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 = '73736Q' 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 = '73736Q' 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 CA191205007Adapter · failed(CAN) LPV APPROACH ANOMALY: GLIDE SLOPE DEVIATION POINTER MOMENTARILY SCALLOPED UP FOR A SPLIT SECOND AT FINAL APPROACH FIX ON RNAV LPV APPROACH TO RUNWAY. THIS RESULTED IN THE AUTOPILOT MOMENTARILY PITCHING THE AIRCRAFT NOSE UP FOLLOWING THE GLIDE SLOPE SCALLSDR CA140811011Clutch · undertorqued(CAN) ON FLAP EXTENSION TO 15 UNITS AND BEYOND, THE AIRCRAFT EXPERIENCES A ROLL THAT REQUIRES A TRIM INPUT. WHEN THE FLAPS ARE AT 15, 1.5 UNITS LT ROLL TRIM REQUIRED TO KEEP AIRCRAFT LEVEL. WHEN THE FLAPS ARE AT 30, 2.5 UNITS OF LT ROLL TRIM TO KEEP AIRCRAFT LSDR CA140707008Jackscrew · failed(CAN) ON THE 27TH OF JUNE 2014 THE ACFT WOULD NOT DEPLOY THE FLAPS BEYOND 27 DEGREES IN FLIGHT. ON THE GROUND THE FLAP SYS OPERATED CORRECTLY. THE AMM TROUBLESHOOTING PROCEDURE WAS FOLLOWED AND A COUPLE SCREW JACKS THAT WERE MARGINAL FOR THE TORQUE CHECK WERESDR CA140311005Tie Bolt · failed(CAN) REJECTED TAKEOFF WHERE TWO MAIN WHEELS ON THE LT MLG BLEW OUT AT APPROXIMATELY 100 KNOTS. THE CREW NOTICED THE VIBRATION, REJECTED THE TAKEOFF, AND HAD THE AIRPORT PERSONNEL CONFIRM THAT THE WHEELS HAD BLOWN. WHEN MAINTENANCE REMOVED THE DAMAGED WHEEL SDR CA130830014Cable · frayed(CAN) ON APPROACH CREW INDICATED THAT THEY HAD TO ADD MORE AILERON TRIM FOR EACH SELECTION OF FLAPS. WHEN FLAPS 40 WERE SELECTED THE CREW HAD TO HAVE LT AILERON TRIM OF 2.5-3.0 SELECTED TO MAINTAIN LEVEL FLIGHT. MAINTENANCE FOUND THE LT INBD FLAP, AFT FLAP BSDR CA110627018Bearing · stiffPILOT COMPLAINT OF ELEVATOR BEING STIFF, FOUND BEARING VERY HARD TO TURN, BEARING REPLACED ACFT RETURNED TO SERVICE.SDR F3LA200500004Floorbeam · brokenDURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AND WEB BROKEN AT STA 685 FROM LT FRAME TO SEAT TRACK BEAM. REPLACED L STUB FRAME PER SRM 51-40-02 AND 51-10-02.SDR F3LA200400118Control Cable · out of adjustFLIGHT CREW REPORTED ON SHORT FINAL APPROACH, FULLY CONFIGURED AILERON ROLL FELT TO BIND. ALL OTHER PHASES OF FLIGHT NORMAL. ADJUSTED LT AND RT AILERON BOS CABLES TO BRING LT AILERON WITHIN LIMITS.SDR F3LA200400111Warning Light · false indicationREJECTED TAKEOFF. FLIGHT CREW REPORTED FWD ENTRY DOOR LIGHT ILLUMINATED. CHECKED DOOR PROXIMITY SENSOR PER MM 52-71-11 AND CHECKED NORMAL.SDR F3LA200300124Panel · misinstalledABORTED TAKEOFF. DURING TAKEOFF ROLL, FLIGHT CREW REPORTED AIRCRAFT WOULD NOT STEER TO LT. TAKEOFF REJECTED AT APPROXIMATELY 60 KNOTS. FOUND LOWER SIDEWALL PANEL IN FLIGHT DECK, RT SIDE BETWEEN STA 178 AND 254, IMPROPERLY INSTALLED AND INTERFERRING WITH FIRSDR F3LA200200390Intercostal · corrodedDURING C-6 