# GE CF6-80C2B7F

- Type: Engine model (FAA registry)
- Registry code: 30114
- Manufacturer (registry): GE
- Model: CF6-80C2B7F
- 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: 10 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-80c2b7f

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 2023-20-08](https://openairdocs.org/ad/2023-20-08): Engine (Turbine/Turboprop) · General Electric CF6-80C2B1F, CF6-80C2B2F, CF6-80C2B4F and 4 more. Effective Oct 19, 2023
- [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 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 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 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 2000-03-04](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 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 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

## 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 (10)

- [N1013A](https://openairdocs.org/aircraft/N1013A): [Andromeda Leasing I LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20I%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1999, S/N 30110
- [N1049A](https://openairdocs.org/aircraft/N1049A): [Andromeda Leasing II LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20II%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1999, S/N 30109
- [N1093A](https://openairdocs.org/aircraft/N1093A): [Andromeda Leasing II LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20II%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1999, S/N 30111
- [N1399A](https://openairdocs.org/aircraft/N1399A): [Andromeda Leasing I LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20I%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1996, S/N 27959
- [N1487A](https://openairdocs.org/aircraft/N1487A): [Andromeda Leasing I LLC](https://openairdocs.org/faa-owner/ANDROMEDA%20LEASING%20I%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1997, S/N 28865
- [N423AX](https://openairdocs.org/aircraft/N423AX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1996, S/N 27569
- [N468AX](https://openairdocs.org/aircraft/N468AX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 2002, S/N 30115
- [N486AX](https://openairdocs.org/aircraft/N486AX): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 2002, S/N 30843
- [N645GT](https://openairdocs.org/aircraft/N645GT): [Atlas Air Inc](https://openairdocs.org/faa-owner/ATLAS%20AIR%20INC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1995, S/N 27393
- [N767CJ](https://openairdocs.org/aircraft/N767CJ): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1996, S/N 28270

## 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 DCA20WA140](https://openairdocs.org/ntsb/DCA20WA140), Aug 28, 2020: Boeing 767 (N423AX), Bucure?ti, Romania, 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 20200828021529A](https://openairdocs.org/incident/20200828021529A), Aug 28, 2020: Boeing 767-324 (N423AX), Bucharest, Substantial damage. After main gear touchdown, the left main landing gear failed causing the left wing to drop to the runway. The left engine contacted runway and subsequently the…
- [Incident 20180326010259I](https://openairdocs.org/incident/20180326010259I), Mar 26, 2018: Boeing 767-304 (N284DH), El Paso, TX, Minor damage. On March 26,2018,at 2320 MDT, a Boeing 767-304, N284DH, regestered to wells fargo bank northwest na trustee, departed El Paso (elp), TX and the landing gear…

