# GE CF6-80C2B6

- Type: Engine model (FAA registry)
- Registry code: 30103
- Manufacturer (registry): GE
- Model: CF6-80C2B6
- Engine type: Turbo-fan
- Power: 60,070 lb thrust
- Data sheet: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 25 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-80c2b6

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 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 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 2007-11-20](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 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
- [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 (25)

- [N307AZ](https://openairdocs.org/aircraft/N307AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1997, S/N 28725
- [N311AZ](https://openairdocs.org/aircraft/N311AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1991, S/N 25316
- [N313AZ](https://openairdocs.org/aircraft/N313AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1990, S/N 24930
- [N317CM](https://openairdocs.org/aircraft/N317CM): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1988, S/N 24317
- [N331AZ](https://openairdocs.org/aircraft/N331AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1991, S/N 24875
- [N347AZ](https://openairdocs.org/aircraft/N347AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1994, S/N 26264
- [N347CM](https://openairdocs.org/aircraft/N347CM): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1993, S/N 26995
- [N351CM](https://openairdocs.org/aircraft/N351CM): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1992, S/N 25201
- [N359AZ](https://openairdocs.org/aircraft/N359AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1988, S/N 24036
- [N362CM](https://openairdocs.org/aircraft/N362CM): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), S/N 24316
- [N367AZ](https://openairdocs.org/aircraft/N367AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1993, S/N 26912
- [N371CM](https://openairdocs.org/aircraft/N371CM): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1994, S/N 25577
- [N372CM](https://openairdocs.org/aircraft/N372CM): [Airborne Maintenance And Engineering Serives Inc](https://openairdocs.org/faa-owner/AIRBORNE%20MAINTENANCE%20AND%20ENGINEERING%20SERIVES%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1992, S/N 25575
- [N373CM](https://openairdocs.org/aircraft/N373CM): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1990, S/N 24929
- [N379AZ](https://openairdocs.org/aircraft/N379AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1992, S/N 25200
- [N389AZ](https://openairdocs.org/aircraft/N389AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1995, S/N 26915
- [N419AZ](https://openairdocs.org/aircraft/N419AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1994, S/N 26913
- [N431AZ](https://openairdocs.org/aircraft/N431AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1989, S/N 24632
- [N433AZ](https://openairdocs.org/aircraft/N433AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1989, S/N 24400
- [N443AZ](https://openairdocs.org/aircraft/N443AZ): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1992, S/N 25202
- [N503AZ](https://openairdocs.org/aircraft/N503AZ): [Amazon.Com Services LLC](https://openairdocs.org/faa-owner/AMAZON.COM%20SERVICES%20LLC), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle), built 1991, S/N 25274
- [N762CK](https://openairdocs.org/aircraft/N762CK): [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti), built 1992, S/N 26236
- [N763CK](https://openairdocs.org/aircraft/N763CK): [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti), built 1993, S/N 26233
- [N764CK](https://openairdocs.org/aircraft/N764CK): [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti), built 1994, S/N 26234
- [N765CK](https://openairdocs.org/aircraft/N765CK): [Kalitta Air LLC](https://openairdocs.org/faa-owner/KALITTA%20AIR%20LLC), [Ypsilanti, MI](https://openairdocs.org/faa-place/MI/Ypsilanti), built 1992, S/N 26238

## NTSB investigations (7)

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 DCA26WA355](https://openairdocs.org/ntsb/DCA26WA355), Sep 6, 2026: Boeing 767-338 (N373CM), Guatemala City, Guatemala, substantial damage
- [NTSB DCA26LA097](https://openairdocs.org/ntsb/DCA26LA097), Jan 16, 2026: Boeing 767 (N443AZ), San Bernardino, CA, substantial damage, investigation ongoing
- [NTSB ENG25LA053](https://openairdocs.org/ntsb/ENG25LA053), Apr 26, 2025: Boeing 767 (N347AZ), Honolulu, HI, incident, no damage, investigation ongoing
- [NTSB DCA25WA164](https://openairdocs.org/ntsb/DCA25WA164), Mar 23, 2025: Boeing 767 (N373CM), Managua, Nicaragua, incident
- [NTSB DCA24WA132](https://openairdocs.org/ntsb/DCA24WA132), Mar 23, 2024: Boeing 767-338 (N372CM), Panama City, Panama, substantial damage
- [NTSB DCA18WA173](https://openairdocs.org/ntsb/DCA18WA173), May 3, 2018: Boeing 767 323 (N396AN), Guayaquil, Ecuador, incident, no damage
- [NTSB DCA17WA037](https://openairdocs.org/ntsb/DCA17WA037), Nov 29, 2016: Boeing 767-319ER (N767WA), Georgetown, Guyana, substantial damage

