Douglas DC-10-30F
Service difficulty reports · 1,152
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 = 'DC1030F' 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 = 'DC1030F' 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 22AA201000043Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL FOUND UPPER LONGERON WITH CRACK. NON-ROUTINE NR 393, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW ENGINEERING NOTE (EN) 1006-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2SDR 22AA201000042Skin · wornDURING "C" CHECK , NR 2 ENGINE LT CORE COWL UPPER SKIN FOUND WITH WEAR MARKS. NON-ROUTINE NR 440, WEAR MARKS ON NR 2 ENGINE LT CORE COWL UPPER SKIN AREA REPAIRED IAW EN 1007-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.SDR 22AA201000041Fairing · crackedDURING "C" CHECK, NR 1 ENGINE PYLON FWD FAIRING FWD SIDE FOUND WITH CRACK. NON-ROUTINE NR 224, CRACK AREA AT NR 1 ENGINE PYLON FWD FAIRING FWD SIDE AREA REPAIRED IAW EN 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.SDR 22AA201000040Skin · crackedDURING "C" CHECK, NR 2 ENGINE RT CORE COWL FWD LOWER SKIN FOUND WITH CRACK. NON-ROUTINE NR 439, CRACK AREA AT NR 2 ENGINE RT CORE COWL FWD LOWER SKIN AREA REPAIRED IAW EN 1009-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.SDR 22AA201000039Fairing · crackedDURING "C" CHECK, NR 3 PYLON FWD FAIRING FOUND WITH CRACKED AT 02 LOCATIONS. NON-ROUTINE NR 227, 02 EACH CRACK LOCATIONS AT NR 3 ENGINE PYLON FWD FAIRING AREA REPAIRED IAW 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3, DATED 26 FEB 2010.SDR 22AA201000038Skin · crackedDURING "C" CHECK, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN FOUND CRACK. NON-ROUTINE NR 372, LT WING FIXED L/E AT APPROX STA XFS 675 UPPER INTERNAL SKIN REPAIR IAW EN 1003-10 AND FAA APPROVED FORM 8110-3 DATED 24 FEB 2010.SDR FDEA201002120402Skin · wornLT WING, SLAT NR 2 FOUND DEEP WEAR ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 31, VOL I.SDR FDEA201002080357Skin · dentedEXT FUSELAGE LOWER SURFACE FOUND 1 EA DENT ON SKIN 3" X 1" DEEP .060". (UNDER CUTOUT UPPER CARGO DOOR). REPAIRED SKIN IAW SRM 53-50-00, FIG 6, VOL I.SDR FDEA201002030312Floor Support · corrodedAFT CARGO COMPT BILGE FOUND NR 4 HOLES ON NUTPLATE CORROSION ON ANGLE SUPPORT FLOOR PANEL. REPAIRED AREAS IAW SRM 53-00-01 FIG.9 SH.7 VOL.1SDR FDEA201002030311Skin · wornRT WING L/E SLAT DROOPED FOUND DEEP WEAR ON EXT SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG.4 VOL.1SDR FDEA201002030310Skin · dentedDURING INSP LT HOR STAB INBD ELEVATOR FOUND DEEP DENT 1.50" X 1.50" DEEP.068" ON UPPER SKIN. REPAIRED SKIN IAW SRM 55-10-00 FIG.8 VOL.1SDR FDEA201001290286Skin · crackedRT HORIZ STAB FOUND CRACK ON UPPER SKIN OF DETACHABLE ELEVATORS. REPAIRED SKIN IAW SRM 55-00-01 FIG.3 VOL1SDR FDEA201001280280Frame · corrodedAFT CARGO COMPT BILGE FOUND CORROSION ON CAP FRAME AND FRAME LONGERON. TRMIMED AND REPLACED FRAME SECTION, SPLICE IAW SRM 53-30-00 FIG.5 VOL.1 & 53-00-01 FIG.10 VOL.1 & DWG AGA7125.SDR FDEA201001270271Skin · dentedDURING INSP RT HOR STAB L/E EXT SURFACE FOUND 1 EA DEEP DENT 1" X 1" DEEP .118" ON SKIN ( REMOVED PART ). REPAIRED L/E SKIN IAW SRM 55-10-00 FIG.13 SH.1-2-3 VOL.1SDR FDEA201001250244Web · crackedMAIN CABIN R3 DOOR UPPER JAMB CRACK ON WEB. REPAIRED WEB IAW SRM 53-50-00 FIG.19 VOL1SDR