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 = '1900C' 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 = '1900C' 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 YADA20170216001Flap System · failedFLAPS FAILED TO EXTEND.SDR JIKA2017021401Unknown · smokeIN CRUISE FLIGHT FROM KSMX TO KSBA WHEN HE NOTICED A BURNING SMELL AND SAW A SMALL AMOUNT OF SMOKE COMING FROM BETWEEN THE GLARE SHIELD AND THE INSTRUMENT BEZEL OF THE PILOT’S ATTITUDE INDICATOR. THE PILOT CHECKED ALL INSTRUMENTATION AND NOTED NO DEFECTS. THSDR JIKA2017020401Amplifier · shortedDURING ILS APPROACH THE LEFT RMI WENT INOPERATIVE FOLLOWED BY THE NUMBER TWO HSI TURNING 90 DEGREES AND PILOT SIDE ATTITUDE INDICATOR SHOWING A 15-30 DEGREE ROLL. EXECUTED A MISSED APPROACH AND INFORMED ATC OF THE ISSUE. ATC DIRECTED HIM TO HIS ALTERNATE KSJT.SDR TIMA20170203002Rib · crackedNUMEROUS CRACKS WERE FOUND IN THE VERTICAL STAB RIBS. THE CRACKS WERE LOCATED IN THE STRINGER TO RIB JUNCTIONS. SIX CRACKS WERE ON THE RIGHT SIDE AND SEVEN ON THE LEFT SIDE OF THE VERTICAL STAB.SDR YADA20170202001Stringer · corrodedDURING MAINTENANCE, COLLECTOR TANK INSPECTION. CORROSION WAS FOUND ON STRINGER STATION 305.7.SDR EPUA2017012517001Connector · failedDUAL GPS FAILURE DURING FLIGHT. AIRCRAFT RETURNED TO BASE DUE TO THIS FAILURE AND LANDED WITHOUT INCIDENCE. MAINTENANCE REPLACED THE NR 2 GPS (GNC420)UNIT AS WELL AS BOTH GPS ANTENNA TNC CONNECTORS.SDR JIKA201801220001Valve · bypassingTHE PILOT REPORTED THAT ON APPROACH TO KLBB WHEN THE LANDING GEAR WAS SELECTED “GEAR DOWN” THE PILOT DID NOT SEE THREE GREEN LIGHTS ON THE GEAR INDICATOR, THEN ALSO NOTICED THE GEAR CIRCUIT BREAKER HAD POPPED OUT. THE PILOT ATTEMPTED TO RESET THE CIRCUIT BREAKSDR JIKA2017011601Circuit Breaker · faultedPILOT WAS ON APPROACH AND WHEN THE LANDING GEAR WAS SELECTED TO THE DOWN POSITION. THE LANDING GEAR DID NOT EXTEND AND HAD NO INDICATION. THE PILOT THEN EXECUTED A LOW PASS AT AIRPORT TOWER AND COULD NOT VERIFY LANDING GEAR POSITION. THE PILOT FOLLOWING PROCEDSDR YADA20160109001Gusset · crackedDURING MAINTENANCE A,B,C STRUCTURAL INSPECTION, FOUND LT INTERCOSTAL GUSSET CRACKED AT FUSELAGE STATION 107. PART HAS BEEN REMOVED AND REPLACED IAW STRUCTURAL REPAIR MANUAL.SDR YADA20161231001Blower · burnedSMELL OF POSSIBLE ELECTRIC ON CLIMB.SDR TIMA20161213019Windshield · crackedTHE PILOT’S SIDE WINDSHIELD CRACKED DURING FLIGHT. THERE WAS A 3 INCH WIDE BAND OF SHATTERING OF THE OUTER LAYER THAT RAN FROM THE TOP TO THE BOTTOM OF THE WINDSHIELD ON THE INBOARD EDGE NEXT TO THE CENTER POST.SDR YADA20161130001Windshield · crackedLT WINDSHIELD CRACKED INFLIGHT.SDR TIMA20161125017Doubler · crackedDURING A SCHEDULED SIM CHECK, CRACKS WERE DISCOVERED IN THE DOUBLERS OF THE HORIZONTAL STABILIZER FORWARD ATTACHMENT TO THE VERTICAL STABILIZER. TWO, ONE INCH