# GE CF6-80A2

- Type: Engine model (FAA registry)
- Registry code: 30095
- Manufacturer (registry): GE
- Model: CF6-80A2
- Engine type: Turbo-fan
- Power: 48,670 lb thrust
- Data sheet: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 5 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-80a2

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 2018-07-05](https://openairdocs.org/ad/2018-07-05): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 11, 2018
- [AD 2011-23-04](https://openairdocs.org/ad/2011-23-04): Forward engine mount assembly side links · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Dec 12, 2011
- [AD 2009-08-06](https://openairdocs.org/ad/2009-08-06): Stage 1 high-pressure turbine (HPT) rotor  
 disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 18, 2009
- [AD 2009-07-10](https://openairdocs.org/ad/2009-07-10): High-pressure turbine rotor (HPTR) · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 6, 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 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 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 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 95-17-16](https://openairdocs.org/ad/95-17-16): Compressor Rear Frame · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Nov 7, 1995
- [AD 94-07-04](https://openairdocs.org/ad/94-07-04): High Pressure Turbine Disk · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective May 23, 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 92-04-08](https://openairdocs.org/ad/92-04-08): Stage 1 Disk/Shafts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Mar 27, 1992
- [AD 91-23-13](https://openairdocs.org/ad/91-23-13): Fan Disks · General Electric CF6-50A, CF6-50C, CF6-50C1 and 12 more. Effective Nov 22, 1991
- [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 91-01-04](https://openairdocs.org/ad/91-01-04): Fan Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 19 more. Effective Jan 22, 1991
- [AD 89-16-08](https://openairdocs.org/ad/89-16-08): Manifold · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Aug 31, 1989
- [AD 86-15-04](https://openairdocs.org/ad/86-15-04): Stage 1 High Pressure Turbine (HPT) Disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jul 23, 1986
- [AD 85-15-51](https://openairdocs.org/ad/85-15-51): Fuel Manifold Supply Tube · General Electric CF6-80A and CF6-80A2. Effective Dec 23, 1985

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 2006-12-24](https://openairdocs.org/ad/2006-12-24) (historical): Five-link forward mount assembly · General Electric CF6-45A, CF6-45A2, CF6-50A and 14 more. Effective Jul 21, 2006
- [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 2003-01-05](https://openairdocs.org/ad/2003-01-05) (historical): Dovetail slots · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 1 more. Effective Jan 28, 2003
- [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 2000-08-12](https://openairdocs.org/ad/2000-08-12) (historical): Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 10 more. Effective Oct 23, 2000
- [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000
- [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000
- [AD 99-18-19](https://openairdocs.org/ad/99-18-19) (historical): Inadvertent Thrust Reverser · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 7 more. Effective Sep 24, 1999
- [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999

## Information bulletins (advisory) (2)

- [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

## Registered aircraft (5)

- [N740AX](https://openairdocs.org/aircraft/N740AX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1983, S/N 22213
- [N744AX](https://openairdocs.org/aircraft/N744AX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1983, S/N 22221
- [N749AX](https://openairdocs.org/aircraft/N749AX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1984, S/N 22226
- [N750AX](https://openairdocs.org/aircraft/N750AX): [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 1984, S/N 22227
- [N761CX](https://openairdocs.org/aircraft/N761CX): [Cargo Aircraft Management Inc](https://openairdocs.org/faa-owner/CARGO%20AIRCRAFT%20MANAGEMENT%20INC), [Wilmington, OH](https://openairdocs.org/faa-place/OH/Wilmington), built 1985, S/N 22318

