Mcdonnell Douglas MD-11
Service difficulty reports · 7,956
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 aircraft_model_key = 'MD11' 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.
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 aircraft_model_key = 'MD11' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 07FDEA00497Skin · crackedLEFT WING ANTI-ICING TELESCOPING DUCT DOOR CUTOUT FOUND CRACKED. LT WING ANTI-ICING TELESCOPIC DUCT CUTOUT CRACK REPAIRED AS PER SRM 57-10-00 FIG. 42 VOL.I. (TR) REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00475Longeron · corrodedFORWARD CARGO COMPARTMENT: BILGE AREA LONGERON 52 AT STA 979 UPPER FLANGE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5330-105625, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00465Hinge · corrodedRIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A. 1-5750-107788, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00464Hinge · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A.1-5750-107787, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00463Hinge · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A.1-5750-107786, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00462Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE), CLEVIS ASSEMBLY BORE FOUND CORRODED. REPAIRED AS PER FEDEX E.A.1-5750-107785, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00451Longeron · crackedAFT CARGO COMPARTMENT RT TUNNEL AREA, LONGERON 38R AT STA 1863 FOUND CRACKED. REPAIRED AS PER SRM 53-10-00 VOLUME I, FIGURE 2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00448Longeron · corrodedCENTER CARGO COMPARTMENT BILGE AREA LONGERON 52 AT STA 1531 FOUND CORRODED REPAIR CARRIED OUT PER FEDEX EA 1-5310-105623, FUSELAGE, LONGERON L52 AT STA 5-102, SRM SPLICE CLASSIFICATION. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00450Longeron Splice · crackedAFT CARGO COMPARTMENT, RIGHT TUNNEL AREA LONGERON 38R SPLICE AT STA 1863 FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00449Longeron · corrodedCENTER CARGO COMPARTMENT, BILGE AREA LONGERON 50L AT FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5310-105620, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00447Longeron · corrodedWASTE TANK COMPARTMENT, LONGERON 43R END FITTING AT STA 2007 FOUND CORRODED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR WRLA2007033Skin Panel · crackedFOUND NR 1 PYLON PRECOOLER TORQUE BOX SKIN PANEL GOUGE. PERFORM NR 1 PYLON PRECOOLER TORQUE BOX SIDE SKIN PANEL GOUGE AREA DOUBLER INSTALL REPAIR PER MD-11 SRM VOL 1, 54-00-01 FIG 3 REV:38.SDR WRLA2007034Torque Box · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND ENG 2 RT TORQUE BOX LOWER SIDE CASCADE FWD RING CAP OUTER CRACK APPROX 1" AND DOOR AND CRACK ABOUT 1.5". REF CMM 78-32-35 PAGE 1007 ITEM 121 AND PAGE 1021 ITEM 505. PER ENGINEERING INSTRUCTION NO:W2007A78B-110 REV:00SDR WRLA2007035Torque Box · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND ENG 2 LT TORQUE BOX LOWER SIDE CASCADE FWD RING CAP OUTER CRACK APPROX 1". REF CMM 78-32-35 PAGE 1021 ITEM 505.SDR WRLA2007031Skin · debondedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND LEFT WING OUTBOARD FLAP WEDGE INBOARD SIDE DISBOND ABOUT 4 INCHES. CHECK THE DAMAGE AREA AND CLEANUP. BONDED FIBERGLASS FABRIC USE WET LAYUP AT TEMP 160 DEGREE F, 90 MINS VACUUM;22 INCH/HG CURE PER MD11F SRM VOL 57-SDR WRLA2007032Skin · delaminatedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND RIGHT OUTBOARD FLAP UPPER SURFACE TRAILING EDGE WEDGE IS DELAMINATED. REMOVE RT WING OUTBD FLAP WEDGE. PERFORM THE ENGINEERING INSTRUCTION NO.W2007A57B-095 REV.00, PAGE 1 OF 3 ITEM 1~7, PAGE 2 OF 3 ITEM 8~10. INSTASDR 07FDEA00389Skin · crackedLOWER FUSELAGE EXTERIOR, NR 1 AIRCON EXHAUST CUTOUT CORNER FOUND CRACKED. REPAIRED AS PER SRM 53-50-00 VOLUME I, FIGURE 16. