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 = '402B' 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 = '402B' 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 XGN2006F00029Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR TZR2005F00012Cylinder · crackedCYLINDER CRACKED FROM EXHAUST VALVE. (K)SDR XGN2006F00027Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR 2004F00430Turbine Wheel · excess playSHORTLY AFTER DEPARTURE FROM SIOUX, THE PILOT NOTICED THE LEFT ENGINE MANIFOLD PRESSURE DROPPING OFF AND THE ENGINE LOSING POWER. ALL OTHER ENGINE INDICATORS SHOWED NORMAL BUT, AS A PRECAUTION, THE LEFT ENGINE WAS SHUT DOWN AND SECURED. THE PILOT RETURNED TOSDR XGN2006F00031Cylinder · crackedCYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)SDR 2008F00023Pushrod · failedENGINE HAD MANIFOLD AND FUEL PRESSURE VARIATION IN FLT, THE ACFT BEGAN TO VIBRATE AND THE PILOT SHUTDOWN ENGINE. THE NR 1 AND NR 2 ROD`S FAILED AND SEPARATED FROM THE CRANKSHAFT AND CREATED (2) LARGE HOLES IN THE CASE AND KNOCKING BOTH MAGNETOS LOOSE. THERE ASDR CA040930006Pad · missing(CAN) AFTER FLIGHT, PILOT SAW ON RT PROPELLER, ONE PROP DE-ICE PAD MISSING ON ONE BLADE. AFTER INSPECTION OF THE DEFECT, WE SAW THE GLUE WAS NOT HARD. THE DE-ICE PAD WAS INSTALLED AT O/H SHOP WITH NEW KIND OF GLUE. WE REMOVED THE OLD GLUE AND REINSTALLED A NSDR FAAJIKA81204Bellcrank · wornAT 13000 FT PIC GOT DOOR OPEN IND LITE, WHEN HE WHEN TO CLOSE DOOR CAME OPEN IN FLIGHT. INVESTIGATION REVEAL BELLCRANK ASSY WORN. MM DOES NOT REQUIRE PULL TEST OF THE BREAK OVER PRESS OF THE HANDLE. LATER MODEL HAS DIFFERENT CONFIG HANDLE ASSY.SDR T4C2004F00001Screw · brokenTHIS AIRCRAFT WAS STOPPED, WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION A BOLT NAS 464P4-26 AND ADJUSTING SCREW 0841113-1 WERE BROKEN. NOT SURE WHICH BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVERY 5 YEARS OR 5000 HOUSDR T4C2004F00000Bolt · brokenTHIS AIRCRAFT WAS STOPPED WAITING TO TAXI, WHEN THE LT GEAR COLLAPSED. UPON INSPECTION, A BOLT NAS464P4-26 AND ADJUSTING SCREW 0841113-1 WERE BROKEN. UNSURE WHICH WAS BROKE FIRST. RECOMMEND THAT ALL BOLTS ON LANDING GEAR BE REPLACED EVERY 5 YEARS OR 5000 HOSDR 2004F00145Idler Gear · brokenFOLLOWING TAKE OFF, THE PILOT NOTICED THAT THE LT ENGINE WAS TRAILING SMOKE AND OIL. THE ENGINE WAS SHUT DOWN AND SECURED AND THE AIRCRAFT RETURNED TO THE AIRPORT AND MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION IT WAS DETERMINED THAT DURING START UP, THE ENSDR FFK2004F00004Pump · failedAFTER