# Service difficulty reports: GE CF6-6D

A list on [GE CF6-6D](https://openairdocs.org/engine/ge-cf6-6d.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 22 · 1,051 reports

- [SDR UIEA2026010300003](https://openairdocs.org/sdr/UIEA2026010300003.md): Plug · leaking · Jan 3, 2026 · N476MC · Boeing 74747UF · Turbine Engine Oil System
  > 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 SEAL PLUG MISSING & INSTALLED DRIVE SEAL PLUG PER MEL 24-11-01A. RAN ENG IAW AMM 71-00-00, LEAK CHECK
- [SDR KRDY2025061714786](https://openairdocs.org/sdr/KRDY2025061714786.md): Engine · fire · Jun 13, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop)
  > 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.md): Engine · fire · Jun 12, 2025 · N476MC · Boeing 74747UF · Engine (Turbine/Turboprop)
  > 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. A RIDING MECHANIC FROM ATLAS IS IN CHARGE OF THE TECHNICAL RELEASE AND WE PROVIDE MECHANIC ASSI
- [SDR IXXA20241002002](https://openairdocs.org/sdr/IXXA20241002002.md): Retainer · gouged · Aug 23, 2024 · N491AZ · Boeing 767323 · Engine Thrust Reverser
  > #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.md): Shutoff Valve · failed · Jan 26, 2023 · N321CM · Boeing 767323 · Engine Bleed Air System
  > 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. PART UNKNOWN TO TRAX.
- [SDR MK1Y01292021003](https://openairdocs.org/sdr/MK1Y01292021003.md): Cowling · unknown · Jan 29, 2021 · N394AN · Boeing 767323 · Engine Cowling System
  > UNDOCUMENTED REPAIR DOUBLERS FOUND AT LT ENGINE ON OUTBOARD CORE COWL OUTER SKIN.
- [SDR FDEA202010102523](https://openairdocs.org/sdr/FDEA202010102523.md): Door Frame · gouged · Oct 10, 2020 · N562FE · Doug MD1010F · Nacelle/Pylon, Main Frame
  > 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 WITH FABRICATED DOOR JAM, REF SRM 51-31-01, DWG AJC 7415.
- [SDR FDEA2020040630686](https://openairdocs.org/sdr/FDEA2020040630686.md): Engine · unknown · Apr 3, 2020 · N550FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 A COMPRESSOR STALL. AS WE WERE RUNNING THE QRH FOR ENG COMPRESSOR STALL WE RECEIVED LEVEL 2 ENG
- [SDR FDEA201905291179](https://openairdocs.org/sdr/FDEA201905291179.md): Engine · failed · May 29, 2019 · N560FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 CHECKS NORMAL. PER SDR REQUIREMENTS, ENGINE P/N CF6-6D, S/N 451447.
- [SDR FDEA201902286504](https://openairdocs.org/sdr/FDEA201902286504.md): Wire Harness · damaged · Feb 26, 2019 · N560FE · Doug MD1010F · Engine Indicating System Wiring
  > 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 EGT INDICATION SYSTEM PER E.O. 8-7720-E0330327. R & R LT UPPER, RT UPPER AND LT LOWER HARNES
- [SDR FDEA201811163266](https://openairdocs.org/sdr/FDEA201811163266.md): Lead · defective · Nov 16, 2018 · N550FE · Doug MD1010F · Engine EGT/TIT Indicating System
  > 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 LEADS I/R/T MM 77-21-01-2. RAN ENGINE NR 1 AND NR 3 FOR COMPARISON. ENGINE NR 1 START EGT 560, EGT 375 A
- [SDR FDEA2018102653006](https://openairdocs.org/sdr/FDEA2018102653006.md): Engine · fire · Oct 25, 2018 · N566FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 DEBRIEF NO FIRE IND IN COCKPIT, NO EGT LIMIT EXCEDED FIRE DEPT CALLED. FIRE DEPT DISCHARGED FOAM INT
- [SDR FDEA201805221271](https://openairdocs.org/sdr/FDEA201805221271.md): Heat Exchanger · failed · May 22, 2018 · N383FE · Doug MD1010F · Engine Oil Temperature
  > 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 ENGINE ALL OTHER ENGINE PARAMETERS NORMAL. NO VIBRATIONS. COMPLETED INSTALLATION OF THE NR 2
