GE CF6-80 series

Service difficulty reports · 1,092

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Query with SQL
duckdb -csv -c "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 = 'CF680'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 04FDEA01491Hinge · corrodedLT WING, OB FLAP AFT OB HINGE, FOUND IB ACTUATOR HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIG. DIA: 1.062, FINAL DIA: 1.191. REPAIR CARRIED-OUT AS PER FEDEX EA 1-5750-76722 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBD FMay 26, 2004 · N594FE · Doug MD11 · Trailing Edge FlapsSDR USA2004F00070Video Monitor · faultyPASSENGER REPORTED THAT THE AFT VIDEO MONITOR EMITTED A MOMENTARY PUFF OF SMOKE AND THEN BLANKED OUT. THE CREW SECURED THE VIDEO SYSTEM. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE VIDEO SYSTEM AND MONITOR WERE OPERATED FOR APPROXIMATELY FORTY-FIVE MINMay 26, 2004 · N648US · Boeing 767201 · Entertainment SystemSDR USA2004F00069Transceiver · overheatedHF NR 2 RADIO TAKES EXCESSIVELY LONG TO CHANNELIZE AND WILL NOT TRANSMIT. ELECTRICAL SMELL NOTED DURING CHANELIZATION PROCESS, BUT DISIPATED AFTER HF WAS TUNED. MAINTENANCE INSPECTED HF RELATED WIRING AND CONNECTION AND COULD NOT FIND A FAULT. THE HF NR 2 TMay 24, 2004 · N653US · Boeing 7672B7 · HF Communications SystemSDR UIEA200400099Actuator · inoperativeTAKEOFF WARNING (CONFIGURATION BODY GEAR) DISPLAYED DURING TAKEOFF. CMC GAVE LT GEAR OB ACTUATOR SWITCH MESSAGE 32055. DEACTIVATED ALL ACTUATORS INDICATION SYS IAW MEL AND TRANSFERRED ITEM TO DMI. (DEACTIVATED RT OB CYLINDER IAW MEL). REMOVED AND REPLACED May 24, 2004 · N408MC · Boeing 74747UF · Steering UnitSDR USA2004F00068Transceiver · overheatedAFTER UNSUCCESSFUL ATTEMPT TO TUNE OR TRANSMIT ON HF NR 1, AND ELECTRICAL SMELL WAS NOTED IN THE COCKPIT. THE HF NR 1 CIRCUIT BREAKER WAS PULLED AND THE SMELL DISSIPATED. MAINTENANCE REPLACED THE NR 1 HF TRANSCEIVER.May 20, 2004 · N653US · Boeing 7672B7 · HF Communications SystemSDR DL764040429Heater · odorHEATER AT 2L GIVES OFF BURNING RUBBER SMELL. WENT AWAY WHEN CB WAS PULLED, C FWD TO MCO HEATER DEACT. ETOPS CATEGORY (E) PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.May 11, 2004 · N828MH · Boeing 767432ER · Heating SystemSDR USAA040211Seat Track · corrodedSEAT TRACK, CORROSION, NO LEVEL, BS1087-1469, RBL 88.5 CABIN FLOOR.May 9, 2004 · N646US · Boeing 767201 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040209Web · crackedWEB CUTOUT, .75 INCH LONG EACH, CRACKS (2) SEAT TRACK AT BS 785, RBL 55 CABIN FLOOR LEVEL. SPLICED IN FABRICATED TEE CAP IAW 53-00-51, FIG 203.Apr 29, 2004 · N646US · Boeing 767201 · Fuselage Miscellaneous StructureSDR USAA040210Web · crackedSEAT TRACK WEB, .75 INCH LONG EACH, CRACKED (2) WEB CUTOUT UNDER SEAT TRACK BS785, LBL 55. REPAIRED IAW SRM.Apr 28, 2004 · N646US · Boeing 767201 · Fuselage Miscellaneous StructureSDR DL764040374Engine · shutdownAT 2000 FEET RIGHT ENG ROLLED BACK HAD HIGH FUEL FLOW AND HIGH VIBS ENG NOT RESPONDING