80C2B7F and 1 more. Effective May 6, 2004
- [AD 2003-12-08](https://openairdocs.org/ad/2003-12-08): Directional pilot valve · General Electric CF6-80A1, CF6-80A3, CF6-80C2A1 and 5 more. Effective Jul 23, 2003
- [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003
- [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003
- [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002
- [AD 2000-12-08](https://openairdocs.org/ad/2000-12-08): Mount Link Assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 4 more. Effective Aug 28, 2000
- [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000
- [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997
- [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996
- [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995
- [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994
- [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993

Historical (superseded or no longer in force):

- [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020
- [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018
- [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009
- [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004
- [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002
- [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001
- [AD 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 2000-04-14](https://openairdocs.org/ad/2000-04-14) (historical): Fuel tube flange seating · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective May 1, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-18-20](https://openairdocs.org/ad/99-18-20) (historical): Inadvertent In-flight Thrust Reverser · General Electric Aircraft Engines CF6-50 Series (all), CF6-80A1, CF6-80A3 and 6 more. Effective Nov 2, 1999
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999

## Information bulletins (advisory) (5)

- [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023
- [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011
- [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010
- [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser  Transcowl Clevis Pin. Issued Sep 3, 2008
- [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006

## Registered aircraft (6)

- [N687FE](https://openairdocs.org/aircraft/N687FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2007, S/N 0873
- [N688FE](https://openairdocs.org/aircraft/N688FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2007, S/N 0874
- [N689FE](https://openairdocs.org/aircraft/N689FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2007, S/N 0875
- [N690FE](https://openairdocs.org/aircraft/N690FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2007, S/N 0876
- [N691FE](https://openairdocs.org/aircraft/N691FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2007, S/N 0877
- [N692FE](https://openairdocs.org/aircraft/N692FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2007, S/N 0878

