Douglas DC-10-30F
Service difficulty reports · 1,152
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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 = '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 WRLA2006004Attach Fitting · corrodedWHILE PERFORMING INSPECTION OF THE FLAP SUPPORT ATTACH FITTINGS DURING A5 CHECK, FOUND CORROSION ON THE RIGHT WING INBOARD FLAP SUPPORT FITTING HOLE. REWORKED AND REPAIRED HOLE PER ERA 06-57-09 AND MM57-44-07, INSPECTED REPAIRS ALL NORMAL.SDR WRLA2006003Attach Fitting · corrodedWHILE PERFORMING INSPECTION OF THE FLAP SUPPORT ATTACH FITTINGS DURING A5 CHECK, FOUND CORROSION ON THE LEFT WING OUTBOARD FLAP SUPPORT FITTING HOLE. REWORKED AND REPAIRED HOLE PER ERA 06-57-09 AND MM57-44-07, INSPECTED REPAIRS ALL NORMAL.SDR WLRA2006002Fitting · corrodedWHILE PERFORMING INSPECTION OF THE FLAP SUPPORT ATTACH FITTINGS DURING A5 CHECK, FOUND CORROSION ON THE LEFT WING INBOARD FLAP SUPPORT FITTING HOLE. REWORKED AND REPAIRED HOLE PER ERA 06-57-09 AND MM57-44-07, INSPECTED REPAIRS ALL NORMAL.SDR 06FDEA0100Spring · unknownFOUND CARTRIDGE SPRING ASSY ITEM 820 P/N ARH 1694-1 WITHOUT EO# 8-2780-7-4308 APPLICABLE. ACCOMPLISHED EO# 8-2780-7-4308 P1 ATTACHED, IN CONJUNCTION WITH NRC FEDEX, N00263/F160263.SDR 06FDEA0099Skin · crackedRT WING OUTBOARD FLAP FOUND 6 CRACKS ON UPPER SKIN FROM STA XOF 543 TO STA XOF 575. BURNICHED AND BLENDED INTERESTED AREAS IAW SRM 57-00-01 FIG 1A SHT 3 VOL 1, CONFIRMED 4 CRACKS STA 549 1 CRACK LONG .300" AT STA 564 FOUND 3EA CRACKS FOR TOTAL LONGEST 1" WOSDR 06FDEA0098Repair · unknownFOUND LT WING SLAT NR 2 INT SKIN FOUND A FLUSH REPAIR DIM 5" BY 4.75" BY 5" XORS 264. REMOVED SLAT NR 2 LT, AND EXISTING REPAIRS, TRIMMED OUT PORTION OF INNER SKIN. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161061-3/N01061-3, F161061-5/N01061-5, F161061-7/SDR 06FDEA0097Structure · crackedLT WING L/E FOUND 1 CRACK 1" LONG ON CHORD FIXED PANEL AT STA XORS 798. REPAIRED STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F160724-3 IAW SRM 57-10-00 FIG 49 VOL 1.SDR 06FDEA0096Repair · unknownPERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P1 FOUND DOUBLER DIMENSION 4" BY 3" RT EXTERNAL FUSELAGE STA 357 LONG 31. PERFORMED INSPECTION ON REPAIR DOUBLER IAW EA NR 8-5330-93226 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P1 E3, TREATESDR CLC2006F00000Door · damagedWITH LANDING GEAR RETRACTION OUT. RT MAIN GEAR INDICATES STAYED RED. DIVERTED, INVESTIGATION FOUND SEQUENCE VALVE CABLE BROKEN, CAUSING RT MAIN GEAR DOOR DAMAGE, AND TIRE DAMAGE. (K)SDR 05FDEA04272Repair · misinstalledDISCREPANCY PERFORMED INSPECTION IAW EO 8-5100-7-5001-1P FOUND 1 DOUBLER DIMENS 13" BY 10" RT EXT FUSELAGE STA 665 LONG 