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 = '440' 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 = '440' 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 CA001020021Tailpipe · broken(CAN) THE FLIGHT CREW OBSERVED A RT ENGINE ZONE 1 FIRE WARNING, THE ENGINE WAS SHUTDOWN AND THE FIRE WARNING WENT OUT PRIOR TO FIRING THE FIRE EXTINGUISHER. RECTIFICATION: THE RT ENGINE TAIL PIPE, UNIVERSAL JOINT P/N 906323-23 REPLACED, SYSTEM TESTED ON GROUNDSDR 20001127AP006Spring · weakEMERGENCY EXIT WINDOW ROW 3 LEFT POPPED OUT AFTER DEPRESSURIZATION ON LANDING. REPLACED LATCH SPRING, REPOSITIONED EXTERIOR HANDLE SEAL, LUBED ALL MECHANISMS AND SEALS. INSPECTED, RE-RIGGED, PULL FORCE TESTED, AND RE-INSTALLED WINDOW IAW CONVAIR SB 53-7. (MSDR 20000728SH008Light · inoperativeCREW EN ROUTE MMCS/ELP, THEY LOWERED LANDING GEAR AND DID NOT RECEIVE A DOWN/LOCKED LIGHT FOR THE LEFT MAIN GEAR (INTRANSIT). LIGHT WAS NOT ILLUMINATED NOR DID THEY RECEIVE A GEAR HORN. THEY OPTED TO MAKE A FLYBY. THE TOWER WOULD NOT CONFIRM THE GEAR WAS DSDR 20000721SH019Light · openCREW EN ROUTE FROM MMCS TO ELP. CREW LOWERED LANDING GEAR AND DID NOT RECEIVE A DOWN/LOCKED LIGHT FOR LT MAIN GEAR (INTRANSIT). LIGHT WAS NOT ILLUMINATED NOR DID THEY RECEIVE GEAR HORN. OPTED TO MAKE FLYBY. TOWER WOULD NOT CONFIRM GEAR DOWN. CREW PERFORMESDR 20000816AP010Seal · looseLT CENTER EMERGENCY EXIT FOUND UNSECURED. REMOVED AND REPLACED WINDOW SEAL. EMERGENCY EXIT LT SIDE ROW 5 POPPED OUT AFTER LANDING. REPLACED SEAL DUE TO SEAL COMING OUT. ADJUSTED LATCH IAW CV580 MM 52-23-1 PARA 7A/B, PAGE 207. ROW 5 EMERGENCY EXIT OPENS ONSDR CA990916017Fire Detector · malfunctioned(CAN) IN CRUISE, A ZONE 1 FIRE WARNING ON THE LEFT ENGINE. ENGINE SHUT DOWN AND PROPELLER FEATHERED. AIRCRAFT LANDED AND AS A PRECAUTION, BOTH BOTTLES FIRED. SENSING ELEMENT, FIRE BOTTLES, AND CARTRIDGES REPLACED.SDR CA990916015Valve · failed(CAN) SELECTION OF PHASE SYNC CAUSED PROPELLER RPM FLUCTUATIONS, NR 1 PROPELLER VALVE REPLACED.SDR 99ZZZM386Edc · failedSMOKE IN CABIN. DISCONNECTED ENGINE DRIVEN COMPRESSOR. (M)SDR 99ZZZX1915Clamp · misinstalledSUSPECTED THAT CLAMP HOLDING TAILPIPE TO THE REAR OF THE TURBINE WAS INSTALLED IMPROPERLY AND CAME LOOSE CAUSING THE TAILPIPE TO SLIDE BACK 6 INCHES AND ALLOWING HOT TURBINE EXHAUSTS ON NACELLE COWLS AND ENGINE FIRE DETECT LOOP. THIS CAUSED AN ENGINE FIRE WARSDR 99ZZZX1658Condition Lever · bindingNTD - ON APPROACH, RIGHT THROTTLE WOULD NOT RETARD PAST 1,500 HP IN-FLIGHT. BINDING IN THROTTLE LINKAGE. IN-FLIGHT SHUT DOWN.SDR 98ZZZX3032Transfer Tube · pluggedAIRCRAFT WAS