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 UPS08M51437Longeron Splice · corrodedINSPECTION TYPE:C CENTER CARGO AT STATION 1708 TO STATION 1716 LONGERON 48RT, LONGERON SP SPLICE DOUBLER FOUND CORRODED. CORROSION SPLICES REMOVED PER SRM 51-33-01 VII R35. NEW SPLICES P/N: AF A3113-1 2EA FAB PER DWG AFA3113 AND FASTENERS HOLE PICKUP PER SRMSDR UPS08M51378Support · crackedINSPECTION TYPE:C FWD CARGO/AT STATION 6-74, X+44 AND X-36 TEE SUPPORT FOUND CRACKED. CRACK TEE SUPPORT REMOVED AS PER SRM 51-31-01 V II R 35. NEW TEE P/N: AD FAB PER DWG ADA7667. NEW TEE FASTENERS HOLE TRANSFERED PER DWG ADA7667 AND SRM51-31-01 VII R35. NSDR UPS08M51695Doubler · crackedINSPECTION TYPE:C CENTER CARGO AT STATION 1538 LONGERON 44LT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O PER DAC NDT SPM R13,06-10-01.001 & CRACK FOUND IN 2 AREA, FWD & AFT AS MARKED APPROX 2" IN LENGTH. CRACK SPLICE REMOVED PER SRM 51-33-01 V.II SDR UPS08M51659Splice · crackedINSPECTION TYPE:C CENTER CARGO / AT STATION 1538 LONGERON 51RT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O PER DAC NDTSPM R.13,06-10-01.001 & FOUND CRACK APPROX 1.5" IN LENGTH. CRACK SPLICE REMOVED PER SRM 51-33-01 V.II R.35. NEW SPLICE P/N:A5A71SDR UPS08M51658Splice · crackedINSPECTION TYPE:C CENTER CARGO/AT STATION 1537 LONGERON 46RT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O PER DAC NDT SPM R13, 06-10-01.001 & CRACK FOUND AS MARKED APPROX 2" IN LENGTH. CRACKED SPLICE REMOVED PER SRM 51-33-01 VII R35. NEW SPLICE P/SDR UPS08M51439Longeron Splice · crackedINSPECTION TYPE:C CENTER CARGO/AT STATION 5-120 LONGERON 44RT FOUND SUSPECTED CRACK ON SPLICE DOUBLER. HFEC INSP C/O PER DAC NDTSPM REV 13, 06-10-01.001 & CRACK FOUND AS MARKED APPROX 2 INCHES IN LENGTH. CRACKED SPLICE REMOVED PER SRM 51-33-01 VII R35. NEW SDR WRLA2007133Bracket · brokenAT GEAR RETRACTION SEVERE VIBRATION AND NOISE BELOW FLIGHT DECK. REPLACED BRACKET P/N ACG7075-501 AND NOSE LANDING GEAR AFT DOOR DRIVE LINKAGE P/N ACG7326-1 IAW MM 32-36-02. GEAR SWING ACCOMPLISHED IAW MM 32-31-00-700-801.SDR UPS08M51778Skin · unknownINSPECTION TYPE:C FWD CARGO DOOR CUTOUT AFT EDGE FROM L36-RT L40 FOUND PREVIOUS EDGE BLEND OUT REPAIRS AS MARKED. REPAIR DOUBLERS REMOVED PER SRM 51-31-01 V II R35. HFEC INSP C/O AS PER DAC NDTSPM R13. 06-10-01.001 ON REWORKED AREA AND FOUND NO CRACK EVIDENTSDR UPS08M51777Scuff Plate · misrepairedINSPECTION TYPE:C FWD CARGO DOOR CUTOUT LOWER AFT CORNER DOUBLER UNDERNEATH SCUFF PLATE IS NON-STANDARD REPAIR FORWARD CARGO DOOR CUTOUT AFT SCUFF PLATE REMOVED PER AMM20-50-00. NON-STANDARD REPAIR DOUBLERS REMOVED PER SRM 51-31-01 V.II R35. HFEC INSP C/ O PSDR WRLA2007131Door Frame · damagedDURING C-CHECK INSPECTION FOUND CENTER CARGO DOOR JAMB LOWER AFT EDGE DAMAGED. REPAIRED DAMAGE PER MD11 SRM 53-50-00 FIG.17 VIEW B REF WOA ERA 7-53-62.SDR WRLA2007132Trunnion · crackedDURING C-CHECK INSPECTION FOUND NOSE LANDING GEAR LEFT HAND TRUNNION FITTING CRACKED. REPAIRED LT NOSE LANDING GEAR FITTING PER MD11 SRM VOL.1 53-40-00 REV.40 REF EGAT NRC U05005.SDR WRLA2007130Skin · debondedDURING C-CHECK INSPECTION FOUND LEFT OUTBOARD FLAP TRAILING EDGE OUTBOARD EDGE SKIN DISBOND 33 X 4.5 INCHES. REPAIRED