# GE CF6-80C2D1F

- Type: Engine model (FAA registry)
- Registry code: 30110
- Manufacturer (registry): GE
- Model: CF6-80C2D1F
- Engine type: Turbo-fan
- Power: 60,690 lb thrust
- Data sheet: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 24 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-80c2d1f

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 2024-24-03](https://openairdocs.org/ad/2024-24-03): Engine Exhaust · Boeing MD-11, MD-11F and CF6-80C2D1F. Effective Jan 13, 2025
- [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 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 2007-22-07](https://openairdocs.org/ad/2007-22-07): Electronic control unit (ECU) · General Electric CF6-80C2D1F. Effective Nov 28, 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 2006-06-08](https://openairdocs.org/ad/2006-06-08): Latching system of the fan reverser · General Electric CF6-80C2D1F. Effective Apr 25, 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 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 2003-02-07](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
- [AD 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991
- [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991
- [AD 91-05-21](https://openairdocs.org/ad/91-05-21): High Pressure Turbine · General Electric CF6-80C2A5, CF6-80C2B6, CF6-80C2B6F and 1 more. Effective Mar 27, 1991

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 2000-16-12](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 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999
- [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991
- [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990

## 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 (24)

- [N257UP](https://openairdocs.org/aircraft/N257UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 1992, S/N 48451
- [N258UP](https://openairdocs.org/aircraft/N258UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 1991, S/N 48416
- [N260UP](https://openairdocs.org/aircraft/N260UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 1992, S/N 48418
- [N261UP](https://openairdocs.org/aircraft/N261UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 2001, S/N 48805
- [N262UP](https://openairdocs.org/aircraft/N262UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 2001, S/N 48806
- [N263UP](https://openairdocs.org/aircraft/N263UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 1998, S/N 48782
- [N264UP](https://openairdocs.org/aircraft/N264UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 2000, S/N 48800
- [N265UP](https://openairdocs.org/aircraft/N265UP): [United Parcel Service Co](https://openairdocs.org/faa-owner/UNITED%20PARCEL%20SERVICE%20CO), [Louisville, KY](https://openairdocs.org/faa-place/KY/Louisville), built 2001, S/N 48803
- [N415JN](https://openairdocs.org/aircraft/N415JN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Fisher Island, FL](https://openairdocs.org/faa-place/FL/Fisher%20Island), S/N 48415
- [N512JN](https://openairdocs.org/aircraft/N512JN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Fisher Island, FL](https://openairdocs.org/faa-place/FL/Fisher%20Island), built 1992, S/N 48512
- [N513SN](https://openairdocs.org/aircraft/N513SN): [M48513 LLC](https://openairdocs.org/faa-owner/M48513%20LLC), [Esters, FL](https://openairdocs.org/faa-place/FL/Esters), built 1994, S/N 48513
- [N542KD](https://openairdocs.org/aircraft/N542KD): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Fisher Island, FL](https://openairdocs.org/faa-place/FL/Fisher%20Island), built 1994, S/N 48542
- [N543JN](https://openairdocs.org/aircraft/N543JN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Fisher Island, FL](https://openairdocs.org/faa-place/FL/Fisher%20Island), built 1994, S/N 48543
- [N545JN](https://openairdocs.org/aircraft/N545JN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Miami Beach, FL](https://openairdocs.org/faa-place/FL/Miami%20Beach), built 1995, S/N 48545
- [N546JN](https://openairdocs.org/aircraft/N546JN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Fisher Island, FL](https://openairdocs.org/faa-place/FL/Fisher%20Island), built 1995, S/N 48546
- [N572FE](https://openairdocs.org/aircraft/N572FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1997, S/N 48755
- [N573FE](https://openairdocs.org/aircraft/N573FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1996, S/N 48769
- [N575FE](https://openairdocs.org/aircraft/N575FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1992, S/N 48500
- [N581JN](https://openairdocs.org/aircraft/N581JN): [Mobility Air LLC](https://openairdocs.org/faa-owner/MOBILITY%20AIR%20LLC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1994, S/N 48581
- [N625FE](https://openairdocs.org/aircraft/N625FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1996, S/N 48753
- [N649FE](https://openairdocs.org/aircraft/N649FE): [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1999, S/N 48801
- [N781SN](https://openairdocs.org/aircraft/N781SN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Fisher Island, FL](https://openairdocs.org/faa-place/FL/Fisher%20Island), built 1998, S/N 48781
- [N783SN](https://openairdocs.org/aircraft/N783SN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Fisher Island, FL](https://openairdocs.org/faa-place/FL/Fisher%20Island), built 1998, S/N 48783
- [N804SN](https://openairdocs.org/aircraft/N804SN): [Atares Funding LLC](https://openairdocs.org/faa-owner/ATARES%20FUNDING%20LLC), [Miami Beach, FL](https://openairdocs.org/faa-place/FL/Miami%20Beach), built 2000, S/N 48804

