# GE CF6-80C2B8F

- Type: Engine model (FAA registry)
- Registry code: 30118
- Manufacturer (registry): GE
- Model: CF6-80C2B8F
- Engine type: Turbo-fan
- Power: 60,030 lb thrust
- Data sheet: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 2 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-80c2b8f

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 2021-14-11](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 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 2012-04-05](https://openairdocs.org/ad/2012-04-05): Electronic control unit (ECU) · General Electric CF6-80C2B1F, CF6-80C2B1F1, CF6-80C2B1F2 and 8 more. Effective Mar 30, 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 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 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 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 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 2000-03-04](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

Historical (superseded or no longer in force):

- [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 2007-12-07](https://openairdocs.org/ad/2007-12-07) (historical): Electronic control units (ECUs) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 5 more. Effective Jul 11, 2007
- [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 2000-16-12](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 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 99-08-13](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 (2)

- [N145FE](https://openairdocs.org/aircraft/N145FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2017, S/N 42727
- [N172FE](https://openairdocs.org/aircraft/N172FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 2019, S/N 63103

## 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 (98, newest 50)

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

- [SDR CALA2026101920439](https://openairdocs.org/sdr/CALA2026101920439), Oct 16, 2026: UNKNOWN. ODOR. 20MIN AFTER TAKE OFF, A FOUL ODOR FROM CAPT GSPR VENT AFTR INCREASES MID & AFT CABIN TEMPS. SMELL STARTED AFTER RAISING CABIN TEMP, ODOR DISSIPATED WHEN CABIN T
- [SDR CALA2026101920473](https://openairdocs.org/sdr/CALA2026101920473), Oct 16, 2026: AILERON. CONTAMINATED. DURING LH OUTBOARD AILERON THERMOGRAFIC INSPECTION WAS NOTICED ONE POINT OF MOISTURE INGRESS ON INBOARD EDGE LOWER SURFACE STA 910.45 DAMAGE C# UPGRADE THE ATTR
- [SDR CALA2026101920475](https://openairdocs.org/sdr/CALA2026101920475), Oct 16, 2026: AILERON. CONTAMINATED. DURING LT OTBD AILERON THERMOGRAFIC INSPECTION WAS NOTICED ONE POINT OF MOISTURE INGRESS ABOUT 25 INCHES FROM INBOARD EDGE LOWER SURFACE, ON A PREVIOUS REPAIR, 
- [SDR DALA2026092205280](https://openairdocs.org/sdr/DALA2026092205280), Sep 19, 2026: EEC. FAULTED. ATB FOR LEFT ENGINE EGT FLUCTUATING. T/S PER WDM 71-51-53. REPLACE W13 WIRE HARNESS AND EGT JUNCTION BOX. REPLACED LEFT EEC. OPS NORMAL.(9523618)(AIRCRAFT GROUN