DAMAGE AS PER EGAT EI NO.W2007A57B-710 REV.1 REF EGAT NRC U07001.SDR UPS08M51513Structure · corrodedINSPECTION TYPE:C LT HORIZ STAB NR 6 BARREL NUT HOLE FOUND CORROSIONS. CORROSION AT B-NUT BORE REMOVED. BORE BOTTOM REMAINING BLEND OUT 0.035" DEEP. BORE REAM TO 0.988" DIA REMAIN BLEND OUT DEPTH 0.030" DEEP FOUND EXCEED LMT PER EO MD11-5510-19409-L. 10X MASDR UPS07M51295Skin · crackedINSPECTION TYPE:C LHW L/E LOWER ACCESS STA XORS 538 AT O/B REFUELING RECEPTACLE TOP FOUND CORRUGATED SKIN CRACKED AS MARKED. LHW L/E LWR CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACH PARTS REMOVED. DAMAGED AREA ON BEADED DOUBLER TRIMMED OFF PER SRMSDR UPS08M51550Structure · corrodedINSPECTION TYPE:C HORIZ STAB CONSTANT SECTION RT NR 09 BARREL NUT BORE FOUND WITH CORROSION. CORROSION AT B-NUT BORE REMOVED. BORE BOTTOM REMAINED BLEND OUT 0.030" BORE REAM TO 0.988" DIA, REMAIN BLEND OUT 0.060" FOUND EXCEED LIMITS 10X MAG INSP C/O AND FOUNSDR UPS08M51512Structure · corrodedINSPECTION TYPE:C HORIZ STAB CONSTANT SECTION LT NR 36 BARREL NUT BORE FOUND WITH CORROSION. CORROSION AT B-NUT BORE REMOVED. BORE BOTTOM REMAINING BLEND OUT 0.075" DEEP. BORE REAM TO 2.538" DIA AND REMAINING BLEND OUT 0.080" DEEP, FOUND EXCEED EO MD 11-551SDR UPS07M51347Stringer · crackedINSPECTION TYPE:C RT WING UPPER FUEL TANK STRINGER NR 12 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 12 END FOUND CRACK OF APPROX 8" LONG. STR NR 12 SPLICE END AND LOCK FASTENERS AT REPAIR AREA REMOVED. CRACK AT STR NR 12 SLOT OUT PER SRM 57-20-00 FIG 10 VSDR WRLA2007127Support Beam · corrodedDURING C-CHECK INSPECTION CORROSION FOUND RT WING TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z=-20. REPAIRED THE RT WING TO BODY FAIRING SUPPORT BEAM AT STA Y=1348 Z-20 PER SRM VOL 1 53-00-01 FIG 9 REV 40. REF EGAT NRC U05030.SDR WRLA2007123Seat Track · corrodedDURING C-CHECK INSPECTION CORROSION FOUND RIGHT HAND SEAT TRACK STA Y=555 X=75.25. REPLACED DAMAGED SEAT TRACK PER MD11 SRM 51-33-01 VOL.II REV.40.SDR WRLA2007120Seat Track · corrodedDURING C-CHECK INSPECTION FOUND CORROSION AFT CABIN FLOOR CURVED SEAT TRACK AT STA Y=2007 X =107.25. REF EGAT NRC U05001. REPLACED THE DAMAGED AREA PER MD11 SRM 53-70-00 VOL.I FIGURE 8 REV.40. REF EGAT NRC U05028.SDR WRLA2007121Skin · corrodedDURING C-CHECK INSPECTION CORROSION FOUND ON RIGHT CENTER WING TANK UPPER SKIN AT XCW=110S1. ACCOMPLISHED ENGINEERING INSTRUCTION NO.W2007A57B-668 REV.00, REPAIR CORROSION ON CENTER WING UPPER SKIN UPPER SURFACE AT XCW=110 S1. REF EGAT NRC U05027.SDR UPS08M51418Doubler · corrodedINSPECTION TYPE:C AFT CARGO/AT STATION 1954 LONGERON 51 RT, DOUBLER FOUND WITH SURFACE CORROSION. AFT CARGO STA 1954 L51 RT LONG END SPLICE FASTENERS REMOVED, END SPLICE CORRODED REMOVED, FOUND EXCEEDED LIMIT PER SRM 53-00-01 FIG1 AVIR35. NEW END SPLICE AGA3SDR UPS07M51339Shear Tie · corrodedINSPECTION TYPE:C AFT CARGO/AT STATION 1954 IN BETWEEN LONGERON 49 LT TO 49 RT FRAME SHEAR CLIP FOUND WITH SURFACE CORROSION. AFT CARGO STA 1954 - 1964 L52 (01EA) AND L51 (01EA) EXISTING INTERCOSTAL ALSO REMOVED. EXISTING BRACKETS 05EA REMOVED AT STA 1954 L4SDR WRLA2007128Floor Support · corrodedDURING C-CHECK INSPECTION CORROSION