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (262, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR FDEA202607030831](https://openairdocs.org/sdr/FDEA202607030831), Jul 3, 2026: ENGINE. DAMAGED. BURNED SMELL ON TAKEOFF. SUSPECT OIL LEAK IN HPC. EMERGENCY DECLARED. O2 USED. ENGINE R & R, COMPLETED RT ENG OPS CHECKS IN REF TO FEDEX WORKCARD 7100000-02-04.
- [SDR FDEA201708312443](https://openairdocs.org/sdr/FDEA201708312443), Aug 31, 2017: LINE. CHAFED. DURING PREFLIGHT, FOUND FLUID LEAKING OUT OF REAR OF THE NR 1 ENGINE. FOUND AN OIL SUPPLY LINE MOUNTING CLAMP BROKEN AND OIL LINE CHAFED THROUGH. REMOVED AND RE
- [SDR FDEA201708082147](https://openairdocs.org/sdr/FDEA201708082147), Aug 8, 2017: DUCT. SEPARATED. APU BLEED PREASURE WAS 4 PSI ON ENGINE START. ACFT RETURNED TO GATE. COULD HEAR BLEED AIR LEAK ON THE NR 2 ENGINE COWL. GAINED ACCESS FOUND MAIN SUPPLY DUCT CLA
- [SDR FDEA201704111130](https://openairdocs.org/sdr/FDEA201704111130), Apr 11, 2017: ENGINE. FAILED. FLYING FROM SJC TO IND AT LEVEL OFF THE OIL BUGS WERE SET AT 16QTS ON EACH GAGE TO MATCH THE CORRECT OIL QUANTITY READING. APPROXIMATELY 15-20 MINS LATER, NR 1 
- [SDR FDEA201703150881](https://openairdocs.org/sdr/FDEA201703150881), Mar 15, 2017: EEC. MALFUNCTIONED. AT FL 200, THE NR 2 ENGINE ROLLED BACK SUDDENLY. WARNING LIGHTS BUT NO HORNS. STARTED A DESCENT, TURNED OFF AUTO THROTTLES AND SELECTED CONTINOUS RELIGHT AFTER 
- [SDR FDEA201606041828](https://openairdocs.org/sdr/FDEA201606041828), Jun 4, 2016: FLOOR PANEL. WORN. MAIN CABIN FLOOR PANEL 242FJ DAMAGED. FABRICATED AFT CARGO FLOOR PANEL 242FJ ON T16 1211786 IAW SRZ 25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.
- [SDR FDEA201512254078](https://openairdocs.org/sdr/FDEA201512254078), Dec 25, 2015: HMU. MALFUNCTIONED. AT TOP OF DESCENT, NR 1 ENG STARTED A SERIES OF 6 - 7 STALLS. FOLLOWED THE QRH & OPERATED AT IDLE. N1 STARTED TO DECREASE & EGT CLIMBED TO 622 AT SHUTDOWN. PARA
- [SDR FDEA201506292123](https://openairdocs.org/sdr/FDEA201506292123), Jun 29, 2015: THRUST REVERSER. DAMAGED. NUMBER 1 OTBD THRUST REVERSER AFT HINGE LUG DAMAGED EXHAUST SYS. THRUST REVERSER BLEND REPAIR OF HINGE BEAM REPAIRED IAW EA 6-7830-T0318435. THIS REPAIR IS CLAS
- [SDR FDEA201408072105](https://openairdocs.org/sdr/FDEA201408072105), Aug 7, 2014: CONNECTOR. UNKNOWN. ON TAKEOFF NR 2 THRUST REVERSER PRESSURIZED. FOUND LT DPV SOLENOID CONNECTOR NOT PROPERLY REMOVED IAW MEL 78-30-01-A. REMOVED CONNECTOR & CONTINUED ON WITH MX P
- [SDR FDEA201403210541](https://openairdocs.org/sdr/FDEA201403210541), Mar 21, 2014: ECU. FAILED. NR 1 ENGINE ROLLED BACK PASSING FL 315, N1 & N2 DECREASED IGNITION TURNED ON. ONE MINUTE LATER ENGINE REGAINED POWER. RETURNED & LANDED. NR 1 ENGINE FADEC FAULT
- [SDR FDEA201401160118](https://openairdocs.org/sdr/FDEA201401160118), Jan 16, 2014: ENGINE. LEAKING. PRIOR TO DECENT, COURIERS NOTIFIED COCKPIT OF SMOKE IN CABIN. NO SMOKE DETECTORS OR ECAM WARNINGS IN COCKPIT OR ODOR OF SMOKE. RAN AIR CONDITIONING SMOKE CHECK 
- [SDR FDEA201311272884](https://openairdocs.org/sdr/FDEA201311272884), Nov 27, 2013: ENGINE. FAILED. PDIS 664 79-310005832 27NOV13 IND OPEN U LOG PAGES 02343904. ENG ADVISORY FOR NR 2 ENG OIL QTY ZERO & FLUCTUATING OIL PRESS ON ECAM & ENG INSTRUMENTS. ADVISORY 
