GE CF6-80 series

Service difficulty reports · 1,092

Newest first. General aviation reporting is voluntary.

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 03FDEA00252Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 11R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00251Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 10R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00250Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 9R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00249Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 8R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00248Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 7R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00247Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 6R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00246Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 4R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00245Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 3R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00244Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 2R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 4, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00243Nut · corrodedRT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 1R FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00241Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 14L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00242Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 36L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00240Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 12L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00232Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 28L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00234Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR30L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00237Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 33L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00238Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 34L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00235Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 31L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00236Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE NR 32L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR 03FDEA00233Nut · corrodedLT HORIZONTAL STABILIZER UPPER BARREL NUT HOLE, NR 29L FOUND CORRODED AT THE SIDE, BOTTOM AND BEARING SURFACES.Mar 3, 2003 · N585FE · Doug MD11F · Horizontal Stabilizer StructureSDR USAABB03029Wire · looseFOUND FOUR EMERGENCY LIGHTS INOPERATIVE AFT OF THE LEFT MID LAVATORY. MAINTENANCE FOUND A WIRE LOOSE ON A LIGHT ASSEMBLY AND SECURED IT.Mar 1, 2003 · N650US · Boeing 767201 · Light System WiringSDR 03FDEA00190Warning System · malfunctionedAFTER TAKEOFF, GEAR RETRACTION RIGHT GEAR UNSAFE RED LIGHT ON PRIMARY PNL ABOVE GEAR HANDLE AND ON CONFIG SYNOPTIC PAGE. RED TABS ACCOMPLISHED, GEAR EXTENDED AND RIGHT GEAR INDICATION IMMEDIATELY WENT GREEN. RAISED GEAR AND ALL INDICATION. T/S FIM 32-30-03,Feb 28, 2003 · N609FE · Doug MD11F · Landing Gear Position and WarningSDR 03FDEA00200Hinge · corrodedLT WING OUTBOARD HINGE, FLAP SIDE PIVOT HOLE CORRODED AFTER REMOVAL OF BUSHINGS.Feb 25, 2003 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00186Structure · corrodedFOUND LT WING OUTBOARD HINGE FLAP SIDE PIVOT HOLE CORRODED, AFTER REMOVAL OF BUSHINGS.Feb 25, 2003 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00171Support · crackedRT WING L/E SLAT TRACK, NR 16 RIB SUPPORT, INBOARD SIDE, FOUND WITH CRACK APPROXIMATELY 1 INCH IN LENGTH.Feb 24, 2003 · N585FE · Doug MD11F · Wing Main, Frame StructureSDR 