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 01FDEA01007Web · corrodedAFT CARGO TUNNEL BS 1897-1902, STR 27R INTERCOSTAL PANEL CORRODED. REMOVED AND REPLACED WEB AND CHANNEL PER SRM 51-00-00, 51-21-01, 51-35-01 & 51-33-01.SDR 01FDEA01032Channel · crackedFWD CARGO BS 939 X=-99 Z=30 CEILING SUPPORT CHANNEL CRACKED. REMOVED AND REPLACED CHANNEL AND BRACKETS PER SRM 51-10-01 & 51-35-01.SDR 01FDEA01031Seat Track · corrodedCORRODED SEAT TRACK AT X=108.00 Z=-19.00 BS 1539-1553. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00.SDR 01FDEA01112Support · corrodedAFT FUSELAGE WASTE TANK COMP BS 1967, STR 47L & 47R Z-ANGLE SIDEWALL PNL SUPPORT CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 53-16-01 & 51-35-01.SDR 01FDEA01030Stanchion · corrodedAFT FUSELAGE BS 1967, STR 50R CORRODED STANCHION SUPPORT. REMOVED AND REPLACED STANCHION PER SRM 51-35-01.SDR 01FDEA00992Support · corrodedBS 1841, LBL 54 TO RBL 54 BELOW AFT FLOOR ROLLER TRAY SUPPORT IS CORRODED. REMOVED AND REPLACED SUPPORT PER SRM 51-35-01 & 51-33-01.SDR 01FDEA00991Floor Support · corrodedBS 1841, LBL 22 TO RBL -52, WL -93 ANGLE FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED ANGLE PER SRM 51-35-01 & 51-33-01.SDR 01FDEA00990Frame · corrodedBS 1841, RBL 56R, WL -96 CORROSION ON FRAME ABOVE LONGERON 43R. REMOVED AND REPLACED CAP PER SRM 51-35-01.SDR 01FDEA00989Frame · corrodedFRAME AT BS 1841 ABOVE LONGERON 43R CORRODED. REMOVED AND REPLACED FRAME PER SRM 51-35-01 & 51-33-01.SDR 01FDEA00950Intercostal · bentBS 450 TO 460 X=-21 LOWER AVIONICS SKIN BENT INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL PER SRM.SDR 01FDEA00949Skin · corrodedBS 1028-1068 LONG 52 OML DEEP PITTED CORROSION TO EXTERIOR SKIN BOTTOM. REMOVED AND REPLACED SKIN PER SRM & EA.SDR 01FDEA00948Skin · corrodedBS 1028-1068 LONG 52 OML DEEP PITTED CORROSION TO EXTERIOR SKIN BOTTOM. REMOVED AND REPLACED SKIN PER SRM & EA.SDR 01FDEA00947Seat Track · corrodedBS 1936, LBL 27, WL 80 SEAT TRACK CORRODED SEAT TRACK CHANNEL. REMOVED AND REPLACED SEAT TRACK PER SRM.SDR 01FDEA00946Frame · corrodedBS 1841, LBL 53-58, WL 97 AFT SIDE FRAME CORRODED. REMOVED AND REPLACED CAP PER SRM.SDR 01FDEA00945Seat Track · corrodedBS 1079-1099 LONG 27R EXFOLIATING CORROSION ON FLOORBOARD SEAT TRACK. REMOVED AND REPLACED SEAT TRACK PER SRM.SDR 01FDEA00944Seat Track · damagedBS 615 AND 635 X=-27 SEAT TRACK IN MAIN CABIN GOUGED AND OBLONG. REMOVED AND REPLACED SEAT TRACK PER SRM.SDR 01FDEA00943Seat Track · gougedBS 1175, X=-48 SEAT TRACK IN MAIN CABIN GOUGE. REMOVED AND REPLACED SEAT TRACK PER SRM.SDR 01FDEA00942Seat Track · corrodedBS 1879, X=-59, Z=-19 SEAT TRACK LOBE HAS CORROSION. REMOVED AND REPLACED SEAT TRACK PER SRM.SDR 01FDEA00941Seat Track · corrodedBS 1877 TO 1887 