## Service difficulty reports (405, newest 50)

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

- [SDR ABXA20261019473](https://openairdocs.org/sdr/ABXA20261019473), Oct 19, 2026: ENGINE. VIBRATION. IN THE CLIMB OUT RIGHT ENGINE VIB INCREASE TO 3.8 AT LEVEL OFF AT FL380 DECREASED BACK TO .6 A/ RETURNED TO FIELD (ATB) AND LANDED MTX GROUNDED A/C AND PERFORME
- [SDR DALA2026100605524](https://openairdocs.org/sdr/DALA2026100605524), Sep 29, 2026: CASE. DAMAGED. ATB DUE TO RIGHT ENGINE OVERHEAT MESSAGE. CREW REDUCED THROTTLE TO EXTINGUISH MESSAGE AND DECLARED EMERGENCY. FOUND DAMAGE ON COMPRESSOR CASE. REPLACED ENGINE. 
- [SDR DALA2026092805376](https://openairdocs.org/sdr/DALA2026092805376), Sep 23, 2026: ENGINE. MAKING METAL. ATB DUE TO RIGHT ENGINE HIGH VIBRATION ON TAKE OFF AND CLIMB. ON ARRIVAL FOUND METAL IN THE TAIL. REPLACED RIGHT ENGINE.(9523648)(AIRCRAFT GROUNDED)
- [SDR ABXA20260731342](https://openairdocs.org/sdr/ABXA20260731342), Jul 31, 2026: ANTI-ICE VALVE. MALFUNCTIONED. LEFT ENG ANTI-ICE VALVE ON TAXI. C/W NNC 3.3 CANNOT TAKEOFF REQUIRES HIGH THRUST CYCLED ENG ANTI ICE AND EICAS/ VALVE LIGHT DISAPPEARED CALLED DISPATCH & MAINTE
- [SDR CALA2026071717847](https://openairdocs.org/sdr/CALA2026071717847), Jul 17, 2026: SPINNER. MISSING. PDA 1 PDA 1 ON ARRIVAL FOR #2 ENG SPINNER CONE DEPARTED PIECE IS TRAPEZOIDAL MEASURING 13 INCHES ON THE TRAILING EDGE 8 INCHES ON THE LEADING EDGE AND 11 INCHES
- [SDR CALA2026071617812](https://openairdocs.org/sdr/CALA2026071617812), Jul 11, 2026: ENGINE. VIBRATION. RIGHT ENGINE MODERATE VIBRATION. FAN VIB AT 5+ ACRID SMELL IN CO CKPIT FL340.
- [SDR CALA2026051116162](https://openairdocs.org/sdr/CALA2026051116162), May 7, 2026: ENGINE. VIBRATION. FAN VIBRATION 4.1 AT CLB THRST TO FL270. AT CRUISE VIB IS 1.0. NO AIR FRM VIB FELT. OIL TEMP AND PRESS PER CREW DEBRIEF: ALL OTHER ENGINE INDICATIONS WERE NORMA
- [SDR CALA2026050415931](https://openairdocs.org/sdr/CALA2026050415931), May 1, 2026: SLEEVE. DAMAGED. DURING WALKAROUND FOUND #2 ENG INB THRUST REVERSER SLEEVE LINER DAMAGED 11 O CLOCK POSITION.AREA OF TRIM OUT 1FT X 2FT AT 11 O'CLOCK POSITON. ACCOMPLISHED INTER
- [SDR IPXA2026050222041](https://openairdocs.org/sdr/IPXA2026050222041), Apr 22, 2026: RING. CRACKED. FOUND ENG-1 RT THRUST REVERSER CASCADE SUPPORT RING CRACK AT 9 O'CLOCK. REFERENCED TASK T3F18E008RMGN INSTALLED THE T/R, FAN COWL AND ACCOMPLISHED THE INSTALLAT
- [SDR CALA2026041715440](https://openairdocs.org/sdr/CALA2026041715440), Apr 15, 2026: SENSOR. FAULTED. RIGHT ENG ANALOG N2 STATUS MSG DISPLAYED DEBRIEFED CREW. CREW STATED AFTER TAKE OFF INTO CRUISE THEY NOTICED RIGHT ENG BLEED LIGHT OFF LIGHT ILLUMINATED. QRH WA
- [SDR DALA2026020500834](https://openairdocs.org/sdr/DALA2026020500834), Feb 2, 2026: FUEL FILTER. CONTAMINATED. FLIGHT RETURNED TO JFK DUE TO RIGHT ENGINE FUEL FILTER MESSAGE. FOUND RIGHT ENGINE FUEL FILTER CONTAMINATED. REPLACED FUEL FILTER AFTER HIGH POWER RUN, CHECKED 
- [SDR ABXA20260115012](https://openairdocs.org/sdr/ABXA20260115012), Jan 15, 2026: CONTROLLER. DEFECTIVE. DURING TAXIT OUT, EICAS MSG LT ENG CONTROL APPEARED AFTER TWO ENGINE STARTS. AIRCRAFT RETURNED TO BLOCKS. (BTB). REMOVED AND REPLACED LEFT ENG EEC IAW B767 AMM 