CRACKS WERE FOUND IN THE LT DOUBLER AND ONE, ONE1 INCH CRACK WAS FOUND IN THE RT DOUBLER. BOTH DOUBSDR YADA20161101001Buss Bar · burnedRIGHT GENERATOR FAILED LIGHT, RIGHT GEN TIE OPEN LIGHT, SECONDARY PROBLEM NR 1 NAV/CO AND TRANSPONDER FAILED WITH NO TRANMITT ON NR 1 COM. FOUND BURNED INSULATION ON RT GEN BUSS BAR AND REPLACED RT STARTER GEN.SDR YADA20161029001Ground Wire · disconnectedDURING DEPARTURE, RECIEVED A BATTERY CHARGE LIGHT THAT DID NOT EXTINGUISH. RETURNED TO DEPARTURE. RECONNECTED BATTERY GROUND TERMINAL AND PERFORMED OPS CHECKED OF BATTERY PASSED.SDR 2016F00213Window · blew outA PORTION OF THE COPILOT SIDE WINDOW DEPARTED THE AIRCRAFT DURING CLIMB AT 15,000 FT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. UPON INSPECTION, THE AIRFRAME STRUCTURE AND WINDOW FLANGE WERE NOT DAMAGED. THE REMNANTS OF THE EXISTING WINDOW WERE REMOVED, AND ASDR YADA20161014001Seal · debondedPILOT REPORTED WITH ENG BLEEDS OFF AND VENT ON HIGH, THE ODOR OF BURNING OIL/FUMES FILLED THE COCKPIT. PILOT HAD PREVIOUSLY REPORTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE WITH BLEEDS ON UNLESS TEMPERATURE SWITCH WAS HELD IN INCREASE & COCKPIT WAS EXTREMELY WASDR TIMA20160923015Unknown · fumesDURING CLIMB OUT, PILOT DETECTED FUMES COMING FROM THE CARGO AREA. THERE WAS NO VISIBLE SMOKE, ONLY A BURNING ODOR. THE FUMES CONTINUED UNTIL CABIN WAS DEPRESSURIZED. WHEN THE CABIN WAS RE-PRESSURIZED THE FUMES DID NOT RETURN. AIRCRAFT LANDED UNEVENTFULLY.SDR YADA20160917001Downlock Switch · failedNOSE GEAR DOWNLOCK SWITCH FAILED FOR WATER INTRUSION.SDR YADA20160908001Circuit Board · burnedTAIL STROBE CIRCUIT BOARD BURNED.SDR YADA20160901001Downlock Switch · out of rigRED HANDLE LIGHT ON, MAINS DOWN AND LOCKED NO NOSE GEAR GREEN LIGHT. GEAR WAS MANUALLY PUMPED DOWN TO GET 3 GREEN DOWN AND LOCKED LIGHTS. NOSE GEAR DOWN LOCK SWITCH RERIGGED.SDR YADA20160815001Wire · chafedSMOKE COMING FROM RIGHT WING TIP IN VICINITY OF FUEL VENT, FUEL FOUND ON UNDERSIDE OF WING NEAR HEATED FUEL VENT. MAINTENANCE REPLACED FUEL VENT ON RT WING DUE TO CHAFFING AND SHORTING WIRE ON OLD FUEL VENT.SDR TIMA20160810013Skin · corrodedCORROSION WAS FOUND ON THE RIGHT FUSELAGE SKIN ABOVE THE SEAT SIDE SUPPORT RAIL DURING MAINTENANCE.SDR TIMA20160810012Skin · corrodedCORROSION WAS FOUND ON THE RIGHT FUSELAGE SKIN ABOVE THE SEAT SIDE SUPPORT RAIL DURING MAINTENANCE.SDR TIMA20160810011Skin · corrodedFUSELAGE BELLY SKIN, CORROSION WAS FOUND DURING MAINTENANCE.SDR TIMA20160810010Seat Track · corrodedDURING MAINTENANCE, THE RIGHT SIDE SEAT TRACK WAS FOUND TO BE CORRODED.SDR YADA20160809001Rudder Pedal · frozenPILOT REPORT RUDDER PEDALS FROZEN AT ALTITUDE WITH YAW DAMP OFF. MAINTENANCE DISCOVERED AND REMOVED ICE AND WATER UNDER FLOOR BOARDS, CLEANED AND INSPECTED, OPS CHECKED GOOD.SDR EPUA20160728001Stringer · corrodedDURING