## FAA accident and incident reports (2)

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 20260115010979A](https://openairdocs.org/incident/20260115010979A), Jan 15, 2026: Boeing 767-323 (N443AZ), San Bernandino, CA, Substantial damage. [privacy data omitted] Departed spokane Washington airport (kgeg) at 2102 pacific time for an arrival into san Bernardino California airport (ksbd) at 2313.…
- [Incident 20201229016439I](https://openairdocs.org/incident/20201229016439I), Dec 29, 2020: Boeing 767-338 (N362CM), Hebron, KY, Minor damage. At approximately 0645, according to testimony from [privacy data omitted] maint. Supervisor, tail # N362CM, a Boeing 767-338, s/n: 24316 began to taxi from…

## Service difficulty reports (563, newest 50)

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

- [SDR IXXA20261008092](https://openairdocs.org/sdr/IXXA20261008092), Oct 8, 2026: SWITCH. INOPERATIVE. AT APPROX 100-400 FT, RT OIL FILTER EICAS MSG APPEARED. QRH PROCEDURES WERE FOLLOWED. BEFORE RT ENG SHUTDOWN, ALL ENG PARAMETERS NORMAL. WAITED 2 MINS AT IDLE &
- [SDR ABXA20260930442](https://openairdocs.org/sdr/ABXA20260930442), Sep 30, 2026: BLEED VALVE. DEFECTIVE. DURING TAXI, R BLD ISLN VAL EICAS MESSAGE. R ISLN VAL DISCRETE LIGHT. CREW RETURNED TO THE GATE (BTB). MTX TROUBLE SHOT AND REMOVED AND REPLACED RH BLEED ISOLAT
- [SDR IXXA20260812001](https://openairdocs.org/sdr/IXXA20260812001), Aug 12, 2026: LONGERON SPLICE. CORRODED. LEFT OVERWING LONGERON IS CORRODED BETWEEN BS 930 - 940.
- [SDR IXXA20260811001](https://openairdocs.org/sdr/IXXA20260811001), Aug 11, 2026: FRAME. GOUGED. PANEL 573BB AFT FRAME IS SEVERELY GOUGED
- [SDR IXXA20260811002](https://openairdocs.org/sdr/IXXA20260811002), Aug 11, 2026: DUCT. CRACKED. INBD CORE COWL EXHAUST DUCT IS CHAFED ON THE LEADING EDGE
- [SDR ABXA20260811358](https://openairdocs.org/sdr/ABXA20260811358), Aug 11, 2026: CONTROL BOX. DISLODGED. AT FL340, LT ENGINE N1 DROP DOWN TO IDLE, NO INDICATION OF OTHER ABNORMAL. CREW DECLARED AN EMERGENCY AND DIVERTED BACK TO CVG. AFTER TROUBLESHOOTING MTX FOUND 
- [SDR ABXA20260806350](https://openairdocs.org/sdr/ABXA20260806350), Aug 6, 2026: BLEED VALVE. DEFECTIVE. L ISLN VALVE LIGHT ON START, L N2 INADEQUATE FOR ENGINE START. A/C RETURNED TO THE GATE (BTB). MTC REMOVED AND REPLACED LEFT ISLN VALVE OPS CHECKS NORMAL IAW B7
- [SDR IXXA20260806001](https://openairdocs.org/sdr/IXXA20260806001), Aug 6, 2026: SKIN. CORRODED. CORROSION ON SKIN AT BS 955 WHERE THE PICKLE FORK COMES IN CONTACT BELOW THE FLOOR.
- [SDR IXXA20260803001](https://openairdocs.org/sdr/IXXA20260803001), Aug 3, 2026: STIFFENER. CHAFED. #1 PYLON HYDRAULIC BAY LOWER RIBS ARE CHAFFED FROM HYDRAULIC SUPPLY HOSE.
- [SDR IXXA20260731002](https://openairdocs.org/sdr/IXXA20260731002), Jul 31, 2026: BRACKET. CRACKED. WHILE REMOVING MDCD FWD LWR CORNER SEAL DEPRESSOR, FOUND MOUNTING CHANNEL/BRACKET TO BE CRACKED.
