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 05FDEA03535Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 0.50" LONG ON SKIN AT STA XOF 563. TRIMMED OUT DAMAGE SKIN FABRICATED FILLER DOUBLER AND INSTALLED PER SRM 57-10-00 FIG 85 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER SDR 05FDEA03534Rib · crackedLEFT WING L/E INT STRUCTURE FOUND 1 EA CRACK 1" LONG ON RIB AT STA XORS 676. REPAIRED L/E FORMER PER SRM 57-20-00 FIG 1 SHT 3 VOL 1. INSTALLED REPAIR ANGLE-31 PER SRM 51-35-01 PAGE 1-13 AND SRM-51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER FSDR 05FDEA03533Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 EA CRACK 3" LONG ON SKIN AT STA XOF 557. TRIMMED OUT DAMAGE SKIN INSTALLED FILLER DOUBLER PER SRM 57-10-00 FIG 85 AND SRM 51-35-01 PAGE 1-13 COLD BOND PER SRM 51-71-00 PAR 16C VOL 2. FABRICATED PART IAW DETAIL PART SDR 05FDEA03532Doubler · crackedRT WING INT L/E, CRACK LONG 0,5" ON INTERNAL DOUBLER AT STA XORS 540. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160799/N00799 PER SRM 57-10-00 FIG 7SDR 05FDEA03531Panel · crackedRT WING INT L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 803. REPAIRED STRINGER DOUBLER PER SRM 57-10-00-00 FIG 49 VOL 1 AND SRM 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F161054/N01054 PER SRM 57-10-00 FIG 49 VOL 1.SDR 05FDEA03530Rib · crackedLEFT WING L/E INT STRUCTURE FOUND 1 CRACK 0.25" LONG ON RIB AT STA XORS 516. REPAIRED L/E FORMER PER SRM 51-20-00 FIG 1 SHT 6 VOL 3 AND SRM 51-33-01 PAGE 34-47.SDR 05FDEA03529Doubler · crackedRT WING INT L/E, 3EA CRACKS ON DOUBLER AT STA XORS 685.REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PART IAW DETAIL PART TRAVELER F160836/N00836 PER SRM 57-10-00 FIG 71 VOL 1.SDR 05FDEA03528Rib · crackedFOUND LT WING L/E INT STRUCTURE FOUND 1 EA CRACK 0.50" LONG ON RIB AT STA XORS 523. REPAIRED RIB PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-33-01 PAGE 34-47.SDR 05FDEA03527Doubler · crackedLT WING L/E INT STRUCTURE FOUND 1 EA CRACK 0,5" ON UPPER DOUBLER AT STA XORS 683. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160726/N00726 PER SRM 57-10SDR 05FDEA03526Skin · crackedRT WIND INT L/E, CRACK LONG 1, 5" ON RIB AT STA XOS 450. REPAIRED CRACK PER SRM 57-20-00 FIG 1 SHT 3 VOL 1 AND SRM 51-35-01 PAGE 1-13 AND 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160840/N00840 PER SRM 57- 20-00 FIG 1 SHT VOL 1.SDR 05FDEA03524Doubler · crackedLT WING L/E INT STRUCTURE FOUND 1 CRACK 5" LONG ON UPPER DOUBLER AT STA XORS 660. REPAIRED BEADED DOUBLER PER SRM 57-10-00 FIG 71 VOL1 AND SRM 