Mcdonnell Douglas DC-10-10

Service difficulty reports · 3,826

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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 = 'DC1010'
  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 SRXR2015042900001Skin · corrodedCORROSION MAIN CABIN LH SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT BS 1119 TO 1139.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR SRXR20150429010Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE SEAL INSTALLATION BETWEEN BS 1099 TO 1119.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR SRXR20150429009Skin · corrodedCORROSION ON MAIN CABIN RT SIDE WINDOW BELT DOUBLER FROM IMPROPER WINDOW PANE SEAL INSTALLATION AT BS 1681 TO 1701.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Miscellaneous StructureSDR SRXR20150429008Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT BS 1521 - 1561.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR SRXR20150429007Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT STA 1521 TO 1541.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Miscellaneous StructureSDR SRXR20150429006Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 1219 TO 1239.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Miscellaneous StructureSDR SRXR20150429005Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 884 .Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR SRXR20150429004Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 874. REF NRC A011633.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR SRXR20150429003Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 603 REF NRC A011632.Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR SRXR20150429002Skin · corrodedCORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 522Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR SRXR20150429001Skin · corrodedCORROSION FOUND ON LH CABIN WINDOW BELT DOUBLERS AT STA 1139 AND 1179 DUE TO IMPROPER WINDOW SEAL INSTALLATION REF NRC#A011277Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR 2013FA0000705Engine · seizedNR 2 ENGINE HAD SUDDEN SEIZURE, NO FIRE INDICATION, PRECEDED BY LOAD BANG, PERFORMED EMERGENCY PROCEDURES.Aug 15, 2013 · N450AX · Doug DC1010 · Engine (Turbine/Turboprop)SDR VGQY2011011700014Skin · corrodedSKIN CORROSION FOUND ON FRAME STA 1921 LT SIDE - BETWEEN LONGERON 45L-48L. REMOVED CORROSION PER SRM 51-21-01 VOLUME II REVISION 97 AND FOUND EXCEEDED SRM 53-00-01 VOLUME I, FIGURE 1A REVISION 97 LIMITS. TRIMMED-OFF CORROSION AREA PER SRM 53-20-00 VOLUME I FJan 17, 2011 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR VGQY2011011700013Skin · corrodedSURFACE CORROSION FOUND AT FRAME STA 1701 - LONGERONS L 46 & L 47. REMOVED CORROSION AT STA 1701 LONGERON 46L TO 47L PER SRM 51-21-01 VOLUME II REVISION 97 AND FOUND EXCEEDED SRM 53-00-01 VOLUME I, FIGURE 1A REVISION 97 LIMITS. TRIMMED-OFF CORROSION AREA PERJan 17, 2011 · N220AU · Doug DC1010 · Fuselage Main, Plate/SkinSDR VGQY2011011500011Structure · crackedRT HORZ STAB I/B ELEVATOR LOWER O/B FWD EDGE FOUND CRACKED. TRIMMED OUT CRACKED AREA ON RT HORIZONTAL STABILIZER INBOARD ELEVATOR LOWER OUTBOARD FORWARD EDGE AS PER DC-10 SRM 55-10-00 FIGURE 7 VOLUME I REVISION 97. INSTALLED FABRICATED REPAIR DOUBLER AND FILJan 15, 2011 · N220AU · Doug DC1010 · Elevator StructureSDR VGQY2011011500012Structure · corrodedEVIDENCE OF CORROSION ON BOTH STREAKES ON NR 1 ENGINE COWLING EVALUATE CORROSION. COMPLIED WITH EA DC10-7110-1169.Jan 15, 2011 · N220AU · Doug DC1010 · Nacelle/Pylon, Main FrameSDR VGQY2011011500010Spar Cap · corrodedRT HORZ STAB FRONT SPAR INTERIOR LOWER SURFACE FOUND WITH CORROSION AT STA APPROX XE 44 - XE 67. COMPLIED WITH EN 1003-11.Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/RibSDR VGQY2011011500008Retainer · corrodedLEFT LOWER VERTICAL STABILIZER, BELOW AIR INTAKE DUCT FOUND WITH CORROSION AFT OF PANEL 361BL. REMOVED AND DISCARDED CORRODED AJC7331-29 RETAINER. FABRICATED NEW RETAINER PER DWG AJC7331 REQUIREMENTS USING MATERIAL 7075-0-0.125". NEW RETAINER INSTALLED AS PJan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer Miscellaneous StructureSDR VGQY2011011500009Spar Cap · corrodedRT MAIN LANDING GEAR WHEEL WELL - FOUND CORROSION AT OUTER WING REAR SPAR CAP, UPPER SIDE-BOTTOM SURFACE - STA XORS 118.200. COMPLIED WITH EA DC10-5730-1133.Jan 15, 2011 · N220AU · Doug DC1010 · Wing SparSDR VGQY2011011500007Spar · corrodedLT WING INNER REAR SPAR APPROX STA XORS 264 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1131.Jan 15, 2011 · N220AU · Doug DC1010 · Wing SparSDR VGQY2011011500005Balance Weight · crackedLT HORZ STAB O/B ELEVATOR BALANCE WEIGHT AFT EDGE FOUND WITH ONE (1) INCH CRACKED. TRIMMED OUT DAMAGED AREA ON LT HORIZONTAL STABILIZER FAIRING AS PER DC-10 SRM 55-00-01 FIGURE 3 VOLUME I REVISION 97. FABRICATED REPAIR DOUBLER AND FILLER AS PER SRM 55-00-01Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer Miscellaneous StructureSDR VGQY2011011500006Spar Cap · corrodedLT WING INNER REAR SPAR APPROX STA XORS 197 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1132.Jan 15, 2011 · N220AU · Doug DC1010 · Wing SparSDR VGQY2011011500004Spar Cap · corrodedLT HORZ STAB FRONT SPAR LOWER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140.Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/RibSDR VGQY2011011500003Spar Cap · corrodedLEFT HORIZONTAL STAB FRONT SPAR UPPER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140.Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/RibSDR VGQY2011011500002Support Bracket · corrodedUPPER LT WING-TO-FUSELAGE AREA FS 1119 - FOUND 1 EA SUPPORT BRACKET WITH CORROSION. REMOVED AND DISCARDED CORRODED ANB7135-5 ANGLE. FABRICATED NEW ANGLE PER DWG LONG BEACH DWG ANB7135 REV A. NEW ANGLE INSTALLED AS PER DC-10 SRM 51-31-01 REVISION 97 VOLUME IJan 15, 2011 · N220AU · Doug DC1010 · Wing Miscellaneous StructureSDR VGQY2011011500001Skin · corrodedLT HORIZONTAL STAB LEADING EDGE MOST I/B SECTION FOUND INTERNAL STRUCTURE LOWER AND UPPER SURFACE WITH CORROSION. COMPLIED WITH EN 1318-10 AND EA DC10-5510-1130.Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Plate/SkinSDR VGQY2012120100132Spar Cap · corrodedRIGHT HORIZONTAL STABILIZER INTEGRAL LOWER CHORD AND STRINGER NR 1, STA XE 48.500 TO XE 67.333 FOUND WITH EXFOLIATION CORROSION. COMPLIED WITH ORBIS EA DC10-5510-1134.Dec 1, 2010 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/RibSDR 2010F00248Structure · corroded(VGQY) RT HORIZ STABILIZER INTEGRAL LOWER CHORD AND STR NR1, STA XE 48.500 TO XE 67.333 FOUND WITH CORROSION.Dec 1, 2010 · N220AU · Doug DC1010 · Horizontal Stabilizer StructureSDR 2010FA0000040Valve · separatedTHIS IS TO REPORT A LOSS OF NR 2 HYD SYS "PRESSURE AND QUANTITY" PRIOR TO TAKE-OFF, ACFT RETURNED TO GATE. INVESTIGATION FOUND VALVE ASY (M1-164) FOR THE 2-1 NON-REVERSIBLE MOTOR PUMP TO BE AT FAULT. REF IPC 29-12-59, FIG 1, PG 9, ITEM 340, PN 148995-1, SN 3Jan 15, 2010 · N910SF · Doug DC1010 · Hydraulic System, MainSDR FDEA200809123854Skin · crackedLT WING L/E FOUND CRACK ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.Sep 12, 2008 · N10060 · Doug DC1010 · Wing, Plate/SkinSDR 08FDEA03854Skin · crackedLT WING L/E FOUND CRACK ON LOWER EXT SKIN L/E.Sep 12, 2008 · N10060 · Doug DC1010 · Wing, Plate/SkinSDR 08FDEA03636Seat Track · corrodedFOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK AT STA 1923 X=-57, Z=-19. REPAIR IAW SRM 53-70-00 VOL 1 FIG 13 SHEET 1-2.Aug 29, 2008 · N40061 · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR ARWA20080803Windshield · shortedFIRST OFFICER`S WINDSHIELD STARTED ARCING, POWER REMOVED. OUTER PANEL CRACKED, CHECK LIST COMPLETED. REMOVED AND REPLACED FIRST OFFICER`S WINDSHIELD PANEL IAW DC-10 MM 56-11-00, OPERATIONAL CHECK NORMAL. REMOVED AND REPLACED RT WINDOW HEAT CONTROLLER IAW MMAug 29, 2008 · N68041 · Doug