- [SDR CALA2025101009905](https://openairdocs.org/sdr/CALA2025101009905), Oct 8, 2025: PRESSURE SWITCH. FAULTED. R ENG FUEL FILT MSG AFTER LEVEL OFF... ALL OTHER ENG INDICATION NORMAL REF FIM 73-11 FAULT TREE 803 T/SHOOTING, R/H FUEL FILTER REPLACED AS PER AMM 73-11-02 NIL
- [SDR CALA2025082208056](https://openairdocs.org/sdr/CALA2025082208056), Aug 15, 2025: CONTROL UNIT. FAULTED. RTO DUE TO LEFT ENG SURGE AND STALLDEBRIEF FROM CREW PUSHING THROTTLES UP TO 70% N1 LH ENG SLOW TO ACCELERATE. ENGAGED AUTO THROTTLE AND ENGINE SPOOLED UP AND T
- [SDR DALA2025081306041](https://openairdocs.org/sdr/DALA2025081306041), Aug 11, 2025: ENGINE. FIRE. ATB- -IFSD- LEFT ENGINE FIRE ON TAKEOFF, PERFORMED ENGINE IFSD. FOUND SEVERE DAMAGE TO THRUST REVERES AND CORE COWLS. REPLACED LEFT ENGINE.
- [SDR DALA2025072305534](https://openairdocs.org/sdr/DALA2025072305534), Jul 18, 2025: ENGINE. FIRE. SHIP 1812 - ATB- -IFSD- LEFT ENGINE FIRE ON TAKEOFF, PERFORMED ENGINE IFSD. CORRECTIVE ACTION: FOUND SEVERE DAMAGE TO THRUST REVERES AND CORE COWLS. ENGINE CHAN
- [SDR IPXA202507074238](https://openairdocs.org/sdr/IPXA202507074238), Jul 5, 2025: LINK. WORN. WORN OUT SUPPORT LINK, NO.2 ENG R/H HPT CASE COOLING FWD DUCT UPPER SIDE, NEAR FUEL SUPPLY LINE. (REPLACE) OK TO WORK
- [SDR IPXA2025070762480](https://openairdocs.org/sdr/IPXA2025070762480), Jul 4, 2025: MANIFOLD. BROKEN. BROKEN - MANIFOLD, NO.2 ENG LPT CASE COOLING, NEAR 11:00 AREA. I.A.W. AMM 75-24-03-004-050-H00 AND 75-24-03-404-037-H00, REV.145, REPLACED THE LPT COOLING MANIF
- [SDR DALA2025070805172](https://openairdocs.org/sdr/DALA2025070805172), Jul 1, 2025: HPC. DAMAGED. SHIP 1806- DIV - DIVERTED TO AMS DUE TO LEFT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE, FOUND MULTIPLE 1ST STAGE HPC BLADES CURLED AND SHI
- [SDR CALA2025062305790](https://openairdocs.org/sdr/CALA2025062305790), Jun 20, 2025: PRESSURE SWITCH. FAULTED. R ENG FUEL FILTER CAUTIO N AND STATUS MESSAGE INSPECTED FUEL FILTER WITH NO DEBRIS FOUND, REPLACED ENG 2 FUEL FILTER AND FUEL PRESS SWITCH REF AMM 73-11-02-404-
- [SDR IXXA2025061301](https://openairdocs.org/sdr/IXXA2025061301), Jun 13, 2025: DOOR. ERODED. #2 ENG IB TR INSIDE LIP ON THE IDG DOOR HAS CHAFFING WEAR ON LANDING
- [SDR CALA2025060205177](https://openairdocs.org/sdr/CALA2025060205177), May 31, 2025: PRESSURE SWITCH. FAULTED. INTERMITTENT RIGHT ENGINE FUEL FILTER BYPASS. REMOVED, INSPECTED AND REPLACED RIGHT ENGINE FUEL FILTER REF AMM 73-11-02. INSPECTION OF FILTER SHOWED CLEAN NO DE
- [SDR CALA2025050204417](https://openairdocs.org/sdr/CALA2025050204417), Apr 30, 2025: BLEED VALVE. FAULTED. L ENG OVERHEAT ON CLIMBOUT WITH ASSOCIATED BLEED OFF AND PACK OF F. COULD NOT RECOVER PERFORMED FIM 26-11 FAULT TREE 807. SEE L/P 4678470 FOR REPLACEMENT OF # 1
- [SDR CALA2025043004350](https://openairdocs.org/sdr/CALA2025043004350), Apr 27, 2025: PRESSURE SWITCH. FAULTED. DEBRIEFED CREW, NO OVWT LANDING, 32K FEET, FUEL FILTER BYPASS R MSG, ENG APPEARED AND SHOWED NORMAL, ALL INDICATIONS NORMAL. 2 HRS OUT. ADVISORY TO STATUS. 304-
- [SDR CALA2025042504220](https://openairdocs.org/sdr/CALA2025042504220), Apr 24, 2025: BLEED VALVE. FAILED. R ENG BLEED FAIL AT 75 KTS ON TAKEOFF... CHECKLIST RAN AND RESET WITH NO DEMAND HPSOV REPLACED AS PER AMM TASK 36-11-07-424-014-003 REV 144, SATIS.