- [SDR FDEA201303210639](https://openairdocs.org/sdr/FDEA201303210639), Mar 21, 2013: ENGINE. INOPERATIVE. PER FLIGHT CREW DEBRIEF, THE NR 1 ENGINE ON TAXI OUT HAD ECAM ENGINE FAILURE AND ASSOCIATED PARAMETERS WINDING DOWN. IAW CAPTAIN, AFTER BEING NOTIFIED BY MEM TO
- [SDR FDEA201209223396](https://openairdocs.org/sdr/FDEA201209223396), Sep 22, 2012: FLOOR PANEL. DAMAGED. MAIN DECK CARGO FLOOR PANEL 242QJ CRUSHED AT CLEVIS ADAPTOR CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209153331](https://openairdocs.org/sdr/FDEA201209153331), Sep 15, 2012: LINK ASSY. CRACKED. MAIN DECK CARGO FRAME 48L BELOW SEAT TRACK 4L SUPPORT STRUCTURE ATTACHMENT LUG CRACKED ONE INCH LONG, STR 27-28. R & R DAMAGED LINK ASSY IAW SRM 51-40-21, PG 7,
- [SDR FDEA201209113283](https://openairdocs.org/sdr/FDEA201209113283), Sep 11, 2012: WEB. CRACKED. MAIN DECK CARGO FLOOR WEB AT FR 79 RT OTBD OF FLOOR RAIL HAS .25" CRACK EXTENDING FROM LIGHTENING HOLE. R & R WEB IAW SRM 51-72-10, P1.
- [SDR FDEA201209113287](https://openairdocs.org/sdr/FDEA201209113287), Sep 11, 2012: FLOORBOARD. CRACKED. MAIN DECK CARGO FLOORBOARD 242UJ CRACKED. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209103275](https://openairdocs.org/sdr/FDEA201209103275), Sep 10, 2012: FLOORBOARD. DAMAGED. FLOORBOARD 131NG CRACKED ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209073251](https://openairdocs.org/sdr/FDEA201209073251), Sep 7, 2012: FLOORBOARD. DAMAGED. FLOORBOARD 151TF HAS TWO AREAS DAMAGED UPPER AND LOWER SKIN PLYS WITH CRUSHED CORE. THE LARGEST AREA IS 8" BY 3". FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 
- [SDR FDEA201209073253](https://openairdocs.org/sdr/FDEA201209073253), Sep 7, 2012: FLOORBOARD. GOUGED. FLOORBOARD 252UH UPPER SURFACE GOUGED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209073254](https://openairdocs.org/sdr/FDEA201209073254), Sep 7, 2012: FLOORBOARD. CRACKED. MAIN DECK CARGO FLOORBOARD 251DF CRACKED, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.
- [SDR FDEA201209073256](https://openairdocs.org/sdr/FDEA201209073256), Sep 7, 2012: FLOORBEAM. DAMAGED. FORWARD SIDE OF FLOORBEAM AT FR 17 Y1456 WEB IS DRILLED THROUGH AND HAS A RIVET IN THE HOLE THAT HAS NOT BEEN BUCKED. FABRICATED AND INSTALLED PICKUP FITTING IA
- [SDR FDEA201209073255](https://openairdocs.org/sdr/FDEA201209073255), Sep 7, 2012: SKIN. CHAFED. LEFT WING OUTER FLAP INBD SIDE L/E CHAFED MARK APPROX LENGTH IS 1 INCH AND WIDTH IS 0.50 REF AMM 27-00-00-06, ZONE 580. REPAIRED WING OUTER FLAP IAW A300-600 FS
- [SDR FDEA201209063248](https://openairdocs.org/sdr/FDEA201209063248), Sep 6, 2012: SKIN. DAMAGED. LEFT INBD FLAP LOWER SURFACE HAS 22 DENTS AND 12 GOUGES LOCATED FROM STGR 2.10 TO T/E AND RIB 3A TO RIB19A, COMPLIED WITH EA 6-5730160178.
- [SDR FDEA201209063245](https://openairdocs.org/sdr/FDEA201209063245), Sep 6, 2012: SPRING. BROKEN. AVIONICS DOOR CAME OPEN IN FLIGHT (121BL). DOOR DID NOT OPEN BUT CREW GOT LIGHT IN COCKPIT. FOUND SPRING BROKEN. R & R THE DOOR HANDLE TENSION SPRINGS IAW MM 52
- [SDR FDEA201209063247](https://openairdocs.org/sdr/FDEA201209063247), Sep 6, 2012: FLOORBEAM. CRACKED. MAIN CARGO DECK FLOORBEAM AT FR 61 BETWEEN SEAT TRACK 4R AND 5R CRACKED ABOUT 0.125" ON THE AFT FACE EXTRUSION REF AMM 53-10-15-06-02, ZONE 250. BLENDED FLOORBE