DC1010 · Windshield/Door Rain/Ice RemovalSDR 08FDEA03381Access Panel · crackedAFTER REMOVAL ACCESS PANELS OF PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND CRACK ON HORIZ WEB UPPER. REPAIRED CRACK IAW SRM 54-00-01 FIG 2B SHT 2 VOL I.Aug 12, 2008 · N10060 · Doug DC1010 · Nacelle/Pylon, Main FrameSDR FDEA200808083319Frame · corrodedAIR CONDITIONING COMPT PACK NR 1, FOUND EXFOLIATION CORROSION ON CAP ANGLE AND CLIP. REPAIRED AREA IAW SRM 53-00-01 FIG 8 SHT 1, 3, 4 VOL I.Aug 8, 2008 · N10060 · Doug DC1010 · Fuselage Main, FrameSDR 08FDEA03319Angle · corrodedAIR CONDITIONING COMPT PACK NR 1, FOUND EXFOLIATION CORROSION ON CAP ANGLE AND CLIP.Aug 8, 2008 · N10060 · Doug DC1010 · APU Cowling/ContainmentSDR 08FDEA03255Skin · wornRT WING L/E DROOPED FOUND DEEP WEAR ON EXT SKIN. REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 39.Aug 5, 2008 · N10060 · Doug DC1010 · Wing, Plate/SkinSDR 08FDEA03101Skin · crackedDURING INSP OF HORIZ STAB UPPER AND LOWER CONSTANT SECTION SKIN PLANK FLANGE, FOUND 4 PANEL WITH CRACK IN FLYABLE LIMIT, P/N 7208-1, P/N 7207-1, P/N 7205-1, P/N 7204-1, SEE ATTACHED INSPECTION FINDING FORM. REPAIRED AREA IAW EA NR 8-5510-120477.Jul 28, 2008 · N40061 · Doug DC1010 · Horizontal Stabilizer, Plate/SkinSDR FDEA200807233028Seat Track · corrodedDURING INSPECTION AFTER REMOVAL FLOOR PANEL WITH OAN J/C 0600C180-1JR FOUND SEVERE CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 SHT 1-4 VOL I.Jul 23, 2008 · N10060 · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03028Seat Track · corrodedDURING INSPECTION AFTER REMOVAL FLOOR PANEL WITH OAN J/C 0600C180-1JR FOUND SEVERE CORROSION ON SEAT TRACK.Jul 23, 2008 · N10060 · Doug DC1010 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03025Fitting · crackedRT WING OUTBD FLAP CRACK ON FITTING. REPAIRED AREA IAW EA 8-5750-120139.Jul 23, 2008 · N40061 · Doug DC1010 · Trailing Edge FlapsSDR ARWA20080701B-Nut · looseNR 1 HYDRAULIC SYSTEM LOSS PRESSURE AND QUANTITY ZERO. RUDDER STAND-BY POWER OFF, IGHT ON. REPAIRED LINE AND FOUND LOOSE B-NUT AT LT HORIZONTAL STABILIZER TRIM MOTOR. TIGHTENED B-NUT IAW DEIO M/M 20-10-0. PERFORMED OPERATIONAL CHECK, FOUND NORMAL IAW DEIO Jul 17, 2008 · N68041 · Doug DC1010 · Rudder Control SystemSDR 08FDEA02957Skin · crackedLT WING OUTBD FLAP CRACK ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.Jul 17, 2008 · N40061 · Doug DC1010 · Wing, Plate/SkinSDR 08FDEA02836Web · crackedAFTER REMOVAL ACCESS PANEL ON PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND HORIZ WEB WITH CRACKS. REPAIRED CRACKS IAW SRM 54-00-01 FIG 2B SHT 2 & FIG 13 SHT 6 VOL I.Jul 12, 2008 · N40061 · Doug DC1010 · Nacelle/Pylon Miscellaneous StructureSDR 08FDEA02704Bracket · crackedPERFORMED INSP AFTER REMOVAL PANEL RT WING WITH OAN J/C MD10-2780620-1JR FOUND NR 3 CRACKS ON BRACKETS, RT WING DROOPED LEADING EDGE INTERNAL SIDE. REPAIRED AREA IAW SRM 57-00-01 FIG 10 SHT 1 VOL I.Jul 4, 2008 · N40061 · Doug DC1010 · Wing, Attach FittingsSDR 08FDEA02632Skin · crackedLT WING L/E CHORD FIXED PANEL FOUND CRACK. REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL I.Jul 2, 2008 · N40061 · Doug DC1010 · Wing, Plate/SkinSDR FDEA200806302577Skin · corrodedRT WING T/E MODERATE CORROSION ON LOWER SKIN SPOILER NR 2. NO ACTION TAKEN SPOILER WILL BE REPLACED WITH NRC N01190.Jun 30, 2008 · N10060 · Doug DC1010 · SpoilersSDR FDEA200806302576Longeron · corrodedFWD CARGO COMPT TUNNEL AREA FOUND CORROSION WITH EXFOLIATION. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I.Jun 30, 2008 · N10060 · Doug DC1010 · Fuselage Main, Longeron/StringerSDR 08FDEA02577Skin · corrodedRT WING T/E MODERATE CORROSION ON LOWER SKIN SPOILER NR 2.Jun 30, 2008 · N10060 · Doug DC1010 · SpoilersSDR 08FDEA02576Longeron · corrodedFWD CARGO COMPT TUNNEL AREA FOUND CORROSION WITH EXFOLIATION.Jun 30, 2008 · N10060 · Doug DC1010 · Fuselage Main, Longeron/Stringer
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