# GE CF6-6D

- Type: Engine model (FAA registry)
- Registry code: 30076
- Manufacturer (registry): GE
- Model: CF6-6D
- Engine type: Turbo-fan
- Power: 39,300 lb thrust
- Data sheet: [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Holder: General Electric Company
- Installed in: 2 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-6d

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 2003-10-01](https://openairdocs.org/ad/2003-10-01): High pressure turbine rotor (HPTR) rear shafts · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 17, 2003
- [AD 2002-05-03](https://openairdocs.org/ad/2002-05-03): Life-Limited Rotating Parts · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Apr 12, 2002
- [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 98-18-10](https://openairdocs.org/ad/98-18-10): Low Pressure Turbine Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 30, 1998
- [AD 94-09-18](https://openairdocs.org/ad/94-09-18): High Pressure Turbine Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Jun 6, 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 91-24-01](https://openairdocs.org/ad/91-24-01): Compressor Rear Frame Casing · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective May 26, 1992
- [AD 91-15-03](https://openairdocs.org/ad/91-15-03): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Aug 5, 1991
- [AD 91-12-09](https://openairdocs.org/ad/91-12-09): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 27, 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 90-19-08](https://openairdocs.org/ad/90-19-08): Low Pressure Turbine Rotor Stage One Disk · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Oct 15, 1990
- [AD 89-20-01 R1](https://openairdocs.org/ad/89-20-01-R1): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Dec 12, 1989
- [AD 88-12-01](https://openairdocs.org/ad/88-12-01): High Pressure Compressor Rear Shafts · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 6, 1988
- [AD 81-19-08](https://openairdocs.org/ad/81-19-08): Low Pressure Turbine Rotor Stage 2 Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 21, 1981
- [AD 80-03-06](https://openairdocs.org/ad/80-03-06): Stage 2 HPT Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Feb 8, 1980
- [AD 78-07-03](https://openairdocs.org/ad/78-07-03): Compressor Spool · General Electric CF6-6D and CF6-6D1. Effective May 22, 1978
- [AD 76-21-04](https://openairdocs.org/ad/76-21-04): High Pressure Compressor · General Electric CF6-6D and CF6-6D1. Effective Nov 30, 1977
- [AD 76-05-10](https://openairdocs.org/ad/76-05-10): Turbofan Engines · General Electric CF6-50A, CF6-50C, CF6-50E and 3 more. Effective Mar 24, 1976
- [AD 75-22-11](https://openairdocs.org/ad/75-22-11): High Pressure Turbine Thermal Shield · General Electric CF6-6D and CF6-6D1. Effective Oct 28, 1975
- [AD 74-14-08](https://openairdocs.org/ad/74-14-08): Turbine Blades · General Electric CF6-6D and CF6-6D1. Effective Jul 12, 1974
- [AD 72-16-03](https://openairdocs.org/ad/72-16-03): Turbine Discs · General Electric CF6-6D and CF6-6D1. Effective Aug 8, 1972

Historical (superseded or no longer in force):

- [AD 99-08-18](https://openairdocs.org/ad/99-08-18) (historical): General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective May 13, 1999
- [AD 95-18-14](https://openairdocs.org/ad/95-18-14) (historical): High Pressure Compressor Rotor · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 21, 1995

## Registered aircraft (2)

- [N367FE](https://openairdocs.org/aircraft/N367FE): [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1971, S/N 46605
- [N369FE](https://openairdocs.org/aircraft/N369FE): [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), built 1972, S/N 46607