INSTALLING AN ENGINE WITHIN 3 FLIGHT HOURS THE ENGINE DRIVEN FUEL PUMP SHAFT FAILED. PUMP FAILED ON TAKEOFF AND QUIT RUNNING.SDR 2004FA0000391Rib · crackedRAMP INSP FOUND OIL CANNING IN LT WING OF HIGH TIME. WING WAS INSPECTED AND ONLY DEFECT FOUND WAS LWR FLANGE ON 4 OF INTERSPAR RIBS WERE CRACKED AT STRINGER PASS-THROUGH. CRACK WAS .5-.75 INCHES LONG AND USUALLY EXTENDED PAST FIRST RIVET. AFTER REPAIRING IAWSDR 2004FA0000336Rib · crackedFOUND OIL CANNING IN LT WING OF HIGH TIME WHEN LIFTING AFT END OF TIP TANK. WING WAS INSPECTED AND ONLY DEFECT WAS LWR FLANGE ON 4 OF INTERSPAR RIBS WERE CRACKED, STRINGER PASS-THROUGH. CRACK WAS .5-.75 INCHES LONG, EXTENDED PAST FIRST RIVET. AFTER REPAIRINGSDR AUS20040191Wire · faulty(AUS) TRANSPONDER WIRING SUSPECT FAULTY. TRANSPONDER AND GPS WIRING PARALLEL WHICH CAN CAUSE INACCURATE ALTITUDE READINGS.SDR TZR2004F00002Magneto · corrodedPILOT REPORTED AN EXCESSIVE MAGNETO DROP ON LT AND RT MAGNETOS. UPON FURTHER INSPECTION FOUND THE MAGNETOS FULL OF CORROSION AT HARNESS CONNECTION AND IN THE AREA WHERE POINTS ARE LOCATED. THIS AIRCRAFT HAD NOT BEEN FLOWN IN A WHILE AND HANGARED FOR MOST OF SDR XGN2004F00002Safety Switch · inoperativeNOSE GEAR LIGHT WOULD NOT ILLUMINATE AND THE GEAR WARNING HORN WAS GOING OFF ON APPROACH. PILOT DID A FLY BY THE TOWER TO VERIFY NOSE GEAR DOWN. AIRCRAFT LANDED WITHOUT INCIDENCES AND NOSE GEAR LIGHT ILLUMINATED AFTER TOUCH DOWN AND GEAR WARNING HORN ALSO SHSDR VAZ2004F00001Web · crackedNLG WW WEB FOUND CRACKED AT THE RT PIVOT POINT OF THE NOSE GEAR RETRACTION LINKAGE.SDR VAZ2004F00000Linkage · crackedPARTS WERE FOUND CRACKED AT THE RT PIVOT POINT OF THE NOSE GEAR RETRACTION LINKAGE OF AIRCRAFT.SDR 2004F00215Connecting Rod · brokenENGINE FAILED IN FLIGHT FROM HNL TO MKK, NR 1 CYL CONNECTING ROD BROKE OFF AT FLT ALT. 1,500 FEET 27 INCHES OF MANIFOLD, 2300 RPM. AIRCRAFT RETURNED TO HNL. (M)SDR XGN2004F00000Bolt · brokenTHE NOSE GEAR WOULD NOT RETRACT AFTER DEPARTURE. AIRCRAFT LANDED WITHOUT PROBLEMS. FOUND THE NOSE GEAR RETRACT FORK BOLT BROKEN. THE BOLT SEPARATED AT THE LAST THREAD BEFORE WHERE THE SHANK STARTS. THE BELLCRANK THAT THE BOLT SCREWS INTO WAS ALSO DAMAGED ASDR 2003F00640Limit Switch · stuckFOLLOWING DEPARTURE, THE PILOT SELECTED THE LANDING GEAR UP POSITION. THE GEAR IN TRANSIT LIGHT ILLUMINATED AND THE GEAR RETRACTED AS NORMAL UNTIL IT REACHED THE FULL UP POSITION. THE PILOT HEARD THE GEAR MOTOR PULL HARD AND THEN THE GEAR MOTOR CIRCUIT BREAKERSDR 2003FA0001120Torque Tube · tornDURING A UNSCHEDULED