- [SDR ABXA20260525226](https://openairdocs.org/sdr/ABXA20260525226), May 25, 2026: THERMOCOUPLE. DEFECTIVE. AFTER ENG STARTS AND TAXI OUT, NOTICED LEFT ENGINE EGT INOP. NOTE: EGT LEFT ENGINE 72C RH 369C. CREW RETURNED TO THE GATE (BTB). MTC REMOVED AND REPLACED THERMO
- [SDR IXXA20260506040](https://openairdocs.org/sdr/IXXA20260506040), May 6, 2026: THRUST REVERSER. NOISE. AT AROUND 80KTS WITH REVERSER DEPLOYED HAD ONE LOUD BANG FROM LEFT ENGINE WITH A FLAME. NO ABNORMAL ENGINE INDICATIONS NOTED. LANDED WITHOUT INCIDENT. ACCOMPLIS
- [SDR IXXA20260411032](https://openairdocs.org/sdr/IXXA20260411032), Apr 11, 2026: COMPRESSOR. STALLED. POSSIBLE LEFT ENGINE COMPRESSOR STALL AT FL390. AIRCRAFT ARRIVED WITHOUT INCIDENT AND HAS BEEN GROUNDED FOR INSPECTION AND MAINTENANCE. ACCOMPLISHED UNUSUAL CON
- [SDR IXX2026F00008](https://openairdocs.org/sdr/IXX2026F00008), Apr 10, 2026: BLOCK. CRACKED. R/H ECS BAY EXHAUST PHENOLIC BLOCK IS BROKEN.
- [SDR IXXA20260420001](https://openairdocs.org/sdr/IXXA20260420001), Mar 31, 2026: CLAMP. CORRODED. HYDRAULIC BLOCK CLAMP AT RMLG GEAR DOOR CUTOUT LOWER INTERNAL SPACER AND SUPPORT BRACKET CORRODING.
- [SDR ABXA20260325131](https://openairdocs.org/sdr/ABXA20260325131), Mar 25, 2026: FUEL LINE. RUPTURED. RIGHT ENG FAILED DURING CLIMB HAD ROTATION - UNABLE TO RESTART. CREW COMPLETED AN IN FLIGHT SHUTDOWN (IFS), DECLARED AN EMERGENCY (EDC) AND DID AN AIR TURN BACK
- [SDR ABXA20260203047](https://openairdocs.org/sdr/ABXA20260203047), Feb 3, 2026: CIRCUIT CARD. DEFECTIVE. DURING TAXI, IDLE DISAGREE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED OLD, THEN INSTALLED NEW EEC DISCRETE CARD PER AMM 73-21-11. OPS CHECKED GOOD,
- [SDR ABXA20260124027](https://openairdocs.org/sdr/ABXA20260124027), Jan 24, 2026: PRESSURE SWITCH. MALFUNCTIONED. AFTER STARTING ENGINES DURING TAXI R OIL FILTER MSG CAME UP A/C RETURNED TO THE GATE AND MTX GROUNDED A/C . MTX REPLACED R ENG SCAVENGE FILTER ELEMENT AND DIFFE
- [SDR IXXA20251201002](https://openairdocs.org/sdr/IXXA20251201002), Dec 1, 2025: INTERCOSTAL. CORRODED. INTERCOSTAL AT STA 566-588 RBL25 HAS CORROSION AROUND FWD FASTENERS
- [SDR IXXA20251119001](https://openairdocs.org/sdr/IXXA20251119001), Nov 15, 2025: SUPPORT CHANNEL. CORRODED. LEFT WING LOWER PANEL CHANNEL SUPPORT CORRODED AROUND MULTIPLE NUTPLATES AT WBL 97.5 STA 955 TO STA 999 (REFERENCE STREAMER TAG (22582) (SWISHER)
- [SDR ABXA20251015272](https://openairdocs.org/sdr/ABXA20251015272), Oct 15, 2025: ENGINE. SMOKE. SMELL OF FUMES. SMOKE IN CKPT 5 MILES OUT. LANDED, TOWER SAW SMOKE OUT OF #2 ENG ON TAXI. FIRE MASTER CAUTION CAME ON. SHUT #2 ENG DOWN, FIRE MASTER CAUTION WEN
- [SDR IXXA20250918001](https://openairdocs.org/sdr/IXXA20250918001), Sep 8, 2025: BAFFLE. PUNCTURED. FUEL TANK BAFFLE PANEL 134DZ WAS PUNCTURED ON THE HONEYCOMB FACE. REPAIR WAS ACCOMPLISHED PER FVCI EO#25168-6 REV. 1R B767-300 SRM 51-70-10-2R-2.