## NTSB investigations (6)

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 DCA08FA075](https://openairdocs.org/ntsb/DCA08FA075), Jun 14, 2008: Douglas MD-10 (N554FE), Raymond, PA, substantial damage. Probable cause: The flight crew's failure to adequately monitor the airplane's airspeed during the holding pattern, leading to the onset of an aerodynamic stall and subsequent structural damage to the tail from…
- [NTSB CHI99IA100](https://openairdocs.org/ntsb/CHI99IA100), Mar 2, 1999: McDonnell Douglas DC-10 (N40061), Salina, KS, incident, no damage. Probable cause: The ARTCC personnel failed to maintain radio communications with both airplanes and failed to maintain IFR separation standards. Factors relating to the incident were the FAA does not require cargo…
- [NTSB MIA98LA124](https://openairdocs.org/ntsb/MIA98LA124), Apr 4, 1998: Douglas DC-10-10F (N68053), Memphis, TN, substantial damage. Probable cause: The tug operator's (maintenance representative) inadequate visual lookout during pushback.
- [NTSB LAX90FA148](https://openairdocs.org/ntsb/LAX90FA148), Apr 18, 1990: McDonnell Douglas DC-10-10F (N68056), Los Angeles, CA, substantial damage. Probable cause: PILOT FAILED TO ADHERE TO ESTABLISHED LANDING PROCEDURES, MAINTAIN A STABILIZED APPROACH, AND ALLOWED THE AIRSPEED TO GO BELOW THE PREDICTED V.
- [NTSB DEN83FA021](https://openairdocs.org/ntsb/DEN83FA021), Nov 19, 1982: Mcdonald Douglas DC-10 (N68056), Denver, CO, substantial damage
- [NTSB ANC78IA036](https://openairdocs.org/ntsb/ANC78IA036), May 9, 1978: Douglas DC-10 (N68054), Anchorage, AK, incident, minor damage

## FAA accident and incident reports (20)

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 20080614839519A](https://openairdocs.org/incident/20080614839519A), Jun 14, 2008: Doug MD1010F (N554FE), Elmira, NY, Substantial damage. (-23) While holding on J-106 at hoxie intersection the flightcrew allowed the aircraft airspeed to detiorate to the point that they could no longer maintain…
- [Incident 20050727025569I](https://openairdocs.org/incident/20050727025569I), Jul 27, 2005: Doug DC1010 (N397FE), Newark, NJ, Substantial damage. (-23) Crew reported no. one engine fire, after hearing a loud bang. Engine was shut down and one fire bottle discharged that extinguished the fire. The fire…
- [Incident 20050603012339I](https://openairdocs.org/incident/20050603012339I), Jun 3, 2005: Doug DC1010F (N68053), Kansas City, MO. (-23) See attached for flight engineer information. Facts given by the director of operations: aircraft was in cruise flight at FL350 and all indications were…
- [Incident 20011113034209I](https://openairdocs.org/incident/20011113034209I), Nov 13, 2001: Doug DC1010F (N68059), Newark, NJ, Minor damage. (-23) Report from mem aod powerplant engineering senior engineer larry andrews attached. [privacy data omitted]
- [Incident 19980909032699I](https://openairdocs.org/incident/19980909032699I), Sep 9, 1998: Doug DC1010 (N397FE), Indianapolis, IN. While on final approach for runway 5R, the outboard vane stop assemble for the right side inboard flap fell off of the aircraft. The stop assemble struck a…