41. REMOVED DOUBLER IAW SRM 51-30-00 AND SRM 51-35-02 STRIPPED PAINT IAW SRM 51-21-01 VOL 2. REMOVED FINGER DOUBLER EXTERNAL IAW SRM 51-3SDR 05FDEA04271Repair · unknownFWD LOWER CARGO DOOR FOUND EXTERNAL DOUBLER FROM STA 885 TO STA 959 DIM 11 X 12 INCHES. REMOVED AND REPLACED REPAIR IAW SRM 52-10-00 FIG 6 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F161770-3, DOUBLER IAW SRM 52-10-00 FIG 6 VOL 1.SDR 05FDEA04270Repair · unknownPERFORMED INSPECTION IAW EO# 8-5100-7-5001-1D FOUND DOUBLER LENGTH 12" WIDTH 9" ON TOP INTERNAL BULKHEAD NLG AT STA 560 Z-38 X11. NO ACTION TAKEN IAW EO NR 8-5100-7-5001 P1 E3 ATTACHMENT "A" NOTE 3 TREATED AND PRIMED AREA IAW SRM 57-21-01 VOL 1.SDR 05FDEA04269Intercostal · crackedFWD CARGO COMPT AT STA 879 RT AT LONG 39 AFTER REMOVAL INTERCOSTAL WITH N/R C40124 FOUND ON STRUT 1 CRACK 2.50" LONG. REMOVED PLATE IAW SRM 51-33-01 PAGE 34/47 VOL 2. TRIMMED OUT CRACKED FLANGE. FABRICATED PART IAW DETAIL PART TRAVELER F161706/3 IAW SRM 53-SDR 05FDEA04243Fitting · failedREMOVED NR 2 ENG REF W/C 71T1101 WHILE LOWERING ENGINE AFT LT MOUNT BROKE, TEARING WEB AND CRACKED ANGLES ALSO BOTH T/R HALVES DAMAGED. TURNED OVER TO DAY SHIFT FOR FURTHER EVALUATION. REPLACED WEB AND FITTINGS AS REQUIRED REF DWG AVB7318 AND SRM 51-00-01 SDR 05FDEA04142Repair · damagedDISCREPANCY IN THE UPPER SURFACE OF RT DETACHABLE ELEVATOR AT STA XE 80 FOUND 1EA REPAIR DOUBLER 3.5 INCH DIA. PERFORMED A GVI OF REPAIR IAW SRM 55-00-01 FIG 3 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P, RESTORED PAINT ON STRIPSDR 05FDEA04140Repair · unknownLEFT OUTBOARD ELEVATOR REPAIR ASSESSEMENT FOUND 1EA EXT DOUBLER ON LOWER SIDE AT XE 345 DIMENIONS 7 X 4.5 INCH. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3. RESTOREDSDR 05FDEA04139Repair · unknownRIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON UPPER SKIN AT STA XIFH 236 DIMENIONS 3.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P. RESTORED PAINT ON STRIPPED AREA IASDR 05FDEA04138Repair · unknownRIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 189 DIMENIONS 8.5 X 5 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2. RESTORED PAINT ON STRIPPED AREA ISDR 05FDEA04137Repair · unknownRIGHT WING INBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XIFH 155 DIMENIONS 3.25 INCH. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-2P E3. RESTORED PAINT ON STRIPPED AREA IASDR 05FDEA04135Repair · unknownINBOARD LT ELEVATOR UPPER SIDE FOUND 1 EXTERNAL DOUBLER REPAIR DIA 3" AT XE 160. PERFORMED INSPECTION OF REPAIR DOUBLER IAW SRM 55-00-01 VOL 1 FIG 3. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED AREA IAW SDR 05FDEA04136Repair · unknownFOUND UPPER INBOARD LT ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR BETWEEN XE 240 AND XE 191 DIMENS. 