- [SDR UIEA2025012100100](https://openairdocs.org/sdr/UIEA2025012100100), Jan 22, 2025: FRAME. CORRODED. ENG 1, FAN FRAME, BTWN 4-8 O'CLOCK SURFACE WITH SEVERAL POINTS OF CORROSION.(<P>ENG 1, FLOWPATH EXTENSION BETWEEN 4 TO 8 O'CLOCK WERE REPLACED IAW AMM 72-33-00-
- [SDR CALA2025011701944](https://openairdocs.org/sdr/CALA2025011701944), Jan 16, 2025: WIRE HARNESS. BROKEN. ENG 2 EGT FLUX DRAMATICA LLY JUST AFTER TO POWER SET. NO OVERTE MP INDICAT ED. OTHER ENG PARAM S DEBRIEFED FLIGHT CREW ALL OTHER INDICATIONS WERE NORMAL EGT WAS
- [SDR ABXA2025011207](https://openairdocs.org/sdr/ABXA2025011207), Jan 12, 2025: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI RH BLEED OFF AFTER START . AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX RAN RH ENGINE AND RESET RT BLEED AIR IAW AMM 71-00-00 OPS CHECK GOOD 
- [SDR ABXA20241223270](https://openairdocs.org/sdr/ABXA20241223270), Dec 23, 2024: SHUTOFF VALVE. MALFUNCTIONED. DURING TAXI OUT , RH ENGINE BLEED VALVE OFF REGARDLESS OF THE POSITION AFTER STARTING ENGINE. AC RETURNED TO GATE(BTB) AND MTX GROUNDED AC , TROUBLE SHOT AND RE
- [SDR IPXA2024121872254](https://openairdocs.org/sdr/IPXA2024121872254), Dec 12, 2024: INLET. CRACKED. *SUPPLEMENTAL SDR* R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED AND REPLACED R/H INLE
- [SDR ABXA20241126235](https://openairdocs.org/sdr/ABXA20241126235), Nov 26, 2024: ANTI-ICE VALVE. FAULTED. DURING TAXI WITH BOTH ENGINES RUNNING AND ENGINE ANTI-ICE SELECTED ON WE OBSERVED THE RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED AND A RIGHT ENGINE ANTI-ICE 
- [SDR DALA2024112211156](https://openairdocs.org/sdr/DALA2024112211156), Nov 21, 2024: HPC. LEAKING. SHIP 1819 -ATB- AIR TURN BACK TO JFK DUE TO DIRTY SOCK SMELL IN CABIN. RAN ENGINE AND FOUND ODOR TO BE COMING FROM RIGHT ENGINE. PERFORMED BORESCOPE INSPECTION 
- [SDR IPXA2024101886334](https://openairdocs.org/sdr/IPXA2024101886334), Oct 17, 2024: FAN. VIBRATION. **ATB**DURING CLIMB LFT ENG FAN VIB IND 4.1 AIRFRAME VIB ALSO NOTED ACCOMPLISHED INSPECTION OF L/H ENG IAW 77.00.00.206.001.H00 NO DAMAGED FOUND. ACCOMPLISHED F
- [SDR CALA2024102102692](https://openairdocs.org/sdr/CALA2024102102692), Oct 17, 2024: BLEED VALVE. FAULTED. L ENG BLEED OFF EICAS W/ ASSOC L ENG BLEED LIGHT OCCURED MULTIP LE TIMES IN FLT. THEY NOTICED THIS FLUCTUATION AT LEAST 6 TIMES. UPON DEBRIEFING FLT CREW MAINT 
- [SDR DALA2024100909868](https://openairdocs.org/sdr/DALA2024100909868), Oct 9, 2024: SHIM. DAMAGED. SHIP 1817 -DIV- CREW REPORTED #2-ENGINE HIGH N1 VIBES IN FLIGHT. CORRECTIVE ACTION: FOUND #32 FAN BLADE SHIM DAMAGED. REPLACED SHIM AND LUBED FAN BLADES. ALL CH
- [SDR IPXA2024093054655](https://openairdocs.org/sdr/IPXA2024093054655), Sep 28, 2024: ENGINE. LEAKING. ON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROME
- [SDR IPXA2024100454655](https://openairdocs.org/sdr/IPXA2024100454655), Sep 28, 2024: ENGINE. LEAKING. ON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROME
- [SDR DALA2024082608451](https://openairdocs.org/sdr/DALA2024082608451), Aug 25, 2024: BLADES. OUT OF LIMITS. DIV - ON CLIMB OUT NOTED HIGH N1 VIBES ON RIGHT ENGINE DIVERSION TO CDG. ENGINE HAD PREVIOUS BIRD STRIKE IN NCE WHICH RESULTED IN SPINNER AND FAN BLADE DAMAGE. 