X=10.Z=-19 SEAT TRACK HAS CORRODED. REMOVED AND REPLACED SEAT TRACK PER SRM.SDR 01FDEA00933Control Handle · lack of lubeWHEN GEAR HANDLE LOWERED FOR LAND AT BOTH PANELS IND. CLEANED AND LUBED GEAR HANDLE PER MM 32-31-02-7, 32-31-02-2. OPS CHECK NORMAL.SDR 02FDEA00004Seat Track · crackedUPPER CARGO SEAT TRACK AT BS 595 TO 765 HAS CRACK AT 655. REMOVED AND REPLACED SEAT TRACK PER SRM 53-70-00 & 51-21-01.SDR 01FDEA00900Landing Gear · malfunctionedAFTER T/O, LANDING GEAR WOULD NOT RETRACT.SDR 01FDEA00889Seat Track · corrodedSEAT TRACK AT BS 1865 TO BS 1871 X=49Z=19 CORRODED. REMOVED AND REPLACED SEAT TRACK PER IAW SRM 53-10-00 FIG 1.SDR 01FDEA00878Floor Support · corrodedBS 1741, X=71.5 TO X=103 FLOOR SUPPORT CORRODED. R&R FLOOR SUPPORT PER SRM 51-00-01 & 51-30-00.SDR 01FDEA00863Structure · corrodedNR 491 AFT PIN RBL 22 AT BS 1967 VERTICAL CORROSION LVL 2 UNDER SEALANT AROUND ACCESS PNL. ** S/D ** COMINGSDR 01FDEA00987Frame · corrodedHEAVY CORROSION ON FRAME AFT SIDE X=60, Z=-96, BS 1841 LT. REMOVED AND REPLACED FRAME PER SRM 51-35-01 & 51-33-01.SDR 2002F00060Adc · faultyABORTED TAKEOFF AT 80 KNOTS CALLED BY FIRST OFFICER DUE TO 25 KNOTS AIRSPEED DISCREPANCY BETWEEN FIRST OFFICER AND CAPTAINS AIRSPEED INDICATORS. TAXI BACK TO GATE FIRST OFFICER AIRSPEED INDICATOR READS 70 KNOTS. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER P/SDR MZA2001F00000Control Cable · brokenDURING C-CHECK, FOUND NR 3 RIGHT SLAT EXTEND CABLE BROKEN. CAUSE UNDER INVESTIGATION.SDR 01FDEA00811Pressure Panel · corrodedCTR WHEEL WELL, LT SIDEWALL, LWR FWD CORNER, CORROSION UNDER SEALANT, AROUND ACCESS PNL.SDR 01FDEA00988Web · crackedCRACK NR 3 SLAT RT WING BS XO8 464 & CRACK IN WEB. REMOVED AND REPLACED WEB PER SRM 51-41-01 EA 8-5510-56177.SDR 01FDEA00736Proximity Sensor · faultySLAT DISAGREE LIGHT ILLUMINATED. FOLLOW RED TABS. REMOVED AND REPLACED PROX BOX PER IAW MM 32-61-01-2. OPS CHECK GOOD.SDR RRXA010063Structure · tornLT INBOARD ELEVATOR TRAILING EDGE CAP TORN, 4 IN. BY 2 IN. AREA. REPAIRED PER DC-10 SRM 55-30-00 P2-P4, ELEVATOR TRAILING EDGE REPAIRS PER 55-30-00, TRAIL EDGE REPAIR P 1,3. A6.SDR 01FDEA00634Warning System · malfunctionedON T/O FROM ALT RED LIGHT ON LMG STAYED ON. RAN RED TAB PROC, LIGHT STAYED ON. NO FAULT FOUND SWAPPED PILOTS DISPLAY PLUG ON PROX BOX TO ALTERNATE POS, A/C DISPATCH IAW MEL 32-8C.SDR 01FDEA00610Threshold · corrodedCENTER CARGO DOOR FWD CORNER DOOR SILL THRESHOLD HAS HEAVY SURFACE CORROSION FWD OF NR 1 SPOOL FITTING. *S/D* REMOVED AND REPLACED DOUBLER AND HI-LOKS PER EA 8-5310-56792.SDR 01FDEA00579Controller · inoperativeON ROTATION ENG 2 A/I DISAGREE LIGHT ILLUM (SW OFF) COMPL W/RED TABS. FLT RECORDER CAUTION LIGHT ILLUM ON S/O PNL AND AOA HT C/B POPPED. REMOVED AND REPLACED HEATER