TO THROTTLE INPUTS. AFTER LANDING ENG SHUTDOWN DUE HIGH VIBS. METAL FOUND IN TAILPIPE. REPLACED ENGINE.Apr 26, 2004 · N831MH · Boeing 767432ER · Engine (Turbine/Turboprop)SDR USAA040207Floorbeam · corrodedFLOORBEAM, 2 INCHES X 2 INCHES AREA, CORROSION; NO TASK/ LEVEL, CABIN FLOOR, TOP OF FLOORBEAM STA 1502, LBL 28. SPLICE REPAIR INSTALLED IAW SRM.Apr 26, 2004 · N646US · Boeing 767201 · Fuselage Main, Floor BeamSDR USAA040208Floorbeam · corrodedFLOORBEAM 16 INCHES X 2 INCH AREA, CORROSION; NO LEVEL/ TASK AFT CABIN FLOOR STA 1480, LBL 27-43. INSTALLED REPAIR IAW SRM.Apr 26, 2004 · N646US · Boeing 767201 · Fuselage Main, Floor BeamSDR UPS04642147Engine · flamed outINSPECTION TYPE: ETOP, RT ENGINE FLAMED OUT WHEN POWER WAS REDUCED FOR LANDING. OBVIOUSLY NO RE-START ATTEMPTED. NO ENG PARAMETER EXCEEDENCE OBSERVED. REPLACED RIGHT ENG PER TC 6002 & TC 6001 OP'S CHECK SATISFIED.Apr 16, 2004 · N315UP · Boeing 76734AF · Engine (Turbine/Turboprop)SDR P5CA0401099Nozzle · dentedNR 1 ENGINE EXHAUST NOZZLE HAS A DENT AT 7 O`CLOCK 5.125 LONG .5 INCH WIDE AND .001 INCH DEEP, BEYOND .80 LIMIT. REMOVED AND REPLACED EXHAUST NOZZLE.Apr 12, 2004 · N450PA · Boeing 74746NF · Engine Collector/Tailpipe/NozzleSDR AUS20040259Apu · failed(AUS) APU FAILED TO START DURING TAXI.Apr 4, 2004 · Airbus A330* · APU Core EngineSDR DL764040282Transmitter · malfunctionedON APPROACH TO ATL RT ENG OIL PRESS WENT TO 0 AND ENG WAS SHUTDOWN. ALL OTHER PARAMETERS WERE NORMAL. FOUND RT ENG OIL PRESSURE TRANSMITTER FAILED PER FIM 79-11-00 PAGE 105. REPLACED TRANSMITTER AND ACCOMPLISHED POST WINDMILL INSP PER M/M 72-00-00-206-096-HMar 29, 2004 · N838MH · Boeing 767432ER · Engine Oil Indicating SystemSDR 04FDEA00682Line · contaminatedDURING DESCENT AT 6000 MSL, 250 KIAS IDLE THRUST ENG 2 RPM LO ALERT, FOLLOWED BY FLAMEOUT, EGT 75 DEG WITH IGNITION OVERRIDE ENGINE ACCELERATED TO NORMAL IDLE. ENGINE OPERATION DURING APPROACH, LANDING AND ROLLOUT WAS NORMAL. INSPECTED NR 2 ENG OIL MASTER CHMar 19, 2004 · N595FE · Doug MD11 · Fuel Control/Turbine EnginesSDR 04FDEA00602Autothrottle Sys · failedON FINAL APPROACH, NR 1 THROTTLE STUCK AT ABOUT 15 DEGREES. DECLARED EMERGENCY AND FINISHED APPROACH. AFTER LANDING, THROTTLE MOVED FREELY. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01 CATEGORY: C EXPIRATION: 16MAR04 MEL 22-30-01: AUTOTHROTTLE SYSTEM INOP. AMar 6, 2004 · N682FE · Airbus A300F4605R · Auto Throttle SystemSDR USAA040060Floorbeam · corrodedTOP OF FLOORBEAM, STA 287, RBL 26, RBL53 CORROSION (3 AREAS). INSTALLED CAP IN FLOORBEAM IAW SRM 53-00-51, FIG 201.Feb 28, 2004 · N645US · Boeing 767201 · Fuselage Main, Floor BeamSDR USAA040056Attach Angle · crackedFWD CABIN FLOOR UPPER ATTACH ANGLE, WEB STA 287-303, RBL 40, CRACKED. FABRICATED NEW ANGLE AND FILLER AND INSTALLED IAW SRM 51-10-02.Feb 25, 2004 · N645US · Boeing 767201 · Fuselage Miscellaneous StructureSDR USA2004F00009Light · faultyTHE COCKPIT EMERGENCY LIGHT DID NOT TEST. MAINTENANCE REPLACED THE COCKPIT EMERGENCY