GE CF6-80C2D1F

Service difficulty reports · 536

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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 = 'CF680C2D1F'
  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 04FDEA02870Sleeve · crackedENG 1R T/R TRANSLATING SLEEVE UPPER SLIDING TRACK AFT EDGE FOUND CRACKED. CRACK REPAIRED REFER FAA FORM 8130-3 NO 5488(J009681-000) FOR WORK DETAILS.Oct 5, 2004 · N615FE · Doug MD11F · Engine Thrust ReverserSDR 04FDEA02871Sleeve · crackedENG 2L T/R TRANSLATING SLEEVE UPR SLIDING TRACK AFT EDGE FOUND CRACKED. CORRECTIVE ACTION: SNRM N0308: CRACK REPAIRED REFER FAA FORM 8130-3 NO 5489(J009682-000) FOR WORK DETAILS.Oct 5, 2004 · N615FE · Doug MD11F · Engine Thrust ReverserSDR 04FDEA02814Control Unit · malfunctionedIN CRUISE FLT, AT FL 330, AT APPROX TAKEOFF PLUS FOUR HOURS, RECEIVED (LEVEL 1 TANK 2 FUEL QTY LO) ALERT S.D. FUEL READINGS WERE: 1- 900 2- 0 3-900 AUX- 900 TAIL- 12900. FUEL INDICATIONS AND USAGE TO THAT POINT HAD BEEN NORMAL. FSC WAS IN AUTO, ALSO GOT Sep 24, 2004 · N605FE · Doug MD11F · Fuel Indicating SystemSDR 04FDEA02804Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.251, FINAL DIAMETER= 1.314. COMPLIED WITH FEDEX EA 1-5750-79749,Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02805Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03 PAGES 442 TO 443.Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02806Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER = 1.249, FINAL DIAMETER = 1.257. COMPLIED WITH FEDEX EA 1-5750-79749,Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02807Hinge · corrodedRT WING, IB FLAP, OB AFT HINGE PIVOT HOLE OB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02808Hinge · corrodedLT WING, IB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AND FOUND EXCEEDED LIMTS PER CMM 57-52-03, PAGES 442 TO 443. ORIGINAL DIAMETER= 1.289, FINAL DIAMETER= 1.291. COMPLIED WITH FEDEX EA 1-5750-79749Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02809Hinge · corrodedLT WING, IB FLAP, OB AFT HINGE PIVOT HOLE IB SPOTFACE CORRODED. CORROSION REMOVED AND FOUND WITHIN LIMITS PER CMM 57-52-03.Sep 23, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02811Frame · dentedTRANSVERSE FRAME AT LT STA Y= 1721 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 FLIGHT CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES PER THE GUIDELINES OF MD-11 SRM 53-Sep 23, 2004 · N585FE · Doug MD11F · Fuselage Main, FrameSDR 04FDEA02812Frame · dentedTRANSVERSE FRAME AT LT STA Y= 1701 BETWEEN LONGERON 12L AND 13L DENTED BY CARGO IMPINGEMENT. REPAIRED PER SRM 53-30-00 VOLUME I FIGURE 1. INITIAL INSPECTION TO BE CARRIED OUT AT 22, 951 CYCLES AND REPETITIVE INSPECTION THEREAFTER EVERY 9, 500 FLIGHT CYCLES Sep 23, 2004 · N585FE · Doug MD11F · Fuselage Main, FrameSDR 04FDEA02813Pneumatic System · malfunctionedON CLIMB OUT FROM ZSPD GOT LEVEL 3 ALERT AIR MANF 2 FAIL. COMPLIED /W QRH, DUMPED FUEL, LANDED RJBB. ACN RELEASED FOR SERVICE IAW MEL/CDL: 36-10-02-A CATEGORY: C EXPIRATION: 03OCT04) MEL 36-10-02-A: PNEUMATIC SUPPLY SYS NR 2 INOPERATIVE.**** S/D COMING***Sep 23, 2004 · N594FE · Doug MD11F · Pneumatic Indicating SystemSDR 04FDEA02786Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02787Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, OB PIVOT HOLE SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02788Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02789Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 21, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02775Hinge · corrodedSNRM NR N0484 LT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, OB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02776Hinge · corrodedSNRM NR N0483 LT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02777Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE PIVOT HOLE, IB SPOTFACE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02778Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02779Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02780Hinge · corrodedSNRM NR N0488- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, OB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA1-5750-79749.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02781Hinge · corrodedLT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB SPOTFACE ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02782Hinge · corrodedSNRM NR N0486- LT WING, OB FLAP, IB AFT HINGE ACTUATOR ROD END HOLE, IB ATTACHMENT CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 TO 4. ORIGINAL DIAMETER=1.187, FINAL DIAMETER=1.189 AND REPAIRED AS PER EA#1-5750-79749.