- [SDR DALA2026082604837](https://openairdocs.org/sdr/DALA2026082604837), Aug 23, 2026: OIL SYSTEM. LEAKING. ATB- RIGHT ENGINE ROLLED BACK ON TAKEOFF ABOVE V1. AFTER AIRBORNE, ENGINE POWER RETURNED TO NORMAL. ON CLIMB, HAD A FUMES EVENT. PREFORMED BORESCOPE WITH NO FIN
- [SDR DALA2026082604838](https://openairdocs.org/sdr/DALA2026082604838), Aug 22, 2026: HMU. FAULTED. ATB- RETURNED TO JFK DUE TO NR 2 ENGINE COMPRESSOR STALL ON TAKEOFF. CREW HEARD SEVERAL POPS AND NOTICED N1 ERRATIC. BORESCOPE COMPLETED WITH NO FINDINGS. REPLA
- [SDR DALA2026063003863](https://openairdocs.org/sdr/DALA2026063003863), Jun 30, 2026: HMU. CRACKED. ATO - ABORTED TAKEOFF AT 80 KTS DUE TO LEFT ENGINE STALL. FOUND HMU CRACKED AND SPRAYING FUEL. REPLACED SAME AND PERFORMED BSI DUE TO REPORTED COMPRESSOR STALL 
- [SDR DALA2026061803634](https://openairdocs.org/sdr/DALA2026061803634), Jun 16, 2026: SENSOR. DAMAGED. ABORTED TAKE OFF AT 60KTS DUE TO BIRD STRIKE ON LEFT ENGINE. ALL PARAMETERS REMAINED NORMAL. ON INITIAL INSPECTION FOUND SEVERAL LEFT ENGINE DAMAGED. REPAIRED D
- [SDR CALA2025050904587](https://openairdocs.org/sdr/CALA2025050904587), May 6, 2025: BLEED VALVE. FAULTED. AFTER ADDING TAKEOFF POWER R ENG BLEED AND R PACK MESSAGE APPEA RED. REJECTED AT 85KTS. REQUEST APPROVAL TO DEFER RH HPSOV IAW MEL 3611BR. ENGINE HIGH PRESSURE 
- [SDR CALA2025041703956](https://openairdocs.org/sdr/CALA2025041703956), Apr 16, 2025: IDG. FAULTED. RT GEN OFF. RESET ONCE. FAILED A SECOND TIME. PERFORMED BPCU BITE PER MM 24-11- 00. FOUND MM 24-35002 FOR RIDG PHASE A CURRENT DISAGREE. PERFORMED BPCU BITE PER
- [SDR DALA2024120611493](https://openairdocs.org/sdr/DALA2024120611493), Dec 5, 2024: PRIORITY VALVE. OUT OF ALIGNMENT. SHIP 1809 -ATB- RETURN TO ATL DUE TO LOSS OF RT BLEED WITH ICING CONDITIONS ENROUTE. DURING RETURN DESCENT LOST LT HPSOV. AIRCRAFT LANDED OVERSPEED AND OVERWEIG
- [SDR DALA2024112611240](https://openairdocs.org/sdr/DALA2024112611240), Nov 23, 2024: SHUTOFF VALVE. WARNING MESSAGE. -DIV- TO ATL DUE TO RT HPSOV STATUS MESSAGE WITH ICING CONDITIONS ENROUTE AND LT HPSOV ALREADY DEFERRED. R/R RT HPSOV. PRESSURE GOOD BUT PI1 SENSOR FAULTED. REP
- [SDR DALA2024101410030](https://openairdocs.org/sdr/DALA2024101410030), Oct 9, 2024: VALVE. FAULTED. SHIP 1813 -DIV- DISPATCH DECISION TO DIVERT TO JFK DUE TO LT PNEUMATIC BLEED PRESSURE LOW. CORRECTIVE ACTION: RPLCD PRV DUE TO BINDING. RPLCD PRV MUSCLE LINE DU
- [SDR DALA2024070706830](https://openairdocs.org/sdr/DALA2024070706830), Jul 4, 2024: BLADES. DAMAGED. SHIP 1810 - DIV FLIGHT 0131 MUC-ATL DIVERTED TO CDG DUE TO RIGHT ENGINE HIGH VIBRATIONS AFTER TAKE OFF. CORRECTIVE ACTION: REMOVE AND REPLACED DAMAGED FAN ROTOR
- [SDR DALA2023080806435](https://openairdocs.org/sdr/DALA2023080806435), Aug 4, 2023: UNKNOWN. UNKNOWN. SHIP 1807 -ATB -TO LHR DUE TO RIGHT ENGINE OIL FILTER STATUS MESSAGE. CORRECTIVE ACTION: T/S PER B767-400FIM, OIL FILTER AND MASTER CHIP DETECTOR CHECK OK-NO DE
- [SDR DALA2023032802373](https://openairdocs.org/sdr/DALA2023032802373), Mar 26, 2023: UNKNOWN. UNKNOWN. SHIP 1810 - ATO- AT APPROXIMATELY 110 KNOTS DUE TO NUMBER 1 ENGINE SLOW TO ACCELERATE. PRESSURE CHECKED AND INSPECTED PS3 LINES WITH NO DEFECTS NOTED. EEC INSTA
