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 04FDEA00547Hinge · corrodedREWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING, REPAIRED HINGE PER FEDEX EA 8-5710-75067 DATED 01-23-04.SDR 04FDEA00546Hinge · corrodedREWORK RT OUTBOARD FLAP INBOARD HINGE FITTING FLAP ATTACH POINT BUSHINGS HAD CORROSION BORE NR 4 WRITTEN FOR CLARIFICATION ON JPF. REMOVED CORRODED BUSHING AND FOUND BORE TO BE 2.322, OUT OF LIMITS IAW DC10 CMM 57-44-08. HEAT TREATED MATERIAL FOR BUSHING IAWSDR WRLA200410Controller · intermittentSMOKE IN COCKPIT AFTER TAKE OFF TURNED NR 2 PACK OFF. SMOKE STOPED.RETURNED TO BGR. NOTE INSPECTED PACK & ON OPS TEMP DISCHARGE TEMP 95 PERCENT PACK AUTO OFF PLACED NR 2 PACK ON DMI M21FE2704-124 MEL 21-1 CAT C.. CLEARED DMI M21FE2704 REMOVED AND REPLACED NRSDR G6OA022404Air Duct · blownON TAKEOFF CREW REPORTED A LOSS OF POWER ON NR 3 ENGINE THEY ABORTED TAKEOFF AT THIS TIME. A VISUAL INSPECTION IDENTIFIED THE 14 STAGE DUCT HAD BLOWN.SDR G60A073Fire Warning · false indicationDURING CLIMB PASSING FL240 MASTER WARNING LIGHT AND FWD CARGO FIRE LIGHT ILLUMINATED.SDR G6OA093003Fire Detector · faultyNR 3 LOWER FWD CARGO FIRE LIGHT CAME ON STEADY THEN BECAME INTERMITTENT. SMELLED SMOKE IN CARGO BAY BRIEFLY.SDR 03FDEA01596Line · leakingHYD SYSTEM NR 1 FAILED. NOTE: DUE TO LOSS OF HYD FLUID. FOUND HYD LINES CHAFED TOGETHER JUST AFT OF 1-3 REVERSIBLE MOTOR PUMP IN CENTER W/W CHANGED LINE, LEAK CHECK OK.SDR 03FDEA01240Hinge · corrodedMDIS 311 57-10 0008862 01AUG03 BFM CLOSE RD COMPLY WITH E.A. 8-5750-70999 WINGS-RT OB 27D FLAP-IB HINGE-ACTUATOR ATTACH LUG FACE CORROSION REPAIR ENT BY 3A 39014C RPT BY 3A 39014C. FACT08AUG03 04 3A29 BFM R COMPLIED WITH E.A. 8-5750-70999 WINGS-RH OB FLAPSDR 03FDEA01241Spar Cap · corrodedMDIS 311 55-30 0008866 05AUG03 BFM CLOSE COMPLY WITH E.A.8-5530-72245. STABILIZER-VERT-REWORK OF CORROSION ON SPARS AMC7107 AND AMC7185 ENT BY3A 60601C RPT BY 3A 60601C. FACT 08AUG03 19 PERCENT 3A29 BFM COMPLIED WITH EA 8-5530-72245 STABILIZER-VERT-REWORK SDR 03FDEA01205Ring · corrodedR/H WING FUEL TANK ACCESS PANEL CHAFE RING HAS PITTED CORR. REMOVED AND REPLACED CHAFE RING AND GANG CHANNEL IAW SRM 51-42-04 AND SRM 51-31-01 AT MAE ON N/R N00926SDR G6OA071Bolt · wornAIRCRAFT PERFORMED AN AIR RETURN SAFELY DUE TO UNABLE TO PRESSURIZE AFTER TAKE OFF. DURING TROUBLESHOOTINGFOUND GROUND SENSE ROD LOOSE. R/R UPPER BOLT PER MM 32-21-01SDR P8UF200300001Duct · leakingMANIFOLD FAIL LIGHT ON NR 2. SMOKE DETECT CABIN CARGO NR 8, 9, 10 LIGHT ON. SMOKE DETECT AFT CARGO NR 1, 2, 3 AND HEAT DET AND AFT CARGO FIRE LIGHT ON. PRESENCE OF SMOKE IN ALL