- [Accident 19980404005999A](https://openairdocs.org/incident/19980404005999A), Apr 4, 1998: Doug DC1010F (N68053), Memphis, TN, Substantial damage. Collided with nose dock on pushback from gate. Tug driver cut it around too soon. (.4)the tug operator (maintenance representative) was pushing back an…
- [Accident 19900418010239A](https://openairdocs.org/incident/19900418010239A), Apr 18, 1990: Doug DC1010F (N68056), Los Angeles, CA, Substantial damage. Excessive pitch up on landing flare causing tail strike.
- [Incident 19860323014249I](https://openairdocs.org/incident/19860323014249I), Mar 23, 1986: Doug DC1010F (N68051), Houston, TX, Minor damage. While taxiing into a gate not normally used by DC10 engine inlet struck at tug.
- [Incident 19820205002059I](https://openairdocs.org/incident/19820205002059I), Feb 5, 1982: Doug DC1010F (N68051), Chicago, IL. Aborted takeoff due to a differential in takeoff power. Replaced a malfunctioning EGT indicator.
- [Incident 19801006082419I](https://openairdocs.org/incident/19801006082419I), Oct 6, 1980: Doug DC1010F (N68056), Houston, TX. Hydraulic quantity dropped to one gallon en route. Replaced isolation valve and one hydraulic pump.
- [Incident 19800924070799I](https://openairdocs.org/incident/19800924070799I), Sep 24, 1980: Doug DC1010F (N68052), Denver, CO, Substantial damage. Takeoff aborted after loud bang. Found engine turbine section failed.
- [Incident 19800308024329I](https://openairdocs.org/incident/19800308024329I), Mar 8, 1980: Doug DC1010F (N68051), Chicago, IL. Engine shutdown in flight due to vibration.
- [Incident 19790915049249I](https://openairdocs.org/incident/19790915049249I), Sep 15, 1979: Doug DC1010F (N68051), Chicago, IL. Turn back due to loud noise, rise in EGT and engine shut down. Hole burned through 7th stage case.
- [Incident 19790222200169I](https://openairdocs.org/incident/19790222200169I), Feb 22, 1979: Doug DC10/ (N68052), Houston, TX. Main landing gear wheel & tire departed aircraft on takeoff. Uneventful landing at destination.
- [Incident 19781105023449I](https://openairdocs.org/incident/19781105023449I), Nov 5, 1978: Doug DC10/ (N68052), Austin, TX. Engine shutdown due to RPM sticking. Replaced jammed throttle cable.
- [Incident 19780826039089I](https://openairdocs.org/incident/19780826039089I), Aug 26, 1978: Doug DC1010F (N68052), San Antonio, TX. Phone call to reservations stated bomb onboard flight. Returned for search.
- [Incident 19780601041459I](https://openairdocs.org/incident/19780601041459I), Jun 1, 1978: Doug DC10/ (N68053), Denver, CO. Complete instrument failure after failure of a generator drive end bearing failure. Landed safely.
- [Incident 19780510032939I](https://openairdocs.org/incident/19780510032939I), May 10, 1978: Doug DC10/ (N68052), Dallas, TX. Engine shutdown, flight diverted. Found compressor dragging, changed the engine.
- [Incident 19780509032769I](https://openairdocs.org/incident/19780509032769I), May 9, 1978: Doug DC10/ (N68054), Anchorage, AK, Minor damage. Aircraft taxiing to gate truck improperly adjusted jetway.
- [Incident 19780128004359I](https://openairdocs.org/incident/19780128004359I), Jan 28, 1978: Doug DC1010 (N68051), Seattle, WA, Minor damage. Loud bang after slat extension. Disagreement lights. Inspection revealed damage from over extension.