- [SDR DALA2023021401142](https://openairdocs.org/sdr/DALA2023021401142), Feb 12, 2023: NONE. NONE. SHIP 1811 -ATB- DUE TO LOSS OF RT PNEUMATIC BLEED WITH ICING CONDITIONS ENROUTE. CORRECTIVE ACTION: R/R RT PRV SENSE LINE AND PRVC. (9932174)
- [SDR DALA2021122408039](https://openairdocs.org/sdr/DALA2021122408039), Dec 22, 2021: NONE. NONE. SHIP 1806 -DIV- TO SLC DUE LT ENGINE COMPRESSOR STALL WHEN ADVANCING THE THROTTLE IN CLIMB. CORRECTIVE ACTION: MAINTENANCE IN PROGRESS. PERFORMED BITE TEST OF E
- [SDR DALA2017091406890](https://openairdocs.org/sdr/DALA2017091406890), Sep 13, 2017: IDG. MALFUNCTIONED. RECEIVED A RT GENERATOR EICAS AND RT GENERATOR DRIVE EICAS. ABOUT ONE MINUTE AFTER, NOTICED ELECTRICAL (MOTOR RUNNING HOT) ODOR. DISSIPATED AFTER 20 SECONDS. TH
- [SDR DALA2017083006451](https://openairdocs.org/sdr/DALA2017083006451), Aug 29, 2017: EEC. MALFUNCTIONED. ATB TO ATL DUE TO A RIGHT ENGINE EEC CONTROL MESSAGE. MTC FOUND FADEC FAULT 155-23 FMV DISAGREE ON RIGHT EEC. CREW CONTACTED DISPATCH AND MC AND DECISION WAS MA
- [SDR DALA2017082906450](https://openairdocs.org/sdr/DALA2017082906450), Aug 26, 2017: ENGINE. MAKING METAL. RT ENG OIL FILTER MESSAGE DISPLAYED, OIL QUANTITY AND PRESSURE GOOD, ALL OTHER INDICATIONS NORMAL. DIVERTED. MAINTENANCE FOUND METAL DEBRIS ON MCD AND IN OIL FI
- [SDR CALA2017082502863](https://openairdocs.org/sdr/CALA2017082502863), Aug 25, 2017: TUBE. LEAKING. RIGHT ENGINE OIL QTY 5, WITH ENGINE AT IDLE AT 10000 FT. REMOVED THE TUBE B SCAVENGE INTO THE REAR CASE. THE TUBE THAT GOES INTO THE CASE HAS A SEAL WHICH LOOKS
- [SDR DALA2017032002222](https://openairdocs.org/sdr/DALA2017032002222), Mar 19, 2017: ENGINE. LEAKING. DIVERTED DUE TO APPROXIMATELY ONE HOUR INTO FLIGHT, THE LEFT ENGINE OIL QUANTITY DROPPED TO ZERO. OIL PRESSURE ALSO DROPPED. CREW CONSULTED QRH, AND CONTACTED D
- [SDR FDEA201603311128](https://openairdocs.org/sdr/FDEA201603311128), Mar 31, 2016: RELAY. INOPERATIVE. DURING PUSHBACK, REV ISLN, LIGHT ON THROTTLE QUADRANT ILLUMINATED. ADVISED MX THEY SAID IT WOULD EXTINGUISH AFTER TAKEOFF. AFTER TAKEOFF, REV ISLN, REMAINED ILL
- [SDR CALA2015102100864](https://openairdocs.org/sdr/CALA2015102100864), Oct 21, 2015: ENGINE. MALFUNCTIONED. ZERO OIL QTY & LOW OIL PRESS ON NR 1 ENG, FOLLOWED BY ENG SHUTDOWN. COMPLETED SINGLE APPROACH & LANDING. R & R NR 1 ENG IAW TASK CARD 64-7100-1-9800. PERFORMED 
- [SDR CALA2015082100694](https://openairdocs.org/sdr/CALA2015082100694), Aug 21, 2015: BLADE. DAMAGED. RIGHT ENG VIB FAN EXCEEDED 4.2, SUSPECTED BIRD STRIKE. ENG OPERATED WITHIN NORMAL PARAMETERS AT REDUCED POWER DURING DIVERSION. REMOVED 3 DAMAGED FAN BLADES 23,
- [SDR CALA2013052300350](https://openairdocs.org/sdr/CALA2013052300350), May 21, 2013: HMU. INOPERATIVE. NR 2 ENG COMPRESSOR STALL. R & R NR 2 HMU IAW AMM 73-21-14-404-030- HOO. OPS AND LEAK CHECKED GOOD.