CHECK, INSPECTION REPORTED INTERCOSTAL AT STR. 26-R BETWEEN STA.747-767 CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER DRAWING 69-16500, ITEM 4, AND SRM 51-40-02.SDR F3LA200200257Skin · damagedDURING C-5 CHECK, INSPECTION REPORTED 3 CREASES ON TOP SURFACE OF RIGHT INBOARD FOREFLAP. REMOVED, REPAIRED AND REINSTALLED RT INBOARD FOREFLAP PER MM 27-51-07, SRM 57-53-02 AND SRM 51-70-10.SDR F3LA200200252Skin · gougedDURING C-5 CHECK, INSPECTION REPORTED SMALL GOUGE IN OUTER FUSELAGE SKIN AT BS 203, STR 18R. REPAIRED DAMAGE PER SRM 53-00-01 FIG 202.SDR F3LA200100091Actuator · leakingAIR TURN BACK. FLIGHT CREW REPORTED "B" SYSTEM ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED AND LOSS OF "B" SYSTEM HYDRAULIC FLUID. MAINTENANCE REPLACED NO. 2 ENGINE DRIVEN HYDRAULIC PUMP AND NO. 5 LEADING EDGE SLAT ACTUATOR.SDR F3LA200100006Control Unit · malfunctionedUPON ARRIVAL, MAINTENANCE REPORTED CARGO COMPARTMENT FIRE DETECTION/SUPPRESSION SYSTEM OK LIGHT WOULD NOT ILLUMINATE. REPLACED CENTRAL CONTROL UNIT AND SYSTEM CHECKED OK. SYSTEM WAS ACTIVATED ON 1/12/01.SDR F3LA00152Skin · damagedLGA - FLT 417 - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED BELT LOADER STRUCK AIRCRAFT AFT OF FORWARD CARGO DOOR, SECTION 43, FS 500, BETWEEN STRINGER 23R AND 25R, CREATING A VERTICAL HOLE IN THE FUSELAGE SKIN APPROXIMATELY 12 TO 14 INCHES LONG. MAINTENANCE INSSDR F3LA00119Light · inoperativeSFO - PRIOR TO DEPARTURE, MAINTENANCE REPORTED EMERGENCY FLOOR PROXIMITY PATH LIGHTING INOPERATIVE AT ROWS 6 THROUGH 11. MAINTENANCE REPAIRED FAULTY GROUND WIRE PER EA 25-737-064. (M)SDR F3LA00003Battery · dischargedDEN - DURING C-3 CHECK INSPECTION, REPORTED AFT ENTRY DOOR ESCAPE SLIDE BATTERY FAILED BATTERY CHECK. MAINTENANCE REPLACED AFT ENTRY DOOR ESCAPE SLIDE. (M)SDR F3LA99047Battery · dischargedDEN - DURING C-CHECK INSPECTION REPORTED L-2 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOTLAGE TEST. REPLACED L-2 EMERGENCY ESCAPE SLIDE. CYCLES: 2,724. (X)SDR F3LA99046Battery · dischargedDEN - DURING C-CHECK, INSPECTION REPORTED L-1 EMERGENCY ESCAPE SLIDE BATTERY FAILED VOLTAGE TEST. REPLACED L-1 EMERGENCY ESCAPE SLIDE. CYCLES: 2,724. (X)SDR F3LA98173Bolt · missingUPON ARRIVAL, FLIGHT CREW REPORTED NR 2 LEADING EDGE FLAP INDICATOR SHOWED FLAP IN EXTENDED MODE AT ALL SETTINGS. MAINTENANCE INSTALLED MISSING BOLT AND NUT ASSY AT ATTACH FITTING FOR FLAP AND TAIL GATE ASSY AND CHECKED OK. (M)SDR F3LA98003Bolt · missingSEA - FLT 640 - AIR TURN BACK. FLIGHT CREW REPORTED LEADING EDGE FLAPS/SLATS WOULD NOT FULLY RETRACT WHEN TRAILING EDGE FLAPS SELECTED TO '0' DEGREES. MAINTENANCE FOUND BOLT (P/N NAS1104-8), NUT (P/N NAS6794W), AND WASHER (P/N 960D416) MISSING FROM THE LEADI
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