45" BY 8". PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2, RESTORED PAINSDR 05FDEA04134Repair · properUPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 70 DIMENSION 4" BY 3.5". PERFORMED INSPECTION ON DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPESDR 05FDEA04133Repair · properUPPER LT DETACHABLE ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 60 DIMENSION 7" BY 6.5. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 VOL 1 FIG 8 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EONR 8-5100-7-5001 P2 E3, RESTORED PAINT ON STRIPPED ARSDR 05FDEA04132Repair · properDISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P1 FOUND DOUBLER DIMENS 14" BY 4" RT, EXTERNAL FUSELAGE STA 959 LONG 40 TO LONG 42. PERFORMED A GVI OF REPAIR IAW SRM 53-50-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100SDR 05FDEA04130Repair · properDISCREPANCY PERFORMED INSPECTION IAW EO NR 8-5100-7-5001-P2 FOUND DOUBLER DIMENS 12" BY 7.5" EXTERNAL FUSELAGE AT STA 1370 LONG 51 RT TO 51 LT. PERFORMED A GVI OF REPAIR IAW SRM 53-40-00 FIG 20 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-51SDR 05FDEA04129Repair · properDISCREPANCY LT WING INBOARD FLAP FOUND A FLUSH DOUBLER 7.75" BY 4.75" ON LOWER SKIN AT STA XIFH 133. PERFORMED A GVI OF REPAIR IAW EA NR 8-5710-90133 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 AND TREATED STRIPPED AREA IAW SRM 51-21-SDR 05FDEA04128Repair · properDISCREPANCY IN THE AFT FUSELAGE SECTION ZONE 316 AT STA Y 2140 FOUND 1 REPAIR ANGLE ON THE FRAME'S CAP AT X10 SIZE 10" X 2.5". PERFORMED A GVI OF REPAIR IAW SRM 53-30-00 VOL 1 FIG 2 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2D E3, RSDR 05FDEA04127Repair · properLT WING INBOARD FLAP FOUND A DOUBLER 8" BY 1" ON UPPER SKIN AT STA XIFH 147.300. PERFORMED A GVI OF REPAIR IAW SRM 57-20-00 FIG 11 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 RESTORED PAINT ON STRIPPED AREA IAW SRM 51-21-01 VSDR 05FDEA04126Repair · properLT LOWER INBOARD ELEVATOR FOUND 1 EXTERNAL DOUBLER REPAIR AT XE 243 DIMENS 17" BY 6". PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2 E3 RESTORED PAINT ON STRIPPED AREA SDR 05FDEA03964Duct · chafedNR 1 ENG HIGH PRESSURE CONTROL VALVE CHAFING INTO 7TH STAGE AIR PRESSURE TURBINE CONTROL LINE. REMOVED 7TH STAGE COOLING TUBE, PER DC10-30 MM 75-22-00-02. REPAIRED DUCT PER EM 72-09-03. REINSTALLED DUCT AND HIGH PRESSURE VALVE. PERFORMED OPS AND LEAK CHECKSDR 05FDEA03928Frame · crackedNR 1 ENG NOSE INLET COWL INTERIOR AFT BULKHEAD CHORD ANGLE IS CRACK AT 7 O`CLOCK POSITION CAN BE VIEWED FROM OUTBOARD SIDE. REMOVED AND REPAIRED CRACKED CHORD ANGLE IAW DC10 SRM 