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 07FDEA01598Frame · dentedMAIN DECK CARGO COMPARTMENT, MAIN FRAME STA 1721 AT LONGERON 12L FOUND WITH DENT. [SUP 05-08-07] REPAIRED AS PER SRM 53-30-00 VOLUME I, FIGURE 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01597Vane · misrepairedLEFT WING, INBOARD FLAP VANE LOWER SURFACE FOUND WITH EXISTING REPAIR WHICH IS NOT COVERED BY SRM. [SUP 05-16-07] REMOVED AND REPLACED AS PER AMM 27-50-22-04. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-05. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01596Vane · delaminatedRIGHT WING, INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. [SUP 05-15-07] REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR UPS07M50117Stiffener · crackedINSPECTION TYPE:C LT LE LWR COMPT ACCESS NR 519DB FOUND STIFFENER DOUBLER SUSPECTED CRACK AS MARKED, JUST O/B OF REFUEL PNL NR 519CB. HFEC INSP C/OUT FOUND CRACK APPROX 1/4". LT LE LWR COMPT ACCESS NR 51 9DB CLAMPS REMOVED. DAMAGED AREA AT LT LE LWR COMPT NSDR UPS07M50116Hinge · corrodedINSPECTION TYPE:C RT O/B FLAP I/B AFT HINGE LOWER BORE (02EA) FOUND RUSTY. RT AFT O/B FLAP I/B HINGE PIVOT I/B AND O/B BORE BUSHING REMOVED. SPOT FACE CORROSION REMOVED FOUND EXCEED LIMIT. FPI C/OUT ON REWORK AREA FOUND NO CORROSION AND NO CRACK. REWORK ARSDR 07FDEA01551Fitting · crackedNOSE LANDING GEAR, LEFT TRUNNION FITTING WITH 1.25 INCH CRACKED. [SUP 05-14-07] REPAIRED PER SRM 53-40-00 VOLUME I, FIGURE 23 OPTION 2. COMPLIED WITH FEDEX EA 1-5310-109864. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 07FDEA01546Stringer · crackedCRACK FOUND AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 50L (XORS 152), APPROX 8" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSDR 07FDEA01545Stringer · crackedCRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK FOUND AT STRINGER END 13L (XORS 629), APPROX 14" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPSDR 07FDEA01544Stringer · crackedCRACK FOUND AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 12L (XORS 642), APPROX 4.5" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAISDR 07FDEA01543Stringer · crackedCRACK FOUND AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 10R (XORS 760), APPROX 12.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. RSDR 07FDEA01542Stringer · crackedCRACK FOUND AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 11R (XORS 704), APPROX 9.5" LENGTH ON RIGHT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPSDR 07FDEA01541Stringer · crackedCRACK FOUND AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT WING TANK DURING HFEC INSPECTION. [SUP 05-11-07] CRACK AT STRINGER END 11L (XORS 704), APPROX 13" LENGTH ON LEFT HAND WING TANK REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAISDR 07FDEA01540Skin · crackedLEFT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-11-07] CRACK AT LEFT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57- 10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 07FDEA01539Skin · crackedRIGHT WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT FOUND CRACKED. [SUP 05-09-07] CRACK AT RIGHT HAND WING FIXED LEADING EDGE TELESCOPIC DUCT CUTOUT REPAIRED AS PER SRM 57 -10-00 FIGURE 42 VOLUME I TR 57-8. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR UPS07M50074Rib · deformedINSPECTION TYPE:C RT WING LOWER SURFACE FIXED L/E COMPARTMENT BETWEEN STA XOS 657 AND XO S 714 APPROX FOUND 04 SUPPORT RIB DEFORMED. 4 SUPPORT DEFORMED RIBS REMOVED. NEW SUPPORT RIBS FAB PER DWG ARB2924-8, ARB2924-6, ARB2924-4 AND ARB2930-16. RIBS HEAT TREASDR UPS07M50061Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-128 LONGERON 45 LT FOUND SUSPECTED CRACKED ON DOUBLER AREA AS MARK. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CARGO STA 5-128 L45 LT REMOVED. SDR UPS07M50059Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-128 LONGERON 43 RT FOUND SUSPECTED CRACK ON DOUBLER AREA AS MARKED. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CGO STA5-128 L43RH REMOVED. NEW SDR 07FDEA01508Seat Track · damagedCABIN SEAT TRACK CROWN AREA FOUND CHIPPED OFF AT STA 899 X = -47. CABIN SEAT TRACK AT STA 899 X= -47 CARRIED OUT REPAIR AS PER SRM 53-70-00 VOL I FIG 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR UPS07M50072Web · crackedINSPECTION TYPE:C AFT FUSELAGE COMPARTMENT HAS UPPER TORQUE BOX WEB CRACKED AT STA 2015 APPROX RBL 25 AT MAN HOLE ACCESS CUTOUT STICKER 8344. AFT FX COMPT STA2015 APPROX RBL 25 UPP TORQUE BOX WEB CRACK AREA ATTACHING PARTS REMOVED. HFEC INSP C/OUT FOUND CRACSDR 07FDEA01415Wire · burnedFOUND SEVERAL WIRES AND MOD BLOCKS BURNED AT S3-438 IN CENTER ACCESSORY LT SIDE JUST AFT OF EPC BAY NR 1 AT STA 1136 JUST BELOW FLOOR PANEL. INSPECTED AND REPAIRED DAMAGED WIRES AND MOD BLOCKS PER EA 1-2821-109931 "FUEL SYSTEM REPAIR/INSPECT DAMAGED WIRES". SDR UPS07M50060Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT AT STA 5-128 LONGERON 45 RT FOUND SUSPECTED CRACKED ON DOUBLER AREA. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CGO STA 5-128 L45R REMOVED. NEW SPLICE P/N SDR WRLA2007054Unknown · smokeLAD/IAH AIR TURNBACK DUE TO FLIGHT CABIN CREW REPORTED ELECTRICAL SMOKE AFT OF L2 DOOR LT SIDE ROW 15AV CABINET, F/A'S ISOLATED ELECTRICAL AND ALL SMOKE DISSIPATED. RAN CHECKLIST AND RETURNED TO FNLU. AFTER DOING A SEARCH OF THE SUSPECTED AREA OF CABIN FROM SDR 07FDEA01353Skin · crackedLEFT WING DROOPED LEADING EDGE UPPER SURFACE FOUND CRACKED. [SUP 4-19-07] REMOVED AND REPLACED AS PER AMM 27-80-10. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA01352Seat Track · corrodedMAIN DECK CARGO COMPARTMENT STA 635 RBL 8 SEAT TRACK FOUND WITH CORROSION. [SUP 4-20-07] REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA01222Spar Cap · damagedLT WING, REAR SPAR UPPER CAP XORS 680 HOLE FOUND ELONGATED. [SUP 4-20-07] COMPLIED WITH FEDEX E.A. 1-5710-109851 CLASSIFIED AS MAJOR. REPAIRED IAW FEDEX GMM 6-2-100.SDR UPS07M50058Skin · damagedINSPECTION TYPE:C RHW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. RHW I/B FLAP LWR AFT I/B AND O/B SEGMENTS REMOVED. RHW RELATED PARTS AND I/B FLAP I/B AND O/B SEGMENTS LWR SKINS REMOVED. NEW SKINS FAB PER DWG ARC2736 AND ARC2444. NEW SKINS SDR UPS07M50046Skin · damagedINSPECTION TYPE:C LTW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. LHW I/B FLAP LWR AFT I/B AND O/B SEGMENTS REMOVED. DAMAGED SKIN REMOVED. NEW SKIN FAB PER DWG ARC2736. NEW SKIN PROTECTED, PAINTED AND INSTALLED. LHW I/B FLAP O/B SEGMENT FABSDR 07FDEA01154Unknown · unknownRIGHT MAIN GEAR WOULD NOT RETRACT ON TAKEOFF. LANDED DXB WITHOUT INCIDENT. RT/MLG BUNGEE ACTUATOR REMOVED AND REPLACED AND HYDRAULICS BLED C/O AND LEAK CHECK SATIS AS PER AMM 32-33-02-4. RT MLG TRIM CYLINDER REMOVED AND REPLACED AND BLEED CHECK SATISFACTORISDR WRLA2007048Skin · gougedDURING C-04 CHECK, RIGHT WING NR 8 SLAT INTERNAL SURFACE SKIN GOUGE STATION XOS 1009. REPAIRED PER MD-11 SRM 57-10-00 FIG.=10 VOL.1 REV.38SDR WRLA2007052Seat Track · corrodedDURING C-04 CHECK IN TPE, CORROSION FOUND CABIN SEAT TRACK STA Y=855-860, X=10, Z=-18. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38.SDR WRLA2007051Seat Track · corrodedDURING C-04 CHECK IN TPE, CORROSION FOUND CABIN SEAT TRACK STA Y=460-470, X=-27, Z=-18. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38.SDR WRLA2007053Channel · crackedDURING C-04 CHECK IN TPE, CRACK .55 INCH FOUND ON UPPER HORIZONTAL DECK OF FORWARD AFT FUSELAGE COMPARTMENT AT EMPENNAGE STA Y=2015, X=-14, Z=+61. INSTALLED REPAIR PER MD-11 SRM VOL.I 53-00-01 REV.38 FIG.10SDR 07FDEA00975A/C Pack · contaminatedAT 100KTS ON T/O ROLL RECEIVED LEVEL-3 CABIN SMOKE ALERT. TAKEOFF ABORTED. LIGHT REMAINED ON 3 SECONDS AND NEVER REILLUMINATED. ALL OTHER INDICATIONS OF FIRE NEGATIVE. COMPLIED WITH RTS ON ESC ALL RTS PASS. A/C WAS DEICED PRIOR TO A/C DEPERATURE SUSPECT DSDR WRLA2007047Frame · corrodedDURING C-04 CHECK, CORROSION FOUND AT BULKHEAD TEE CHORD STA Y=2007, Z=20, X=-20. REPAIR PER MD-11 SRM 51-33-01 & 51-35-01 REV.38SDR WRLA2007045Longeron · corrodedDURING C-04 CHECK, FOUND LONGERON L52 CORRODED STA Y=1541. REPAIRED PER MD-11 SRM VOL II 51-33-01 REV.38.SDR WRLA2007044Longeron · corrodedDURING C-04 CHECK, FOUND LONGERON L42R CORRODED STA Y=1953. PERFORM LONGERON REPAIR PER MD-11 SRM VOL.I 53-10-00 FIG.2 TABLE 1 R=5. 2. INSTALLED REPAIR FITTING AND LONGERON PER SRM VOL.II 51-33-01,51-35-01 REV.38.SDR WRLA2007043Longeron · corrodedDURING C-04 CHECK, FOUND LONGERON L40R CORRODED STA Y=1953. PERFORM LONGERON REPAIR PER MD-11 SRM VOL.I 53-10-00 FIG.2 TABLE I R=5. 2.INSTALLED REPAIR FITTING AND REPAIR LONGERON PER MD-11 SRM VOL.II 51-33-01 & 51-35-01 REV.38.SDR 07FDEA00770Frame · dentedFOUND UPPER CARGO COMPARTMENT, RT SIDEWALL FRAME AT STA 1761 INNER CHORD DENTED AT L-12R. UPPER CARGO COMPARTMENT, RH SIDEWALL FRAME AT STA 1761 INNER CHORD DENTED AT L-12R REPAIR CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPETITIVE INSPECTION REQUIRED. ISDR 07FDEA00758Longeron · crackedCTR CARGO BILGE AREA LONGERON 43L SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 43L SPLICE AT STA 1531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00757Longeron Splice · crackedCTR CARGO BILGE AREA LONGERON 49R SPLICE AT STA 1531 SUSPECT CRACKED. CTR CARGO BILGE AREA LONGERON 49R SPLICE AT STA 1531 REMOVED & REPLACED AS PER SRM 51-33- 01 VOL.II. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR WRLA2007042Seat Track · corrodedDURING C-04 CHECK, FOUND SEAT TRACK AREA Y=840-855 X=44 CORRODED. INSTALLED SEAT TRACK AND SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38.SDR WRLA2007046Floorbeam · brokenDURING C-04 CHECK, FOUND FLOORBEAM BULKHEAD BROKEN AT STA Y=1841 X=42. REPAIRED PER SRM VOL.III 53-16-01 REV.38 AND SRM 53-00-01 VOL.I FIG.10 REV.38SDR WRLA2007050Seat Track · corrodedDURING C-04 CHECK IN TPE, CENTER GALLEY AREA SEAT TRACK CORRODED AREA Y=840-850, X=27.5. INSTALLED SEAT TRACK & SPLICE PER MD-11 SRM VOL.II 51-33-01 REV.38SDR WRLA2007049Rib · crackedDURING C-04 CHECK IN TPE, FOUND RT WING FIXED LEADING EDGE SLAT TRACK RIB R16 CRACK .5 INCH XORS:885. REPLACED RIB AND FASTENERS PER MD-11 SRM 51-33-01 VOL.II REV.38.SDR 07FDEA00731Stringer · crackedRIGHT HAND WING TANK - APPROX 15.5 INCHES LENGTH CRACK FOUND AT STRINGER END 14R (XORS 521) DURING HFEC INSPECTION STRINGER END 14R (XORS 521)AT RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PSDR 07FDEA00730Stringer · crackedRIGHT HAND WING TANK - APPROX 13 INCHES CRACK FOUND AT STRINGER END 13R (XORS 577) DURING HFEC INSPECTION STRINGER END 13R (XORS 577)AT RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX SDR 07FDEA00729Stringer · crackedRIGHT HAND WING TANK - APPROX 13 INCHES CRACK FOUND AT STRINGER END 12R (XORS 642) DURING HFEC INSPECTION STRINGER END 12R (XORS 642) RIGHT HAND WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-SDR 07FDEA00728Vane · delaminatedRIGHT HAND WING - INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED COMPLIED WITH FEDEX EA 1-5750-109837, CLASSIFIED AS MINOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 07FDEA00724Stringer · crackedLT WING TANK - APPROX 12 INCHES LENGTH CRACK FOUND AT STRINGER END 14L (XORS 521) DURING HFEC INSPECTION STRINGER END 14L (XORS 521) AT LT WING TANK REPAIR CARRIED OUT AS PER SRM 57-20-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100SDR WRLA2007041Skin · crackedDURING C-04 CHECK FOUND CRACK LT WING FIXED LEADING EDGE ACCESS DOOR CUTOUT BOTH UPPER SIDE XOS:464 TO XOS:470, NR 3 SLAT. PERFORM REPAIR PER MD-11 SRM 57-10-00 FIG 42 VOL 1 REV 38 TR 57-8
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