FOUND AFT FUSELAGE FLOOR SUPPORT AT STA Y=2007 X=-23.5. REPLACED DAMAGED SUPPORT PER MD11 SRM VOL II 51-31-01 REV 40. REF EGAT NRC U05025.SDR WRLA2007126Floor Support · corrodedDURING C-CHECK INSPECTION CORROSION FOUND ON AFT FUSELAGE FLOOR SUPPORT AT STA Y=1990 X=27.5. REPLACED DAMAGE SUPPORT PER MD11 SRM VOL.1 51-31-01 REV.40 REF EGAT NRC U05024.SDR WRLA2007125Tee Fitting · corrodedDURING C-CHECK INSPECTION, CORROSION FOUND ON BULKHEAD TEE CHORD STA Y=2007 X=27.5. REPLACED DAMAGE TEE CHORD PER MD11 SRM VOL.II 51-35-01 REV.40 REF EGAT NRC U05014.SDR WRLA2007122Floor Support · corrodedDURING C-CHECK INSPECTION FOUND CORROSION AFT FUSELAGE FLOOR SUPPORT AT STA Y=2007 X=23.5. REPLACED DAMAGED FLOOR SUPPORT PER SRM 51-31-01.SDR UPS07M51289Longeron Splice · crackedINSPECTION TYPE:C CTR CARGO/AT STATION 1535 LONGERON 40 LT FOUND DOUBLER WITH SUSPICIOUS CRACKED AS MARKED. HFEC C/O IAW DAC NDT SRM R13, PT06-10-01.001 ON CRACKED AREA. CRACK CONFIRMED APPROX 1 INCH LONG. CRACKED LONGERON SPLICE REMOVED. NEW SPLICE FAB FRSDR UPS07M51225Longeron · corrodedINSPECTION TYPE:C CTR CARGO AT STATION 5-32 TO STA 5-52 LONGERON 46L 14 EACH FASTENERS FOUND WITH RUSTY NUT AS MARK. CENTER CARGO STA 5-32 TO 5-52 LONGERON 46 LT RUSTY NUTS 14 EA REMOVED PER SRM 51-33-01VIIR35. NEW NUTS 3D0006-3 (14 EA). INSTALLED AT CTR CASDR CO1Y200700009Skin · crackedAT RT AIR CONDITIONING COMPARTMENT AFT DOOR JAMB FOUND 0.25 INCH CRACK ON EXTERNAL SKIN STA 535 L NR32RH.SDR UPS07M51282Seat Track · corrodedINSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK CROWN AT STA1911 AND STA1964 X=107. DAMAGED SEAT TRACK FOUND OUT OF LIMIT PER SRM 53-70-00 FIG 3 (ORG MAT'L: 0.145", REMVD: 0.090") AND REMOVED FROM STA1831 - 2007 X=107 PER SRM 51-31. -01VIIR35. NEW SEAT SDR WRLA2007119Skin · crackedDURING C CHECK INSPECTION FOUND CRACK IN RIGHT HAND NR 3 AIR CONDITION COMPARTMENT DOOR OUTER UPPER SKIN L=4". REF EGAT NRC U05001. REPAIRED RIGHT NR 3 AIR CONDITION COMPARTMENT DOOR OUTER UPPER SKIN PER MD-11 SRM VOL 1 52-10-00 FIG 1 REV 40.SDR UPS07M51291Skin · dentedINSPECTION TYPE:C LT WING I/B FLAP I/B LOWER SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT I/B FLAP I/B SEGMENT REMOVED AND SKIN REMOVED PER SRM 51-35-01VIIR 35. NEW SKIN FAB USING 2.24-T3 0.040" MAT'L PER DOUGLAS DWG ARC2736 REV B. FASTENER HOLES DRILLED SDR UPS07M51290Skin · dentedINSPECTION TYPE:C LT WING I/B FLAP O/B LOWER SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT I/B FLAP O/B SEGMENT REMOVED PER CMM 51-52-03R59. LHW I/B FLAP O/B LOWER SEGMENT SKIN REMOVED PER SRM51-35-01VIIR 35. NEW SKIN FAB USING 2024T3-0.040" MAT'L PER DOUGSDR UPS07M51340Skin · crackedINSPECTION TYPE:C LT WING L/E LOWER ACCESS, 12" O/B OF SLAT TRACK NR 11, FOUND CORRUGATED SKIN CRACKED AT 05 EA PLACES AS MARKED. LHW L/E CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACHED PARTS REMOVED. DAMAGED AREA ON BEADED DOUBLER TRIM OFF PER SRMSDR UPS07M51338Skin · crackedINSPECTION TYPE:C LT WING L/E LOWER ACCESS, IN BETWEEN REFUELING RECEPTACLES FOUND CORRUGATED SKIN CRACKED AT 04 EA PLACES AS MARKED. LT WING REFUELING RECEPTACLE O/B SIDE REMOVED. LT WING L/E CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACH PARTS REMSDR UPS07M51248Structure · corrodedINSPECTION TYPE:C LT HORIZ STAB NR 7 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01V.2R.40.10X MAGNIFICATION DETAILED VISUAL INSP FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUS SSDR UPS07M51244Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB NR 25 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01V.2R.40.10 BY MAGNIFICATION DET VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSDR UPS07M51223Seat Track · corrodedINSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 902 X=27. CORROSION ON SEAT TRACK SECTIONAL TRIM OUT BTWN STA830 - 909, X=27 AND REMOVED PER SRM 51-31-01 VIIR 35. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 ON TRIM OUT AREA AND FSDR CO1Y200700008Hinge · out of limitsON FWD AND AFT CORE COWLS HINGES HAVE BEEN FOUND HOLES OUT OF DWG LIMITS.SDR WRLA2007114Rib · crackedDURING 4C+12A CHECK, FOUND LT OUTBOARD FLAP NR 2 STOP FITTING CRACKED REF EGAT NRC U05061. PERFORMED BOEING SERVICE BULLETIN MD11-57-075, REPLACED DAMAGED RIB REV 00.SDR WRLA2007115Rib · crackedDURING 4C+12A CHECK, FOUND RT OUTBOARD FLAP NR 2 STOP FITTING CRACKED. REF EGAT NRC U05062. PERFORMED BOEING SERVICE BULLETIN MD-11-57-075, REPLACED DAMAGE RIB REV 00.SDR UPS07M51253Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB NR 17 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01V.2R.35. REAM BORE FURTHER TO 1.089:DIAM PER EN1704-07. REAM B/NUT BORE FURTHER TO 1.12 1"DIA PER EN 1704-07. B/NUT BORE BLEND OUT VOSDR UPS07M51247Structure · corrodedINSPECTION TYPE:C LT HORIZ STAB NR 36 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01V.2R.35. BARREL NUT BORE BOTTOM MACHINE DOWN 0.050" DEEPER AND BORE REAM FURTHER TO2.586" DIA PER EN1697-07. B/NUT BORE BLEND OUT VOIDSDR UPS07M51246Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB NR 20 BARREL NUT HOLE FOUND CORRODED CORROSION AT BARREL NUT REMOVED PER SRM 51-21-01V.2R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADISDR UPS07M51243Structure · corrodedINSPECTION TYPE:C LT HORIZ STAB NR 17 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01V.1R.35.10X MAGNIFICATION DETAILED VISUAL INSPECTION C/OUT AND FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PSDR UPS07M51245Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB NR 28 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED PER SRM 51-21-01 V2.R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RSDR WRLA2007113Seat Track · corrodedDURING 4C+12A CHECK, FOUND RIGHT AFT FLOOR CURVED SEAT TRACK HAS CORROSION AT STA Y=2007 X=107.25. PER MD11 SRM VOL.I 53-70-00 FIG. 1 REV.40.SDR UPS07M51252Structure · corrodedINSPECTION TYPE:C LT HORIZ STAB NR 21 BARREL NUT HOLE FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE PER SRM 51-21-01V.2R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RSDR UPS07M51251Structure · corrodedINSPECTION TYPE:C RT HORIZ STAB NR 15 BARREL NUT HOLE FOUND CORRODED. CORROSION AT BARREL BORE REMOVED PER SRM51-21-01 V.2R.35.10X MAGNIFICATION DETAILED VISUAL INSP C/OUT FOUND NO CORROSION EVIDENT. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIU
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