Mcdonnell-Douglas DC-10-10F
Service difficulty reports · 510
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 = 'DC1010F' 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 = 'DC1010F' 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 08FDEA01937Panel · corrodedLEFT WING FUEL TANK PLATE / PANEL 534 CT; INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION; NICKS & GOUGES. REMOVED DAMAGE FROM THE PANEL & FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00; VOL I; PG 217. MACHINED A NEW 534 CT PANEL IAW DAC DWG ARB0872SDR 08FDEA01833Skin · damagedEXISTING EXTERNAL REPAIR DOUBLER AT FIXED L/E STA XIS 150 REMOVE REPAIR AND ACCOMPLISH A NEW IAW SRM 57-10-00 FIG 40 BECAUSE REPAIR DETECTED WAS FOUND WITH A SIGNIFICANT LOSS OF MATERIAL DUE TO A LIP CONTACT.SDR 08FDEA01748Skin · damagedDURING REPAIR ASSESSMENT WAS FOUND AN EXISTING EXTERNAL REPAIR AT FUSELAGE SKIN STA 1019, LONG NR 37R REPAIR FOUND NOT IN CONFORMITY WITH APPROVED DATA AND HAS BEEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6 SH 3 AND 4.SDR 08FDEA01698Web · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR L3 FOUND CRACK 0.5 INCH LONG ON THE WEB UPPER SIDE. PERFORMED REPAIR FOR SRM 53-50-00 FIG 19 VOL. ISDR 08FDEA01637Door Frame · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR R3 FOUND CRACK 0.5 INCH LONG ON THE WEB. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.SDR 08FDEA01636Door Frame · crackedDURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND N2 CRACK TO 2 INCH LONG ON THE WEB LOWER SIDE. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I AND REPLACED CHANNEL P/N AEA0210-40.SDR 08FDEA01635Seat Track · corrodedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK AT STA 502 X= 63, FOUND CORROSION AND SCREW BROKEN. REPLACED TRACK AFA7789-521 FOR DWG AND SRM 53-70-00 FIG 1 VOL I.SDR 08FDEA01633Door Frame · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND CRACK 0.5" LONG ON THE WEB UPPER SIDE REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.SDR 08FDEA01631Seat Track · corrodedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK X -107 STA 1581 TO 1661 FOUND SEVERAL POINT OF CORROSION. REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.SDR 08FDEA01629Seat Track · wornDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK STA 635- 615 X -28, FOUND USURED AND MISSING MATERIAL REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.SDR 08FDEA01478Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1273 AND X -47.250 FOUND MISSING MATERIAL ON SEAT TRACK. REPAIRED SEAT TRACK FOR SRM 53-10-00 FIG 1 VOL I.SDR 08FDEA01441Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1209 X= 47.250 SEAT TRACK WITH MISSING MATERIAL. REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.SDR 08FDEA01440Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE FROM STA 1099 TO STA 1159 ON SEAT TRACK FOUND HOLES OVALIZED REPAIRED FROM SRM 53-70-00 FIG 1 VOL I.SDR 08FDEA01439Seat Track · crackedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1341 X = -75.250 FOUND SEAT TRACK WITH CRACK .5" LONG REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.SDR 08FDEA01438Rib · damagedDURING MD10 ACF MODIFICATION ON SLAT NR 3 RT WING FOUND RIB P/N ARB1666-502 WITH HOLE OVALIZED