## Service difficulty reports (1,051, newest 50)

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

- [SDR UIEA2026010300003](https://openairdocs.org/sdr/UIEA2026010300003), Jan 3, 2026: PLUG. LEAKING. DIVERSION ENGINE 3 OIL QUANTITY LOSS. INSPECTED #3 ENG AND FOUND OIL LEAKING FROM #3 IDG. DEACTIVATION BLANKING PLATE, REMOVED BLANKING PLATE AND FOUND DRIVE SE
- [SDR KRDY2025061714786](https://openairdocs.org/sdr/KRDY2025061714786), Jun 13, 2025: ENGINE. FIRE. N476MC FLT 5Y 8208 AFTER T/O ENGINE # 1 WAS FIRE, SO CREW TAKE THE DECISION TO DIVERT TO GYE. PLS SEE ALSO MSR-14785.
- [SDR KRDY2025061714785](https://openairdocs.org/sdr/KRDY2025061714785), Jun 12, 2025: ENGINE. FIRE. ACFT N476MC FLT 5Y8208 B747C DEPARTED FROM UIO, AFTER DEPART ENG #1 WAS FIRED SO CREW TOOK THE DECISION TO DIVERT TO GYE. ACFT LAND ON GYE, TOWED TO POSITION 13
- [SDR IXXA20241002002](https://openairdocs.org/sdr/IXXA20241002002), Aug 23, 2024: RETAINER. GOUGED. #1 ENGINE OB TR UPPER BIFURCATION FWD SEAL RETAINER CHANNEL IS WORN. HAECO WO 320008 NON ROUTINE 40293
- [SDR NACA2023013020001](https://openairdocs.org/sdr/NACA2023013020001), Jan 26, 2023: SHUTOFF VALVE. FAILED. ENG BLEED OFF LIGHT DOESNT ILLUMINATE WITH ENGINE NOT RUNNING. REMOVED LH ENG PRSOV PER M2, INSTALLED LH PRSOV PER AMM 36-11-09 OPS CHECKS AND LEAK CHECKS GOOD.
- [SDR MK1Y01292021003](https://openairdocs.org/sdr/MK1Y01292021003), Jan 29, 2021: COWLING. UNKNOWN. UNDOCUMENTED REPAIR DOUBLERS FOUND AT LT ENGINE ON OUTBOARD CORE COWL OUTER SKIN.
- [SDR FDEA202010102523](https://openairdocs.org/sdr/FDEA202010102523), Oct 10, 2020: DOOR FRAME. GOUGED. NR 2 ENGINE LT SIDE, APPROXIMATELY STA YTN 133, 6 O`CLOCK POSITION, GOUGED METAL ON FWD LT FAN COWL LAND. MARKED DOT NR 45. REMOVED GOUGED DOOR JAM & REPLACED W
- [SDR FDEA2020040630686](https://openairdocs.org/sdr/FDEA2020040630686), Apr 3, 2020: ENGINE. UNKNOWN. CLIMBING THRU FL340 WITH ENGINES ALL AT CLIMB POWER WE FELT A BUMP LIKE MINOR TURBULENCE. THEN ANOTHER AND ANOTHER. WE SAW ENG 2 N1 FLUCTUATING SO WE SUSPECTED 
- [SDR FDEA201905291179](https://openairdocs.org/sdr/FDEA201905291179), May 29, 2019: ENGINE. FAILED. PDIS 560 72-57 4731 29MAY19 CLT OPEN U LOGPAGES:3089200 ENGINE 2 FIRE WARNING ON DEPT FROM CLT FACT 15JUN19 18:57 CLT R & R`D #2 ENGINE PER W/C 71T1701 SYSTEM C
- [SDR FDEA201902286504](https://openairdocs.org/sdr/FDEA201902286504), Feb 26, 2019: WIRE HARNESS. DAMAGED. NR 3 ENGINE HAS HAD A SHIFT IN EGT TRENDS WITH ALL OTHER PARAMETERS STABLE. THIS NORMALLY INDICATES AN IMPENDING EGT INDICATION SYSTEM FAILURE. TESTED NR 3 ENG 
- [SDR FDEA201811163266](https://openairdocs.org/sdr/FDEA201811163266), Nov 16, 2018: LEAD. DEFECTIVE. AS AUTO THROTTLES WENT TO CLIMB TRUST, NR 1 EGT WENT TO 1018' WITH "ENG 1 EXCEEDANCE" ALERT. C/W MTSI, R&R ALL NR 1 EGT THERMOCOUPLE PROBES AND FWD AND AFT LEAD