- [SDR IXXA20250915001](https://openairdocs.org/sdr/IXXA20250915001), Sep 5, 2025: LINK. GOUGED. FWD LOWER LOBE CARGO DOOR FWD UPPER ACTUATOR ARM ON FWD SIDE HAS SEVERAL GOUGES.
- [SDR IXXA20250909004](https://openairdocs.org/sdr/IXXA20250909004), Aug 21, 2025: BRACKET. CRACKED. #6 SLAT, INSIDE LOWER CLIP HAS CRACKED BRACKET 42" FROM OB EDGE
- [SDR IXXA20250909005](https://openairdocs.org/sdr/IXXA20250909005), Aug 21, 2025: BRACKET. CRACKED. #6 SLAT, INSIDE LOWER CLIP HAS CRACKED BRACKET 52" FROM OB EDGE
- [SDR IXXA20250909006](https://openairdocs.org/sdr/IXXA20250909006), Aug 21, 2025: BRACKET. CRACKED. #6 SLAT, INSIDE LOWER CLIP HAS CRACKED BRACKET 63" FROM OB EDGE
- [SDR IXXA20250909008](https://openairdocs.org/sdr/IXXA20250909008), Aug 20, 2025: WEB. CRACKED. #1 PYLON FAIRING, 437DB BULKHEAD WEB IS CRACKED
- [SDR IXXA20250908002](https://openairdocs.org/sdr/IXXA20250908002), Aug 19, 2025: SKIN. CRACKED. RIGHT WING LEADING EDGE SKIN CRACKED AT OSS 570
- [SDR IXXA20250923001](https://openairdocs.org/sdr/IXXA20250923001), Aug 17, 2025: LATCH. BENT. #2 ENGINE, INBOARD THRUST REVERSER, LOWER END, FWD LATCH BOX HAS CHAFE MARK AND BENT.
- [SDR IXX2025F00020](https://openairdocs.org/sdr/IXX2025F00020), Aug 16, 2025: SHEAR TIE. CRACKED. #2 PYLON, UNDER DOOR 447BR FWD SIDE BELOW FITTING, SHEAR TIE IS CRACKED
- [SDR IXXA20250909001](https://openairdocs.org/sdr/IXXA20250909001), Aug 16, 2025: SUPPORT ANGLE. CRACKED. #2 PYLON,DOOR 447BR CUTOUT, AFT SIDE SUPPORT ANGLE IS CRACKED
- [SDR IXX2025F00022](https://openairdocs.org/sdr/IXX2025F00022), Aug 16, 2025: SUPPORT ANGLE. CRACKED. #2 PYLON,DOOR 447BR CUTOUT, AFT SIDE SUPPORT ANGLE IS CRACKED
- [SDR IXXA20250909002](https://openairdocs.org/sdr/IXXA20250909002), Aug 16, 2025: CHANNEL. CRACKED. #2 PYLON,AFT FAIRING SUPPORT BULKHEAD ATTACH ANGLE IS CRACKED O/B
- [SDR IXXA20250909003](https://openairdocs.org/sdr/IXXA20250909003), Aug 16, 2025: ATTACH ANGLE. CRACKED. #2 PYLON, AFT FAIRING SUPPORT BULKHEAD ATTACH ANGLE IS CRACKED I/B
- [SDR IXXA20250908003](https://openairdocs.org/sdr/IXXA20250908003), Aug 13, 2025: BRACKET. CRACKED. #1 ENGINE PYLON, OUTBD SIDE, HYDRAULIC BAY ACCESS PANEL 437BL CUT OUT, LOWER EDGE, AFT BULB SEAL RETAINER ATTACH BRACKET CRACKED
- [SDR IXXA20250909007](https://openairdocs.org/sdr/IXXA20250909007), Aug 12, 2025: CHANNEL. CRACKED. NO. 1 PYLON FAIRING 437DB, OUTBOARD CHANNEL ON BULKHEAD IS CRACKED
- [SDR IXXA2025080117038](https://openairdocs.org/sdr/IXXA2025080117038), Aug 7, 2025: ENGINE. FAULTED. UPON LANDING HEARD A LOUD BANG AND FLASH OF LIGHT BOTH FROM THE LEFT SIDE OF AIRCRAFT. NO OTHER IRREGULAR ITEMS NOTED. ACCOMPLISHED EXTERIOR INSPECTION WITH NO 