- [SDR FDEA201209043220](https://openairdocs.org/sdr/FDEA201209043220), Sep 4, 2012: SKIN. DAMAGED. LT ELEVATOR TIP LOWER SURFACE HAS A LIGHTNING STRIKE. REPAIRED IAW EA 6-5520-157869, AND RAS 70566303/003/2012, ISSUE A.
- [SDR FDEA201209043221](https://openairdocs.org/sdr/FDEA201209043221), Sep 4, 2012: SKIN. DAMAGED. LT ELEVATOR TIP PANEL UPPER SURFACE HAS 2 EA LIGHTNING STRIKES. REPAIRED IAW EA 6-5520-157869 PART 1 AND RAS, ISSUE A.
- [SDR FDEA201209043218](https://openairdocs.org/sdr/FDEA201209043218), Sep 4, 2012: FLOOR SUPPORT. CORRODED. AFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR64 SECOND FROM LT SIDE FOUND CORRODED AT ANCHOR NUT LOCATIONS. AFT HOLD SUPPORT BEAM AT FR63 AND FR64 SECOND FROM LT S
- [SDR FDEA201209043217](https://openairdocs.org/sdr/FDEA201209043217), Sep 4, 2012: SEAT TRACK. CORRODED. CENTER MAIN DECK, FOUND RT 5TH SEAT TRACK CORROSION AREA FROM FR45 TO 54 AT -Y1959 POSITION. FABRICATE AND R & R THE SEAT TRACK IAW DWG NR A53813618 AND AB6F SR
- [SDR FDEA201209043215](https://openairdocs.org/sdr/FDEA201209043215), Sep 4, 2012: FLOORBEAM. CRACKED. FWD CARGO COMPT CEILING AREA OF M/D FLOORBEAM RT SIDE EDGE AREA GOT CRACK AT FR29 POSITION. REPAIRED IAW EA 6-5310-149065 WITH AB6F SRM 53-10-15. THE REPAIR CLA
- [SDR FDEA201208273183](https://openairdocs.org/sdr/FDEA201208273183), Aug 27, 2012: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO FRAME 11A THRU 13A, Y1456 HAS SURFACE CORROSION ON TOP AND BOTTOM AROUND THE MOUNTING SCREWS ON TEE PROFILE. AFTER REMOVAL OF LEVEL 1 CORROSION 
- [SDR FDEA2012082631710](https://openairdocs.org/sdr/FDEA2012082631710), Aug 26, 2012: FLOOR PANEL. DAMAGED. CENTER MAIN DECK FLOOR PANEL 242EJ HAS INSERT DAMAGE.
- [SDR FDEA201208263177](https://openairdocs.org/sdr/FDEA201208263177), Aug 26, 2012: CARGO TRACK. CORRODED. MAIN DECK CARGO TRACK L4 BETWEEN FR 46 & 47 HAS 2EA AREAS OF CORROSION APPROXIMATELY 8" LONG. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 205.
- [SDR FDEA201208263172](https://openairdocs.org/sdr/FDEA201208263172), Aug 26, 2012: FLOOR PANEL. DAMAGED. FWD CARGO FLOOR PANEL 131QG EDGE AREA HAS IMPACT DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201208263168](https://openairdocs.org/sdr/FDEA201208263168), Aug 26, 2012: COVER. CRACKED. LT WING T/E FOUND 1EA COVER CRACKED POSITION NEAR LT MAIN LT MLG AFT TRUNNION INBD SIDE. REMOVED COVER FOR FABRICATION IAW DWG A57240775 THEN REPLACED IAW SRM 5
- [SDR FDEA201208253164](https://openairdocs.org/sdr/FDEA201208253164), Aug 25, 2012: SEAT TRACK. CORRODED. MAIN DECK CARGO BETWEEN FR 53 AND 54 SEAT TRACK 3R HAS CORROSION APPROX 2" IN THE CENTER OF THE TRACKS IN BET SCALLOPS. AFTER REMOVAL OF LEVEL 1 CORROSION, AREA
- [SDR FDEA201208243154](https://openairdocs.org/sdr/FDEA201208243154), Aug 24, 2012: SKIN. GOUGED. LT WING NR 2 SLAT LWR SURFACE GOUGED 1 SQUARE INCH, LOCATED 3 INCHES FROM INBD EDGE AND 6 INCHES FWD OF T/E SMOOTHED AND BLENDED GOUGE IAW FSRM 51-73-10 MATERIA
- [SDR FDEA201208243155](https://openairdocs.org/sdr/FDEA201208243155), Aug 24, 2012: FLOORBOARD. DAMAGED. FWD CARGO BAY FLOORBOARD 131RG BROKEN AT 2 CORNERS AND CRUSHED BY TOOL ON THE EDGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWGSRZ 25-005 REV J.