- [SDR FDEA2018102653006](https://openairdocs.org/sdr/FDEA2018102653006), Oct 25, 2018: ENGINE. FIRE. MDIS 566 78-10 5297 24OCT18 MEM OPEN U ENG 2 TAIL PIPE FIRE DURING START. INSTRUCTED FLT CREW TO USE ENG FIRE PROCEDURES. BOTH BOTTLES DISCHARGED. PER FLT CREW 
- [SDR FDEA201805221271](https://openairdocs.org/sdr/FDEA201805221271), May 22, 2018: HEAT EXCHANGER. FAILED. DURING CLIMBOUT, THE NR 2 ENGINE OIL TEMP PEAKED AT 184 DEGREES IN THE RED BAND AND ALSO RECEIVED A LEVEL 2 ALERT FOR NR 2 ENG OIL TEMP HIGH. SHUTDOWN THE NR 2 
- [SDR FDEA201710243035](https://openairdocs.org/sdr/FDEA201710243035), Oct 24, 2017: PUMP. MALFUNCTIONED. NR 2 ENGINE WOULD NOT ACHIEVE CLIMB POWER. THE THROTTLE WAS FIRE WALLED DURING CLIMB, ALL INDICATIONS CONSISTANTLY LESS THAN 1 & 3. REMOVED AND REPLACED THE NR 
- [SDR FDEA201708052122](https://openairdocs.org/sdr/FDEA201708052122), Aug 5, 2017: WIRE HARNESS. DAMAGED. DURING CLIMBOUT, NOTICED THE NR 2 ENGINE EXCEEDENCE LEVEL 1 ALERT. EGT GAUGE FOR NR 2 SHOWED MAX 998. NORMAL EGT AT REDUCED POWER FOR LEVEL FLIGHT AT 7000 FT. O
- [SDR FDEA201704041065](https://openairdocs.org/sdr/FDEA201704041065), Apr 4, 2017: COMPRESSOR. STALLED. AT FLT LEVEL 370, HEARD A LOUD BANG AND NOTICED THE NR 2 ENGINE STALLED & N1 DECREASED TO 30%. DESCENDED TO FL 310 & RAN QRH FOR ENGINE COMPRESSOR STALL & WAS A
- [SDR FDEA201702210606](https://openairdocs.org/sdr/FDEA201702210606), Feb 21, 2017: FUEL CONTROL. FAILED. AFTER SHUTTING DOWN THE NR 1 ENGINE FOR A FUNCTIONAL CHECK. FUEL FLOW EGT AND N2 PROGRESSED NORMAL DURING START, BUT THE N1 WOULD NOT ADVANCE PAST 28%. ADVANCIN
- [SDR UIEA2017021600195](https://openairdocs.org/sdr/UIEA2017021600195), Feb 15, 2017: RECEPTACLE. DAMAGED. FOUND THE NR 1 ENGINE FUEL TRANSMITTER RECEPTACLE AND CONNECTOR DAMAGED. IAW SWPM 20-60-06 REV.63 AND WDM 73-33-11 REV.41 REPLACED THE TRANSMITTER RECEPTACLE AN
- [SDR FDEA201701310285](https://openairdocs.org/sdr/FDEA201701310285), Jan 31, 2017: THROTTLE CABLE. INOPERATIVE. AT TOP OF DESCENT , NR 2 THROTTLE WAS STUCK AT 85% N1. SHUT DOWN NR 2 ENGINE AT 10.000. NORMAL LANDING, WAS ABLE TO MOVE NR 2 THROTTLE TO IDLE DURING TAXI TO CH
- [SDR AALA20161215022](https://openairdocs.org/sdr/AALA20161215022), Dec 14, 2016: FUEL CONTROL. FAULTY. LEFT ENGINE WOULD NOT SHUT DOWN WITH FUEL CONTROL IN OFF POSITION. CYCLED SWITCH AND ENGINE SHUT DOWN. ENGINE VALVE LIGHT REMAINED ON. AIRCRAFT WAS GROUNDED. RE
- [SDR FDEA201610153643](https://openairdocs.org/sdr/FDEA201610153643), Oct 15, 2016: ENGINE. FAILED. LEVEL FLIGHT, HEARD BOOM NOISE, FELT MOMENTARY HEAVY RUMBLE, AND YAW TO THE RIGHT. NR 3 ENGINE FAILED. COMPLIED WITH QRH. DURING DESCENT, N1-21 EGT-30 N2-10.5 F