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02784Hinge · corrodedRT WING, OB FLAP, OB AFT HINGE, IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 20, 2004 · N585FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02700Structure · corrodedCORROSION REMOVED ON 31R BARREL NUT BORE FOUND EXCEEDED LIMIT IAW EO 1-5510-7-5000 C3 PT1 FIG 03. RT HORIZONTAL STABILIZER, EXCEEDED LIMIT BARREL NUT BORE NR 31R, REPAIRED AS PER EA 1-5510-81555.Sep 16, 2004 · N615FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02687Track · crackedENGINE NR 3 LT T/R COWL UPPER SLIDER TRACK END FOUND WITH CRACK. REMOVED AND REPLACED AS PER AMM 78-33-01-4 AND REPAIR CARRIED OUT, PLS REFER TO FAA 8130-3 FORM TRACKING NR 5480 FOR FURTHER WORK DETAILS AND INSTALLED AS PER AMM 78-33-01-04 AND FUNCTIOSep 16, 2004 · N593FE · Doug MD11 · Engine Thrust ReverserSDR 04FDEA02688Track · crackedENGINE NR 2, RT, T/R COWL AT UPPER SLIDER TRACK END FOUND WITH CRACK. T/R COWL REMOVED AS PER AMM 78-33-01-4. REPAIR CARRIED OUT, REFER TO FAA 8130-3, FORM TRACKING NO. 5479 RIGHT HAND THRUST REVERSER COWL RE-INSTALLED AS PER AMM 78-33-01-4. ADJUSTMENT ASep 16, 2004 · N593FE · Doug MD11 · Engine Thrust ReverserSDR 04FDEA02607Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02608Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02609Hinge · corrodedLT WING - OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02610Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02611Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02612Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02613Hinge · corrodedLT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02614Hinge · corrodedSNRM N0442: LT WING, OB FLAP OB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02624Hinge · corrodedRT WING-OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02625Hinge · corrodedSNRM N0453: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02626Hinge · corrodedSNRM N0454: RT WING- OB FLAP IB HINGE (FLAP SIDE), PIVOT ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02627Hinge · corrodedSNRM N0455: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02628Hinge · corrodedSNRM N0456: RT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02629Hinge · corrodedRT WING-OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, IB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02630Hinge · corrodedRT WING- OB FLAP IB HINGE (FLAP SIDE), ACTUATOR ATTACH LUG, OB BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Sep 3, 2004 · N615FE · Doug MD11F · Trailing Edge FlapsSDR 04FDEA02566Isolator · defectiveMANIFOLD NR 2 FAILURE. INFLIGHT QRH COMPLIED WITH. LANDED CDG. PERFORMED DECAY CHECK IAW MM 36-00-02 WITH ALL OK, PERFORMED FLIGHT FAULT, REVIEW ON THE MFC FOUND (SENSOR ZONE 15 ELE A). DURING TEST FOUND BAD ISOLATION ON LOOP D1-98 REMOVED AND REPLACED MAAug 25, 2004 · N610FE · Doug MD11F · Pneumatic Distribution SystemSDR 04FDEA02537Structure · damagedTO COMPLY EA NR 1-5510-79807, STABILIZERS, HORIZONTAL STABILIZER, BARREL NUT BORE'S REWORKED BEYOND MFG S/B MD-11 55-023 REVISION 2 AND EO NR 1-5510-7-5000 LIMITS, MASTER EA COMPLIED WITH FEDEX E.A. NO. 1-5510-79807, STABILIZERS - HORIZONTAL STABILIZER BARRELAug 21, 2004 · N613FE · Doug MD11F · Horizontal Stabilizer StructureSDR 04FDEA02531Deu · faultyON DEPARTURE CLIMBING THROUGH 800 FEET, DEU 1,2,3 SHOWED RED(X) ACCOMPANIED BY MASTER WARNING LIGHT AND BELL, MASTER CAUTION LIGHT, AND ALL ALERTS INDICATING ON EAD. COULD NOT SILENCE WARNING HORN. INTERROGATED CFDS AND FOUND NR 1 DEU FAULTY. REMOVED ANDAug 19, 2004 · N595FE · Doug MD11F · Central WarningSDR 04FDEA02532Bulkhead · damagedTO TRIM OUT HORIZONTAL STABILIZER LT OPERATING BULKHEAD FITTING TO GAIN ACCESS FOR LT UPPER AFT PLANK NR 34L BARREL NUT REWORK. LT HORIZONTAL STABILIZER, OPERATING BULKHEAD FITTING TRIMMED OUT FOR ACCESS IAW EA 1-5510-79819. TITLE: STABILIZERS, HORIZONTAL STAAug 19, 2004 · N613FE · Doug MD11F · Horizontal Stabilizer StructureSDR 04FDEA02465Sensor · malfunctionedCAPTAINS PLI DROPPED TO FD PITCH BAR WHEN SLATS RETRACTED AND STICK SHAKER ACTUATED CAPTAINS SPEED INDICATOR BECAME RED, ALT MISS COMPARE, W/S DETECT FAIL ILLUMINATED, EVERYTHING WENT NORMAL WHEN SLATS EXTENDED. RETURNED TO MEM. FACT: REPLACED LT AOA SENAug 13, 2004 · N586FE · Doug MD11F · Stall Warning SystemSDR UPS04M42406Engine · malfunctionedON DESCENT, 8000 FT ALL ENGS DID NOT RESPOND TO THROTTLE COMMAND. PUSHED THROTTLES FULL FWD NO RESPONSE. TURNED ON IGN OVRD END CAME BACK. BOTH MCP PNLS CONFIRMED ENG OUT THRUST LIMITS SHOWED MCT EAD. OIL PRESS ON 1&3 FELL BELOW 19 PSI, ENG 2 OIL 22 PSI. N1'May 24, 2004 · N254UP · Doug MD11F · Engine (Turbine/Turboprop)SDR 03FDEA02203Case · chafedNEW ENGINE AT 4 O'CLOCK AFT FAN CASE AREA FOUND CHAFING MARK. CHAFING MARK AT NR 3 ENGINE ON 4 O'CLOCK POSITION, AFT FAN CASE 'T' RIB SMOOTHED OUT WITH FINAL DIMENSION : LENGTH = 0.470, WIDTH = 0.300 AND DEPTH APPROX. = 0.120, FOUND WITHIN LIMITS AS PER GE MADec 17, 2003 · N608FE · Doug MD11 · Turbine Engine Compressor Section
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