54-11-00 FIG 1C VOL 1. N/R N00405, W/O N/R 00030375.SDR 05FDEA03903Indication Sys · malfunctionedOAK - LEFT MAIN GEAR UNSAFE IN UP POSITION ON BOTH MAIN GEAR INDICATOR AND SYNOPTIC DURING DESCENT. ACCOMPLISHED RED TAB PROCEDURES, BOTH INDICATIONS NML. INTERROGATED CFDS FOUND PSEU LT GEAR UP AND LATCHED A/B SENSOR DISAG INTER. FAULT MSG(317075) FAULT CSDR 05FDEA03820Angle · crackedFOUND CENTER ACCESSORY COMPARTMENT FOUND 1 CRACK 3'' LONG ON T ANGLE, FRAME TO BULKHEAD ATTACH AT STA 1156 Z-29 X-107 RT SIDE. REMOVED FASTENERS FROM AEA0159 FRAME IAW SRM 51-33-01 PAG 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160433-3 SPLICE PLATE,SDR 05FDEA03810Repair · properLT HORIZONTAL STABILIZER T/E FOUND NR 1 OLD REPAIR ON UPPER SURFACE AT XE 99.195. THE MEASURE 24'' LONG 5.5'' LARGE. PERFORMED INSPECTION ON SKIN REPAIR DOUBLER IAW EA NR 8-5510-63525, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.SDR 05FDEA03809Repair · properFOUND UPPER FUSELAGE LT SIDE FOUND DOUBLER REPAIR ON EXTERNAL SKIN AT STA 775 FROM LONG 23 TO LONG 24 Z 5. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 53-50-00 FIG 9 VOL 1 FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P1.SDR 05FDEA03808Repair · properFOUND UPPER FUSELAGE NR 2 LT DOOR FOUND EXTERNAL DOUBLER AT STA 808. PERFORMED INSPECTION ON REPAIR DOUBLER IAW SRM 52-10-00 FIG 12A VOL 1. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.SDR 05FDEA03807Repair · properLT WING SLAT NR 1 ON INT SKIN FOUND 1EA FLUSH DOUBLER 22'' BY 22'' AT STA XORS 80. PERFORMED INSPECTION ON SLAT NR 1 REPAIR DOUBLER IAW EA NR 8-5710-90122. FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 E3 P2.SDR 05FDEA03800Repair · undamagedPERFORMED INSPECTION IAW EO NR 8-5100-7-5001 1D P1 FOUND 3EA DOUBLER REPAIR DIMENSION 9'' BY 8'' ON INTERNAL FUSELAGE SKIN AT STA 275 TO 300 LONG 36 LT. PERFORMED INSPECTION ON REPAIR FRAME AND SKIN IAW EA NR 8-5310-46689 FOUND IN COMPLIANCE WITH CRITERIA RSDR 05FDEA03768Spar · crackedRT WING, TRAILING EDGE HAS A TWO INCH LONG CRACK IN FITTING AT XORS, 14 INCHES AFT OF INNER REAR SPAR. REMOVED AND REPLACED SUPPORT FITTING ARCO472-42, ( PO# 509448.1) IAW DC10-30 SRM 51-33-01 VOLII. TIMCO MECHANIC 7921, QC INSPECTOR #QC35.SDR 05FDEA03660Pressure Panel · crackedRT MLG WHEEL WELL 2EA CRACKS ON VERTICAL WEB AT STA 1485 X-95 OUTBOARD SIDE. REPAIRED IAW SRM 53-50-00 FIG 2A. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F161133-29 REPAIR WEB, F161133-3 FILLER (QTY 2), F161133-31 STRAP, F161133-31A STRAP AND F161133-31B STRSDR WRLA2005146Engine · overheatedBRU-DAY DIVERSION TO YYZ BECAUSE OF NR 1 ENGINE HIGH EGT AND HIGH FUEL FLOW. BEGINNING/DURING DESCENT INTO YYZ THE ENGINE FIRE WARNING BEGIN FLICKERING LIGHT AND ENGINE WAS SHUTDOWN PER ENGINE FIRE/FAILURE CHECKLIST. FLICKERING LIGHT WAS IN FIRE HANDLE AND SSDR 05FDEA03613Skin · dentedRIGHT WING INBOARD FLAP HAS SPEED TAPE (LINE REPAIR) AFT OF NR 7 TIRE. REMOVED TEMP REPAIR AND REPAIRED SKIN IAW DC10 SRM 57-10-00 VOL I AND FEDEX EA 8-5750-91110 PART 3. P3 MOD TYPE T MOD REV NO A PS P3. EA IS ATTACHED TO WORK CARD 57501429, WORK ORDER 000SDR CLC2006F00005Switch · malfunctionedON APPROACH THE FLAP/SLAT HANDLE ON EXTENSION HAD SLAT DISAGREE LIGHT (ON). WENT TO ABNORMAL CHECK LIST A-5-1, AND A-5-9, AND COMPLIED WITH SAME. EMERGENCY WAS DECLARED. LANDING AT DESTINATION UNEVENTFUL. FINDINGS: RT GROUND SENSING SWITCH BAD. REPLACED RSDR 05FDEA03566Doubler · crackedFOUND DOUBLER LENGTH 8.5 INCH WIDTH 6 INCHES ON RT EXTERNAL FUSELAGE AT STA 885 FROM L 31 TO L32. REMOVED AND REPLACED REPAIR IAW SRM 53-50-00 FIG 8 AND FEDEX EA NR 8-5350-88889 FAB PARTS IAW DETAIL PARTS TRAVELER F160357-1 AND F160357-2 IAW SRM 53-50-00 FIG SDR 05FDEA03544Rib · crackedLEFT WING L/E ON INTERNAL STRUCTURE FOUND 1 CRACK 0.50'' LONG ON RIB AT STA XORS 427. PERFORMED INSPECTION IAW NDT SRM 06, NO CRACK FOUND ON RIB AT STA XORS427 LT WING L/E ONLY PENCIL MARK.SDR 05FDEA03543Frame · corrodedFWD CARGO COMPT UNDERFLOOR SUMP AREA AT STA 959 FOUND SEVERE CORROSION WITH EXFOLIATION ON THE FRAME'S CAP BETWEEN L51 RT TO L51 LT. CUT AND REMOVED SECTION OF FRAME CAP IAW SRM 51-35-01 PAGE 1-13. FAB PART IAW DETAIL PART TRAVELER F160315-3 REPAIR SPLICE ANSDR 05FDEA03542Attach Fitting · corrodedFWD CARGO FOUND STA 595 LT SIDE X-95 CORROSION ON POTABLE WATER SYSTEM ATTACHMENT. ACCURATELY POLISHED AREA ON SUPPORT AND BULKHEAD IAW MM 12-22-01-7 PERFORMED VISUAL INSPECTION ON AREA FOUND LIGHT CORROSION ON SUPPORT CLAMP REMOVED CORROSION IAW SRM 51-21-SDR 05FDEA03538Structure · corrodedIN THE CENTER CARGO COMPT BILGE SUMP AREA AT STA 1781 BETWEEN L 51 RT TO L 51 LT. FOUND MODERATE CORROSION ON THE FRAME'S CAP. REMOVED CORROSION IAW SRM 51-21-01 PAR 34 VOL 2. ORIGINAL THK MATERIAL IS .071'', AFTER REMOVED MATERIAL FOUND THK .042''. MATERISDR 05FDEA03537Frame · damagedMAIN CABIN AT STA 959 LT AT L6 DURING REM/INST STAND OFF PER J/C SP10240303-7003-17F FOUND ON FRAME EXISTING HOLE OVALIZED (1/4 INCHES DIA). CUT OUT DAMAGED AREA OF FRAME FABRICATED PARTS IAW DETAIL PART TRAVELER F161528-1 REPAIR ANGLE IAW SRM 53-30-00 FIG 13SDR 05FDEA03536Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 2 EA CRACKS 0.25" LONG ON SKIN AT STA XOF 787. TRIMMED OUT DAMAGE SKIN INSTALLED DOUBLER AND FILLER IAW SRM 57-10-00 FIG 85 COLD BOND IAW SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3/9. FABRICATED PARTS IAW DETA
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