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA26MA024](https://openairdocs.org/ntsb/DCA26MA024), Nov 4, 2025: Mcdonnell Douglas MD-11F (N259UP), Louisville, KY, destroyed, 14 fatal, investigation ongoing

## FAA accident and incident reports (4)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20251104016149A](https://openairdocs.org/incident/20251104016149A), Nov 4, 2025: Mcdonnell Douglas MD-11F (N259UP), Louisville, KY, Destroyed, 14 fatal. The airplane took off from sdf about 1713 and video of the airplane shows the no. 1 (left) engine and pylon separating and subsequent fire on the left Wing.…
- [Incident 20250722020559I](https://openairdocs.org/incident/20250722020559I), Jul 22, 2025: Mcdonnell Douglas MD-11F (N262UP), Miami, FL, Minor damage. At touchdown, runway 8L, the #10 center landing gear tire failed with debris striking the center gear right-hand flying gear door causing minor deformation to…
- [Incident 20190716016209I](https://openairdocs.org/incident/20190716016209I), Jul 16, 2019: Mcdonnell Douglas MD-11 (N512JN), Prestwick, OC, No damage. The crew made an erroneous waypoint input during the flight Planning phase, and subsequently failed to follow established procedures designed to trap these…
- [Incident 20100604035079I](https://openairdocs.org/incident/20100604035079I), Jun 4, 2010: Mcdonnell D MD-11F (N260UP), Anchorage, AK, Substantial damage. Aircraft N260UP departed rwy 14. At approximately 600' AGL, the #3 engine fire indication came on for approximately 5 seconds and then extinguished. The…