51-35-01 PAGE 1-13 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160729/N00729 PER SRM 5SDR 05FDEA03523Rib · crackedLT WING L/E INT STRUCTURE FOUND 1 CRACK 0.25" LONG ON RIB AT STA XORS 770. REPAIRED FORMER PER SRM 57-20-00 FIG 1 SHT 6 VOL 1 AND SRM 51-35-01 PAGE 1 3 AND SRM 51-33-01 PAGE 34-47.SDR 05FDEA03522Panel · crackedFOUND RT WING L/E, CRACK ON CHORD FIXED PANEL AT STA XORS 442. INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 49 AND SRM 51-33-01 PAGE 34-47. FABRICATED PARTS IAW DETAIL PART TRAVELER F160798/N00798 PER SRM 57-10-00 FIG 49.SDR 05FDEA03521Rib · crackedLT WING L/E INTERNAL STRUCTURE FOUND 1 CRACK 0.50" LONG ON RIB AT STA XORS 490. REPAIRED RIB IAW SRM 57-20-00 FIG1 SHT 6 VOL 2 AND SRM 51-33-01 PAGE 34-37.SDR 05FDEA03520Skin · crackedLEFT WING OUTBD FLAP UPPER SURFACE FOUND 1 CRACK 1" LONG ON SKIN AT STA XOF 575. TRIMMED OUT DAMAGED SKIN INSTALLED FILLER AND DOUBLER IAW SRM 57-10-00 FIG 85 AND COLD BOND SRM 51-71-00 PAR 16C VOL2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PARTS IAW DETAIL PARTSDR 05FDEA03519Skin · crackedFOUND LT WING OUTBD AILERON WITH ONE CRACK 2" LONG WITH A STOP HOLE ON SKIN LOWER SURFACE AT STA XOA 824. TRIMMED BLEND OUT DAMAGE SKIN INSTALLED DOUBLER IAW SRM 57-10-00 FIG 85 AND SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PART IAW DESDR 05FDEA03518Skin · nickedLT WING OUTBD FLAP UPPER SURFACE FOUND DEEP DENT AND NICK ON SKIN AT STA XOF 467. TRIMMED OUT DAMAGE SKIN INSTALLED REPAIR DOUBLER PER SRM 57-10-00 FIG 85 SHT 1 AND SRM 51-35-02 PAGE 3/9 VOL 2. COLD BOND PER SRM 51-71-00 PAR 16C VOL 2 FABRICATED PARTS IAW DESDR 05FDEA03517Floor Panel · crackedINTERNAL LWR COCKPIT AREA FOUND 2 CRACKS ON SAME MEMBRANE 1ST .50" LONG; 2ND IS 2" LONG; BETWEEN STA 304 TO STA 318; AND BETWEEN X12 TO X13 LT SIDE. REPAIRED MEMBRANE IAW SRM 53-00-01 VOL 1 FIG 10 SHT 4 AND SRM 51-35-01. FABRICATED PARTS IAW DETAIL PARTS TRASDR 05FDEA03516Frame · damagedIN THE AIR CONDITIONING COMPARTMENT LT SIDE AT STA 485 AND Z=-84 THERE IS DEEP WORN ON THE FRAME. TRIMMED OUT DAMAGE TO FRAME AND INSTALLED REPAIR CHANNEL IAW SRM 53-30-00 FIG 4 AND SRM 51-33-01 PAGE 34-4. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F160563/NSDR 05FDEA03515Longeron · corrodedFOUND IN THE AIR CONDITIONING COMPARTMENT LT SIDE AT STA 485 ON THE SKIN SPLICE LONGERON 36 MODERATE CORROSION AND N35 SELF ALIGNMENT NUTS RUST. REPLACED NUTS IAW SRM 51-31-01 PAR 6 VOL 2. REMOVED CORROSION IAW SRM 51-21-01 PAGE 28 ORIGINAL MATERIAL IS .094 SDR 05FDEA03511Fitting · crackedDURING ACCOMPLISHMENT OF B- CHECK MX, IND