- [SDR DALA2024072007303](https://openairdocs.org/sdr/DALA2024072007303), Jul 20, 2024: ENGINE. BIRD INGESTION. SHIP 1811 - ATB/IFSD - AIR TURNBACK DUE TO LEFT ENGINE BIRD STRIKE THAT CAUSED AN ENGINE FAILURE. CORRECTIVE ACTION: REPLACED ENGINE. REPLACED RIGHT MAIN GEAR U
- [SDR DALA2024070706832](https://openairdocs.org/sdr/DALA2024070706832), Jul 3, 2024: BLADES. DAMAGED. SHIP 1812 - ATO - ABORTED TAKEOFF AT 150KTS DUE TO AN AIRCRAFT YAW AND SUDDEN ENGINE EGT EXCEEDANCE. LEFT ENGINE FOUND TO HAVE DAMAGE TO TURBINE BLADES. CORRECT
- [SDR IPXA2024032667475](https://openairdocs.org/sdr/IPXA2024032667475), Mar 26, 2024: UNKNOWN. LEAKING. FUEL LEAKING FROM LEFT ENGINE ACCOMPLISHED LEFT ENGINE RUN AT IDLE (CREW RAN IT) AS PER B767 71-00-00 TEST NO.3 IDLE LEAK CHECK AND CHECKED DRAINS PER B767 AMM 
- [SDR DALA2024032603758](https://openairdocs.org/sdr/DALA2024032603758), Mar 24, 2024: CARBON SEAL. LEAKING. SHIP 1813 -DIV- DUE TO RIGHT ENGINE OIL QUANTITY LOSS, ALL OTHER ENGINE INDICATIONS NORMAL. CREW AND DISPATCH CHOSE TO DIVERT TO DTW. CORRECTIVE ACTION: FOUND T
- [SDR UIEA2022102201169](https://openairdocs.org/sdr/UIEA2022102201169), Oct 24, 2022: NONE. NONE. THREE DENTS ON ENGINE #2 PRIMARY EXHAUST OUTER SKIN BETWEEN 6/8 O´CLOCK AND BETWEEN NAC STA 323.42/344.67(<P>WELD FILL REPAIR IAW BOEING MSG: CMA-TLS-22-0022-0
- [SDR UIEA2022070700739](https://openairdocs.org/sdr/UIEA2022070700739), Jul 7, 2022: NONE. NONE. #2 ENG EXHAUST CASE ( CORE COWL ) RUB PADS HAS SEVERAL LOOSE/WORN PADS(<P><SPAN>REMOVED AND REPLACED LOOSE&NBSP; OR&NBSP; WORN OUT&NBSP; RUB PADS&NBSP; AT # 2 E
- [SDR UIEA2022070700735](https://openairdocs.org/sdr/UIEA2022070700735), Jul 7, 2022: TAPE. NONE. MAIN DECK CARGO DOOR FORWARD AND AFT DOOR FRAME HAS LOOSE AND WORN TAPE.(<P><SPAN>REMOVED&NBSP; AND&NBSP; REPLACED&NBSP; LOOSE&NBSP; AND&NBSP; WORN&NBSP; TAPE&N
- [SDR KCSA2022042308](https://openairdocs.org/sdr/KCSA2022042308), Apr 23, 2022: ENGINE. STALLED. RIGHT ENGINE COMPRESSOR STALL, FOLLOWED BY EXHAUST GAS TEMPERATURE INCREASE, RIGHT ENGINE UNRESPONSIVE. RIGHT ENGINE LEFT AT IDLE FOR REMAINDER OF FLIGHT, EMERG
- [SDR KCSA2022041505](https://openairdocs.org/sdr/KCSA2022041505), Apr 15, 2022: NONE. NONE. DECLARED EMERGENCY FOR LEFT ENGINE FUEL FILTER ENGINE INDICATING AND CREW ALERTING SYSTEM MESSAGE
- [SDR UIEA2022041000282](https://openairdocs.org/sdr/UIEA2022041000282), Apr 12, 2022: FIRE LOOP. DAMAGED. ENG #1 WIRING OF FIRE LOOP LOWER DAMAGED LOCATED AT 6 O'CLOCK FWD OF PRESSURE SWITCH REPAIRED #1 ENG FIRE LOOP WIRED DETECTOR TS683 PER W/D 26-11-11 ; SWPM 20-1
- [SDR P5CA2022012400017](https://openairdocs.org/sdr/P5CA2022012400017), Jan 25, 2022: LEAD. NONE. ENGINE #2 LOWER IGNITION LEAD IS DAMAGED(<P>REMOVED &AMP; REPLACED ENG #2 LOWER IGNITION LEAD PER AMM&NBSP; 74-21-00. OPS CHECK GOOD</P>)
- [SDR P5CA2022012400011](https://openairdocs.org/sdr/P5CA2022012400011), Jan 25, 2022: NONE. NONE. RIGHT ENGINE THRUST REVERSER INOP REF. MDDR # 159690.(<P>REACTIVATED RH ENGINE T/R PER AMM 78-31-01. OPS CHECK GOOD. NO DEFECTS NOTED. THIS ITEM CLEARS MDDR&NBS

All 405: https://openairdocs.org/engine/ge-cf6-80c2b7f/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. 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 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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