- [SDR FDEA201710243035](https://openairdocs.org/sdr/FDEA201710243035.md): Pump · malfunctioned · Oct 24, 2017 · N375FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 2 ENGINE FUEL PUMP IAW AMM 73-12-01-2. REMOVED AND REPLACED MEC IAW AMM 73-20-01-2. PREFORMED
- [SDR FDEA201708052122](https://openairdocs.org/sdr/FDEA201708052122.md): Wire Harness · damaged · Aug 5, 2017 · N394FE · Doug MD1010F · Engine Indicating System Wiring
  > 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. ON ADVANCING POWER FOR CLIMB, NR 2 EGT CLIMBED RAPIDLY. PERFORMED GVI OF THE VSV FEED BACK CABLE
- [SDR FDEA201704041065](https://openairdocs.org/sdr/FDEA201704041065.md): Compressor · stalled · Apr 4, 2017 · N383FE · Doug MD1010F · Turbine Engine Compressor Section
  > 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 ABLE TO REGAIN NORMAL ENGINE OPERATION FOR APPROXIMATELY 5 MINUTES, WHEN THE NR 2 ROLLED BACK AGAIN T
- [SDR FDEA201702210606](https://openairdocs.org/sdr/FDEA201702210606.md): Fuel Control · failed · Feb 21, 2017 · N389FE · Doug MD1010F · Fuel Control/Turbine Engines
  > 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%. ADVANCING THROTTLE DID NOT CHANGE ANY NR 1 ENGINE PARAMETERS UNTIL REACHING 10,000 FT, AT WHICH TIME THE
- [SDR UIEA2017021600195](https://openairdocs.org/sdr/UIEA2017021600195.md): Receptacle · damaged · Feb 15, 2017 · N476MC · Boeing 74747UF · Engine Fuel System Wiring
  > 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 AND CONNECTOR. IAW AMM 73-33-01-000-801 REV.88 AND AMM 73-33-01-400-801 REV.88 REPLACED FUEL PRESSURE
- [SDR FDEA201701310285](https://openairdocs.org/sdr/FDEA201701310285.md): Throttle Cable · inoperative · Jan 31, 2017 · N363FE · Doug MD1010F · Power Lever
  > 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 CHOCKS. REMOVED AND REPLACED THROTTLE CABLE.
- [SDR AALA20161215022](https://openairdocs.org/sdr/AALA20161215022.md): Fuel Control · faulty · Dec 14, 2016 · N398AN · Boeing 767323 · Fuel Control/Turbine Engines
  > 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. REMOVED AND REPLACED LEFT MAIN ENGINE CONTROL IAW WC 73-94-02 AND 71-95-20. OPERATIONAL CHECKED G
- [SDR FDEA201610153643](https://openairdocs.org/sdr/FDEA201610153643.md): Engine · failed · Oct 15, 2016 · N358FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 FF - 0 OIL PRESS - 1 OIL TEMP - 60 OIL QTS - 16. FAILED BORESCOPE, REPLACED THE ENGINE.
- [SDR FDEA201607162482](https://openairdocs.org/sdr/FDEA201607162482.md): Engine · failed · Jul 16, 2016 · N564FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 NR 2 ENGINE. SHUTDOWN ENGINE, BLEW BOTH FIRE BOTTLES. REMOVED NR 2 ENG PER WORK CARD 71T1101
- [SDR FDEA201603230995](https://openairdocs.org/sdr/FDEA201603230995.md): Mec · inoperative · Mar 23, 2016 · N383FE · Doug MD1010F · Fuel Control/Turbine Engines
  > 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 73-20-01-2 AND ADJUSTMENT AND TEST PER EO 8-7320-7-5000 C. RAN ENGINE PER JRH CHPT 7.7. ENGINE LEA
- [SDR AALA20160219014](https://openairdocs.org/sdr/AALA20160219014.md): Controller · failed · Feb 19, 2016 · N398AN · Boeing 767323 · Pneumatic Distribution System
  > AIRCRAFT WAS NOT GNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, RT ENG HPSOV, EICAS MSG DISPLAYED & BLEED LIGHT REMAINED ILLUMINATED. ACCOMPLISHED PNEUMATIC SYS HEALTH CHECK IAW AMM 36-00-21 WITH RT HIGH PRESSU
- [SDR FDEA201601160166](https://openairdocs.org/sdr/FDEA201601160166.md): Nose Cowl · cracked · Jan 16, 2016 · N560FE · Doug MD1010F · Engine Cowling System
  > 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.md): Engine · bird ingestion · Jan 10, 2016 · N554FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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. REPLACED NR 3 ENG.
