GE CF6-80C2D1F

Service difficulty reports · 536

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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 06FDEA03830Stringer · crackedCRACK FOUND (APPROX. 1.5 INCHES LONG) DURING HFEC INSPECTION ON RT WING TANK AT THE END OF LOWER STRINGER 41 XORS 685. CRACK ON RIGHT HAND WING TANK AT THE END OF LOWER STRINGER 41 XORS 685 SLOTTED OUT AND RESIZING ARROWHEAD REPAIR CARRIED OUT AS PER SRM Nov 2, 2006 · N619FE · Doug MD11F · Wing, Longeron/StringerSDR 06FDEA03689Seat Track · gougedM/D CARGO SEAT TRACK AT STA 1089 LT X=47.5 FOUND CHANNEL EDGE BROKEN. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1089 LT X=47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03690Seat Track · gougedM/D CARGO SEAT TRACK AT STA 1010 LT X=47.5 FOUND CHANNEL EDGE GOUGED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1010 LT X=47.5 AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03691Seat Track · gougedM/D CARGO SEAT TRACK AT STA 785 LT X=47.5 FOUND CHANNEL EDGE GOUGED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK, STA 785 LH X=47.5 AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03692Seat Track · chafedM/D CARGO SEAT TRACK AT STA 1029 RT X=47.5 FOUND CHANNEL EDGE CHAFED. REPAIR CARRIED OUT AT M/D CARGO SEAT TRACK AT STA 1029 RH X=47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03693Stringer · crackedCRACK FOUND DURING HFEC INSPECTION AT LT WING TANK END OF STRINGER 43. REPAIR CARRIED OUT AT LT WING TANK END OF STRINGER 43, XORS 565 AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03694Stringer · crackedCRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 14. REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 14, XORS 521 AS PER SRM 57-20- 00 FIGURE 10 COLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03695Stringer · crackedCRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 13. REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 13, XORS 577 AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03696Stringer · crackedCRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 10.REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 10, XORS 760 AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03697Stringer · crackedCRACK FOUND DURING HFEC INSPECTION AT RT WING TANK END OF STRINGER 11. REPAIR CARRIED OUT AT RT WING TANK END OF STRINGER 11, XORS 704 AS PER SRM 57-20- 00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA03698Doubler · crackedLT WING FIXED L/E BEADED DOUBLER FOUND CRACKED AT XOS 636-643. REPAIR CARRIED OUT AT LT WING FIXED L/E BEADED DOUBLER, XOS 636-643 AS PER FEDEX EA 1-5730-104811, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA03699Slat Track · crackedLT WING FIXED L/E NR 12 SLAT TRACK LOWER CUTOUT FOUND CRACKED AT XOS 636-643. REPAIR CARRIED OUT AT LH WING FIXED L/E NR 12 SLAT TRACK LOWER CUTOUT, XOS 636-643 AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 19, 2006 · N604FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA03700Frame · crackedSTA 859 LONGERON 6 BETWEEN FRAME AND LONGERON ATTACHMENT HOLE 1, FOUND CRACK. REPAIR CARRIED OUT AS PER E.A.1-5330-103545. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100.Oct 19, 2006 · N522FE · Doug MD11 · Fuselage Main, FrameSDR 06FDEA03687Duct · crackedLT WING FIXED L/E TELESCOPE DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT LT WING FIXED L/E TELESCOPING DUCT CUTOUT AS PER FEDEX EA 1-5730-104808, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 18, 2006 · N604FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA03688Duct · crackedRT WING FIXED L/E TELESCOPE DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING FIXED L/E TELESCOPING DUCT CUTOUT AS PER FEDEX EA 1- 5730- 104809, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.Oct 18, 2006 · N604FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA03542Engine · bird ingestionON ROTATION SUSPECT BIRD STRIKE, MODERATE ENGINE VIBRATION EVM COMP 5.0 CARRIED-OUT BIRDSTRIKE INSPECTION CHECK PER MM 5-52-01-6 1 - SATISFACTORY; THIS ENGINE WAS APPROVED FOR REPLACEMENT. REPLACED THE NR 1 ENGINE AND NOSE COWL.Oct 2, 2006 · N614FE · Doug MD11 · Engine (Turbine/Turboprop)SDR 06FDEA03443Frame · dentedM/D CARGO RT STA 1701 FOUND FRAME DENT. REPAIR CARRIED OUT AT M/D CARGO RH STA 1701 FRAME AS PER SRM 53-30--00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 27, 2006 · N589FE · Doug MD11 · Fuselage Main, FrameSDR 06FDEA03444Frame · dentedM/D CARGO LT STA 1721 FOUND FRAME DENT. REPAIR CARRIED OUT AT M/D CARGO LT BS 1721 FRAME AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 27, 2006 · N589FE · Doug MD11F · Fuselage Main, FrameSDR 06FDEA03445Frame · damagedM/D CARGO LT BS 1701 FOUND DOUBLER SURFACE WITH SCRATCH. REPAIR CARRIED OUT AT M/D CARGO LT BS 1701 FRAME AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 27, 2006 · N589FE · Doug MD11F · Fuselage Main, Plate/SkinSDR 06FDEA03446Seat Track · damagedM/D CARGO SEAT TRACK BS 755, RT X=8.5 FOUND EDGE BROKEN. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Sep 27, 2006 · N589FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03441Wire · burnedLEVEL-1 ALERT TANK 2L AFT PUMP LOW. TANK 2L LT AFT CB POPPED. REPLACED NR 2 L PUMP IAW MM 28-22-01-4 NO HELP. REMOVED ELC TERMINAL FROM R2-56 2X AND CB STAYED IN. REINSTALLED ORIGINAL NR 2 L PUMP IAW MM 28-22-01-4. FOUND ELECTRICAL WIRES BURNED UNDER Sep 26, 2006 · N585FE · Doug MD11 · Fuselage Main, Bulkhead Fuselage wiringSDR 06FDEA2444Blades · damagedDURING DEPARTURE FROM KIX, GOT AMBER BOXED EVM OF 5.0 ACCOMPLISHED BY MODERATE VIBRATION FELT IN AIRFRAME AND RUDDER PEDALS. N1 DROPPED TO 83 PERCENT N2 GOT AMBER INDICATION OF 113.3 EGT WAS IN WARNING RANGE. GOT CONFIRM ENG OUT PROMPT ON MCDU. DID PRECAUTIJun 30, 2006 · N601FE · Doug MD11 · Engine (Turbine/Turboprop)SDR UPS06M46740Cover Plate · leaking20 MINS INTO FLIGHT THE NR 3 ENGINE OIL QTY DROPPED TO 17 QTS AND CONTINUED TO DROP UNTIL TOUCHDOWN AT NRT WHERE IT WAS INDICATING 1 QTS. INITIAL LOSSES AVERAGED 1 QTS EVERY 15 MINUTES. FOUND COVER PAD PLATE OF EDP DEACTIVATE KIT WAS INSTALLED BACKWARD WHEN Apr 22, 2006 · N250UP · Doug MD11F · Turbine Engine Oil SystemSDR UPS06M46750Cover · misinstalledDIVERSION 20 MINS INTO FLIGHT, THE NR 3 ENG OIL QTY DROPPED TO 17 QTS AND CONTINUED TO DROP UNTIL TOUCHDOWN AT NRT, WHERE IT WAS INDICATING 1 QTS. INITIAL LOSSES AVERAGED 1 QT EVERY 15 MINUTES. FOUND COVER PAD PLATE OF EDP DEACTIVATION KIT WAS INSTALLED BACKApr 22, 2006 · N250UP · Doug MD11F · Engine Fuel PumpSDR 06FDEA1172Structure · chafedSNRM N00623 : CENTER CARGO - DOOR CUTOUT AFT LOWER SECTION APPROX FLOOR LEVEL FOUND CHAFED. REPAIRED AS PER SRM 53-50-00.Mar 21, 2006 · N588FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA1173Stringer · crackedSNRM N00606 : HFEC INSPECTION FOUND CRACK ON LT UPPER WING OB END OF STRINGER S-14L APPROX 13 INCHES LONG. REPAIRED AS PER SRM57-20-00.Mar 21, 2006 · N588FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA1174Stringer · crackedSNRM N00604 : HFEC INSPECTION FOUND CRACK ON LT UPPER WING OB END OF STRINGER S-13L APPROX. 