SCHEDULED INSPECTION OF LEFT AND RIGHT SYSTEM MAIN FUEL TANK WING STATION 124 TO 130 FOR VIA X-RAY INSPECTION, CORROSION PITS WERE NOTED AT WING STATION 126 ON BOTH THE LEFT AND RIGHT WINGS AT STRINGER K. DEFECTS WERE REPAIRED IAW HAWKER BEECHCRAFT FIESDR YADA20160713001Windshield · crackedCOPILOT WINDSHIELD CRACKED IN FLIGHT. MAINTENANCE REPLACED COPILOT WINDSHIELDSDR EPUA20160709001Stringer · corrodedDURING SCHEDULED INSPECTION OF LEFT AND RIGHT MAIN FUEL TANK WING STATION 124 - 130 VIA X-RAY INSPECTION, X-RAY INSPECTION REVEALED CORROSION ON RIGHT COLLECTOR TANK STRINGER 6-7 INCHES IN FRONT OF RIGHT FUEL PUMP. REPAIRED BY SPLICING STRINGER IAW SRM 57-90SDR YADA20160629001Circuit Breaker · burnedCIRCUIT BREAKER PANEL STARTED SMOKING AFTER LANDING. FLIGHT CREW SHUTDOWN ACFT AND EVACUATED SAFELY. MAINTENANCE LOCATED AND REPLACED OVERHEATED 5 AMP CIRCUIT BREAKER FOR ENGINE INSTRUMENT LIGHTING.SDR YADA20160611001Unknown · odorWITH LT BLEED AIR OPEN EXHAUST ODOR IN CABIN, MAINTENANCE COULD NOT DUPLICATE ON GROUND RUNS. ACFT GOING INTO CAMP INSPECTION.SDR TIMA20160510009Powerpack · weakWHEN LANDING GEAR WAS LOWERED FOR LANDING THE TIME DELAY FEATURE OPENED THE CIRCUIT. PILOT USED MANUAL GEAR EXTENSION & LANDED UNEVENTFULLY. PROBLEM WAS FOUND TO BE A WEAK HYD POWER PACK.SDR TIMA20160509008Windshield · cracked3 TO 4 MINUTES AFTER LEVEL OFF AT FL230 THE RT WINDSHIELD INNER PLY DEVELOPED MULTIPLE CRACKS. PILOT LANDED AT THE NEAREST SUITABLE AIRFIELD. DESCENT & LANDING WAS UNEVENTFUL.SDR YADA20160504001Skin Panel · debondedPOST LANDING INSPECTION REVEALED THAT THE NR 1 ENG HAD A SEPARATION OF PN 114-980077-17 SKIN FROM THE PN 114-980077-5 BOND ASSEMBLY & WAS NO LONGER ATTACHED TO THE ACFT. MX VERIFIED THAT ALL BOND ASSEMBLY FASTENERS WERE IN PLACE & THAT THE FAILURE WAS THE BONSDR JIKA2016050301Bleed Valve · stickingTHE TRAINING CAPTAIN REPORTED WHILE PERFORMING TRAINING STALL MANEUVERS, THE FIRST OFFICER REDUCED POWER, A MOMENTARY COMPRESSOR STALL OCCURRED, BETWEEN 500 - 1000 FT & LBS TORQUE ON THE LT ENG. TRAINING CAPTAIN REDUCED POWER, THIS RESULTED IN ANOTHER STALL. SDR YADA20160501001Motor · burned outBURNING/SMOKE ODOR COMING FROM FRESH AIR VENTS WHEN BLOWER MOTOR ON. MAINTENANCE REPLACED AFT VENT BLOWER DUE BAD MOTOR.SDR YADA20160428001Rib · corrodedCORROSION FOUND BY X-RAY INSPECTION ON LOWER FLANGE LT ENG RIB PN 118-110050-5, ADJACENT TO FWD SPAR LOWER CAP. BLENDED & TREATED AREA.SDR EPUA20160428001Reinforcement · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED IN THE 101-430142-63 LOWER CLOSURE REINFORCEMENT, WHICH IS A PART OF KIT NR 114-4023-3, THAT WAS PREVIOUSLY USED TO REPAIR A CRACK IN THE AIRSTAIR DOOR BOND ASSEMBLY LOWER CLOSURE. THE DEFECTS FOUND REQUIRSDR YADA20160422001Printed Ckt Board · failedIN FLIGHT, AFTER LG HAD BEEN RETRACTED & STOWED, THE