FLYING LOCAL WHEN THE PILOT NOTICED NR 2 PROP STARTING TO OVERSPEED. PILOT USED EMERGENCY PROCEDURES TO SHUT DOWN NR 2 ENGINE AND FEATHER NR 2 PROP. NR 2 PROP DID NOT FEATHER. PILOT DECLARED EMERGENCY, ACFT LANDED WITHOUT INCIDENT. UPON INSPECSDR 98ZZZX2976Fcu · failedIN CRUISE AT 18,000 FEET, LEFT ENGINE GRADUALLY LOST POWER. HP DROPPED FROM 2,000 TO ZERO, TIT FROM 847 TO 450, FF FROM 1,110 TO 600. TRIED TD NULL OFF, POWER LOSS GOT WORSE. TRIED ENGINE HEAT, NO EFFECT. SHUT ENGINE DOWN. DISCONNETED EDC PER CHECKLIST. SDR 98ZZZM639Actuator · failedPROPELLERS WILL NOT SYNC IN K1 POSITION. RIGHT 13500 RPM, LT 14,000 RPM AND RISING. PITCH LOCKED PROPELLER, RPM STILL UNSTABLE. E-HANDLED LT ENGINE AND MADE UNEVENTFUL LANDING AT ANC. REPLACED LT ROTARY ACTUATOR AND REPAIRED BROKEN WIRE TO RT PROP ALTERNATSDR CA980707066Gasket · failed(CAN) DURING CLIMB AT 7,000 FEET, TWO ENGINE FIRE WARNING SYSTEMS ACTIVATED ZONE TWO. ENGINE FIRE BOTTLES BLOWN AND SHUT DOWN IAW EMERGENCY PROCEDURES, AIRCRAFT LANDED OK. BLOWN GASKET DOWNSTREAM OF THE UPPER 14TH STAGE BLEED AIR CHECK VALVE. GASKET AND CLASDR CA980417017Shaft · sheared(CAN) DURING CRUISE, LT ALTERNATOR LIGHT CAME ON. GENERATOR WOULD NOT RESET. MAINTENANCE INVESTIGATION FOUND THAT THE SHAFT WAS SHEARED. THE GENERATOR WAS NOT FOUND TO BE SEIZED.SDR CA980402018Fitting · cracked(CAN) DURING ROUTINE INSPECTION OF THE TAIL, THE LH FWD UPPER STABILIZER ATTACHMENT FITTING WAS FOUND CRACKED. DEFECTIVE FITTING REPLACED AND NO OTHER FAULTS FOUND. A/C FLOWN AND NO VIBRATION FELT.SDR CA970926014Engine · failed(CAN) LEFT ENGINE NOT PRODUCING POWER IN FLIGHT. ENGINE SHUTDOWN, AND AIRCRAFT RETUNED TO BASE. UPON INITIAL INSPECTION, THERE WAS AN OIL LEAK AND THE PROPELLER HAD A SLIGHT NOSE DOWN TILT.SDR CA970325015Windshield · cracked(CAN) LEFT HAND WINDSHIELD CRACKED DURING FLIGHT. AIRCRAFT DEPRESSURIZED AND DESCENDED TO SAFE ALTITUDE. WINDSHIELD DEVELOPED THREE CRACKS, TWO CRACKS 8 INCHES LONG AND ONE AT THREE INCHES STARTING FROM BOTTOM LH CORNER ON OUTER PANE. WINDSHIELD REPLACED.SDR CA970310006Bearing · failed(CAN) NR 1 ENGINE SHUT DOWN AFTER LANDING DUE TO LOW OIL PRESSURE QUANTITY. MAINTENANCE FOUND THAT THE TURBINE SECTION REAR BEARING SCAVENGE PUMP WAS DAMAGED AND LEAKING. THE ENGINE TURBINE HAD SHIFTED BACK AND DAMAGED THE PUMP. IT IS SUSPECTED THE COMPRESSSDR CA970225004Fuel Contrl Unit · failed(CAN) ENGINE NR 1 WOULD NOT RESPOND TO POWER LEVER WHEN PULLED BACK. FUEL FLOW AND EGT REMAINED THE SAME. ENGINE SHUT DOWN ON APPROACH. FUEL CONTROL UNIT SUSPECTED OF INTERNAL FAILURE. REPLACED FUEL CONTROL UNIT.SDR 