1 INCH LONG. REPAIRED AS PER SRM 57-20-00.Mar 21, 2006 · N588FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA1176Skin · crackedSNRM N00719 : RT WING AT STA XOS 908 FIXED LEADING EDGE FOUND CRACKED. CRACK ON RIGHT HAND WING STA XOS 908 FIXED LEADING EDGE REPAIRED AS PER SRM 57-10-00 FIGURE 37 VOLUME I. NR 7 SLAT ASSEMBLY REMOVED AND INSTALLED AS PER AMM 27-80-30-4 AND RANGE OF MOVEMar 21, 2006 · N588FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA1175Doubler · crackedRT WING AT STA XOS 550 LEADING EDGE CAVITY BEADED DOUBLER FOUND CRACKED. CRACK ON RIGHT HAND WING STA XOS 550 LEADING EDGE CAVITY BEADED DOUBLER REPAIRED AS PER FEDEX EA 1-5730-95802, TITLE: WINGS - LEADING EDGE BEADED DOUBLER -PERMANENT REPAIR. THIS REPAMar 21, 2006 · N588FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA1143Bracket · corrodedRT WING OB FLAP IB AFT HINGE BRACKET FWD ATTACHMENT OB CENTER HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-95793. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 17, 2006 · N612FE · Doug MD11 · Wing Main, Frame StructureSDR UPS06M46420Engine · flamed outENG FAILURE, JUST AFTER COMING OUT OF REVERSE THRUST NR 3 ENG FLAMEOUT. VISUALLY INSP'D NR 3 ENG, NO DEFECTS NOTED. RAN ENG, ALL INDICATIONS NORMAL. NO ALERTS. OK FOR SERVICE. HEAVY SNOW ON RNWY AT LANDING.Mar 7, 2006 · N252UP · Doug MD11F · Engine (Turbine/Turboprop)SDR 06FDEA0809Skin · corrodedFWD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN AT STA 899, RT LONGERON, 42R FOUND DAMAGED. DAMAGE AT FUSELAGE FORWARD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN STATION 899 RT LONGERON 42R REPAIRED AS PER SRM 53-50-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AFeb 23, 2006 · N602FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA0810Skin · dentedFWD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN AT STA, 999 RT IN BETWEEN LONGERON 40R AND LONGERON 41R FOUND DAMAGED. DAMAGE AT FORWARD LOWER CARGO DOOR CUTOUT ON FUSELAGE SKIN AT STATION 999 RT IN BETWEEN 40R AND LONGERON 41R REPAIRED AS PER SRM 53-50-00 FIFeb 23, 2006 · N602FE · Doug MD11 · Fuselage Main, Plate/SkinSDR 06FDEA0811Skin · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT ON RT LOWER SKINS PANEL/ACCESS DOOR CUT-OUT BETWEEN STA XORS = 683.4 AND XORS = 713.6 - FASTENER HOLES FOUND CRACK INDICATIONS ON QTY: 02 EA. HOLES. REPAIR CARRIED OUT AS PER FEDEX E.A 1-5710-90773.Feb 23, 2006 · N602FE · Doug MD11 · Wing, Plate/SkinSDR 06FDEA0801Door · crackedRT WING, NR 3 SLAT TELESCOPIC ANTI-ICE LEADING EDGE SPRING DOOR CUTOUT AREA UPPER CORNER WITH APPROXIMATELY ONE (1) INCH CRACKED. COMPLIED WITH FEDEX EA 1-5740-94606.Feb 21, 2006 · N585FE · Doug MD11 · Leading Edge DevicesSDR 06FDEA0403Valve · unknownPDIS: HAD UNSAFE GEAR INDICATION ON ALL 4 GEAR ON BOTH PRIMARY AND SECONDARY INDICATORS. EXECUTED MISSED APPROACH AND COMPLIED W/QRH. GEAR RECYCLED ON OUTSIDE DOWNWIND IAW/QRH AND WE RECEIVED 4 DOWN AND LOCKED INDICATIONS ON PRIMARY AND SECONDARY INDICATORS.Jan 27, 2006 · N594FE · Doug MD11 · Landing Gear Retraction/Extension SystemSDR 06FDEA00023Tape · crackedSNRM NO.: N00556 - CRACK FOUND DURING HFEC INSPECTION AT RT WING TANK AT THE END OF STRINGER 12 (UPPER STRINGER) ARB7512-2.Jan 4, 2006 · N613FE · Doug MD11 · Wing Main, Frame StructureSDR 06FDEA00024Tank · crackedCRACK FOUND DURING HFEC INSPECTION AT RT WING TANK AT THE END OF STRINGER 14 (UPPER STRINGER) ARB7514-2. **S/D COMING**Jan 4, 2006 · N613FE · Doug MD11 · Fuel StorageSDR 05FDEA02597Pump · malfunctionedAT CRUISE FL 340 GOT (HYD 3 ELEV OFF) LEVEL 1 ALERT. NR 3 QTY DECREASED SLOWLY TO 3.2 GAL. THEN