MX FOUND THE UPPER SECTION OF BOTH THE ARB7158-1 AND ARB7158-2 KEEL FITTING WERE CRACKED, EA 8-5740-79133P4 ISSUED TO COMPLY WITH REPAIR.SDR ARWA20051001Unknown · unknownAT TOP OF CLIMB; AIR TRAFFIC CONTROL (ATC) REPORTED AIRCRAFT OFF COURSE. COULD NOT CORRECT AND REQUESTED VECTORS BACK TO SJU. RESET POWER IN A/C, REPROGRAMMED I.N.S. 1-2-3, ALL CHECKED NORMAL. NO FAULTS FOUND IN ACCORDANCE WITH M/M 34-43-0.SDR 05FDEA03072Computer · malfunctionedPDIS - WHILE IN CRUISE FLIGHT AT FL330, LOST NR 1 INU WITH LOSS OF ADI AND HSI, WENT TO ATT REF POS, NO HELP AND THEN WENT TO OFF AND THEN TO ATT REF POS AND GOT ADI AND HSI BACK. DIVERTED TO ATL. REMOVED AND REPLACED NR 2 ROLL AXIS COMPUTER AND NR 1 INU, LOSDR ARWA20050801Wire Harness · burnedNR 1 AUXILIARY PUMP POPS C/B. T/S FOUND WIRE BUNDLE IN RT WHEEL WELL BURNED AT STA. 1381 FORWARD BULKHEAD; REROUTED WIRE BUNDLE RT WHEEL WELL FORWARD BULKHEAD STATION 1381 IN ACCORDANCE WITH 20-50-02; AUXILIARY PUMP CHECKED NORMAL IN ACCORDANCE WITH M/M 29-21SDR ARWA20050706Windshield · crackedAFTER LANDING CAPTAIN'S WINDSHIELD OUTSIDE CRACKED. REMOVED AND REPLACED CAPT WINDSHIELD IN ACCORDANCE WITH M/M 56-11-00; OPERATIONAL CHECK IN ACCORDANCE WITH M/M 30-41-00 AND M/M 30-42-00 FOUND NORMAL.SDR ARWA20050607Connector · unsecureWEATHER RADAR SYSTEM FAILED DURING FLIGHT (CLIMBOUT); UNABLE TO FIX; RETURNED TO KMIA. CLEANED AND RE-SECURED CONNECTORS AT ANTENNA RADOME; PERFORMED TEST RADAR SYSTEM IN ACCORDANCE WITH M/M 34-41-00; NO DUPLICATE FAIL AT THIS TIME.SDR ARWA20050604Pump · failedAFTER LANDING IN KMIA, NR 2 ENGINE OIL PRESSURE DROP DOWN TO 20 PSI; SHUTDOWN ENGINE NR 2. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER AND REMOVED AND REPLACED OIL PUMP IN ACCORDANCE WITH DC-10 M/M 9-20-04. OPERATIONAL CHECK NORMAL IN ACCORDANCSDR WRLA2005086Coupler · damagedAIR TURNBACK INITIAL CLIMB OBSERVED MASTER WARNING & ENG FIRE WARNING LIGHT & BELL CAME ON & THEN OFF. NR 2 ENG NACELLE TEMP 260 DEG, NR 1 & 3 160 DEG. REDUCED ENG THRUST LEVER TOWARD IDLE TEMP FOLLOWED, PUSHED LEVER FORWARD & TEMP INCREASED, TESTED FIRE WARSDR ARWA20050506Transmitter · malfunctionedLOG PAGE NR 117738. DURING TAXI, ENGINE NR 1 OIL PRESSURE INDICATOR DROPPED TO (ZERO). ALL OTHER PARAMETERS NORMAL, RETURN TO BLOCK IAW AOM ALTERNATE PROCEDURES. REMOVED AND REPLACED ENGINE NR 1 OIL PRESSURE TRANSMITTER IAW MM 79-33-01. OPERATIONAL CHECK SDR 05FDEA01370Bracket · corrodedCOMPLY WITH EA 8-5740-55486, WINGS, NR 1 SPOILER ACTUATOR MOUNT HOLD-DOWN BRACKET CORROSION. COMPLIED WITH EA 8-5740-55486, WINGS NR 1 SPOILER