03FDEA00164Hinge Bracket · corrodedLT WING OUTBOARD FLAP, OUTBOARD AFT HINGE ACTUATOR ROD END, OUTBOARD FITTING FOUND CORROSION . WING TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD. FLAP OUTBOARD HINGE BRACKET REPAIR CARRIED OUT IAW E.A. 1-5750-67572.Feb 20, 2003 · N613FE · Doug MD11F · Wing, Control SurfacesSDR 03FDEA00160Hinge Bracket · corrodedLT WING OUTBOARD FLAP, OUTBOARD AFT HINGE, OUTBOARD BORE FITTING, FOUND CORROSION. TRAILING EDGE AND TRAILING EDGE DEVICES - LT OUTBOARD FLAP, OUTBOARD HINGE BRACKET REPAIR CARRIED-OUT IAW EA 1-5750-67572.Feb 20, 2003 · N613FE · Doug MD11F · Wing, Control SurfacesSDR 03FDEA00159Skin · corrodedRT WING, TOP SKIN JUST FWD OF FUEL DUMP VALVE PIPE FOUND WITH CORROSION. CENTER OUTER WING, UPPER SKIN CORROSION REWORK CARRIED OUT IAW EA 1-5720-67573.Feb 20, 2003 · N613FE · Doug MD11F · Wing, Plate/SkinSDR 03FDEA00161Rib · crackedRT WING, FOUND TRACK NR 16 INBOARD STRUCTURAL RIB CRACKED. REMOVED AND REPLACED INBOARD STRUCTURAL RIB IAW SRM 51-31-01 SHT.1 VOL. II.Feb 18, 2003 · N613FE · Doug MD11F · Wing, Rib/BulkheadSDR 03FDEA00162Rib · crackedLT WING, FOUND TRACK NR 16 INBOARD STRUCTURAL RIB CRACKED. LT WING LEADING EDGE AND LEADING EDGE DEVICES, RIB INBOARD SLAT TRACK NR 16. SUPPORT FABRICATION CARRIED OUT IAW EA 1-5740-67574. CRACKED RIB REMOVED IAW SRM 51-31-01 VOL. II. AND REPLACED NEW FABFeb 18, 2003 · N613FE · Doug MD11F · Wing Main, Frame StructureSDR 03FDEA00119Thrust Reverser · deployedNR 2 ENGINE THRUST REVERSER PRESSURIZED ON TAKEOFF ROLL, REJECTED TAKEOFF AT 70KTS. WHILE DEACTIVATING THE NR 2 ENGINE THRUST REVERSER, WE WERE UNABLE TO LOCK OUT THE SLEEVE DUE TO THE HOLE NOT LINEING UP TO INSTALL BOLTS. DIRECTIONAL PILOT VALVE HAS BFeb 12, 2003 · N655FE · Airbus A300F4605R · Engine Thrust ReverserSDR 03FDEA00113Warning Light · false indicationAFT AND BULK SMOKE LIGHT CAME ON DURING LANDING APPROACH AT 1000 FT AGL. FIRED AGENT 1. LIGHT WENT OUT AFTER A SHORT DELAY. FIRE PERSONNEL REPORTED NO EXTERIOR INDICATION OF SMOKE OR FIRE AFTER LANDING. FIRST OFFICER REPORTED MUSTY ODOR PRIOR TO DONNING OFeb 6, 2003 · N676FE · Airbus A300F4605R · Fire DetectionSDR 03FDEA00067Tailpipe · damagedSIGNIFICANT TAIL PIPE FIRE DAMAGE FOUND ON POSTFLIGHT WALKAROUND, ON INBOARD AILERON, AND BOTH CANOE FAIRINGS ADJACENT TO THE AILERON ON THE NR 2 ENGINE SIDE (INWORK) WORKING IN CONJUNCTION WITH WRI 73-10/4991, CHECKED COMBUSTER DRAIN VALVE IAW M/M. NO DEFECTJan 21, 2003 · N430FE · Airbus A310 · Engine Collector/Tailpipe/NozzleSDR 03FDEA00128Hinge · looseLT WING OUTBOARD FLAP, INBOARD HINGE (AIRFRAME SIDE) AT ACTUATOR HINGE INBOARD AND OUTBOARD BORE CORRODED. REMOVED AND REPLACED INBOARD FLAP HINGE IAW EA. 1-5750-67563.Jan 21, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00129Hinge · corrodedLT WING OUTBOARD, FLAP OUTBOARD HINGE, (AIRFRAME SIDE) ACTUATOR HINGE, INBOARD AND OUTBOARD HINGE BORE CORRODED. REMOVED AND REPLACED OUTBOARD FLAP HINGE IAW EA. 1-5750-67564.Jan 21, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00047Bearing · wornON ROTATION FOR TAKEOFF ELEVATOR RESPONSE WAS VERY SLUGGISH AS IF A/P WAS ON IN CONTROL WHEEL STEERING. NO CHANGE IN HOW THE ELEV FELT AT 250 KIAS AND 320 KIAS. NO WARNING LIGHTS ILLUMINATED AT ANY TIME. DURING APPROACH ELEV RESPONSE FELT THE SAME FOUND CAPT Jan 19, 2003 · N665FE · Airbus A300F4605R · Elevator Control SystemSDR 03FDEA00048Structure · damagedAT 23,000 FT WHILE ACCEL, FELT AIRFRAME VIB AND RETURNED. FOUND NR 1 VERT, LE, FIN ASSY DAMAGED. COAX ENDS PULLED FROM MOUNT, NUMEROUS FIBERGLASS SUPPORTS BROKEN, ANTENNA CONDUIT BENT AND STANDOFFS BROKEN. THIS INCLUDES ANTENNA ITSELF. FOUND STIFFENER 4.5 Jan 19, 2003 · N426FE · Airbus A310203 · Vertical StabilizerSDR 03FDEA00096Hinge Bracket · corrodedSNRM