- [SDR CALA2012091800609](https://openairdocs.org/sdr/CALA2012091800609), Sep 18, 2012: SKIN. CRACKED. RT WING 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED, RT WING 10 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND AT
- [SDR CALA2012091800610](https://openairdocs.org/sdr/CALA2012091800610), Sep 18, 2012: SKIN. CRACKED. RT WING 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING 9 SLAT, OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01. REPAIR 2, FIG 201 AND HFEC CRACK FOUND ATTACH 
- [SDR CALA2012091800611](https://openairdocs.org/sdr/CALA2012091800611), Sep 18, 2012: SKIN. CRACKED. RT WING 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING 9 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTAC
- [SDR CALA2012091800612](https://openairdocs.org/sdr/CALA2012091800612), Sep 18, 2012: SKIN. CRACKED. RT WING 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED RT WING 10 SLAT OTBD SKIN REPARED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTACH MX
- [SDR CALA2012091800613](https://openairdocs.org/sdr/CALA2012091800613), Sep 18, 2012: SKIN. CRACKED. LT WING 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTAC
- [SDR CALA2012091800614](https://openairdocs.org/sdr/CALA2012091800614), Sep 18, 2012: SKIN. CRACKED. LT WING 4, SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 4 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NIL CRACK FOUND ATTA
- [SDR CALA2012091800615](https://openairdocs.org/sdr/CALA2012091800615), Sep 18, 2012: SKIN. CRACKED. LT WING 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 3 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01. REPAIR 2, FIG 201 AND HFEC CRACK FOUND ATTACH MX
- [SDR CALA2012091800616](https://openairdocs.org/sdr/CALA2012091800616), Sep 18, 2012: SKIN. CRACKED. LT WING 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED LT WING 3 SLAT OTBD NOSE SKIN RIVET AREA. REPAIRED IAW SRM 57-43-01. REPAIR 2, FIG 201 AND HFEC NIL CRACK
- [SDR CALA2012092000617](https://openairdocs.org/sdr/CALA2012092000617), Sep 18, 2012: SHEAR TIE. CORRODED. FOUND CORROSION ON THE SHEAR TIE AT BULK CARGO BS1417 BL0 BULK CARGO, BS1417 BL0. SHEAR TIE REPLACED IAW SRM 31-10-02 AND FASTENER INSTALLED IAW SRM 51-40-01 AT
- [SDR CALA2012091700601](https://openairdocs.org/sdr/CALA2012091700601), Sep 14, 2012: FLOORBEAM. CORRODED. CABIN BS 303, LBL 21-53, FLOORBEAM CORRODED CABIN BS 303 LBL9" TO LBL 65" FLOORBEAM UPPER CHORD FLANGE REPAIR ED IAW SRM 53-00-51, REPAIR 1, FIG 201 AND HFEC CR
- [SDR CALA2012091700602](https://openairdocs.org/sdr/CALA2012091700602), Sep 14, 2012: FLOORBEAM. CORRODED. CABIN BS 325, LBL 21-55 FLOORBEAM CORRODED CABIN BS325, LBL 11-65 FLOORBEAM UPR CHORD FLANGE REPAIRED IAW SRM 53-00-51. REPAIR 1, FIG 201 AND HFEC NIL CRACK FOU
- [SDR CALA2012091000586](https://openairdocs.org/sdr/CALA2012091000586), Sep 8, 2012: FLOORBEAM. CORRODED. CABIN BS 303, LBL 20-26 FLOORBEAM CORRODED. FLOORBEAM REPAIRED IAW SRM 53-0051, FIG 201 REPAIR AND HFEC NO CRACK FOUND.