FDEA201001250243Bulkhead · crackedRT MLG WHEEL WELL FOUND CRACK ON HORIZONTAL WEB. REPAIRED IAW SRM 53-00-01 FIG.10 SH.1 VOL.1SDR FDEA201001250242Cargo Track · crackedFWD CARGO COMPT FOUND CRACK ON TRACK. REPLACED TRACK SECTION, USED EXISTING SPLICES IAW SRM 53-70-00 FIG.1 SH.1 VOL.1.SDR FDEA201001250241Cargo Track · crackedFWD CARGO COMPT FOUND CRACK ON TRACK. REMOVED AND REPLACED SECTION OF TRACK IAW SRM 53-70-00 FIG.1 SH.1 VOL.1.SDR FDEA201001250240Frame · crackedRT MLG WHEEL WELL, FOUND CRACK ON FRAME. TRIMMED OUT DAMAGED SECTION OF FRAME IAW SRM 53-30-00 FIG.5 VOL.1. INSTALLED NEW SECTION OF FRAME & SPLICE IAW SRM 53-00-01 FIG.10 SH.5 VOL.1SDR FDEA201001250239Intercostal · crackedMAIN CABIN COCKPIT FOUND CRACK ON HORIZONTAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 53-00-01 FIG.2 SH.2 VOL.1SDR FDEA201001250238Intercostal · crackedMAIN CABIN, COCKPIT FOUND CRACK ON HORIZONTAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 53-00-01 FIG.2 SH.2 VOL.1.SDR FDEA201001250236Skin · crackedDURING INSP OF HORIZONTAL STAB CONSTANT SECTION, FOUND 2 PANELS CRACKED PN 7229-1 POS NR3 & 7226-1 POS NR18, PLEASE VERIFY APPLICABILITY & REVISION OF EO 8-5510-7-4308 IAW SECTION C. ACCOMPLISHED E.A.8-5510-133497 IAW SB DC10-55-016. REMOVED AND REPLACED SDR FDEA201001220219Seat Track · wornMCD CARGO COMPT. SEAT TRACK BETWEEN F.S. 1431 TO F.S. 1531 AT LBL 47.5 HAVE 6 EACH WORN LOBES. REMOVED AND REPLACED SEAT TRACK FROM F.S. 1431 TO F.S. 1531 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, CLASSIED AS MAJOR REPAIR.SDR FDEA201001220217Seat Track · wornMCD CARGO COMPT SEAT TRACK BETWEEN FS 1431 TO FS 1531 AT LBL 47.5 HAS 6 EACH WORN LOBES. REMOVED AND REPLACED SEAT TRACK BETWEEN F.S. 1431 TO F.S. 1531 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, REPAIR CLASSIFIED AS MAJOR.SDR FDEA201001220222Seat Track · wornMCD CARGO COMPT SEAT TRACK AT FS 635 AT LBL 47.5 HAS 1 EACH WORN LOBE. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 AND SRM 57-70-00, SEAT TRACK FABRICATED IAW SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR.SDR FDEA201001220221Seat Track · wornMCD CARGO COMPT. SEAT TRACK BETWEEN FS 1159 TO FS 1259 AT LBL 27.5 HAS 4 EACH WORN LOBES. BLENDED SEAT TRACK AND FOUND OUT OF LIMIT AT STA 1249, REMOVED AND REPLACED SEAT TRACK BETWEEN STA 1239 TO STA 1259 AT LBL 27.5 IAW SRM 51-31-01 AND SRM 53-70-00, SEAT TSDR FDEA201001220220Seat Track · wornMCD CARGO COMPT SEAT TRACK AT FS 795 HAS 1 EACH WORN LUG AT RBL 47.5. REMOVED AND REPLACED SEAT TRACK IAW SRM 57-70-00 AND SRM 51-31-01, SEAT TRACK FABRICATED IAW SRM 53-42-01, REPAIR CLASSIFIED AS MAJOR.SDR FDEA201001220218Seat Track · wornMCD CARGO COMPT. SEAT TRACK AT FS 1391 AT LBL8 HAS 1 EACH WORN LOBE. REMOVED SEAT TRACK IAW SRM 51-31-01, FABRICATED NEW SEAT TRACK IAW SRM 53-42-01 AND SRM 51-00-00-1, INSTALLED SEAT TRACK IAW SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.SDR FDEA201001220214Skin · chafedFUSELAGE EXTERNAL SKIN IS CHAFED AND GOUGED AT LWR CTR CARGO DOOR LWR AFT JAMB BELOW SEAL RETAINER. REPAIRED FUSELAGE EXTERNAL SKIN AT CTR CARGO DOOR LOWER AFT JAMB BELOW SEAL RETAINER IAW SRM 53-50-00.MAJOR REPAIR.SDR FDEA201001210212Seat Track · chafedUPPER CARGO COMPARTMENT BL100R TRACK RAIL, F.S. 745 TO 765 HAS 3 EACH CHAFE MARKS. SEAT TRACK CHAFING MARKS OUT OF LIMITS