- [SDR FDEA201607162482](https://openairdocs.org/sdr/FDEA201607162482), Jul 16, 2016: ENGINE. FAILED. UPON ADVANCING POWER FOR TAKEOFF, FELT A RUMBLING IN THE RUDDER PEDALS. ABORTED T/O AT AT 10 KTS. TURNED OFF RUNWAY, ANOTHER ACFT ADVISED SEEING FLAMES FROM THE
- [SDR FDEA201603230995](https://openairdocs.org/sdr/FDEA201603230995), Mar 23, 2016: MEC. INOPERATIVE. ON APPROACH, NR 1 THROTTLE WOULD NOT GO BELOW 65% N, AT THE IDLE STOP F FLOW 2350 RAN THE ENG. SHUTDOWN IN FLIGHT CHECK LIST. R&R THE ENGINE NR 1 MEC PER AMM 73
- [SDR AALA20160219014](https://openairdocs.org/sdr/AALA20160219014), Feb 19, 2016: CONTROLLER. FAILED. AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, RT ENG HPSOV, EICAS MSG DISPLAYED & BLEED LIGHT R
- [SDR FDEA201601160166](https://openairdocs.org/sdr/FDEA201601160166), Jan 16, 2016: NOSE COWL. CRACKED. NUMBER 3 ENG INLET NOSE COWL APPROX 6:00 POSITION HAS HORIZONTAL CRACK UNDER BOLTS. R & R NR 3 ENG NOSE COWL IAW MM 71-11-00-2.
- [SDR FDEA201601100105](https://openairdocs.org/sdr/FDEA201601100105), Jan 10, 2016: ENGINE. BIRD INGESTION. MULTIPLE FAN BLADES DAMAGED ON NR 3 ENG DUE TO BIRD STRIKE. DURING BORESCOPE OF NR 3 ENG FOR BIRD STRIKE, FOUND LARGE TEAR ON LE 10TH STAGE THROUGH PORT B1-10. 
- [SDR FDEA201601090091](https://openairdocs.org/sdr/FDEA201601090091), Jan 9, 2016: ANTI-ICE VALVE. FAILED. NR 1 ENG ANTI-ICE DISAGREE DURING CLIMB WITH ENG ANTI-ICE SELECTED ON. R & R ANTI-ICE VALVE IAW AMM 30-22-02-0-0. OPS CHECKED NORMAL, OK FOR SERVICE.
- [SDR FDEA201601050044](https://openairdocs.org/sdr/FDEA201601050044), Jan 5, 2016: ATTACH BOLT. LOOSE. NUMBER 3 ENG LT THRUST REVERSER, UPPER LATCH ATTACH BOLTS LOOSE, 5 EACH. TORQUED UPPER LATCH ATTACH BOLTS IAW AMM 78-32-11-2.
- [SDR FDEA201601050045](https://openairdocs.org/sdr/FDEA201601050045), Jan 5, 2016: BOLT. LOOSE. NUMBER 3 ENG LT THRUST REVERSER, MOUNTING RING LATCH ASSEMBLY HAS 16 LOOSE BOLTS. QUALITY CONTROL REQUESTS, TORQUE CHECK, ON ALL MOUNTING RING ATTACHMENT FASTEN
- [SDR FDEA201510163252](https://openairdocs.org/sdr/FDEA201510163252), Oct 16, 2015: CABLE. DAMAGED. REJECTED TAKEOFF DUE TO NR 3 ENGINE NOT SPOOLING UP TO TAKEOFF POWER. REJECT SPEED LESS THAN 80 KIAS NR 1 & 2 APPROX 103% N1, NR 3 STOPPED ACCELERATING AT APPRO
- [SDR FDEA201510143211](https://openairdocs.org/sdr/FDEA201510143211), Oct 14, 2015: ENGINE. FAULTY. DURING CLIMB OUT PASSING FL 260, NR 3 N1 WENT TOWARD ZERO WHILE ACFT EXPERIENCED MODERATE VIBRATION. MOVED THROTTLE TO IDLE EGT & N2 APPEARED NORMAL & WERE SIMI
- [SDR UIEA2015101300577](https://openairdocs.org/sdr/UIEA2015101300577), Oct 12, 2015: FUEL FILTER. FAULTY. INFLIGHT DIVERT DUE TO QRH 7.16, REF TO LP 733225 01 & LP 733226 4. NR 1 & NR 4 FUEL FILTER WERE REPLACED, FUEL LEAK CHECKED SATISFACTORY. ENG 1 & 4 GND IDLE RU