## 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 (307, newest 50)

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

- [SDR IXXA20260809001](https://openairdocs.org/sdr/IXXA20260809001), Aug 9, 2026: STRINGER. CRACKED. STRINGER 25L CRACKED AT FUSELAGE BS 676.
- [SDR ABXA20260404148](https://openairdocs.org/sdr/ABXA20260404148), Apr 4, 2026: WARNING MESSAGE. ILLUMINATED. DURING TAXI OUT, LEFT ENGINE OIL PRESS ILLUMINATED. A/C RETURNED TO GATE. (BTB) MAINTENANCE DEFERRED IAW ABX-79-33-1-1. A/C RETURNED TO SERVICE.
- [SDR ABXA20251030282](https://openairdocs.org/sdr/ABXA20251030282), Oct 30, 2025: OIL SYSTEM. LOW. DURING TAXI, RIGHT ENGINE OIL QUANTITY INDICATION INOP. A/C RETURNED TO BLOCKS (BTB). DEFERRED RT ENGINE OIL QTY. INDICATION IAW MEL 79-31-1-1. MBCB 11/02/2025.
- [SDR ABXA20250929241](https://openairdocs.org/sdr/ABXA20250929241), Sep 29, 2025: BLEED VALVE. WARNING MESSAGE. ON T/O ROLL, (R ENG BLEED VAL) CAUTION MSG APPEARED. ABORTED TAKE-OFF AT 68 KNTS AND RETURNED TO GATE (BTB) AND MTX GROUNDED A/C .MTX DEFERRED RH ENGINE BLEED I
- [SDR ABXA2025521098](https://openairdocs.org/sdr/ABXA2025521098), May 21, 2025: ACTUATOR. MALFUNCTIONED. STATUS MSG: "R HYD SYS MAINT" DISPLAYED IN CRUISE. RH HYD PRESSURE AT 1620 AT CRUISE. NOTICED RT ENGINE OIL PRESSURE INDICATED RED, AND MAINT FAULT OF RT IDG, A
- [SDR ABXA20241207244](https://openairdocs.org/sdr/ABXA20241207244), Dec 7, 2024: OIL SYSTEM. LOW. AFTER BLOCK OUT, ON ENGINE STARTS & ENGINES RUNNING 8 MINUTES (APPROX) LEFT ENGINE QUANTITY 11, RIGHT ENGINE 14, CONTACTED MAINTENANCE & TOLD TO RETURN TO GATE 
- [SDR IXXA20241107001](https://openairdocs.org/sdr/IXXA20241107001), Nov 7, 2024: PAD. CHAFED. #1 ENG OTBD T/R UPPER V BAND TAB CHAFFING IN THE FAN CASE AT THE 12:00 POSITION (
- [SDR IXXA20240915064](https://openairdocs.org/sdr/IXXA20240915064), Sep 13, 2024: ENGINE. FAULTED. WHILE CLIMBING THROUGH 31,000 FEET CREW REPORTED A LOUD BANG SUSPECT FROM RH ENGINE FOLLOWED BY A VIBRATION, RISE IN EGT AND LOSS OF ENGINE POWER. FOLLOWING ATI
- [SDR IXXA202301276013](https://openairdocs.org/sdr/IXXA202301276013), Jan 26, 2023: ENGINE. FAULTED. RIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RT ENG
- [SDR ABXA2023013016](https://openairdocs.org/sdr/ABXA2023013016), Jan 26, 2023: REGULATOR VALVE. DEFECTIVE. LEFT ENGINE BLEED OFF, 0 DUCT PRESSURE DURING TAXI. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED LEFT HPSOV IAW B767 AMM
- [SDR IXXA20230126013](https://openairdocs.org/sdr/IXXA20230126013), Jan 26, 2023: NONE. NONE. RIGHT ENGINE OIL FILTER EICAS MESSAGE DISPLAYED DURING CLIMB OUT FROM DEPARTURE STATION KRIV. PER ATI-QUICK REFERENCE HANDBOOK, CREW ELECTED TO SHUT DOWN RIGHT 
- [SDR ABXA20221222156](https://openairdocs.org/sdr/ABXA20221222156), Dec 21, 2022: ELECTRONIC UNIT. FAILED. ON TAXI OUT N1 ON RT ENG FAILED. INDICATED ZERO. STBY ALSO, ALL OTHER INDICATIONS NORMAL. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REPLAC
- [SDR ABXA20221117126](https://openairdocs.org/sdr/ABXA20221117126), Nov 16, 2022: CONTROLLER. FAILED. LT ENG BLEED OFF EICAS MSG DISPLAYED AFTER BOTH ENGINES WERE STARTED. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE R&R'D LH HIGH PRESSURE CON