N0927, LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORES FOUND CORROSION. SNRM N0927 REPAIR CARRIED OUT AT LT WING INBOARD FLAP OUTBOARD HINGE PIVOT BORES IAW EA 1-5750-67559: WING TRAILING EDGE AND TRAILING EDGE DEVICES, LT INBOARD FLAP HINGE BRACKET REPAJan 19, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA00127Hinge · looseRT WING OUTBOARD FLAP, OUTBOARD HINGE, ACTUATOR HINGE, INBOARD AND OUTBOARD BUSHING (AIRFRAME SIDE) LOOSE. REMOVED AND REPLACED OUTBOARD FLAP HINGE IAW EA. 1-5750-67564.Jan 18, 2003 · N607FE · Doug MD11F · Trailing Edge FlapsSDR 03FDEA0043Beam · corrodedTEE CAP AEA 7097-1, STA.1521 WAS FOUND CORRODED AT RT STA.-80.125 WHERE VERTICLE BEAM A0024-2 ATTACHES. THE BEAM ATTCHMENT TO THE TEE CAP CREATES A (V) WHERE WATER CAN PUDDLE. AWAITING APPROVED REPAIR FROM BOEINGJan 16, 2003 · N306FE · Doug DC1030F · Fuselage Main, StructureSDR ABXA030031Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED SPARE BATTERY PACK FOR EMERGENCY LIGHTS. OPS CHECKED GOOD IAW MM.Jan 6, 2003 · N775AX · Boeing 767200 · Emergency LightingSDR DL764030004Blade · damagedWORKING MSU TO BORESCOPE THE NR 2 ENGINE DUE TO PARAMETERS SHIFTING (N2 F/F & EGT UP). ATL BORESCOPE TEAM FOUND THE 6TH STAGE HPC HAD BLADE TIPS MISSING AND THE 12TH STAGE HPC HAD BLADES WITH TEARS IN THE MID BLADE AREA. FOUND BOTH AREAS TO BE OUT THE ALLOWAJan 2, 2003 · N828MH · Boeing 767432ER · Turbine Engine Compressor SectionSDR 02FDEA00982Anti-Ice Valve · failedEN ROUTE, DESTINATION ICING CONDITIONS EXISTED. NR 1 ENGINE NACELLE ANTI-ICE VALVE FAILED TO OPEN WHEN SELECTED. RELEASED FOR SERVICE IAW MEL/CDL. NR 1 ANTI-ICE INOPERATIVE ENGINE NACELLE. VALVES SECURED OPEN. REMOVED AND REPLACED NR 1 ENGINE NACELLE ANTDec 31, 2002 · N655FE · Airbus A300F4605R · Air Intake Anti/De-Ice SystemSDR 02FDEA00981Seat Track · damagedMAIN CABIN, SEAT TRACK DAMAGED AT FS 1350.5 X=-47.50. TRIMMED OUT DAMAGED SEAT TRACK IAW SRM. FABRICATED SEAT TRACK AND SPLICE HAT IAW SRM. INSTALLED SEAT TRACK AND SPLICE HAT IAW SRM.Dec 30, 2002 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00979Valve · leakingDECLARED INFLIGHT EMERGENCY, SMOKE IN COCKPIT. SOURCE OF SMOKE WAS BELIEVED TO BE AIR CONDITIONING SYSTEM. NOTICED A DIRTY SOCK ODOR DURING TAXI. IN FLIGHT, THE SMOKE KEPT INCREASING, RETURNED TO BASE. USED EMERGENCY ESCAPE SLIDE TO EGRESS ON RUNWAY. FIREDec 28, 2002 · N602FE · Doug MD11 · Cabin Cooling SystemSDR 02FDEA00973Smoke Detector · malfunctionedAVIONICS SMOKE ECAM WARNING ON TAKEOFF. REJECTED AND PERFORMED ECAM AND AVIONICS SMOKE PROCEDURES, NO SNIFFER SMOKE DETECTED, DID RTO CHECKLIST AND RETURNED TO GATE AVIONICS SMOKE WARNING CAME ON 2 MORE TIMES BEFORE BLOCKING IN. REMOVED AND REPLACED E/E SMDec 27, 2002 · N404FE · Airbus A310203 · Smoke DetectionSDR 02FDEA00978Relay · failedMID-FLIGHT, EMERGENCY POWER ON ALERT ILLUMINATED. REVIEWED CHECK 20-30 WEST OF LIT, BATTERY LOW ALERT ILLUMINATED. SHORTLY THEREAFTER MULTIPLE ELECT ALERTS OCCURRED. INCLUDING FCC 1B FAULT, FADEC ALT, ALL 3 ENGINES AND OTHERS. CAPTAIN, NR 1 AND NR 3 DU FAIDec 27, 2002 · N591FE · Doug MD11 · AC Power Distribution SystemSDR 02FDEA00965Seat Track · corrodedMDCC FLOOR SEAT TRACK FOUND WITH CORROSION AT STA 585, 685 X -75.25. TRIMMED OUT DAMAGED AREA ON SEAT TRACK FLANGE IAW SRM, FABRICATED FILLER AND STRAP IAW SRM. INSTALLED FILLER AND STRAP IAW SRM.Dec 23, 2002 · N606FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00980Stringer · crackedMDCC FUSELAGE FRAME STA 1139-1159, STRINGER 17R, FOUND WITH CRACK.Dec 20, 2002 · N606FE · Doug MD11 · Fuselage Main, Longeron/StringerSDR 02FDEA00983Rib · gougedLEFT WING, MAIN LANDING GEAR RIB 5 HOLE NR 52, GOUGED.Dec 18, 2002 · N669FE · Airbus A300F4605R · Wing, Rib/Bulkhead
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