## Service difficulty reports (536, newest 50)

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

- [SDR 9WGA2026071678101](https://openairdocs.org/sdr/9WGA2026071678101), Jul 16, 2026: ENGINE. POWER LOSS. AIRCRAFT TAKEOFF FROM JIB AIRPORT, DURING CLIMB OUT ENG 1 VIB 5.1 FOLLOWED BY RAPID DECELERATION OF N1 W/HIGH BUFFETING, SHUTDOWN ENG 1, AIRCRAFT RETURNED SAFEL
- [SDR IPXA2025061983508](https://openairdocs.org/sdr/IPXA2025061983508), Jun 18, 2025: ENGINE. FLAMED OUT. EMERGENCY DECLARED. DURING FLIGHT AT FL390 WE GOT A LEVEL 1 TANK 2 PUMPS OFF. FUEL SYSTEM WAS IN MANUAL MODE PER MEL 28-01-1-2. THIS WAS FOLLOWED BY A LEVEL 2 E
- [SDR 9WGA2025061054502](https://openairdocs.org/sdr/9WGA2025061054502), May 2, 2025: CASE. CORRODED. DURING HEAVY CHECKENGINE #1 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION. CLEANED CORROSION, APPLIED ALODINE, & PRIMER IAW MD-11 SR
- [SDR 9WGA2025061054503](https://openairdocs.org/sdr/9WGA2025061054503), May 2, 2025: CASE. CORRODED. DURING HEAVY CHECK ENGINE #3 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION (RUSTY). CLEANED CORROSION (RUSTY) AT ENGINE #3 FAN CASE 
- [SDR 9WGA20250428016](https://openairdocs.org/sdr/9WGA20250428016), Apr 14, 2025: RING. CORRODED. #2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF.
- [SDR 9WGA20250428017](https://openairdocs.org/sdr/9WGA20250428017), Apr 14, 2025: RING. CORRODED. #1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ THE 8' O'CLOCK POSITION.
- [SDR 9WGA2025042854616](https://openairdocs.org/sdr/9WGA2025042854616), Apr 14, 2025: RING. CORRODED. DURING HEAVY MAINTENANCE CHECK NR 2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVAL ANF REPLACEMENT IAW MD-11 
- [SDR 9WGA2025042854617](https://openairdocs.org/sdr/9WGA2025042854617), Apr 14, 2025: RING. CORRODED. DURING HEAVY MAINTENANCE CHECK NR 1 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ 8 O'CLOCK POSITION. ACCOMPLISHED WITH ENGINE REMOVAL AND REPLACEMENT IAW MD
- [SDR 9WGA2025042954618](https://openairdocs.org/sdr/9WGA2025042954618), Apr 14, 2025: RING. CORRODED. #3 ENGINE CONTAINMENT RING FWD SIDE HAS CORROSION @ THE 8 O'CLOCK POSITION.
- [SDR 9WGA2025042954619](https://openairdocs.org/sdr/9WGA2025042954619), Apr 14, 2025: INLET. CORRODED. #3 INLET HAS PITTING CORROSION BETWEEN 5 & 6 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 5 & 6 O'CLOCK POSI
- [SDR 9WGA2025042954620](https://openairdocs.org/sdr/9WGA2025042954620), Apr 14, 2025: INLET. CORRODED. 3# INLET HAS PITTING CORROSION AT 3 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET AT 3 O'CLOCK POSITION. FOUND WITHIN
- [SDR 9WGA2025042954621](https://openairdocs.org/sdr/9WGA2025042954621), Apr 14, 2025: INLET. CORRODED. #3 INLET HAS PITTING CORROSION BETWEEN 8 & 9 O'CLOCK POS. REMOVED MILD SURFACE CORROSION AND LITE PITTING BY HAND RUBBING ON #3 INLET BETWEEN 8 AND 9 O'CLOCK PO
- [SDR 9WGA2025042854601](https://openairdocs.org/sdr/9WGA2025042854601), Apr 14, 2025: RING. CORRODED. NR# 286 - DURING HEAVY MAINTNENANCE #2 ENGINE L/E OF CONTAINMENT RING HAS CORROSION AROUND BOTTOM HALF. ACCOMPLISHED WITH ENGINE REMOVED AND REPLACEMENT IAW MD-