- [SDR IXXA20221101143](https://openairdocs.org/sdr/IXXA20221101143), Oct 28, 2022: PUMP. DAMAGED. DESCENT THRU FL190, OIL PSI RT ENGINE DECREASING. ENG NEAR IDLE & SHUTDOWN BEFORE OIL WENT TO 0. SINGLE ENG APPR & LDG PROCEDURES COMPLIED WITH. DECLARED EMERGE
- [SDR ABXA2022091191](https://openairdocs.org/sdr/ABXA2022091191), Sep 11, 2022: MEC. FAULTED. AFTER ENGINE START, RIGHT ENGINE SURGE AND EGT NOT GOING OVER 500. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED MAIN ENG
- [SDR 2022F00265](https://openairdocs.org/sdr/2022F00265), Jun 20, 2022: NONE. NONE. DURING RT ENG START, NO N2; NO START VALVE; NO ROTATION VERIFIED ON GRIND. AIRCRAFT BTB AND GROUNDED BY MAINTENANCE. MAINTENANCE RE-SECURED CANNON PLUG ON START
- [SDR IXXA2022050301](https://openairdocs.org/sdr/IXXA2022050301), May 3, 2022: NONE. CRACKED. #1 ENGINE I/B CORE COWL UPPER LOUVER EXHAUST ON AFT FLANGE CRACKED
- [SDR IXXA2022041502](https://openairdocs.org/sdr/IXXA2022041502), Apr 15, 2022: SEAL BRACKET. CRACKED. FAN COWL SEAL RETAINER BRACKET CRACKED
- [SDR ABXA20210913091](https://openairdocs.org/sdr/ABXA20210913091), Sep 13, 2021: WARNING MESSAGE. FALSE ACTIVATION. RT. ENG FUEL VALVE EICAS MSG APPEARS DURING ENGINE START. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS CHECK OF FUEL CONDITION M
- [SDR ABXA2021830-28081](https://openairdocs.org/sdr/ABXA2021830-28081), Aug 28, 2021: CONTROLLER. FAULTY. LH ENG BLEED VALVE EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE.R&R LH HIGH PRESSURE CONTROLLER IAW AMM 36-11-08 LEAK & BITE CHECK GOOD. AI
- [SDR ABXA2021430029](https://openairdocs.org/sdr/ABXA2021430029), Apr 30, 2021: BLEED VALVE. INTERMITTENT. AFTER ENGINE START EICAS MSG "L ENG BLEED VAL" AND L DISCRETE LIGHT " BLEED" ILLUMINATED.AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORM
- [SDR ABXA20200803217](https://openairdocs.org/sdr/ABXA20200803217), Nov 19, 2020: ACTUATOR. FAILED. RT ENGINE WOULD NOT START, AIRCRAFT BACK TO BLOCK AND AIRCRAFT GROUNDED. TROUBLESHOT, PER B767 FIM 76-11-FT803 VERIFIED 28 VDC ON PIN 8, GROUND ON PIN 7. REMOVE
- [SDR ABXA20200803213](https://openairdocs.org/sdr/ABXA20200803213), Nov 13, 2020: WARNING MESSAGE. FALSE ACTIVATION. LT FUEL VALVE EICAS DURING START NO FUEL FLOW. AIRCRAFT BACK TO BLOCK AND GROUNDED. TROUBLESHOT BOTH LT ENGINE SPAR VALVE & ENGINE VALVE NO DEFECTS NOTED. PERFO
- [SDR ABXA20200803198](https://openairdocs.org/sdr/ABXA20200803198), Oct 19, 2020: WARNING MESSAGE. FALSE ACTIVATION. RT REV ISOLATION VALVE EICAS MESSAGE AFTER ENGINE START. AIRCRAFT RETURNED TO GATE, AIRCRAFT WAS GROUNDED. MAINTENANCE INVESTIGATED PROBLEM. OPERATIONAL CHECK O
- [SDR ABXA20200803181](https://openairdocs.org/sdr/ABXA20200803181), Sep 24, 2020: WARNING LIGHT. ILLUMINATED. LEFT REVERSER ISOLATION VALVE LIGHT AND EICAS MESSAGE. AIRCRAFT BACK TO BLOCK AND GROUNDED. REVERSER WAS DEFERRED AND A/C RELEASED FOR FLIGHT.
- [SDR ABXA202005153061](https://openairdocs.org/sdr/ABXA202005153061), May 13, 2020: GUIDE VANE. DAMAGED. #1 ENGINE 12 OCLOCK POSITION EXIT GUIDE VANE FAIRING DAMAGED. AIRCRAFT WAS GROUNDED.