REPLACED RIB FOR SRM 51-35-01 VOL II AND DWG NRB6027.SDR 08FDEA01424Skin · dentedDURING MD10 ACF MODIFICATION ON LOWER FUSELAGE EXTERNAL FOUND DENT 0.047" BY 2" BY 1.5 INCH LONG ON EXTERNAL SKIN STA 1049 RT SIDE LONGERON 46 TO LONGERON 47. REPAIRED FOR SRM 53-20-00 FIG 6 VOL I.SDR 08FDEA01423Rib · damagedDURING MD10 ACF MODIFICATION ON WING LT SIDE OUTBOARD SLAT NR 3 FOUND RIB P/N ARB1666-501 WITH EA 7 HOLES OVALIZED. REPLACED RIB FOR SRM 51-35-01 VOL II AND DWG ARB1666.SDR 08FDEA01401Frame · crackedDURING MD10 MODIFICATION TO ACF IN AVIONIC COMPARTMENT RT SIDE STA 469 X =-61 FOUND FRAME WITH CRACK 1 INCH REPAIRED FOR SRM 53-30-00 FIG 11 VOL I.SDR 08FDEA01400Floorbeam · damagedDURING MD10 MODIFICATION ACF FOUND IN AFT CARGO COMPT STA 1857 AT X 30 BEAM FLOOR WITH DOUBLE HOLE. REPAIRED FOR SRM 53-60-01 FIG 3 VOL I.SDR 08FDEA01399Seat Track · damagedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA.939 X -47.50 FOUND SEAT TRACK WITH HOLE OVALIZED REPAIRED FOR SRM 53-70-00 FIG 1 VOL I.SDR 08FDEA01331Skin · crackedDURING MD10 ACF MODIFICATION FOUND ON UPPER FUSELAGE AT STA 1305 JAMB DOOR R NR 3 NUMBER 2 CRACK 2 INCHES LONG ON THE WEB IN POSITION LOWER REPAIRED FOR SRM 53-50-00 FIG 19 VOL I.SDR 08FDEA01330Skin Panel · delaminatedDURING MD10 ACF MODIFICATION ON HORIZONTAL STABILIZER RT SIDE FOUND DISBONDING THE UPPER SKIN TIP OUTBOARD ELEVATOR REPLACED SKIN ASSY FOR SRM 51-35-01 AND DWG ALC7347,ALC7348, ALC7602.SDR 08FDEA01297Frame · crackedDURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1781 LT STRINGER 13 FOUND FRAME WITH CRACK 5 INCHES LONG. REPAIRED FOR SRM 53-30-00 FIG 5 SECT.SDR 08FDEA01209Skin · misrepairedDURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-50-00 FIG 26, VOL I.SDR 08FDEA01208Skin · misrepairedDURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS BEEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6, SH 3/4.SDR 08FDEA01187Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "A" AND "D" OF FITTING NR 4 WITH CORROSION (DIAMETER .456") (REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI ANSDR 08FDEA01185Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "C" OF FITTING NR 1 WITH CORROSION (DIAMETER .456"), REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AND INSTALLED BUSHSDR 08FDEA01183Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "C" AND "D" OF FITTING NR 7 WITH CORROSION DIAMETER .456 INCH (REF.E.O. FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDISDR 08FDEA01182Fitting · corrodedDURING MD10 ACF MODIFICATION MAIN CARGO DOOR COVER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B" OF FITTING NR 3 WITH CORROSION (DIAMETER .58") (REF EO FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AND INSTALLED BUSSDR 08FDEA01180Seat Track · corrodedDURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1099 BETWEEN SEAT TRACK X= -78 AND X=-81 FOUND CORROSION ON FLOOR SUPPORT REMOVED CORROSION IS OUT LIMIT THE REWORK. REPLACED SUPPORT FOR DWG ADA3615 AND SRM 51-35-01 VOL II.SDR 08FDEA01151Hinge Bracket · corrodedDURING MODIFICATION MD10 ACF RT OUTBOARD FLAP INBOARD HINGE WITH RUST, BUSHING WITH PLAY AND SHIM WITH OXIDE. REPLACED HINGE FLAP P/N ARC0502-501 FOR DWG ARC0504.SDR 08FDEA01136Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD FLAP OUTBOARD HINGE WITH ATTACH POINTS WITH OXIDE. REPLACED BRACKET ASSY P/N ARC0503-501 FOR DWG ARC0505.SDR 08FDEA01135Hinge Bracket · corrodedDURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD INBOARD FLAP HINGE WITH ATTACH POINT (FWD) RUST AND BUSHING WITH PLAY. REPLACED BRACKET ASSY FOR DWG ARC0504.SDR 08FDEA00998Structure · debondedLT MLG STRUT DOOR; LOWER AFT END HAS THE METAL EDGE PROTECTOR DISBONDING. LT MLG STRUT DOOR WAS REPLACED. ALL WORK WAS ACCOMPLISHED ON N00122.SDR 08FDEA00872Frame · crackedDURING MODIFICATION DC10 CARGO TO MD10 ACF, AT REMOVAL BRACKET IS NOTED CRACK 1.5 INCH LONG ON FRAME STA 1851 RT SIDE LONGERON 10 TO 11. PERFORMED REPAIR FOR EA FEDEX 8-5310-111515.SDR 08FDEA00774Bracket · damagedFOUND ON PYLON NR 3 ON STA YN=240 THE BRACKET WITH DAMAGED AND DO NOT INSTALLED FOR DWG REPLACE WEB FOR SRM 51-33-01 VOL II AND DWG AUB7027.SDR 08FDEA00730Skin · gougedGOUGED INTERNAL SKIN ON PANEL 535GL, ON THE PARTS RACK. REPAIRED INTERNAL SKIN PANEL 535 GL BY REMOVING THE DAMAGE & BLENDING & REMOVING BURRS. FABRICATED REPAIR DOUBLER & BONDED DOUBLER TO THE PANEL. VACUUMED COMPLETING CURE OF BOND & REMOVING EXCESS ADHESSDR 08FDEA00678Fitting · crackedDURING MODIFICATION DC10 FREIGHTER TO MD10 ACF, FOUND IN AIR CONDITION COMPARTMENT NR 3 RT SIDE STA 555 X= -96 Z=-37,50 THE END FITTING FRAME WITH CRACK. INSPECTED AREA AND REPLACED SUPPORT P/N ACA3137-1.SDR 08FDEA00057Skin · crackedOUTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE.SDR 07FDEA04985Longeron · corrodedFWD CARGO COMPT BILGE AREA FOUND CORROSION WITH EXFOLIATION ON LONGERON, REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5.SDR 07FDEA04982Longeron · corrodedFWD CARGO COMPT BILGE AREA FOUND SEVERE CORROSION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 10 VOL I.SDR 07FDEA04981Longeron · corrodedFWD CARGO COMPT SUMP AREA FOUND CORROSION WITH EXFOLIATION, SEE NRC N00315, N00316, N00294, N00253. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 5 SHEET 1.SDR 07FDEA04977Beam · crackedFWD CARGO COMPT BILGE AREA FOUND CRACK ON BEAM. REPAIRED BEAM IAW SRM 53-60-01 VOL I FIG 3.SDR 07FDEA04902Frame · crackedINT CAC CRACK ON FRAME. PERFORMED FRAME REPAIR IAW SRM 53-30-00 VOL I FIG 7.SDR 07FDEA04901Intercostal · damagedLT WING L/E INTERNAL STRUCTURE ON HORIZONTAL INTERCOSTAL EXISTING ANGLE REPAIR. REPLACED INTERCOSTAL IAW DWG ARB2408 AND ARB1333.SDR 07FDEA04900Longeron · crackedFWD CARGO COMPT BILGE AREA FOUND CRACK ON LONGERON, SEE NRC N00293, N00294, N00295, N00297. REPAIRED LONGERON IAW SRM 53-10-00 VOL I FIG 1-2.SDR 07FDEA04859Skin · looseLT WING I/B FLAP UPPER SKIN EXISTING REPAIR. REPAIRED SKIN IAW SRM 57-10-00 FIG 86 VOL I.SDR 07FDEA04856Skin Panel · crackedDURING STB INSP FOUND PANEL P/N 7206-1 AND P/N 7207-1 OF CONSTANT SECTION SKIN PANEL PLANKS, SEE ATTACHED SHEET FOR BEST DETAIL. CRACK IS IN FLYABLE LIMITS. ACCOMPLISHED EA NR 8-5510-99384.SDR FDEA200710244665Seat Track · crackedFOUND 1 CRACK 4 INCH ON SEAT TRACK AT STA 635 X= 67 CUT APPROX AT STA 666 AND 624 AND REPAIR IAW SRM 53-70-00 VOL 1 FIG 1 AND FIG 11.SDR 07FDEA04628Longeron · crackedCTR CARGO COMPT CRACK ON LONGERON. REPAIRED LONGERON IAW SRM 53-10-00 FIG 1-2 VOL I.
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