- [SDR FDEA201601090091](https://openairdocs.org/sdr/FDEA201601090091.md): Anti-Ice Valve · failed · Jan 9, 2016 · N10060 · Doug MD1010F · Engine Anti-Icing System
  > 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.md): Attach Bolt · loose · Jan 5, 2016 · N560FE · Doug MD1010F · Engine Thrust Reverser
  > 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.md): Bolt · loose · Jan 5, 2016 · N560FE · Doug MD1010F · Engine Thrust Reverser
  > NUMBER 3 ENG LT THRUST REVERSER, MOUNTING RING LATCH ASSEMBLY HAS 16 LOOSE BOLTS. QUALITY CONTROL REQUESTS, TORQUE CHECK, ON ALL MOUNTING RING ATTACHMENT FASTENERS. TIGHTENED AND TORQUE CHECKED ALL BOLTS ON MOUNTING RING LATCH ASSY IAW AMM 78-32-11-2.
- [SDR FDEA201510163252](https://openairdocs.org/sdr/FDEA201510163252.md): Cable · damaged · Oct 16, 2015 · N68053 · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 APPROX 96 % N1 WHERE THROTTLE POSITION HAD NO FURTHER EFFECT. TROUBLESHOT IAW FIM 71-00-00-2 FIM AND I
- [SDR FDEA201510143211](https://openairdocs.org/sdr/FDEA201510143211.md): Engine · faulty · Oct 14, 2015 · N567FE · Doug MD1010F · Engine (Turbine/Turboprop)
  > 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 SIMILAR TO 1 & 2 ENG, WHEN NR 3 THROTTLE WAS ADVANCED FROM IDLE, MODERATE VIBRATIONS WERE FELT. RAN
- [SDR UIEA2015101300577](https://openairdocs.org/sdr/UIEA2015101300577.md): Fuel Filter · faulty · Oct 12, 2015 · N476MC · Boeing 74747UF · Engine Fuel Distribution
  > 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 RUN CUT OUT NIL PLF & EXISTING FAULT NOTED IAW AMM 71-00-00.
- [SDR UIEA2015101300576](https://openairdocs.org/sdr/UIEA2015101300576.md): Fuel Filter · faulty · Oct 12, 2015 · N476MC · Boeing 74747UF · Engine Fuel Distribution
  > 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 & SATISFACTORY IAW AMM 73-11-02. ENG NR 4 GND IDLE RUN TEST PERFORMED IAW AMM 71-00-00. NIL PLF & EXIS
- [SDR FDEA201508062490](https://openairdocs.org/sdr/FDEA201508062490.md): Unknown · malfunctioned · Aug 6, 2015 · N564FE · Doug MD1010F · Engine Oil Indicating System
  > 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 REMAINED. SHUTDOWN NR 1 ENG IAW QRH GUIDANCE, NO OTHER INDICATIONS. ENG 1 CONTINUED TO WINDMILL
- [SDR FDEA201503040646](https://openairdocs.org/sdr/FDEA201503040646.md): Wire Harness · damaged · Mar 4, 2015 · N358FE · Doug MD1010F · Engine Indicating System Wiring
  > 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. SHUTDOWN NR 2 ENG & RAN APPROPRIATE CHECKLISTS. REMOVED AND REPLACED BOTTOM LT, BOTTOM RT HARNESSES, A
- [SDR FDEA201411233868](https://openairdocs.org/sdr/FDEA201411233868.md): Cowling · worn · Nov 23, 2014 · N550FE · Doug MD1010F · Engine Cowling System
  > 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. REPAIRED IAW SRM 51-71-00 VOL II & PAINTED IAW SRM 51-21-02 VOL II.
- [SDR FDEA201410083007](https://openairdocs.org/sdr/FDEA201410083007.md): Seat Track · worn · Oct 8, 2014 · N40061 · Doug MD1010F · Fuselage, Seat/Cargo Attach Fittings
  > 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.md): Frame · chafed · Oct 5, 2014 · N10060 · Doug MD1010F · Engine Cowling System
  > 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 CORE COWL CHAFE. WELD ACCOMPLISHED ON T14 1096831. MINOR REPAIR.