- [SDR FDEA202503300539](https://openairdocs.org/sdr/FDEA202503300539), Mar 30, 2025: ENGINE. FAILED. PDIS 595 79-36 8740 30MAR25 02:47 NRT OPEN ENG 3 OIL FILTER LEVEL 2 ALERT @FL350. AIRFRAME VIBRATION STARTED JUST PRIOR TO ALERT AND CONTINUED UNTIL THROTTLE AT
- [SDR FDEA202407141001](https://openairdocs.org/sdr/FDEA202407141001), Jul 14, 2024: DEU. FAULTED. ENGINE FAIL LIGHT ILLUMINATED AT ABOUT 100 KTS ON THE TAKEOFF ROLL. THE TAKEOFF WAS REJECTED. ALL ENGINES WERE OPERATING NORMALLY AFTER THE REJECT. REPLACED DEU
- [SDR FDEA202407090975](https://openairdocs.org/sdr/FDEA202407090975), Jul 9, 2024: ENGINE. VIBRATION. NR 3 ENGINE HIGH VIBE 5.0 & ABOVE.VERBAL FROM FLIGHT CREW. REF ER 24-01792 COMPLETED #3 ENGINE INSTALLATION REF WIC 7100000-03-91. REPLACED THE ENGINE
- [SDR FDEA202405080615](https://openairdocs.org/sdr/FDEA202405080615), May 8, 2024: COMPRESSOR. STALLED. ON TAKE OFF ENGINE 1 COMPRESSOR STALLED WITH N1 ROLL BACK X 3. NO OTHER INDICATIONS. DUMPED 130K AND RETURNED TO CDG. REPLACED #1 ENGINE HP FUEL PUMP PER MM 73-
- [SDR FDEA202303310535](https://openairdocs.org/sdr/FDEA202303310535), Mar 31, 2023: ENGINE. INOPERATIVE. ON APPROACH TO 18R IN MEM, AIRCRAFT WAS STRUCK ON THE NOSE BY LIGHTNING. SUBSEQUENTLY LOST CONTROL OF THE NUMBER 2 ENGINE. ATTEMPTED TO TROUBLESHOOT BUT NO RESP
- [SDR 9WGA2022111280401](https://openairdocs.org/sdr/9WGA2022111280401), Nov 12, 2022: ANTI-ICE VALVE. INOPERATIVE. DISCREPANCY: LEVEL 3 ENGINE 2 A/I DUCT ALERT. CORRECTIVE ACTION: REMOVED AND REPLACED #2 ANTI-ICE VALVE PER AMM 30-22-01 AND C/W FIM 30-22-05. OPS CHECK GOOD.
- [SDR IPXA2022101487138](https://openairdocs.org/sdr/IPXA2022101487138), Oct 13, 2022: PUMP. FAILED. INSPECTION TYPE:N/A**SUPPLEMENTAL SDR**EMERGENCY DECLARED**#2 ENGINE FLAMED OUT IN CRUISE AT FL280. FUEL SYS DEFERRED IN MANUAL PROCEDURES. ATTEMPTED RESTART PE
- [SDR FDEA202208272080](https://openairdocs.org/sdr/FDEA202208272080), Aug 27, 2022: HOSE. LEAKING. ON CLIMB OUT PASSING APPROXI 2500 FT FELT A BRIEF THUMP. APPROX 10 SECS LATER, NR 2 ENG ROLLED BACK TO BELOW IDLE. GOT LVL 2 ENGINE 2 RPM LO ALERT. ENG STILL WI
- [SDR 9WGA2022081978301](https://openairdocs.org/sdr/9WGA2022081978301), Aug 19, 2022: OIL SYSTEM. LEAKING. #1 ENGINE HAS NO OIL, AIR RETURN. : R & R #1 ENGINE PER AMM 71-00-01. ENGINE RUN SATISFACTORY. REPLACE #1 ENGINE ACCOMPLISHED IAW JC RNR 11071001 R0. THIS COMPL
- [SDR 2022FA0000333](https://openairdocs.org/sdr/2022FA0000333), Jul 7, 2022: DISK. CRACKED. INDICATION IN BORE A ZONE CORNER, AMPLITUDE 2020MV. GE ENGINE SHOP MANUAL (ESM) EVALUATION/REJECTION LIMIT IS 1500MV.
- [SDR FDEA202207021673](https://openairdocs.org/sdr/FDEA202207021673), Jul 2, 2022: ENGINE. FLAMED OUT. ENG 2 FLAMED OUT AT FL380. EMERGENCY DECLARED DIVERTED TO TPA, LANDED SAFELY, TAXIED TO RAMP UNDER OWN POWER WITHOUT ASSISTANCE. ENGINE 2 FLAME OUT CAUSE VERIFI
- [SDR 2022F00269](https://openairdocs.org/sdr/2022F00269), Jun 22, 2022: NONE. NONE. #2 ENGINE SHUTDOWN DURING CRUISE, TAIL PUMPS LO, ALT PUMPS LO
- [SDR 9WGA2022062141201](https://openairdocs.org/sdr/9WGA2022062141201), Jun 21, 2022: FUEL SYS. ABNORMAL. TAIL PUMPS LOW, ALT PUMPS LOW, ENGINE 2 SHUTDOWN IN FLIGHT. FOUND FSC FAULTING. REPLACED AFSC, FSC AND FSC CONTROL PANEL. OPS TEST FOUND NORMAL. ACCOMPLISHED MP