- [SDR UIEA2015101300576](https://openairdocs.org/sdr/UIEA2015101300576), Oct 12, 2015: FUEL FILTER. FAULTY. ENG 4 FUEL FILT IN CRUISE, SELF-CLEAR WITHIN 10 - 15 SECONDS STATUS MSG. ENG 4 FUEL FILT NR 4 ENG FUEL FILTER ELEMENT REPLACED. FUEL LEAK CHECKED CUT OUT & SATI
- [SDR FDEA201508062490](https://openairdocs.org/sdr/FDEA201508062490), Aug 6, 2015: UNKNOWN. MALFUNCTIONED. LEVEL 2 ENG 1 OIL FILTER ALERT DURING CLIMB PASSING FL 200. ALL OIL PRESS & TEMP INDICATIONS WERE NORMAL, NO VIBRATION. REDUCED THROTTLE TO IDLE. LEVEL 2 ALERT 
- [SDR FDEA201503040646](https://openairdocs.org/sdr/FDEA201503040646), Mar 4, 2015: WIRE HARNESS. DAMAGED. IN FLIGHT GOT EGT 2 HI 997 DEG ENG 2 EXCEEDANCE. PULLED TO IDLE TEMP DROPPED BELOW LIMITS ON LEVEL OFF WITH THROTTLE AT IDLE. TEMP EXCEEDED LIMITS AGAIN. SHUTDO
- [SDR FDEA201411233868](https://openairdocs.org/sdr/FDEA201411233868), Nov 23, 2014: COWLING. WORN. NUMBER 3 ENG LT FAN COWL AFT EDGE AT 10:00 HAS BEEN DAMAGED, WORN THROUGH TO HONEYCOMB. DAMAGE APPEARS TO HAVE BEEN CAUSED BY RIDING CONDITION WITH STRUCTURE. R
- [SDR FDEA201410083007](https://openairdocs.org/sdr/FDEA201410083007), Oct 8, 2014: SEAT TRACK. WORN. MAIN DECK FLOORS STATION 1741 LBL 47 TWO EACH SEAT TRACK WORN. REMOVED AREA OF DAMAGED SEAT TRACK IAW SRM 53-70-00 VOL 1.
- [SDR FDEA201410052972](https://openairdocs.org/sdr/FDEA201410052972), Oct 5, 2014: FRAME. CHAFED. NUMBER 2 ENG LT CORE COWL 2ND FRAME FROM AFT HAS CHAFE MARK. REPAIR ACCOMPLISHED IAW EA 8-7113-T0312063 REV NO PS P1. TITLE POWER PLANT COWL NR 2 END LT PYLON C
- [SDR FDEA201409092547](https://openairdocs.org/sdr/FDEA201409092547), Sep 9, 2014: DUCT. CRACKED. NR 2 NOSE COWL INLET DUCT, CRACKED THROUGHOUT CIRCUMFERENCE. R & R WITH NEW NOSE COWL ASSEMBLY IAW AMM 54-22-01-2.
- [SDR FDEA201407051633](https://openairdocs.org/sdr/FDEA201407051633), Jul 5, 2014: WIRE. DAMAGED. DURING CLIMB OUT AT 11,000 FT THE NR 1 ENG EGT WAS AMBER, XED OUT THEN CAME BACK ON & EXCEEDED THE EGT LIMIT ABOVE 965 DEGREES C. THE EGT RETURNED TO NORMAL AFT
- [SDR FDEA201406151464](https://openairdocs.org/sdr/FDEA201406151464), Jun 15, 2014: POWER SUPPLY. NO TEST. EMERGENCY LIGHT BATTERY 1 LOW ILLUMINATED DURING TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01-4
- [SDR FDEA201406141452](https://openairdocs.org/sdr/FDEA201406141452), Jun 14, 2014: SKIN. CRACKED. WHILE PERFORMING FCD, FOUND A CRACK ON NR 1 INBD SLAT TRACK SKIN CUT OUT LT WING. VERIFIED CRACK USING HFEC IAW NDTSPM 06-10-01. CRACK 1/2 INCH IN LENGTH. REMOV
- [SDR FDEA201406141448](https://openairdocs.org/sdr/FDEA201406141448), Jun 14, 2014: SKIN. CRACKED. FOUND A CRACK ON RT WING SKIN AT NR 3 SLAT TRACK BETWEEN NR 1 & 2 SLATS. TRIMMED OUT DAMAGED AREA. PERFORMED INTERNAL & EXTERNAL VISUAL INSPECTION WITH NO ADDIT