- [SDR ABXA201912106177](https://openairdocs.org/sdr/ABXA201912106177), Nov 26, 2019: EEC. MALFUNCTIONED. THE RIGHT ENGINE DID NOT REACH CLIMB POWER AT HIGH ALTITUDE (FL260) WITH THE ELECTRONIC ENGINE CONTROL ON. THE ENGINE ONLY PRODUCED 105% WITH THE THRUST LEVER F
- [SDR HALA20181009483](https://openairdocs.org/sdr/HALA20181009483), Oct 8, 2018: SLEEVE. TORN. ETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER
- [SDR HALA2018100900483](https://openairdocs.org/sdr/HALA2018100900483), Oct 8, 2018: SLEEVE. TORN. ETOPS SIGNIFICANT SYSTEM - FOUND SEVERAL OGV SLEEVES TORN AT 4 O CLOCK POSITION ON NR 2 ENGINE. REPLACED OGV SLEEVES AT POSITIONS 33, 35, 36, 37, 38, 39, 32 PER
- [SDR DALA201806200001](https://openairdocs.org/sdr/DALA201806200001), Jun 19, 2018: MOUNT. DAMAGED. DURING ACCOMPLISHMENT OF REPAIR 3-2 PER DAL CMM 310T1020-3 ATA 71-21-11, AFTER REMOVAL OF ALL DAMAGE BEARING LUG INDEX 14 WAS FOUND TO MEASURE 0.714 INCH, WHICH
- [SDR HALA2018062000289](https://openairdocs.org/sdr/HALA2018062000289), Jun 19, 2018: MEC. MALFUNCTIONED. RIGHT ENGINE DID NOT REDUCE TO IDLE ON INITIAL DESCENT, FL370 - 11,000, CORRECTED ITSELF FOR FINAL DESCENT N1 53.0 & N2 80.9, FF 1.2. REMOVED & REPLACED THE RT 
- [SDR HALA2018062000290](https://openairdocs.org/sdr/HALA2018062000290), Jun 19, 2018: MEC. MALFUNCTIONED. IDENTICAL RT ENGINE IDLE POWER PROBLEM AS PREVIOUS FLIGHT 23 BUT WITH EEC OFF THRUST LEVER IDLE N1 42.7, N2 79.1, FF 1.3. REMOVED & REPLACED THE RT ENGINE MEC I
- [SDR HALA2018060400274](https://openairdocs.org/sdr/HALA2018060400274), Jun 3, 2018: ENGINE. MALFUNCTIONED. RIGHT ENGINE PARAMETERS HIGH DURING DECENT AND LANDING, N1 32.0 (L), N2 65.1 (L), N1 48 (R), N2 79.4 (R), > 18000. SUSPECT LEFT ENGINE WENT TO GROUND IDLE ON AP
- [SDR HALA2018060400273](https://openairdocs.org/sdr/HALA2018060400273), Jun 1, 2018: SENSOR. MALFUNCTIONED. DURING DECENT, AT IDLE POWER. THE RIGHT ENGINE INDICATION WAS 47% N1, THE LEFT ENGINE WAS 33% N1. AUTO THROTTLE OFF, RIGHT ENGINE HAD AT HIGH FLIGHT IDLE. TROUB
- [SDR HALA2018060400272](https://openairdocs.org/sdr/HALA2018060400272), May 31, 2018: ENGINE. MALFUNCTIONED. DURING DESCENT, THE RIGHT ENGINE STAYED AT 41% N1 AND LEFT AT30 % N1, EQUALIZE AT 10000 FEET. TROUBLESHOT IAW FIM 71.01 F/T 804 EEC BITE WITH NO FAULT. PERFORME
- [SDR HALA2017052200239](https://openairdocs.org/sdr/HALA2017052200239), May 21, 2018: ENGINE. POWER LOSS. LEFT THRUST LEVER REQUIRED MANUAL ADJUSTMENT TO OBTAIN TAKEOFF THRUST AT FULL FORWARD STOP. EGT, N1, FUEL FLOWS MATCHED. THREE INCH THRUST LEVER SPLIT FROM FM 1
- [SDR HALA2018051600228](https://openairdocs.org/sdr/HALA2018051600228), May 12, 2018: FILTER. CONTAMINATED. RIGHT ENGINE FUEL FILTER EICAS MESSAGE ILLUMINATED INTERMITTENTLY THROUGHOUT FLIGHT. REMAINED FOR LAST 2 HOURS OF FLIGHT. REPLACED THE FUEL FILTER, FOUND DEBRIS
- [SDR 9JLA201801269691](https://openairdocs.org/sdr/9JLA201801269691), Dec 19, 2017: FUEL CONTROL. DEFECTIVE. DURING THE LANDING PHASE, THE FLIGHT CREW REPORTED THAT THE RT ENGINE COMPUTER INDICATED A FAIL ANNUNCIATION. INVESTIGATED AND DETERMINED THAT THE RT ENGINE FUE