CARGO MAIN UPPER & COCKPIT.SDR G6OA070Control Panel · burnedWHILE IN FLT, PITOT INOP LIGHT CAME ON. SWITCH WAS ROTATED TO ALL POSITIONS AND ALL HEATERS WERE WORKING. SHORTLY THERE AFTER SMOKE STARTED COMING OUT FROM BEHIND THE METER SEL AND HEAT CONTROL PANEL. SWITCH WAS IMMEDIATLY TURNED OFF AND A/C RETURNED TO MIA.SDR G60A069Smoke Detector · false activationNR 3 LOWER FORWARD CARGO SMOKE DETECTOR ILLUMINATED WITH ASSOCIATED LIGHTS, ACCOMPLISHED CHECKLIST E-23 AND DISCHARGED NR 1 AND NR 2 CARGO FIRE BOTTLES. INSPECTED CARGO COMP, NO FAULTS FOUND. REF TAFI 26-14BC. DETECTOR FAULT, MEL 26-15-1, CONTROL NR M80312.SDR 03FDEA0043Beam · corrodedTEE CAP AEA 7097-1, STA.1521 WAS FOUND CORRODED AT RT STA.-80.125 WHERE VERTICLE BEAM A0024-2 ATTACHES. THE BEAM ATTCHMENT TO THE TEE CAP CREATES A (V) WHERE WATER CAN PUDDLE. AWAITING APPROVED REPAIR FROM BOEINGSDR 02FDEA00977Warning Light · illuminatedENGINE NR 3 TEMP LIMITING POWER ALL REGIMES. SHORTLY AFTER TAKEOFF RECEIVED LOOP B FIRE LIGHT. ENGINE 3 FIRE LOOPS, A AND B BOTH TEST PROPERLY, REDUCED PWR, LOOP LIGHT EXTINGUISHED, PARAMETERS STABLE. DIVERTED.SDR 02FDEA00925Beam · crackedCENTER CARGO DOOR COUNTER BALANCE BEAM CRACKED AT FORWARD BRACKET. REMOVED AND REPLACED COUNTER BALANCE BEAM ASSEMBLY IAW MM.SDR WRLA200226Switch · failedAIR CONDITIONING DOOR LIGHT CAME ON IN FLIGHT. AIRCRAFT WAS DEPARTING OZARK AIRCRAFT SYSTEMS AT THE COMPLETION OF SCHEDULED 'A' CHECK AIRCRAFT RETURNED TO REPAIR STATION. TROUBLESHOT FOUND NR 2 AIR CONDITIONING BAY DOOR SWITCH INOPERATIVE. (M)SDR 02FDEA00811Chip Detector · contaminatedENGINE NR 2 OIL FILTER LEVEL 2 ALERT, CAME ON AT TOP OF CLIMB. THROTTLE WAS RETARDED TO IDLE BUT ALERT STAYED ON. ENGINE NR 2 WAS SHUT DOWN IAW THE CHECKLIST. ENGINE FAN COWLS WERE OPENED AND THE MASTER CHIP DETECTOR WAS PULLED, FERROUS METAL STRANDS WERE CSDR 02FDEA00612Keelbeam · corrodedCENTER W/W LEFT WEB CORRODED AT FWD INSP PLATE ON KEELBEAM CORROSION IS STILL EVIDENT. CORROSION MAY ALSO BE UNDER ACCESS PLATE. REMOVED AND REPLACED KEELBEAM PER EA 8-5310-65917.SDR WRLA200217Sensor · erraticENGINE FAIL CAUTION LIGHT ILLUMINATED DURING TAKE OFF DUE TO NR 1 ENGINE N1 TACH GIVING ERRATIC INDICATIONS. (REJECTED TAKE OFF AT 70 KNOTS.) REMOVED AND REPLACED NR 1 ENGINE FAN SPEED SENSOR , RAN ENGINE NR 1 UP TO 85 PERCENT NR 2, FOUND NO ERRATIC FLUCTUASDR WRLA200214Seal · looseCABIN ALTITUDE WENT TO 11,000 FEET UNABLE TO MAINTAIN CABIN PRESSURE. (RETURNED TO STATION.) FOUND FORWARD AND CENTER LOWER CARGO DOOR SEAL PUSHED OUT. REINSTALLED DOOR SEAL, PRESSURE CHECKED AIRCRAFT, AIRCRAFT PRESS CHECK GOOD. REINSTALLED