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR WRLA2007038Bracket · crackedDURING 3C+12A CHECK, EGAT MECHANIC FOUND TAIL SECTION STA 2033-2122 TAIL FUEL SYSTEM HAVE BRACKET CRACK AND CLAMP CRACK. REPLACED TAIL FUEL SYSTEM BRACKET AND CLAMP PER AMM 20-05-02 900-801 REV 57.SDR WRLA2007039Panel · wornDURING 3C + 12A CHECK, EGAT MECHANIC FOUND WORN AT RIGHT WING INBOARD AILERON OUTBOARD FIXED PNL FWD ROW FASTENER HOLES STA XORS + 433 TO 480, REAR SPAR. PERFORM RIGHT WING INBOARD AILERON OUTBOARD FIXED PANEL REPAIRED PER ENGINEERING INSTRUCTION W2007A57B-09SDR WRLA2007029Structure · crackedDURING 3C & 12A CHECK, EGAT MECHANIC FOUND CRACK AT NR 3 AIR CONDITION COMPARTMENT DOOR UPPER SIDE CRACK 3". PERFORM NR 3 AIR CONDITION DOOR SKIN CRACK AREA REPAIR PER MD-11 SRM VOL 1 52-10-00 FIG.1 REV:38. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA2007030Support · crackedDURING 3C + 12A CHECK, EGAT MECHANIC FOUND CRACK AT RIGHT W/W NR 3 HYD SYSTEM REGULATOR SUPPORT CRACK 2.5 INCHES. PERFORM RT WW NR 3 HYD SYSTEM REGULATOR INTERCOSTAL SUPPORT CRACK REPAIRED PER ENGINEERING INSTRUCTION NR W2007A53-094 REV:00 & EI NR W2006 P20A-SDR UPS07M49581Seat Track · corrodedINSPECTION TYPE:C CABIN: LEFT SEAT TRACK AT STA 1961, X=107.25 FOUND CORRODED AS MARKED. FASTENERS AT CABIN SEAT TRACK REMOVED SRM 51-31-01 VOL II. DAMAGED AREA TRIMMED OFF SRM 53-70-00 FIG 1 VOL I. HFEC INSP CARRIED OUT & NO CRACK EVIDENT. HOLES ON NEW SSDR WRLA2007028Rib · crackedDURING 3C &12A CHECK, EGAT MECHANIC FOUND CRACK AT L/H WING FIXED L/E SLAT INTERNAL NO. 16 RIB APPROX 05". REMOVED LT WING NR 16 RIB & REPAIRED AREA, WIRE, CLAMP, PULLEY, TRACK AND CABLE PER NR 0028049, ITEM 1&2. REPLACED WITH NEW RIB AT LT WING NR 16 RIB PERSDR WRLA2007027Rib · crackedDURING 3C & 12A CHECK, EGAT MECHANIC FOUND CRACK AT RT WING FIXED LE SLAT INTERNAL NO. 16 RIB APPROX 05". REMOVED RT WING NR 16 RIB, REPAIRED AREA, WIRE, CLAMP, PULLEY, TRACK AND CABLE PER T/C. REPLACED WITH NEW RIB AT RT WING NR 16 RIB PER MD-11 SRM 51-33-01 SDR 07FDEA00366Stringer · crackedCRACK FOUND AT STRINGER END 12R (XORS 642), APPROX 13 INCHES LENGTH ON RIGHT HAND WING TANK DURING HFEC INSPECTION. CRACK ON RIGHT HAND WING (XORS 642) AT STRINGER END 12R REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2SDR 07FDEA00346Stiffener · crackedLEFT WING LEADING EDGE STIFFENER AROUND XORS 690 FOUND CRACKED. LEFT HAND WING LEADING EDGE CRACKED STIFFENER AROUND XORS 690 REPAIRED AS PER FEDEX E.A. 1-5710-107779, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00345Skin · delaminatedRIGHT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REPAIRED AS PER FEDEX EA 1- 5750-107771, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00344Hinge · corrodedCENTER CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.040" REMAINING THK 0.300". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLSDR 07FDEA00343Hinge · corrodedCENTER CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.028" REMAINING THK 0.312". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02.SDR 07FDEA00342Hinge · corrodedAFT CARGO DOOR HINGE AT FUSELAGE SIDE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.020" REMAINING THK 0.320". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. RESDR 07FDEA00341Hinge · corrodedAFT CARGO DOOR HINGE ASSY FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.035" REMAINING THK 0.305". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSISDR 07FDEA00340Hinge · corrodedFWD CARGO DOOR HINGE FOUND WITH CORROSION. REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10- 00 FIG.14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.025" REMAINING THK 0.315". HINGE REMOVED AND NEW HINGE INSTALLED AS PER AMM 20-50-02. REPAIR CLASSIFIED MAJOR SDR 07FDEA00339Hinge · corrodedFWD CARGO DOOR HINGE AT FUSELAGE AREA FOUND WITH CORROSION. CORROSION ON FUSELAGE CARGO DOOR HINGE ASSY REMOVED AND FOUND OUT OF LIMIT AS PER SRM 52-10-00 FIG. 14 VOL.I. ORIGINAL THK 0.340" MATERIAL REMOVED 0.021" REMAINING THK 0.319". HINGE REMOVED AND NSDR 07FDEA00315Frame · damagedCABIN, LEFT STA 535 AT 9G NET FRAME FOUND DAMAGED BY SUPPORT YOKES. CABIN - LEFT HAND STA 535 AT 9G NET DAMAGED FRAME REPAIRED AS PER FEDEX DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA00314Frame · dentedCABIN, LEFT STA 1661 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTION AT 9,500 CYCLES. REPAIR CLASSIFIEDSDR 07FDEA00313Frame · dentedCABIN, LEFT STA 1641 BETWEEN LONGERON 12 TO LONGERON 14 FRAME FOUND DENT. CARRIED OUT REPAIR AS PER SRM 53-30-00 VOLUME I FIGURE 1. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTION AT 9,500 CYCLES. REPAIR CLASSIFIEDSDR 07FDEA00312Hinge · corrodedRIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107782, REPSDR 07FDEA00311Hinge · corrodedRIGHT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON RIGHT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE HOLE REWORKED AND REPAIR CARRIED OUT AS PER FEDESDR 07FDEA00310Hinge · corrodedRIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON RIGHT HAND WING - OUTBOARD FLAP INBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107784, REPAIRSDR 07FDEA00309Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE, WING SIDE, PIVOT BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), PIVOT BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA00308Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, SDR 07FDEA00307Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), FORWARD ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, RSDR 07FDEA00306Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, SDR 07FDEA00305Hinge · corrodedLEFT WING, OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - OUTBOARD FLAP OUTBOARD HINGE (WING SIDE), ACTUATOR ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107783 PT1, REPSDR 07FDEA00304Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107781 PT1, REPAISDR 07FDEA00303Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON LEFT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107781 PT1, RESDR 07FDEA00302Hinge · corrodedRIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED.SDR 07FDEA00301Hinge · corrodedRIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE FOUND CORRODED. CORROSION ON RIGHT HAND WING - INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT INBOARD BORE REPAIRED AS PER FEDEX E.A. 1-5750-107780 PT1, SDR 07FDEA00300Structure · crackedLEFT WING TELESCOPIC DUCT CUTOUT FOUND CRACKED. LEFT HAND WING CRACKED TELESCOPIC DUCT CUTOUT TRIMMED OFF AND REPAIR DOUBLER AND FILLER FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIGURE 42 VOLUME I AND FEDEX E.A. 1-5710-107772, REPAIR CLASSIFIED AS MINORSDR 07FDEA00244Stringer · crackedCRACK FOUND (APPROX 0.5" LONG) DURING HFEC INSPECTION ON RIGHT WING TANK AT THE END OF UPPER STRINGER 44 (XORS 523). CRACK ON RIGHT HAND WING TANK AT THE END OF UPPER STRINGER 44 (XORS 523) REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED
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