- [SDR 9WGA2022051754301](https://openairdocs.org/sdr/9WGA2022051754301), May 17, 2022: ENGINE. OUT OF RIG. AIR RETURN DUE TO ENGINE 3 NOT DEVELOPING FULL CLIMB POWER 4% LESS N1 @ 10000 & 7% LESS AT 35000. ENGINE 3 EGT, N2 & FF CONFIRM POWER LOSS. ENGINE 3 "T" WOULD N
- [SDR FDEA202112203109](https://openairdocs.org/sdr/FDEA202112203109), Dec 20, 2021: LINE. LEAKING. CLIMBING THROUGH 3,000' GOT INDICATE VISIBLE SMOKE WITH A BITING,ACRID SMELL.RAN CHECK LIST,DECLARED EMERGENCY,LANDED UNEVENTUALLY,NO FUEL DUMP.HOT BRAKES LIGHT
- [SDR MASA2021090800232](https://openairdocs.org/sdr/MASA2021090800232), Sep 8, 2021: ENGINE. OVERTEMP. L / R ENGINE OVERTEMP ON CLIMB OUT. AIRCRAFT IS STILL CURRENTLY OOS.
- [SDR AALA202109083000](https://openairdocs.org/sdr/AALA202109083000), Sep 7, 2021: SHEAR PIN. CORRODED. AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT ENGINE; AFT ENGINE MOUNT INNER SHEAR PIN ON INBOARD LINK UPPER POSITION. REPLACED SHEAR PIN PER AMM 71-22-11-200
- [SDR IPXA2021090473547](https://openairdocs.org/sdr/IPXA2021090473547), Aug 26, 2021: FASTENER. LOOSE. INSPECTION TYPE:1C#2 ENGINE INLET NOSE SKIN HAS 23 LOOSE FASTENERS.REPAIRED #2 ENGINE INLET NOSE SKIN LOOSE FASTENERS IAW VT-SAA EA 011-7110-01-A9334 REV. IR AN
- [SDR FDEA202108222077](https://openairdocs.org/sdr/FDEA202108222077), Aug 22, 2021: COUPLING. MISSING. DURING B CHECK INSPECTION OF NR1 ENGINE, THE UPPER ANTI-ICE DUCT COUPLING WAS FOUND TO BE MISSING FROM THE UPPER ANTI-ICE DUCT ASSEMBLY. THE COUPLING WAS FOUND 
- [SDR IPXA2021090773676](https://openairdocs.org/sdr/IPXA2021090773676), Aug 19, 2021: SLEEVE. DAMAGED. INSPECTION TYPE:1C#1 ENG. R/H THRUST REVERSER TRANSLATING SLEEVE ASLAND PANEL HAS AN ELONGATED HOLE.REPAIRED #1 R/H T/R IAW VT-SAA EA 011-7830-01-A9339 REV. I/R
- [SDR 9WGA2021080655131](https://openairdocs.org/sdr/9WGA2021080655131), Aug 5, 2021: COMPRESSOR. VIBRATION. DIVERSION DUE TO ENG 3 VIB HIGH COMP OVER 4.0 ON CLIMB ON MULTIPLE OCCASION AND HAD TO RETARD #3 MORE THAN 1 CROWN TO REDUCE THE VIBRATION.
- [SDR IPXA2021072972246](https://openairdocs.org/sdr/IPXA2021072972246), Jul 21, 2021: SKIN. CRACKED. INSPECTION TYPE:2C#1 ENGINE L/H T/R AFT FIXED INNER BARREL UPPER SKIN IS CRACKED.REPAIRED CRACKED #1 ENGINE L/H T/R AFT FIXED INNER BARREL UPPER SKIN IAW VT-SAA
- [SDR IPXA2021072772137](https://openairdocs.org/sdr/IPXA2021072772137), Jul 6, 2021: SKIN. GOUGED. INSPECTION TYPE:2C#1 ENGINE I/B T/R LOWER SIDE WALL FACE SHEET IS GOUGED.REPAIRED GOUGED #1 ENGINE I/B T/R LOWER SIDE WALL FACE SHEET IAW VT-SAA EA 011-7830-01-
- [SDR IPXA2021062570951](https://openairdocs.org/sdr/IPXA2021062570951), Jun 24, 2021: START VALVE. FAULTED. ATB ** LANDED WITHOUT INCIDENT ** PASSING FL220 START VALVE LIGHT ILLUMINATED. CREW WAS DIVERTED DUE TO ICING CONDITIONS. CREW WILL WORK WITH DISPATCH ON THAT. 
- [SDR IPXA2021071371618](https://openairdocs.org/sdr/IPXA2021071371618), Jun 18, 2021: FASTENER. LOOSE. INSPECTION TYPE:2C#2 ENGINE INLET LIP HAS LOOSE FASTENERS.REPAIRED #2 ENGINE INLET LIP LOOSE FASTENERS IAW VT-SAA EA 011-7110-01-A9204 REV. IR AND UPS EO MD11-7