DOOR SEAL. LOOSDR 02FDEA00249Mec · out of rigON TAKEOFF NR 3 ENG W/N ATTAIN MAX PWR. ADJUSTED NR 3 ENG MEC 1/2 TURN UPTRIM, RAN ALL ENG PER JRH CHAPTER 5 AND ACCOMPLISHED MAX. ALL ENGINES OPERATING OKAY.SDR 02FDEA00219Periseal · failedAFTER T/O NR 3 PNEU MANIFOLD FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED PERISEALS PER SMP.SDR 02FDEA00140Slat · crackedNR 1 SLAT RT WING CRACKED AT LIGHTNING HOLE AT I/B END AT XFS 145. REMOVED AND REPLACED DOUBLER PER SRM 57-00-01 VOL 1 FIG 4.SDR 02FDEA00137Door · crackedON GEAR RETRACT RT MLG IND UNSAFE ON BOTH PANELS. REMOVED AND REPLACED MAIN GEAR DOOR PER AMM 32-14-01-2.SDR WRLA200203Adc · failedCAPTAIN HAD NO AIRSPEED ON TAKEOFF ROLL, GROUND ABORT. BLEW OUT CAPTAIN PITOT LINE AND GOT A SMALL AMOUNT OF DEBRIS. CLEARED LINE ALSO CADC FAILED AND ALL FLAGS SHOWN ON AIR SPEED INDICATOR. REPLACED CADC WITH FED EX LOANER AND PERFORMED PITOT STATIC TEST OSDR WRLA200202Indicator · inoperativeDURING TAKEOFF ROLL, CAPTAIN AIR SPEED INDICATOR REMAINED AT 0 KNOTS WITH NO FLAG INDICATED ON FIRST OFFICERS AIR SPEED INDICATED NORMAL. REJECTED TAKEOFF AT APPROXIMATELY 95 KNOTS.SDR G60A065Sensor · malfunctionedAFER TAKEOFF, STICK SHAKER STARTED AND THEN SLAT DISAGREE LIGHT CAME ON. RETURNED TO KMIA. REMOVED AND REPLACED AOA SENSOR P/N 2568A13, PER MM 22-33-01 AND NR 1 AT/SC COMPUTER P/N 2593342976 PER MM 22-31-01. STALL WARNING TESTS GOOD. (M)SDR WRLA200205Indicator · inoperativeDURING TAKEOFF ROLL CAPTAIN AIRSPEED WOULD NOT INDICATE ANY AIRSPEED. NO CADC FLAG WERE SHOWING. FIRST OFFICERS AND AUX AIRSPEED INDICATORS WERE READ 100 KNOTS PRIOR TO REJECTING THE TAKEOFF. REPLACED CAPTAINS AIR SPEED INDICATOR PART NR 2594466-905 S/N ON SDR G6OA064Engine · flamed outNR 3 ENGINE FLAMED OUT AT CRUISE. AFTER TROUBLESHOOTING NR 3 ENGINE, REMOVED AND REPLACED NR 3 ENGINE FUEL FILTER ELEMENT PER MM 73-11-02. REMOVED AND REPLACED NR 3 FUEL PUMP PER MM 73-12-01. REMOVED AND REPLACED MEC UNIT ON NR 3 ENGINE PER MM 73-20-01. PESDR 02FDEA00130Cargo Track · crackedSTA 959 UPPER CARGO SEAT TRACK HAS 10 INCH CRACK C/T RADIUS AT SPLICE X-27.SDR 02FDEA00089Control Unit · failedDURING FLIGHT TEST BRAKE LAND ALL MAIN LANDING GEAR TIRES BLEW (10) EACH. REMOVED AND REPLACED ALL MLG WHEEL AND TIRE ASSY. REMOVED AND REPLACED ANTI-SKID CONTROL UNIT PER AMM 32-45-01-2.SDR 02FDEA00069Tire · blownDURING FLIGHT TEST ALL MAIN LANDING GEAR TIRES BLEW (10) EA.SDR 02FDEA00065Controller · malfunctionedINTERMITTENT PILOT MASTER CAUTION LIGHT WITH NO OTHER IND. REMOVED AND REPLACED MASTER WARN CONTROLLER. GROUND CHECK NORM.SDR 02FDEA00058Pressure