97ZZZM259Spar · crackedDURING B-1/B-2 INSPECTION, THE VERTICAL STABILIZER RT FRONT SPAR RAIL AT WL 151 WAS FOUND TO BE CRACKED. REPLACED RAIL WITH NEW UNIT. AIRCRAFT WILL BE RETURNED TO SERICE AT END OF INSPECTION.SDR 97ZZZX1570Frame · crackedLEFT WING STA 25 FRAME CRACKED UPPER 'Z'.SDR 97ZZZX1569Beaver Tail Rib · corrodedRIGHT WING BEAVER TAIL, NUMEROUS RIBS HAVE EXFOLIATION.SDR 97ZZZX1568Skin · corrodedLEFT WING UPPER SURFACE HAS CORROSION ON PLANK AND STRINGER BULKHEAD, STA 235 TO 28.5SDR 97ZZZX1567Skin · crackedFUSELAGE INNER SKIN SURFACE CRACKED STA 344, STR'S 13L-14L.SDR 97ZZZX1566Skin · corrodedSKIN CORRODED IN FORWARD CARGO BAY AROUND BELT FRAME 193/210.SDR 97ZZZX1565Shroud · crackedCRACK IN INNER SHROUD RT OTBD L/E STA 290.SDR 97ZZZX1564Skin · crackedAFT ADF ANTENNA SKIN CUT-OUT CRACKED.SDR 97ZZZX1563Skin · corrodedSURFACE CORROSION RIGHT WING BAY WING PLANK STA 23 TO STA 29.SDR 97ZZZX1562Skin · corrodedWING SKIN, STRINGERS (4 EACH), FORWARD SPAR WEB, AND AFT SPAR WEB CORRODED FROM WET BAY TO WING TIP.SDR 97ZZZX1561Floor Beam · corrodedFLOOR BEAM STA 681 CORRODEDSDR 97ZZZX1559Fitting · crackedRIGHT UPPER FORWARD HORIZONTAL STABILIZER ATTACH FITTING ATTACHED.SDR 97ZZZX1558Fitting · crackedLEFT MLG INBOARD TRUNNION FITTING CRACKED.SDR 97ZZZX1580Fitting · crackedRT UPPER FORWARD HORIZ STAB FITTING CRACKED.SDR 97ZZZX1579Floor Beam · crackedFLOOR BEAM CRACKED STA 718 RBL 8 AND 12.SDR 97ZZZX1578Doubler · crackedDOUBLER CRACKED RT INBD NR 2 ENGINE TAILPIPE ACCESS.SDR 97ZZZX1577Skin · crackedLEFT MLG WHEELWELL AFT LOWER SKIN CRACKED.SDR 97ZZZX1576Structure · corrodedCOCKPIT FLOOR STRUCTURE CORRODED STA 109 CENTER AREA.SDR 97ZZZX1575Floor Beam · corrodedFLOOR BEAM CORRODED AT STA 712 RT.SDR 97ZZZX1574Floor Support · corrodedFLOOR SUPPORT CORRODED BETWEEN STA 681-712 RT.SDR 97ZZZX1573Hat Section · corrodedFUSELAGE HAT SECTION CORRODED STA 681, RT SIDE.SDR 97ZZZX1572Stringer · corrodedFUSELAGE STRINGER CORRODED, STA 698 RT.SDR 97ZZZX1571Stringer · corrodedFUSELAGE STRINGER 10 RIGHT, CORRODED STA 712.SDR 97ZZZX1560Skin · crackedSKIN CRACKED STA 140 STR 11R.SDR 97ZZZX1557Frame · crackedFRAME FLANGE CRACKED STA 641 OUTBOARD AT STR 25L.SDR 97ZZZX1556Belt Frame · corrodedBELT FRAME AT STA 698 CORRODED RT SIDE.SDR 97ZZZX1555Stringer · crackedSTRINGER 29R CRACKED STA 760.SDR 97ZZZX1554Skin · crackedSKIN CRACKED STR 29R, STA 798.SDR 97ZZZX1553Skin · crackedFUSELAGE INNER SKIN CRACKED STA 344 BETWEEN STR 13 AND 14R.SDR 97ZZZX1552Skin · crackedFUSELAGE SKIN INNER SURFACE CRACKED STA 420, STR'S 13, 14L.
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