- [SDR FDEA201409092547](https://openairdocs.org/sdr/FDEA201409092547.md): Duct · cracked · Sep 9, 2014 · N390FE · Doug MD1010F · Engine Air Intake System
  > 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.md): Wire · damaged · Jul 5, 2014 · N399FE · Doug MD1010F · Engine Indicating System Wiring
  > 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 AFTER PULLING TO IDLE. SECOND TIME AFTER THROTTLE MOVED HALF WAY FWD EGT SPIKED TO 1089 DEGREES C WI
- [SDR FDEA201406151464](https://openairdocs.org/sdr/FDEA201406151464.md): Power Supply · no test · Jun 15, 2014 · N372FE · Doug MD1010F · Emergency Lighting
  > 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.md): Skin · cracked · Jun 14, 2014 · N370FE · Doug MD1010F · Wing, Plate/Skin
  > 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. REMOVED CRACK. COMPLIED WITH HFEC INSPECTION, NO CRACKS FOUND. REPAIRED IAW EA 8-5710-F0308207.
- [SDR FDEA201406141448](https://openairdocs.org/sdr/FDEA201406141448.md): Skin · cracked · Jun 14, 2014 · N68057 · Doug MD1010F · Wing, Plate/Skin
  > 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 ADDITIONAL DAMAGE NOTED. HFEC INSPECTION DONE WITH NO CRACKS NOTED. REPAIRED IAW EA 8-5730-T0308776
- [SDR FDEA201406141450](https://openairdocs.org/sdr/FDEA201406141450.md): Skin · cracked · Jun 14, 2014 · N370FE · Doug MD1010F · Wing, Plate/Skin
  > 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 & VERIFIED THE CRACK TO BE A 3/8 - 1/2 INCH LONG. CUT OUT DAMAGED AREA IAW SRM. VERIFIED CRACK REMOVED US
- [SDR FDEA201404010605](https://openairdocs.org/sdr/FDEA201404010605.md): Wire Harness · damaged · Apr 1, 2014 · N383FE · Doug MD1010F · Engine Indicating System Wiring
  > 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 EXCEEDANCE MESSAGE DISPLAYED & NR 1 EGT INDICATOR WAS FLAGGED AT 999. OPENED NR 1 CORE COWL & SHO
- [SDR FDEA201403200538](https://openairdocs.org/sdr/FDEA201403200538.md): Wire Harness · damaged · Mar 20, 2014 · N371FE · Doug MD1010F · Engine Indicating System Wiring
  > 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 EXCEEDANCES. THE ACARS EXCEEDENCE SHOWS IT WAS AN EGT INDICATION PROBLEM. R & R NR 3 ENG TOP LT EGT TH
- [SDR FDEA201403190532](https://openairdocs.org/sdr/FDEA201403190532.md): Shutoff Valve · failed · Mar 19, 2014 · N656FE · Airbus A300F4605R · Engine Thrust Reverser
  > DURING CLIMB, RECEIVED ECAM WARNING NR 2 THRUST REVERSER PRESSURIZED. ECAM LASTED FOR SEVERAL SECONDS THEN WENT OUT, REAPPEARED. THROTTLE WAS BROUGHT TO IDLE IAW ECAM & WARNING AGAIN WENT AWAY. MANUAL THRUST USED & EACH TIME NR 2 THROTTLE WAS MOVED ABOVE IDL
- [SDR FDEA201403190535](https://openairdocs.org/sdr/FDEA201403190535.md): Shutoff Valve · inoperative · Mar 19, 2014 · N656FE · Airbus A300F4605R · Engine Thrust Reverser
  > 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 GOOD ON GROUND ENG RUN IAW JRH. FAN COWL CLOSED & LOCKED IAW MM 71-13-02. CLOSED & LOCKED THRU
- [SDR FDEA201403020430](https://openairdocs.org/sdr/FDEA201403020430.md): Push-Pull Cable · malfunctioned · Mar 2, 2014 · N371FE · Doug MD1010F · Power Lever
  > 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 THROTTLE OPERATED NORMALLY. R & R NR 2 ENG THROTTLE PUSH PULL CABLE. RIG & OPERATIONS CHECKED OK IAW
- [SDR FDEA201402140315](https://openairdocs.org/sdr/FDEA201402140315.md): Wire · damaged · Feb 14, 2014 · N360FE · Doug MD1010F · Engine Indicating System Wiring
  > 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. WIRE FOUND DAMAGED, WIRE REPLACED.

Next page: https://openairdocs.org/engine/ge-cf6-6d/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'CF66D'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-6d/reports

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