- [SDR FDEA201208243157](https://openairdocs.org/sdr/FDEA201208243157), Aug 24, 2012: ADAPTER. DAMAGED. MAIN DECK CARGO FLOOR CLEVIS ADAPTER AT FR38.1 BTWN SEAT TRACKS 2R AND 3R HAS BROKEN SCALLOPS, .5 AREA R & R CLEVIS ADAPTER AT FR 38.1 BETWEEN SEAT TRACKS 2R AN
- [SDR FDEA201208243160](https://openairdocs.org/sdr/FDEA201208243160), Aug 24, 2012: ADAPTER. CRACKED. MAIN DECK CARGO ZONE 250, CLS ADAPTER HAS A 8.5 INCH LONG CRACK IN UPPER RADIUS AT FR61 BTWN SEAT TRACKS 4R(-Y1456) AND 5R (-Y1959). R & R CLEVIS ADAPTER AT FR 
- [SDR FDEA201208243161](https://openairdocs.org/sdr/FDEA201208243161), Aug 24, 2012: ADAPTER. CRACKED. MAIN DECK CARGO ZONE 250, CLEVIS ADAPTER HAS A 9.5" LONG CRACK IN UPPER RADIUS AT FR62 BETWEEN SEAT TRACKS 4R(-Y1456) AND 5R (-Y1959). R & R CLEVIS ADAPTER AT F
- [SDR FDEA201208243158](https://openairdocs.org/sdr/FDEA201208243158), Aug 24, 2012: WEB. DAMAGED. FR11 TO FR12 WEB DAMAGED. REMOVED DAMAGED WEB IAW SRM 51-40-21 PARA 6. FABRICATED NEW WEB IAW DWG A53612536. INSTALLED NEW WEB AT FR 12A TO FR 14 STA Y953 IAW S
- [SDR FDEA201208243159](https://openairdocs.org/sdr/FDEA201208243159), Aug 24, 2012: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO SURFACE CORROSION ON TOP AND BOTTOM AROUND MOUNTING SCREWS ON FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-21 PARA 7.
- [SDR FDEA201208233140](https://openairdocs.org/sdr/FDEA201208233140), Aug 23, 2012: SEAT TRACK. CORRODED. SEAT TRACK L4 BETWEEN FR 42 AND 44 HAS 2 AREAS OF CORROSION APPROX 8 INCHES LONG, REF AMM 53-10-16-6 CORROSION AT TRACK 4L FR 42 TO 44 FOUND TO BE OUT OF LIMITS
- [SDR FDEA201208233145](https://openairdocs.org/sdr/FDEA201208233145), Aug 23, 2012: ADAPTER. CORRODED. FLOOR CLEVIS ADAPTER UPPER SURFACE CORRODED 10 SQUARE INCHES LOCATED FR 25 BTWN 2R & 3R SEAT TRACKS AFTER REMOVAL OF LEVEL 1 CORROSION IAW FRSM 51-74-10, PARA 5
- [SDR FDEA201208223112](https://openairdocs.org/sdr/FDEA201208223112), Aug 22, 2012: SEAT TRACK. CORRODED. SEAT TRACK 5R AT FR58 HAS 1 SQUARE INCH OF CORROSION ON INBD FLANGE AROUND NUT PLATE HOLE. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK 5R WAS FOUND TO BE OUT 
- [SDR FDEA201208223108](https://openairdocs.org/sdr/FDEA201208223108), Aug 22, 2012: FLOOR PANEL. DENTED. CARGO BAY 162EF FLOOR PANEL UPPER SURFACE HAS SEVERAL SMALL DENTS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER
- [SDR FDEA201208223109](https://openairdocs.org/sdr/FDEA201208223109), Aug 22, 2012: FLOOR PANEL. DEBONDED. CARGO BAY 161AF FLOOR PANEL EDGE AREA DEBONDED. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
- [SDR FDEA201208223110](https://openairdocs.org/sdr/FDEA201208223110), Aug 22, 2012: FLOOR PANEL. DAMAGED. CARGO BAY 162DF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.

All 262: https://openairdocs.org/engine/ge-cf6-80c2a5f/reports.md

## STCs that may be installed (OpenAirDocs) (5)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic
- [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic
- [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series
- [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc
- [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 Series

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