- [SDR FDEA201406141450](https://openairdocs.org/sdr/FDEA201406141450), Jun 14, 2014: SKIN. CRACKED. DURING POST FLIGHT, FOUND A CRACK ON THE LT WING LE AT NR 4 SLAT, OTBD TRACK CUT OUT, LOWER, INBD RADIUS. HFEC INSPECTED SUSPECTED IAW NDTSPM 06-10 01 & VERIFIE
- [SDR FDEA201404010605](https://openairdocs.org/sdr/FDEA201404010605), Apr 1, 2014: WIRE HARNESS. DAMAGED. DURING DEPARTURE, NR 1 ENGINE EXCEEDED EGT 932 DEGREES WITH MOMENTARY SPIKE IN N1, RETARDED NR 1 THROTTLE, N1 STEADY AT 93 & EGT 700 - 750 AT FL310. FOUND ENG 1
- [SDR FDEA201403200538](https://openairdocs.org/sdr/FDEA201403200538), Mar 20, 2014: WIRE HARNESS. DAMAGED. RTO AT 110KTS FOR, ENG 3 EXCEEDANCE, LVL 1 ALERT. NR 3 EGT SHOWED YELLOW, 1011, FOR EXCEEDANCE, ESTIMATE EXCEEDANCE WAS MOMENTARY. PULLED UP VIA NR 3 ENG EXCEED
- [SDR FDEA201403190532](https://openairdocs.org/sdr/FDEA201403190532), Mar 19, 2014: SHUTOFF VALVE. FAILED. DURING CLIMB, RECEIVED ECAM WARNING NR 2 THRUST REVERSER PRESSURIZED. ECAM LASTED FOR SEVERAL SECONDS THEN WENT OUT, REAPPEARED. THROTTLE WAS BROUGHT TO IDLE IA
- [SDR FDEA201403190535](https://openairdocs.org/sdr/FDEA201403190535), Mar 19, 2014: SHUTOFF VALVE. INOPERATIVE. ABORTED TAKEOFF DUE TO NR 2 ENG MASTER CAUTION. NR 2 ENGINE THRUST REVERSER LIGHT 60KTS AS STANDARD POWER COMING UP. R & R PRSOV IAW MM 78-31-05-04, OPS CHECKED
- [SDR FDEA201403020430](https://openairdocs.org/sdr/FDEA201403020430), Mar 2, 2014: PUSH-PULL CABLE. MALFUNCTIONED. ON TOP OF DESCENT NR 2 THROTTLE FROZE AT 92% N1 FROM FL 370 TO 10,000 FT NO MOVEMENT, SHUTDOWN ENG. CREW REPORTED THAT AFTER ARRIVAL AT GATE & SHUTDOWN NR 2 THR
- [SDR FDEA201402140315](https://openairdocs.org/sdr/FDEA201402140315), Feb 14, 2014: WIRE. DAMAGED. NR 2 ENGINE EGT 1018 DEGREES DURING CLIMB OUT. EGT STAYED HIGH AT REDUCED POWER SETTING. EGT HIGH ALERT, SHUTDOWN ENGINE. DUMPED 8500 LBS FUEL PRIOR TO LANDING.

All 1,051: https://openairdocs.org/engine/ge-cf6-6d/reports.md

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

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA1139NW-D](https://openairdocs.org/stc/SA1139NW-D): Install fireproof blankets on Engine Fan Reverser Intermediate Fireseal in lieu of Fireproof Intumescent Coating. United Airlines Inc
- [STC SE91WE](https://openairdocs.org/stc/SE91WE): Removal of General Electric 'EGT cable and conduit assembly,' P/N9037M17P03 or 9037M17P04, and replacement with Co-Operative Industries P/N 66615. Boeing Company
- [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc
- [STC SE00461LA](https://openairdocs.org/stc/SE00461LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. Hi Temp Insulation Inc

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