Switch · failedNR 3 MANIFOLD FAIL LIGHT ILLUMINATED ON CLIMBOUT SHORTLY AFTER SELECTION OF WING A/I ON. REMOVED AND REPLACED NR 3 MANIFOLD FAILURE DETECTION PRESSURE SWITCH PER MM 36-23-03-4, SYS OPS CHECK GOOD.SDR G60A061Skin · damagedFATIGUE DAMAGE TO THE INNER SKIN OF THE NR 1 SLAT ON THE LEFT WING. MISSING MATERIAL HOLE SIZE IS APPROXIMATELY 8 INCHES BY 11 INCHES WITH ONE AREA EXCEEDING THIS DIMENSION BY AN ADDITIONAL 2.5 INCHES BY 4 INCHES. THERE ARE 4 OBVIOUS FATIGUE CRACKS IN THE ARSDR G6OA059Bellcrank · wornELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BELLCRANK ASSEMBLIES ON LEFT INBOARD ELEVATOR ACTUATOR. REMOVED AND REPLACED BELLCRANK ASSEMBLY IAW MM 20-50-02. OPS CHECKS GOOD IAW MM 27-30-00. (M)SDR G6OA060Bracket · wornFOUND ELEVATOR CONTROL CHECK DOWNWARD MOVEMENT BINDING DURING NOSE DOWN MOVEMENT. FOUND BENT AND WORN BRACKET ASSEMBLIES ON LEFT INBOARD ELEVATOR. REMOVED AND REPLACED BRACKET ASSY IAW MM 20-50-02. OPS CHECKS GOOD IAW MM 27-30-00. (M)SDR 02FDEA00035Door Frame · damagedBS 625 TO 765 UPPER CARGO DOOR FWD AND AFT DOOR JAMB STRUCTURAL DAMAGE. REMOVED AND REPLACED DOOR PER EA 8-5330-56188.SDR 02FDEA00034Seat Track · crackedSEAT TRACK AT BS 630 X = 27.50 HAS CRACK IN LWR INBOARD AND OUTBOARD FLANGES.SDR 02FDEA00006Support · crackedCASTING CRACKED ON O/B SIDE OF LEFT O/B FLAP O/B SUPPORT. REMOVED AND REPLACED RIB ASSY, OUTBOARD CLOSURE, OUTBOARD FLAP PER DRAWING ARC 2217.SDR 02FDEA00005Control Cable · brokenRIGHT WING NR 8 SLAT 2ND SLAT TRACK FROM O/B END CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM 27-89-14-4.SDR 01FDEA01113Floor Support · corrodedFWD LOWER CARGO BS 775 RT FLOOR SUPPORT SIDE STRUT CORRODED. REMOVED AND REPLACED SIDE STRUT PER SRM 53-13-01.SDR 01FDEA01039Longeron · corrodedCORRODED LONGERON 18 LEFT AT BS 1215. REMOVED AND REPLACED LONGERON PER SRM 53-10-00.SDR 01FDEA01015Floor Support · crackedVERTICAL SUPPORT AT BS 555, X=71 HAS CRACK. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-31-01, 51-00-00, 51-21-01.SDR 01FDEA01016Floor Support · crackedVERTICAL SUPPORT AT BS 575, X=73 HAS A CRACK. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-31-01, 51-00-00, 51-21-01.SDR 01FDEA01111Floor Support · crackedVERTICAL SUPPORT AT BS 495 X=73 Z=16 CRACKED BELOW FLOOR. REMOVED AND REPLACED SUPPORT PER SRM 51-10-00 & 51-21-01.SDR 01FDEA01014Support · crackedVERTICAL SUPPORT AT BS 495, X=73 HAS CRACK.SDR 01FDEA01008Intercostal · corrodedAFT CARGO TUNNEL BS 1847-1857, STR 28R INTERCOSTAL PANEL CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM.
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