IAW SRM 53-70-00 FIG.5 MATL LOSS 0.10 AFTER CLEAN-UP. REMOVED SEAT TRACK AND 4EA. FLOOR SUPPORTS FROM STATION 635 TO FS 795, RBL 100 ISDR FDEA201001130100Skin · damagedMAIN CABIN LOCATED AND DRILLED OUT GATELINK ANTENNA DOUBLER IN WRONG POSITION, BTWN LONG NR 2 RT & LONG NR 3 RT IN LIEU OF LONG NR 3 RT & LONG NR 4 RT REF DWG 72749-504. REPAIRED AREA IAW SRM 53-20-00 VOL I, FIG 13.SDR FDEA201001130099Web · crackedMAIN CABIN CRACK ON WEB L3 DOOR LOWER JAMB. REPAIRED CRACK IAW SRM 53-50-00 FIG.19 SH.2 VOL.1SDR FDEA201001110069Intercostal · crackedLT WING L/E FOUND CRACK ON OLD REPAIR OF INTERNAL INTERCOSTAL. REPAIRED INTERNAL INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1SDR FDEA201001110076Skin · crackedRT WING L/E FOUND CRACKS ON SKIN DOUBLER UPPER INT SKIN L/E. REPAIRED BEADED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1.SDR FDEA201001110075Skin · crackedRT WING L/E FOUND CRACK ON DOUBLER UPPER INT SKIN L/E. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110074Skin · crackedRT WING L/E FOUND CRACK ON SKIN DOUBLER UPPER INT SKIN. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110073Skin · crackedRT WING L/E FOUND CRACK ON DOUBLER UPPER INT SKIN. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110072Skin · crackedRT WING L/E FOUND CRACK ON SKIN DOUBLER UPPER INT SKIN L/E. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110071Skin · crackedRT WING LWR SURFACE FOUND CRACK ON SKIN OF WING TIP. REPAIRED SKIN IAW SRM 57-00-01 FIG.4 SH.2 VOL.1SDR FDEA201001110070Skin · crackedRT WING L/E FOUND CRACK ON LWR EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.SDR FDEA201001110068Rib · crackedRT WING L/E FOUND CRACK ON INT RIB L/E. REPAIRED RIB IAW SRM 57-00-01 FIG.10 SH.1 VOL.1.SDR FDEA201001110067Strut · corrodedAFT FUSE WASTE TANK, SEVERE CORROSION ON STRUT. REPAIRED STRUT IAW SRM53-00-01 FIG.9 VOL.1SDR FDEA201001080044Throttle · malfunctionedAFTER TAKEOFF, DURING CLEAN-UP, THROTTLES WOULD CONTINUOUSLY RETARD DUE TO AN UPPER FOOT ON THE PFD LOWERING BELOW PRESENT AIRSPEED. EVEN WITH AUTO THROTTLES OFF, THE THROTTLES WOULD NOT STAY ADVANCED PROBABLY DUE TO THE AIRPLANE TRYING TO PROTECT ITSELF DUE TSDR FDEA200912234511Stiffener · crackedAFT FUSELAGE INT FOUND CRACK ON TEE CAP VERTICAL STIFFENER. REPAIRED AREA IAW SRM 53-00-01, FIG 19, VOL I.SDR FDEA200912234510Beam · crackedFWD CARGO COMPT, FOUND CRACK ON BEAM. PERFORMED REPAIR ON BEAM IAW SRM 53-60-01 FIG.3 VOL.1SDR FDEA200912234509Skin · corrodedDURING INSP LT WING LWR SURFACE FOUND SUSPECT CORROSION UNDER SKIN OF OTBD AILERON AND AROUND HEADS OF FASTENERS. REPAIRED AREA IAW SRM 57-10-00, FIG 85, SHT 3, VOL I.SDR FDEA200912234508Support Angle · crackedDURING INSP, AFT FUSELAGE UPPER ATTIC AREA FOUND CRACK ON ANGLE SUPPORT. REPAIRED AREA IAW SRM 53-30-00 FIG 2B VOL I.SDR FDEA200912234507Bulkhead · dentedDURING INSP AFT FUSELAGE EXT FOUND DEEP NICK ON BULKHEAD SKIN LOWER SIDE. REPAIRED AREA IAW SRM 53-00-01, FIG 10 & SRM 51-00-01, FIG 100, VOL I.SDR FDEA200912234506Frame · crackedDURING INSPECTION CAC INT. FOUND CRACK ON FRAME. REPAIRED FRAMES IAW SRM 53-30-00 FIG.7 VOL.1.SDR FDEA200912224498Panel · crackedLT WING L/E FOUND CRACK ON CHORD FIXED PANEL. REPAIRED L/E LOWER STRINGER IAW SRM 57-10-00 FIG.49 VOL.1.
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