LIGHT. OPERATIONALLY CHECKS, OK.Feb 24, 2004 · N650US · Boeing 767201 · Emergency LightingSDR 04FDEA00457Gearbox · making metalAFTER T/O, PASSING 5000FT, CAPT NOTICED NOSE DOWN TRIM STUCK AT 2.2 ANU USING BOTH. CAPT AND F/O YOKE CONTROLS AND SUITCASE HANDLES TO TRIM NOSE DOWN. ALL UNSUCCESSFUL. ONCE A/C STARTED TO ACCELERATE, PASSING 10K , 310 KTS A/P WOULD DISENGAGE. AT FIRST TRIM WFeb 19, 2004 · N590FE · Doug MD11 · Stabilizer Control SystemSDR AUS20040112Odor · detected(AUS) ELECTRICAL ODOR IN CABIN IN AREA OF SEAT 48JK. INVESTIGATION CONTINUING.Feb 15, 2004 · Airbus A330* · Air Distribution SystemSDR USAABB04015Warning Light · false activationEN ROUTE, THE CREW RECEIVED THE E/M'S (AILERON LOCKOUT) AND (FLAP/SLAT ELEC). FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FIM PROCEDURES FOR BOTH SYSTEMS. NO FAULTS FOUND. AIRCRAFT RELEASED FOR VERIFICATION FLIGHT. (M)Jan 29, 2004 · N651US · Boeing 7672B7 · Central WarningSDR AUS20040027Unknown · fumes(AUS) PLASTIC SMELLING FUMES IN REAR GALLEY. INVESTIGATION COULD FIND NO CAUSE FOR THE FUMES.Jan 18, 2004 · Airbus A330300 · Air Distribution SystemSDR AUS20040026Warning Light · illuminated(AUS) FORWARD CARGO DOOR MESSAGE. LIMITED INFORMATION PROVIDED.Jan 16, 2004 · Airbus A300* · Door Warning SystemSDR 03FDEA02292Hinge · corrodedLT WING, OB FLAP, IB HINGE FITTING OB PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.Dec 29, 2003 · N584FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA02293Hinge · corrodedLT WING, OB FLAP IB HINGE ACTUATOR OB MOUNT IB AND OB SIDE SURFACE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75200 - WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP/INBOARD SUPPORT BRACKET CORROSION REMOVAL AND REPAIRDec 29, 2003 · N584FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 03FDEA02304Panel · crackedLT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT FOUND CRACKED APPROXIMATELY 1.5 INCHES IN LENGTH. C/A: SNRM N0235 LT WING UPPER TRAILING EDGE PANEL ADJACENT TO NR 3 SPOILER ACTUATOR ATTACHMENT CRACKED PANEL REMOVED IAW AMM 20Dec 28, 2003 · N608FE · Doug MD11 · Wing, Plate/SkinSDR 03FDEA02305Fitting · wornLT WING, IB FLAP VANE IB TEE FITTING MOUNT HOLES (3 EA.) WORN. COMPLIED WITH FEDEX EA 1-5750-75214, TRAILING EDGE AND TRAILING EDGE DEVICES - LT INBOARD FLAP VANE ATTACH FITTING REWORK.Dec 27, 2003 · N584FE · Doug MD11 · Wing, Attach FittingsSDR 03FDEA02296Panel · chafedRT TAILCONE UPPER DOOR FORWARD MOST ACCESS PANEL FOUND CHAFED. RT TAILCONE UPPER DOOR FWD MOST ACCESS PANEL FABBRICATED AS PER DWG AKC 7506. PANEL REMOVED AND REPLACED AS PER MM 20-50-02.Dec 26, 2003 · N584FE · Doug MD11 · Aerodynamic FairingsSDR 03FDEA02245Fitting · corrodedLT WING, IB FLAP VANE IB UP STOP FITTING ATTACHMENT BORE CORRODED. LT WING - I/B FLAP VANE I/B UP STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II.Dec 26, 2003 · N584FE · Doug MD11 · Wing, Control Surface Attach FittingsSDR 03FDEA02248Hinge · corrodedLT WING - IB FLAP OB HINGE FITTING