- [SDR CALA2012091000587](https://openairdocs.org/sdr/CALA2012091000587), Sep 7, 2012: FLOORBEAM. CORRODED. FLOORBEAM CORRODED CABIN BS 325 LBL 7 TO 64, UPPER TEE REPAIRED IAW SRM 53-00-51 REPAIR 1, FIG 201 HFEC NO CRACK FOUND.
- [SDR CALA2012091000589](https://openairdocs.org/sdr/CALA2012091000589), Sep 7, 2012: SKIN. CRACKED. NR 10 SLAT EXTERIOR SKIN CRACK AT OTBD MAIN TRACK. NR 10 SLAT EXTERIOR SKIN AT OTBD MAIN TRACK AREA REPLAIRED IAW SRM 57-43-01, FIG 201, REPAIR 2 HFEC NO CRACK 
- [SDR CALA2012091000590](https://openairdocs.org/sdr/CALA2012091000590), Sep 7, 2012: SKIN. CRACKED. LEFT WING NR 3 SLAT L/E EXTERIOR SKIN FOUND CRACK AT INBD MAIN TRACK AREA AS MARK. LT WING NR 3 SLAT L/E EXTERIOR SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 
- [SDR CALA2012091000591](https://openairdocs.org/sdr/CALA2012091000591), Sep 7, 2012: SKIN. CRACKED. NR 9 SLAT EXTERIOR SKIN CRACK AT OTBD MAIN TRACK. NR 9 SLAT EXTERIOR SKIN AT OTBD MAIN TRACK AREA REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NO CRACK
- [SDR CALA2012091000592](https://openairdocs.org/sdr/CALA2012091000592), Sep 7, 2012: SKIN. CRACKED. LEFT WING NR 4 SLAT L/E EXTERIOR SKIN FOUND CRACK AT INBD MAIN TRACK AREA AS MARK. LT WING NR 4 SLAT L/E EXTERIOR SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 
- [SDR CALA2012091000593](https://openairdocs.org/sdr/CALA2012091000593), Sep 7, 2012: SKIN. CRACKED. NR 10 SLAT EXTERIOR SKIN CRACK AT INBD MAIN TRACK. NR 10 SLAT EXTERIOR SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND FORM 44.0008 ITEM 1 TO 15 ACCOMPLIS
- [SDR CALA2012091000594](https://openairdocs.org/sdr/CALA2012091000594), Sep 7, 2012: SKIN. CRACKED. NR 9 SLAT EXTERIOR SKIN CRACK AT INBD MAIN TRACK. RT NR 9 SLAT EXTERIOR SKIN REPAIRED IAW SRM 57-43-01, REPAIR 2, FIG 201 AND HFEC NO CRACK FOUND AND ATTACH FOR
- [SDR CALA2012091000596](https://openairdocs.org/sdr/CALA2012091000596), Sep 7, 2012: SKIN. CRACKED. LT WING NR 4 SLAT L/E EXTERIOR SKIN FOUND CRACK AT OTBD MAIN TRACK AREA. LT WING NR 4 SLAT L/E EXTERIOR SKIN AT OTBD MAIN TRACK AREA REPAIRED IAW SRM 57-43-01. 
- [SDR CALA2012091000588](https://openairdocs.org/sdr/CALA2012091000588), Sep 7, 2012: FLOOR SUPPORT. CORRODED. CABIN BS 303-325 LBL 30 FLOOR SUPPORT CORRODED. FLOOR SUPPORT REPLACED IAW SRM 51-10-02 AND FASTENER INSTALLED IAW SRM 51-40-02.
- [SDR CALA2012090500561](https://openairdocs.org/sdr/CALA2012090500561), Sep 4, 2012: BATTERY. INOPERATIVE. COCKPIT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW GMM 05-20-10, ITEM 9.
- [SDR CALA2012090400560](https://openairdocs.org/sdr/CALA2012090400560), Sep 3, 2012: LIGHT. INOPERATIVE. EMERGENCY EXIT LIGHT WILL NOT TEST, REPLACED PORTABLE FLT DECK EMERGENCY EXIT SIGN L286 AND LIGHT MOUNTING PLATE M744. IAW WDM 33-51-11, OPS CHECKED NORMAL.

All 98: https://openairdocs.org/engine/ge-cf6-80c2b8f/reports.md

## STCs that may be installed (OpenAirDocs) (4)

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. Lists CF6-80C2 Series
- [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 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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.