GOT (HYD 3 OFF) LEVEL 1 ALERT. PUMPS TURNED OFF AND QUANTY STABILIZED AT 3.6. AFTER SLATS EXTENDED AND GEAR EXTENDED, QUANTITY DECREASED TO 1.2. COMPLIED WITH Aug 23, 2005 · N613FE · Doug MD11 · Hydraulic Pump (Electric/Engine), MainSDR 05FDEA01487Flange · crackedNR 2 ENGINE, WHILE CARRYING OUT FEDEX EA 1-7223-74401 PART 2 ENGINE - AFT FAN CASE T-FLANGE GROUND HANDLING MOUNT CRACK DRILL STOP. FOUND FORWARD T-FLANGE AND AFT T-FLANGE CRACKS PROPAGATED. REPAIRED PER AMM 72-33-00-300-801.May 30, 2005 · N584FE · Doug MD11 · Turbine Engine Compressor SectionSDR 05FDEA01489Case · crackedNR 2 ENGINE, RIGHT HAND CASE APPROXIMATELY TWO O' CLOCK POSITION CRACKED, FOUND ON FLANGE AT BORE COOLING VALVE LOWER FASTENER HOLE. COMPLIED WITH FEDEX EA 1-7223-90165.May 30, 2005 · N584FE · Doug MD11 · Engine (Turbine/Turboprop)SDR 05FDEA01488Case · crackedNR 2 ENGINE, LEFT HAND CASE APPROXIMATELY 7 - 8 O' CLOCK POSITION, FOUND CRACKED. REPAIRED PER AMM 72-33-00-300-801.May 30, 2005 · N584FE · Doug MD11 · Engine (Turbine/Turboprop)SDR 05FDEA00001Engine · leakingENGINE 3 OIL QTY DECREASED TO 8 GALLONS AT 4 HOURS AFTER TAKEOFF. QUANTITY DECREASED TO 4 GALLONS EVEN WHILE USING REDUCED POWER ON THAT ENGINE. DIVERTED THE FLIGHT TO EGSS AND QUANTITY WAS AS LOW AS 1 GALLON ON APPROACH. TEMPERATURE AND PRESSURE WERE NORMADec 31, 2004 · N583FE · Doug MD11 · Turbine Engine Oil SystemSDR 04FDEA03084Hydromech Unit · failed"ENG 3 RPM LOW" ALERT RECEIVED AT START OF DESCENT FROM FL330. EGY NR 3 APPROX 50, FUEL FLOW APPROX 700. NO INDICATEIONS OF ENGINE DAMAGED. COMPLIED WITH QRH PROCEDURES FOR ENG RPM LOW AND ENG RESTART INFLIGHT. ENGINE RESTARTED NORMALLY AND OPERATED NORMANov 11, 2004 · N595FE · Doug MD11 · Fuel Controlling SystemSDR UPS04M43407Pitot Tube · pluggedON T/O AIRSPEED WENT BLANK. F/O SIDE APPEARED NORMAL. THIS WAS ACCOMPANIED BY SEL FLAP LIM OVRD AND SEL ELEV FEEL MAN. NUMEROUS OTHER LIGHTS WERE ILLUMINATED. ACCOMPLISHED CHECKLIST. CAPT'S PITOT PROBE CLOGGED WITH DEBRIS. REMOVED AND REPLACED CAPTS PITOT TOct 26, 2004 · N253UP · Doug MD11F · Pitot/Static SystemSDR 04FDEA02966Structure · corrodedEMPENNAGE, UPPER VERTICAL STAB AT AFT CTR SPAR APPROX ZFR 564 RT EXTRUSION. EXTERIOR SURFACE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX EA 1-5530-81578.Oct 22, 2004 · N602FE · Doug MD11F · Ventral StructureSDR 04FDEA02974Vane · corrodedLT WING IB FLAP VANE, IB TEE FITTING BORES HAVE CORROSION AND AFT HOLE IS NOT WITHIN EO LIMITS. CORROSION REMOVED AS PER SRM 51-21-01 VOL2 AND REPAIRED AS PER FEDEX EA 1-5750-81571.Oct 22, 2004 · N602FE · Doug MD11F · Leading Edge DevicesSDR 04FDEA02925Stringer · crackedSNRM N0896: LT WING UPPER STRINGER (S12) END FOUND CRACKED AT INSIDE ACCESS PANEL 536AB. REPAIR CARRIED OUT AT LEFT HAND WING UPPER STRINGER 12 END AS PER SRM 57-20-00 FIG 10 VOL I. FABRICATED REPAIR ANGLES AS PER SRM 57-20-00 FIG 10 VOL I AND INSTALLED AS POct 12, 2004 · N612FE · Doug MD11F · Wing, Longeron/StringerSDR 04FDEA02898Seat Track · crackedSNRM N0631: MAIN DECK, SEAT TRACK RBL 47.5 CRACKED AT STA 5-53. CARRIED OUT REPAIR IAW SRM 53-70-00 FIG 1 SHT 1 VOL I.Oct 11, 2004 · N612FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02869Relay · defectiveCABIN EMERGENCY LIGHTING NOT ILLUMINATED WHEN SWITCHED (ON). CABIN EMERGENCY LIGHTING TROUBLESHOOTING CARRIED OUT IAW FIM 33-51-00. FOUND RELAY R2-5700 AT FAULT. REMOVED AND REPLACED RELAY R2-5700 IAW STANDARD WIRING PRACTICES. OPERATIONAL CHECK CARRIEDOct 5, 2004 · N585FE · Doug MD11F · Emergency Lighting
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