IB PIVOT BORE CORRODED. COMPLIED WITH FEDEX EA 1-5750-75212, TITLE: WINGS TRAILING EDGE AND TRAILING EDGE DEVICES- LT INBOARD FLAP HINGE BRACKET REPAIR.Dec 26, 2003 · N584FE · Doug MD11 · Trailing Edge FlapsSDR 03FDEA02294Stiffener · chafedLT TAILCONE TOP MOST HORIZONTAL STIFFINER BELOW THE UPPER DOOR HINGE ASSY FOUND CHAFED AT ITS END AREA. LT TAILCONE TOP MOST HORIZONTAL STIFFINER BELOW CHAFED TEE SUPPORT REMOVED AND REPLACED AS PER SRM 51-35-01 VOL.II AND DRAWING AKC7543.Dec 26, 2003 · N584FE · Doug MD11 · Aerodynamic FairingsSDR 03FDEA02297Beam · chafedTAILCONE UPPER DOOR CUTOUT AFT HORIZONTAL BRACKET LT AND RT AREA ADJACENT TO TAIL CONE LADDER SUPPORT FITTING FOUND CHAFED. REMOVED CHAFED SUPPORT AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW BEAM AS PER DRAWING AKC 7528. INSTALLED BEAM AT TAILCONE UPPER DDec 26, 2003 · N584FE · Doug MD11 · Aerodynamic FairingsSDR 03FDEA02300Bracket · chafedRT TAILCONE UPPER DOOR FWD MOST TRIANGULAR VERTICAL BRACKET FOUND CHAFED. REMOVED DAMAGED BRACKET AS PER SRM 51-31-01 VOL. II AND FABRICATED NEW STIFFENER AS PER DRAWING AKC 7868. INSTALLED NEW STIFFENER AT RT TAILCONE UPPER DOOR FWD MOST AS PER SRM 51-31-01Dec 26, 2003 · N584FE · Doug MD11 · Aerodynamic FairingsSDR 03FDEA02303Plate · wornTAILCONE AFT SNUBBER TOP AND BOTTOM SUPPORT PLATE FOUND WORN. REMOVED WORN SUPPORT PLATE AS PER SRM 51-31-01 VOL. II AND INSTALLED NEW SUPPORT ASSY AT TAILCONE AFT SNUBBER TOP AND BOTTOM AS PER SRM 51-35-01 VOL. II.Dec 26, 2003 · N584FE · Doug MD11 · Aerodynamic FairingsSDR 03FDEA01923Skin · corrodedHORIZONTAL STAB RIGHT UPPER FWD PLANK NR 6R BARREL NUT BORE FOUND CORROSION ON SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS.Nov 17, 2003 · N583FE · Doug MD11F · Horizontal Stabilizer, Plate/SkinSDR 03FDEA01920B-Nut · looseABOUT 2 HRS AFTER DEPARTURE NOTICED NR 1 OIL QTY DROPPING AND GOING TO ZERO. AT THAT TIME PRESSURE AND TEMP WERE NORMAL, 1 HR AFTER THAT NR 1 OIL PRESSURE STARTED A VERY SLOW DROP, EVENTUALLY TURNED AMBER. DIVERTED TO BKK. ON DESCENT PRESSURE DROPPED TO REDNov 17, 2003 · N607FE · Doug MD11 · Engine Oil Distribution (Airframe Furnished)SDR 03FDEA01924Structure · corrodedHORIZONTAL STABILIZER LT UPPER FWD PLANK NR 5L BARREL NUT BORE FOUND CORROSION ON BOTTOM SURFACE BEYOND EO 1-5510-7-5000 LIMITS. HORIZONTAL STAB LT UPPER FWD PLANK NR 5L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245. HORIZONTAL STABILIZER - BARRELNov 17, 2003 · N583FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA01925Structure · corrodedHORIZONTAL STAB LT UPPER CENTER PLANK NR 25L BARREL NUT BORE FOUND CORROSION ON SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. HORIZONTAL STAB LT UPPER CENTRE PLANK 25L BARREL NUT BORE REPAIR CARRIED OUT AS PER EA 1-5510-74245 STABILIZERS - HORIZONTAL Nov 17, 2003 · N583FE · Doug MD11 · Horizontal Stabilizer StructureSDR 03FDEA01926Spar Cap · corrodedHORIZONTAL STABILIZER RT UPPER AFT SPAR CAP NR 36R BARREL NUT BORE FOUND CORROSION ON BOTTOM AND