CONTROLLER/MONITOR PER MM 30-35-01-2. PER OPS TEST PER 30-30-00-2, SYS OPS NORM. WRI ASSIGNSDR 01FDEA00566Frame · crackedFRAME HAS 1 CRACK AT FASTENER LOCATION AND 1 DOUBLE AT FASTENER. FAB, INSTALLED AND REPAIRED HOLE PER IAW EA 8-5310-56130 & DC10 SRM 53-12-01 FIG 12, SHT 1 & 53-30-00 FIG 5.SDR 01FDEA00565Frame · corrodedFRAME CORRODED IN NR 2 AIR CONDITION BAY FWD LEFT SIDE. REMOVED AND REPLACED FRAMES PER EA 8-5310-56130 & SRM 53-12-01, 53-30-00.SDR 01FDEA00564Support · corrodedPANEL SUPPORT COMMON TO STANCHION HAS CORRODED. REMOVED AND REPLACED CORROSION PER IAW INSTRUCTIONS, EA 8-5310-52551 STEP 7 & DC10 SRM 53-50-00 FIG 1 & 14.SDR 01FDEA00569Frame · corrodedAFT CARGO PIT FRAME CORRODED. REMOVED AND REPLACED FRAME PER IAW EA 8-5310-52551 & DC10 SRM 53-50-00 FIG 1 SHT 1.SDR 01FDEA00568Frame · corrodedLWR FWD CORNER TO AFT CARGO DOOR OPENING, FRAME CORRODED BEYOND LIMITS. FAB DOUBLER, FILLER AND SHIMS PER IAW EA 8-5310-52551 & DC10 SRM 53-50-00.SDR 01FDEA00563Indicator · inoperativeREJECTED T/O DUE TO NO AIRSPEED ON CAPT SIDE.SDR 01FDEA00536Skin · crackedSKIN FWD OF WHERE ENG NR 2 MATES HAS CRACKS AND CORROSION WHERE THE ENG DOOR ACTUATION FLEX SHAFT GOES THRU THE SKIN. REMOVED AND REPLACED FRAME PER SRM 54-10-00, 51-31-01 & EA 8-5230-56137.SDR 01FDEA00538Frame · corrodedBS 1831 LWR AFT FRAME IS CORRODED BEYOND LIMITS PER IAW DC-10 SRM 53-00-31 FIG 1B. REMOVED AND REPLACED FRAME PER IAW DAC AFA3929.SDR 01FDEA00537Angle · corrodedL-ANGLE AFT CARGO, LWR DOOR SILL, INSIDE TORQUE BOX IS CORRODED. REMOVED AND REPLACED FRAME PER EA 8-5310-52551 & SRM 53-50-00.SDR RRXA010057Fairing · damagedUPON WALKAROUND, DISCOVERED DAMAGE TO WING FILLET FAIRING. PERFORMED TEMPORARY REPAIR PER BOECOM EAF-IND-01- 00059H. INSTALLED EXTERNAL DOUBLER AND COVERED WITH SPEED TAPE. TAPE TO BE INSPECTED EACH FLIGHT.SDR 01FDEA00514Skin · gougedSEVERAL GOUGES LT WING LWR MIDDLE SURFACE OF SLATS NR 6, 7, 8. ALSO SEVERAL GOUGES ON UPPER SURFACE OF LT WING AT SLATS NR 6, 7, 8. REPAIRED PER EA 8-5750-56805 AND NR N415 UNDER WO 16747.SDR M8B2001F00000Bolt · shearedPRE DEPARTURE CHECKS FOUND RIGHT MAIN LANDING GEAR AFT AXLE BOLT HAD HEXAGONAL HEAD SHEARED OFF. PROBABLE CAUSE: FATIGUE, STRESS.SDR 01FDEA00478Floor Support · crackedBS 1139 X=+6 THERE IS A 2 INCH CRACK IN FLOOR SUPPORT. *S/D* REMOVED, REPLACED AND FAB PER IAW SRM 51-10-01, 51-21-01, 51-31-01.SDR 01FDEA00506Turnbuckle · brokenCENTER LAND GEAR LT DOWNLOCK SPRING TURNBUCKLE BROKEN. REMOVED AND REPLACED TURNBUCKLE PER IAW AMM 32-16-01. FUNCTION TEST PERF IN CONJUNCTION WITH 32C3301, TEST GOOD.SDR 01FDEA00444Skin · wornSKIN FWD OF NR 2 ENG MATES TO FAN COWL WORN THRU NACELLE SKIN BS YTN138.977. REPAIRED PER IAW EA 8-5410-53241.
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