- [SDR CNMA2025090001](https://openairdocs.org/sdr/CNMA2025090001), Jul 16, 2025: CASE. CORRODED. DURING C CHECK, CORROSION WAS FOUND ON THE NR 2 ENGINE FWD AND AFT CASE AROUND THE EXTERIOR AND INTERIOR SKIN. IT WAS FOUND TO BE OUT OF REPAIRABLE LIMITS FOR T
- [SDR IXXA20250809010](https://openairdocs.org/sdr/IXXA20250809010), Jul 9, 2025: LIMITER. GOUGED. #1 ENGINE, INBD T/R, FWD DEFLECTION LIMITER IS GOUGED
- [SDR IXXA20250509021](https://openairdocs.org/sdr/IXXA20250509021), May 8, 2025: ENGINE. FAULTED. ENROUTE FROM KBWI TO KSBD, CREW REPORTED LT ENG FILTER EICAS MESSAGE. CREW ELECTED A LT ENG SHUTDOWN FOLLOWED BY A DIVERSION WITH AN EMERGENCY DECLARATION TO KD
- [SDR ABXA20250430087](https://openairdocs.org/sdr/ABXA20250430087), Apr 30, 2025: ENGINE. POWER LOSS. ABORTED TAKEOFF (ATO) SLIGHTLY UNDER 80 KTS. RT ENGINE MADE TO POWER, HOWEVER, LT ENGINE ONLY MADE IT TO 88% N1. AIRCRAFT RETURNED TO BLOCKS. (BTB). RAN ENGINES
- [SDR PCSA20250416001](https://openairdocs.org/sdr/PCSA20250416001), Apr 16, 2025: TURBINE. DAMAGED. LEFT ENGINE FAILURE DURING FLIGHT. AFTER INSPECTION FOUND HOT SECTION DAMAGE.
- [SDR NACA2025032800002](https://openairdocs.org/sdr/NACA2025032800002), Mar 28, 2025: COOLING DUCT. CRACKED. #2 ENG MANIFOLD COOLING DUCT CRACK AT 7 AND 12 OCLOCK POSIITION. REPLACED 2 EA LPT COOLING AIR MANIFOLD
- [SDR 2025F00076](https://openairdocs.org/sdr/2025F00076), Mar 24, 2025: ENGINE. FIRE. ENGINE FIRE DURING FLIGHT AT 2500 FT CLIMB.
- [SDR NACA2025032100003](https://openairdocs.org/sdr/NACA2025032100003), Mar 21, 2025: START VALVE. FAILED. #1 ENG START FAIL #1 ENG STARTER. REPLACED #1 ENG START VALVE.
- [SDR NACA2025031300007](https://openairdocs.org/sdr/NACA2025031300007), Mar 13, 2025: HOUSING. LEAKING. FUEL LEAK #1 ENGINE ACCESSORY GEARBOX FORWARD MID LOWER MAIN FUEL CONTROL HOUSING. LEAK CHECK, NO LEAK FOUND.
- [SDR NACA2025031100010](https://openairdocs.org/sdr/NACA2025031100010), Mar 11, 2025: WIRE HARNESS. DAMAGED. RH EGT UPPER WIRE BUNDLE DAMAGED IN SEVERAL AREAS. REPLACED RH UPPER EGT CABLES
- [SDR NACA2025031100011](https://openairdocs.org/sdr/NACA2025031100011), Mar 11, 2025: WIRE HARNESS. DAMAGED. RH ENG LOWER EGT WIRE BUNDLE DAMAGED IN SEVERAL AREAS. REPLACED RH EGT LOWER WIRE CABLES.
- [SDR NACA2025031100012](https://openairdocs.org/sdr/NACA2025031100012), Mar 11, 2025: MANIFOLD. CRACKED. RIGHT ENGINE LPD MANIFOLD COOLING SKIN CRACK LEFT SIDE. REPLACED THE #10 LPT COOLING AIR MANIFOLD
- [SDR NACA2025031000005](https://openairdocs.org/sdr/NACA2025031000005), Mar 10, 2025: PRESSURE SWITCH. NO TEST. FOUND FUEL PRESSURE SWITCH TEST FAIL AT ENGINE 2.

All 563: https://openairdocs.org/engine/ge-cf6-80c2b6/reports.md

## STCs that may be installed (OpenAirDocs) (6)

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 SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc
- [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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