SIDEWALL SURFACES BEYOND EO 1- 5510-7-5000 LIMITATIONS. COMPLIED WITH FEDEX EA 1-5510-74245, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR - 1-5510-7-5000Nov 17, 2003 · N583FE · Doug MD11 · Horizontal Stabilizer, Spar/RibSDR 03FDEA01927Fitting · corrodedHORIZONTAL STABILIZER RT UPPER CENTER PLANK NR 26R BARREL NUT BORE FOUND CORROSION ON BOTTOM AND SIDEWALL SURFACE BEYOND EO 1-5510-7-5000 LIMITATIONS. NEW 26R FITTING FABRICATED AS PER DWG ALC8107 AND EA 1-5510-74245, HORIZONTAL STABILIZER BARREL NUT BORE REWNov 17, 2003 · N583FE · Doug MD11 · Horizontal Stabilizer StructureSDR AUS20031159Actuator · incorrect(AUS) INCORRECT GREASE USED ON TRIM ABLE HORIZONTAL STABILIZER ACTUATOR (THSA). AEROSHELL 22 USED INSTEAD OF CORRECT AEROSHELL 33. USE OF INCORRECT GREASE MAKES AIRCRAFT NON COMPLIANT WITH AD/330/7.UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.Nov 16, 2003 · Airbus A330202 · Stabilizer ActuatorSDR UPS03641541Wire · faultyINSPECTION TYPE: N/A FIRE PROTECTION SYSTEM FAIL LIGHT ILLUMINATED. EICAS MSG: FIRE/OVHT SYS DISPLAYED. EICAS STATUS MSG: R ENG FIRE LP1 DISPLAYED. INDICATION APPEARED ON SHORT FINAL TO LANDING. TESTED SYSTEM, INDICATION EXTINGUISHED. REPLACED ALL WIRINNov 8, 2003 · N324UP · Boeing 767300 · Fire Protection System WiringSDR 03FDEA01870Shear Tie · corrodedCORROSION ON FWD CARGO COMPARTMENT SHEAR TIE ON AFT SIDE OF BS 700 FRAME RBL 9 WL 148. REPAIR PER SRM 53-10-4 FIG 13 SHT 1 AT BS 700, RBL 9, WL 148.Nov 5, 2003 · N270FE · Boeing 727200 · Fuselage Main, StructureSDR 03FDEA01869Line · crackedDURING THE PRESSURE TEST OF TAIL TANK FUEL SHROUD DRAIN SYSTEM FOUND TAIL TANK TRANSFER FUEL SHROUD TUBING LOCATED AT STA. Y 1791 LT SIDEWALL OF CENTER CARGO WITH A CRACK LINE MEASURED APPROX. 1 INCH IN LENGTH. COMPLIED WITH EA 1-2822-71762 FUEL SYSTEM -Oct 30, 2003 · N614FE · Doug MD11 · Aircraft Fuel Distribution SystemSDR 03FDEA01868Shroud · crackedDURING THE PRESSURE TEST OF TAIL TANK FUEL SHROUD DRAIN SYSTEM FOUND TAIL TANK TRANSFER FUEL SHROUD TUBING LOCATED AT STA. Y 1801 LT SIDEWALL OF CENTER CARGO WITH A CRACK LINE MEASURED APPROX. 2.0 INCHES IN LENGTH. COMPLIED WITH EA 1-2822-71762 FUEL SYSOct 29, 2003 · N614FE · Doug MD11 · Fuel Boost PumpSDR 03FDEA01802Fitting · corrodedBFM CLOSER NR S 10 COMPLY WITH EA NR 6-5450-73844 PYLONS/NACELLES-NR 1 ENGINE PYLON FWD MOUNT CORROSION REPAIR. FACT 25OCT03 16:43 BFM U COMPLIED WITH EA NR 6-5450-73844- PYLONS/NACELLES - NR 1ENGINE PYLON FWD MOUNT CORROSION REPAIR. CLOSED ON 10/25/Oct 25, 2003 · N660FE · Airbus A300B4605R · Nacelle/Pylon Miscellaneous StructureSDR 03FDEA01801Skin · gougedMDIS 660 78-30 0007125 22OCT03 BFM CLOSE R NR S 14 COMPLY WITH EA NR 6-7832-73847 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR. FACT 25OCT03 16:46 BFM U COMPLIED WITH EA NR 6-7832-73847 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR. CLOSED ON 10Oct 25, 2003 · N660FE · Airbus A300B4605R · Engine Thrust Reverser
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