ACTUATOR MOUNT/HOLD-DOWN BRACKET CORROSION.SDR 05FDEA01223Loop · shortedLEVEL 2, NR 2 MANIFOLD FAIL ALERT DURING CRUISE, MEL 06MAY05. RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02. NR 2 MANIFOLD FAIL DETECTION LOOP INOP. MX MUST CLEAR ALERT PRIOR TO EACH DISPATCH. DO NOT PRESSURIZE PNEUMATIC SYS NR 2 EXCEPT FOR ENG START. PERSDR 05FDEA00990Tee Fitting · corrodedCOMPLY WITH EA 8-5340-55468, FUSELAGE-CORROSION IN WING-TO-FUSE TEE ATTACH HOLE. CLOSING ACTION ON 04/12/05. ON N/R S00011. COMPLIED WITH EA8-5340-55468SDR 05FDEA00846Hinge · corrodedFLAP MOUNTED HINGE PIVOT BORE CORROSION REPAIR P/NARC2513-1. COMPLIED WITH EA 8-5750-55462.SDR 05FDEA00491Panel · damagedCOMPLY WITH EA 8-5310-55460 MAIN FRAME-AFT BODY PLANK BLEND REPAIR FS 2051, L45L (P/N AJC7164-503). COMPLIED WITH EA 8-5310-55460 MAIN FRAME-AFT BODY PLANK BLEND REPAIR FS 2051, L45L (P/N AJC7164-503).SDR 05FDEA00305Smoke Detector · malfunctionedCRG FIRE LWR AFT ALERT ON DESCENT. CREW FIRED 1 BOTTLE AND DECLARED EMERGENCY, NO EVIDENCE OF ANY FIRE IN AFT OR CENTER CARGO COMPART OR CONTAINERS AS THEY WERE OFF LOADED. REMOVED AND REPLACED LWR FWD CARGO FIRE EXT IAW M/M 26-22-01-4. REMOVED AND REPLACEDSDR 05FDEA00256Access Panel · crackedLEFT HAND WING LEADING EDGE SKIN CRACKED AT STATION XORS 530, AROUND REFUELING STATION ACCESS PANEL INBOARD CORNER. COMPLIED WITH EA 8-5710-8352, WINGS- LEFT HAND LEADING EDGE TEE CRACK AT REFUELING DOOR CUTOUT- REPAIR.SDR 05FDEA00255Frame · corrodedFRAME AND INTERCOSTAL CORRODED AT STATION 1461 RIGHT WHEEL WELL INTERIOR AREA. COMPLIED WITH FEDEX EA 8-5310-83975, FUSELAGE- CORROSION DAMAGE TO LT STATION 1505, LONGERON 35 FRAME- REPAIR, AND FEDEX EA 8-5310-83974, AFT WHEEL WELL- PRESSURE BULKHEAD TEE FRAMSDR 05FDEA00254Hanger Assy · corrodedRIGHT WING LOWER AFT BEAM SUPPORT FITTING PN ARC0459-2 REQUIRES FABRICATION. FABRICATED FITTING ARC0459-2 IAW DAC DWG ARC0459-2 AND FEDEX EA 8-5732-83971, WINGS- RIGHT HAND WING, LOWER AFT BEAM, SUPPORT HANGER.SDR 05FDEA00252Spar · damagedLEFT HAND INBOARD FLAP WEDGE UPPER FORWARD ATTACH POINT AT OUTBOARD EDGE OF PANEL FIFTH (5) HOLE IS ELONGATED. FABRICATED AND INSTALLED BUSHING IAW FEDEX EA 8-5710-83968, WINGS- LEFT HAND INBOARD FLAP, INBOARD FLAP WEDGE OVERSIZE BOLT HOLE- REPAIR, AND DC10 SSDR 05FDEA00251Seal · leakingLAVATORY, WHEN A FLASHLIGHT IS PLACED IN TRASH CAN THE INNER AND OUTER TRASH RECEPTACLE DOORS AND TRASH CAN LEAKS LIGHT. SEALED LAVATORY TRASH RECEPTACLE IAW FEDEX EA 8-2540-83964, EQUIPMENT/FURNISHINGS - LAVATORY WASTE COMPARTMENT SEALS - REPAIR.SDR 05FDEA00250Skin · corrodedLEFT WING INBOARD FLAP, LOWER SKIN AT TRACK LOWER FILLET FAIRING TRAILING EDGE AREA, HAS SURFACE CORROSION, XIFH 126.650-XIFH 120.908. REMOVED FAIRING AND WEDGE, FABRICATED AND INSTALLED REPAIR IAW FEDEX EA8-5710-83969, WINGS - LEFT HAND INBOARD FLAP, LOWER SSDR 05FDEA00249Hinge · corrodedLEFT HAND OUTBOARD FLAP INBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 INCHES, IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83965, WINGS- LEFT HAND OUTBOARSDR 05FDEA00248Hinge · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE, INBOARD PIVOT BORE CORRODED. REMOVED CORROSION, FABRICATED OVERSIZED BUSHING, INSTALLED AND HONED BUSHING TO FINAL INSIDE DIAMETER OF 0.8745-0.8755 IAW DAC CMM 57-52-02 AND FEDEX EA 8-5710-83967, PRIMED BORE IAW DC10-3SDR 05FDEA00247Hinge · corrodedRIGHT WING OUTBOARD FLAP OUTBOARD SUPPORT, PIVOT ATTACH POINT INBOARD BORE CORRODED. REMOVED CORROSION, FABRICATED, INSTALLED AND HONED BUSHING TO FINAL DIAMETER OF .8745 - .8755 INCHES IAW DAC CMM 57-52-02, PRIMED BORE IAW DC10-30 SRM 51-21-01 VOL II, AND FESDR 05FDEA00246Life Vest · brokenBOTH COURIER SEATS LIFE VEST POUCH RETAINING STRAPS MISSING/BROKEN. ACCOMPLISHED FEDEX EA 8-2560-83856, EQUIPMENT/FURNISHING- COURIER SEAT LIFE VEST POUCH RETAINING STRAP-REPAIR.SDR 05FDEA00264Sill · crackedFOUND CRACK IN RIGHT WING ISLAND SILL PART ARC7008-2.SDR WRLA2005005Gps · malfunctionedITEM: WOA174/25 DAY/LAX AIR TURNBACK DUE TO FAILURE OF NAVIGATION SYSTEM. AFTER TO, NR 3 GPS WORKED BUT WOULD NOT CROSS TALK. AFTER 2:30 MIN CAPT LOST HIS ROLL BAR AND NR 1 GPS WOULD NOT PROVIDE NAV DATA. SHORTLY AFTERWARDS NR 2 GPS HAD ALERT "NAV DATA BASESDR 05FDEA00051Valve · stickingDURING CRUISE, SELECTED ENGINE ANTI-ICE ON, ENGINE NR 2 ANTI-ICE WOULD NOT OPEN, RECEIVED LEVEL 1 ALERT - ENGINE NR 2 ANTI-ICE DISAGREE. CONTACTED MX VIA ACARDS, MX SUGGESTED A RESET OF C/B ON MX PANEL UPPER MX R-25. PULLED AND RESET C/B, NO CHANGE. FOUND SDR 04FDEA03410Selector Valve · leakingSHORTLY AFTER LEVEL OFF GOT LEVEL 1 ALERT HYD 3 ELEV OFF, NOTED THAT HYD 3 QUANTITY WAS DECREASING AT 2.5 GALS. HSC SHUTOFF NR 3 HYD. HYD 3 OFF LEVEL 1 ALERT. AFTER SLATS EXTENDED ON APPROACH, HYD 3 RESTORED. REMAINING FLUID LEAKED OUT, HYD 3 FAILED. GEARSDR WLDA2004109Engine · fireBBR/BGR ON LANDING TOWER ADVISED THAT NR 2 ENGINE IS ON FIRE, ACCOMPLISHED ENGINE FIRE CHECKLIST AND FIRED BOTH BOTTLES. ALL FIRE INDICATIONS REMAINED ILLUMINATED, ACCOMPLISHED EVACUATION CHECKLIST AND EXITED L1 DOOR VIA THE ESCAPE SLIDE. REMOVED AND REPLACED
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