LG RELAY CB POPPED. THE LG HANDLE WAS SELECTED DOWN & CB PUSHED IN, CB POPPED AGAIN. MANUAL GEAR EXTENSION WAS THEN ACHIEVED. FOUND THE LG PUMP MOTOR BURNED. THE MOTOR WAS REPLACED AS WELL AS THE SUSPECTSDR JIKA2016033001Squat Switch · shortedDURING CLIMB OUT, THE PILOT REPORTED THAT DURING THE LG RETRACTION THE RED IN TRANSIT LIGHT REMAINED ILLUMINATED & THE LG WOULD NOT FULLY RETRACT. THE PILOT ATTEMPTED TO EXTEND THE LG & THE LG WOULD NOT EXTEND NORMALLY. THE PILOT EXTENDED THE LG USING THE EMSDR TIMA20160326006Bearing · failedPILOT EXPERIENCED AN UNCOMMANDED AILERON INPUT WHEN FLAPS WERE LOWERED FROM TAKEOFF TO APPROACH POSITION, DURING APPROACH. PILOT RETRACTED THE FLAPS TO TAKEOFF POSITION & THE INTERFERENCE WITH THE AILERON WAS ELIMINATED. ACFT WAS LANDED UNEVENTFULLY WITH FLASDR YADA20160312001Knob · brokenPILOT ALTIMETER ALTITUDE SELECTOR KNOB BROKEN, CAN'T SELECT ALTITUDE, BARO, IN COLLSMAN WINDOW. RETURNED TO DEPARTURE AIRPORT. REPLACED ALTIMETER.SDR YADA20160308001Frame · corrodedDURING STRUCTURAL INSPECTION, CORROSION WAS FOUND ON TOP FLANGE OF FUSELAGE FRAME AT FS 468.25. SUSPECT CORROSION WAS CAUSED BY CARGO SPILLAGE. FRAME WAS REPAIRED IAW SRM.SDR TIMA20160305005Sensor · intermittentWHEN GEAR WERE LOWERED FOR LANDING, DID NOT HAVE 3 GREEN GEAR LIGHTS. PILOT TRIED PRESS TO TEST OF BULBS & TURNED DIMMING OFF TO NO AVAIL. PILOT TERMINATED APPROACH & GOT VISUAL CONFIRMATION FROM TOWER THAT GEAR WAS DOWN. PILOT EVENTUALLY SAW ALL 3 GEAR LIGSDR CA160216023Motor · failed(CAN) FLIGHT CREW REPORTED ELECTRICAL SMOKE ODOR IN FLIGHT DECK. FLAP MOTOR FOUND U/S AND CIRCUIT BREAKER TRIPPED.SDR YADA2016FA0000077Flap System · failedFLAPS WOULD NOT RETRACT FROM TAKEOFF TO UP. RETURNED TO DEPARTURE AIRPORT. UNEVENTFUL LANDING MADE FLAPS WORKED ON GROUND AFTER LANDING - MAINTENANCE VERIFIED FLAPS UP AND SECURE - DEFERRED. MAINTENANCE REPLACED FLAP MOTOR RELAY AFTER THE NEXT FLIGHT AND PROBSDR JIKA2016013103Fire Loop · defectiveAFTER TAKEOFF, DURING CLIMB, THE PILOT REPORTED THAT THE RT ENG FIRE WARNING LIGHT ILLUMINATED. THE PILOT SHUTDOWN THE RT ENG & EXTINGUISHED THE RT ENG FIRE BOTTLE. THE PILOT DECLARED AN EMER & LANDED WITHOUT INCIDENT. FOUND THE RT ENG FIRE DETECTION LOOP HSDR JIKA2016010802Check Valve · malfunctionedDURING CRUISE FLIGHT, THE PILOT NOTICED A STRONG ODOR THAT SMELLED LIKE JET FUEL, FOLLOWED BY A SMALL PUFF OF SMOKE FROM THE LT AIR VENT. THE PILOT DESCENDED BELOW 12,000 FT & PERFORMED CABIN PRESS DUMP. THE PILOT ADVISED ATC OF CONDITION, RETURNED & LANDED SDR TIMA20160108001Pressure Switch · faultyIMMEDIATELY AFTER ROTATION THE LT PROPELLER AUTO FEATHERED. PILOT REDUCED POWER & IMMEDIATELY LANDED, ABORTING THE TAKEOFF. THE PROBLEM WAS DISCOVERED TO BE A FAULTY AUTO FEATHER LOW PRESS SWITCH.
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