- [SDR 9WGA2021060454201](https://openairdocs.org/sdr/9WGA2021060454201), Jun 4, 2021: OIL SYSTEM. LOW PRESSURE. AIR RETURN, ENGINE 3 OIL PRESSURE LOW.
- [SDR FDEA202105181286](https://openairdocs.org/sdr/FDEA202105181286), May 18, 2021: ENGINE. FLAMED OUT. NUMBER TWO ENGINE FLAMED OUT WITH THROTTLE ADVANCE FOR TAKE OFF. RAN QRH CONTACTED MOCC, RESTARTED ENGINE, NORMAL START AND CLIMB OUT. SHGN 18MAY21 08:25 MEM U 
- [SDR FDEA202105181287](https://openairdocs.org/sdr/FDEA202105181287), May 18, 2021: ENGINE. FLAMED OUT. ENGINE 2 FLAMEOUT AFTER ADDING POWER FOR TAKEOFF. RAN QRH CONTACTED MOCC , NORMAL RELIGHT AND TAKEOFF. SHGN 18MAY21 08:18 MEM U STARTED AND RAN ENGINE #2 FOR 5 
- [SDR FDEA202105171260](https://openairdocs.org/sdr/FDEA202105171260), May 17, 2021: ENGINE. FAILED. PDIS 573 71-00 6503 17MAY21 STN OPEN U DURING DEPARTURE CLIMBING THROUGH 3000 FEET DURING POWER REDUCTION HAD 3 SEPARATE AUDIBLE BANGS WITH MODERATE RIGHT YAW- 
- [SDR FDEA202104210964](https://openairdocs.org/sdr/FDEA202104210964), Apr 21, 2021: FLANGE. CORRODED. NR 2 ENGINE HAS SIGNS OF CORROSION ON FAN CASE FWD FLANGE FROM APPROXIMATELY 4 TO 8 O'CLOCK POS. REFERENCE NONROUTINE N00018 WORK ORDER 79912 ITEM FOUND DURING 
- [SDR 9WGA2021041841501](https://openairdocs.org/sdr/9WGA2021041841501), Apr 18, 2021: ENGINE. MALFUNCTIONED. LEVEL 2 "ENG 3 RPM LO" ON DESCENT. ATTEMPTED RESTART. SECURED ENGINE. EMERGENCY DECLARED.
- [SDR FDEA202104110885](https://openairdocs.org/sdr/FDEA202104110885), Apr 11, 2021: HMU. MALFUNCTIONED. PASSING - 1000 FT MSL, EXPERIENCED 4-5 LOUD BANGS WITH ACFT VIBRATION. F/O NOTICED A FLUCUATION ON THE #3 ENG N1 GAGE . TOWER REPORTED BLACK SMOKE FROM #3 ENG. 
- [SDR IPXA2021052869913](https://openairdocs.org/sdr/IPXA2021052869913), Apr 11, 2021: RIB. GOUGED. INSPECTION TYPE:3C#1 ENGINE I/B T/R RIB AT NAC STA 210.130 HAS 2 GOUGES.REPAIRED GOUGED #1 ENGINE I/B T/R ZEE RIB AT NAC STA 210.130 IAW VT-SAA EA 011-7832-01-A
- [SDR FDEA202103260774](https://openairdocs.org/sdr/FDEA202103260774), Mar 26, 2021: FUEL CONTROL. FAILED. RIGHT AFTER TAKEOFF ,HEARD ABOUT 5 COMPRESSOR STALLS FROM THE NO 3 ENGINE ALSO NOTICED FLASHES OUT OF THE RIGHT WINDOW . N1 EGT SHOWED FLUCUATIONS UNTIL POWER W
- [SDR IPXA2021022065873](https://openairdocs.org/sdr/IPXA2021022065873), Feb 20, 2021: FADEC. MALFUNCTIONED. INSPECTION TYPE: N/A ATB A/C OOS. NO EMERGENCY DECLARED. LANDED SUCCESSFUL LEVEL ONE FADEC MAIN.
- [SDR 9WGA20210112](https://openairdocs.org/sdr/9WGA20210112), Jan 12, 2021: WARNING MESSAGE. ILLUMINATED. LEVEL 3 ENGINE 2 A-ICE DUCT IN FLIGHT AT 7000 MSL AND 8500 MSL. SHUT DOWN NR 2 ENGINE, PER QRH.
- [SDR IPXA2020123063953](https://openairdocs.org/sdr/IPXA2020123063953), Dec 28, 2020: ENGINE. FLAMED OUT. INSPECTION TYPE: N/A DURING TAXI, NR 2 ENGINE FLAMED OUT, ALL ENGINE PARAMETER ROLLED BACK. NO FCC FAULTS ON ECU 2A ON 2B FAULTS, PER FON MTS NORMAL START, PER 

All 536: https://openairdocs.org/engine/ge-cf6-80c2d1f/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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