- [SDR PCSA2018102525](https://openairdocs.org/sdr/PCSA2018102525), Oct 25, 2017: ENGINE. VIBRATION. LEFT ENGINE SHUTDOWN IN FLIGHT DUE TO VIBRATION.
- [SDR PCSA20171024001](https://openairdocs.org/sdr/PCSA20171024001), Oct 24, 2017: CONNECTOR. CONTAMINATED. LEFT ENGINE SHUTDOWN IN FLIGHT DUE TO A VIBRATION. ACCOMPLISHED FIM 71-05 FT 814, NO METAL PARTICLES FOUND IN THE INLET OR EXHAUST AREAS, NO COMTAMINATION FOUND
- [SDR PCSA2017053101](https://openairdocs.org/sdr/PCSA2017053101), May 31, 2017: FIRE WARNING. FALSE ACTIVATION. THE LEFT ENGINE FIRE WARNING, THE ENGINE WAS SHUTDOWN IAW THE ENGINE SECURING CHECKLIST. THE FIRE WARNING EXTINGUISHED AFTER THE DISCHARGE OF THE SECOND FIRE BO
- [SDR HALA2017012600017](https://openairdocs.org/sdr/HALA2017012600017), Jan 26, 2017: BLADE. BENT. RIGHT ENGINE FAN BLADE DAMAGED, THE TIP IS BENT AND APPEARS TO BE HITTING RUB STRIP. THE RUB STRIP FOUND DAMAGED AND A BIG PIECE AT 6:00 MISSING. RT ENG FAN BLA
- [SDR HALA2017010200571](https://openairdocs.org/sdr/HALA2017010200571), Jan 2, 2017: LINER. DAMAGED. ETOPS, NR 2 ENG ABRAIDABLE LINER DAMAGED AT 6'OCLOCK POSITION. REPAIRED PER E105-594240-PERM AND AMM 72-33-04.
- [SDR ABXA20161106170](https://openairdocs.org/sdr/ABXA20161106170), Nov 6, 2016: ENGINE. POWER LOSS. ON FINAL APPROACH, THERE WAS A COMPRESSOR STALL AND LOSS OF THRUST FROM THE LEFT ENGINE. ON THE GROUND, THE EGT INCREASED TO 700 DEGREES AFTER ROLLOUT AND THE E
- [SDR ABXA20161023151](https://openairdocs.org/sdr/ABXA20161023151), Oct 23, 2016: ENGINE. MALFUNCTIONED. LEFT ENGINE LOST POWER ON FINAL APPROACH. EGT WAS 690 DEGREES CELSIUS. AFTER LANDING, ENGINE WOULD NOT PRODUCE THRUST. THE AIRPLANE WAS REMOVED FROM SERVICE AND
- [SDR HALA2016062800258](https://openairdocs.org/sdr/HALA2016062800258), Jun 28, 2016: UNKNOWN. UNKNOWN. ETOPS SIGNIFICANT SYS. ON TAKEOFF LEFT ENGINE MAX THRUST 103 PERCENT UNABLE TO INCREASE ABOVE 103 PERCENT .29 DEGREES-C AERO DATA REDUCED TARGET 104.1, MAX 107.
- [SDR IXXA2016041300099](https://openairdocs.org/sdr/IXXA2016041300099), Apr 13, 2016: HOSE. BLOWN. EICAS MESSAGE "C HYD QTY", LOSS OF ALL QTY LEADING TO C HYD FAILURE. FOUND HOSE BLOWN.
- [SDR HALA2016031200077](https://openairdocs.org/sdr/HALA2016031200077), Mar 12, 2016: PUMP. MALFUNCTIONED. LT FWD FUEL PUMP EICAS MESSAGE ACCOMPLISHED QRH, CONTINUE NORMAL OPERATION, FUEL 6 OF THE QRH. CHECKED CONNECTOR ON BOOST PUMP, NO SHORTS BETWEEN PHASES AND NO 
- [SDR PCSA2015061701](https://openairdocs.org/sdr/PCSA2015061701), Jun 15, 2015: ENGINE. POWER LOSS. TAKEOFF CANCELLED AT 70 KNOTS DUE TO POWER LOSS RT ENG. PRIOR TO POWER LOSS, ENG PARAMETERS LOOKED NORMAL.
- [SDR HALA2015040400051](https://openairdocs.org/sdr/HALA2015040400051), Apr 4, 2015: WIRE. BROKEN. EICAS MESSAGE, BLEED VALVE AND OVERHEAD PANEL LT ENGINE. BLEED LIGHT ILLUMINATED DURING CRUISE AT FLT 340, PRIOR TO ETOPS AIRSPACE ATB. REPAIRED BROKEN WIRE AT 

All 307: https://openairdocs.org/engine/ge-cf6-80a2/reports.md

## STCs that may be installed (OpenAirDocs) (3)

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

---
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.