INSPECTION, AFTER A PILOT REPORT OF THE RT LANDING GEAR NOT RETRACTING, THE MECHANIC FOUND THE RT MAIN GEAR TORQUE TUBE BROKEN OR TORN. IT IS SUSPECTED THAT FATIGUE COULD BE THE CAUSE.SDR 2003F00518Control Cable · brokenWHILE ON APPROACH AND EXTENDING FULL FLAP POSITION, THE PILOT HEARD A LOUD BANG AND THE AIRPLANE BEGAN TO ROLL LEFT. HE THEN RETRACTED THE FLAPS AND MADE AND UNEVENTFUL LANDING.SDR 2003FA0000656Wire · brokenDURING INSPECTION OF THE GEAR, FOUND WIRE SPLICE BROKEN.SDR CA030523005Fork · sheared(CAN) PILOT REPORTS GEAR WOULD NOT RETRACT ON TAKE OFF. HE ELECTED TO LEAVE DOWN FOR FLIGHT MAINTAINING PROPER SPEED.ON LANDING TRUCKS WERE REQUESTED BUT NO EMERGENCY DECLARED. LANDING WAS UNEVENTFUL. WHEN MAINTENANCE INSPECTED GEAR THEY FOUND ADJUSTING FORSDR CA030521008Tire · blown(CAN) ON LANDING THE RT MAIN WHEEL BLEW. A/C WAS STOPPED SAFELY ON THE RUNWAY AND THEN TOWED OFF ONTO THE NEAREST TAXIWAY. AFTER THE RIM WAS INSPECTED AND THE TIRE REPLACED THE A/C WAS DISPATCHED FOR THE NEXT FLIGHT.SDR BLI2003F00002Wheel · crackedDURING INSPECTION, FOUND MAIN LANDING GEAR WHEEL CRACKED. REPLACED WHEEL ASSEMBLY WITH NEW.SDR CA030225006Oil Cooler · cracked(CAN) OIL COOLER UPPER WELD CRACKED ACROSS.SDR CA030218009Oil Cooler · cracked(CAN) WE DISCOVERED CRACKS DEVELOPING AROUND WELDS ON THE ATTACHING POINTS OF THE OIL COOLER. INSTALLATION PROCEDURE INCLUDING TORQUE, AND ALL THE ATTACHING HARDWARE, WERE CORRECTLY FOLLOWED.SDR 2003F00121Landing Gear · collapsedUPON LANDING, DURING ROLL OUT, THE RT MLG COLLAPSED. THE PILOT WAS INTERVIEWED AND STATED THAT HE HAD ALL THREE GREEN DOWN AND LOCKED INDICATION. UPON INVESTIGATION OF THE LANDING GEAR, ALL DAMAGE WAS LIMITED TO THE RETRACTION/EXTENSION LINKAGE, SPECIFICALLY TSDR 2003FA0000021Bulkhead · crackedINSPECTION IAW AD. CRACK WAS FOUND IN RIGHT ENGINE CANTED BULKHEAD CAP. CRACK WAS LOCATED ON INBOARD SIDE OF CAP JUST INSIDE OF INBOARD WING LIP. CRACK WAS APPROXIAMATELY 1.5 INCHES AND RAN CHORD WISE WITH THE WING, IT WAS LOCATED IN THE AFT OF THE CAP WIDTSDR 2003FA0000020Bulkhead · crackedWHILE CONDUCTING INSPECTION IAW AD 00-01-16(D)A CRACK WAS FOUND IN THE RIGHT ENGINE CANTED BULKHEAD CAP. CRACK WAS LOCATED ON THE INBOARD SIDE OF CAP JUST INSIDE OF THE INBOARD WING LIP. CRACK WAS APPROXIAMATELY 1.5 INCHES AND RAN CHORD WISE WITH THE WING. SDR 2003FA0000019Bulkhead · crackedINSPECTION IAW AD, A CRACK WAS FOUND IN THE RT ENGINE CANTED BULKHEAD CAP. CRACK WAS LOCATED ON THE INBOARD SIDE OF CAP JUST INSIDE OF INBOARD WING LIP. CRACK WAS APPROXIAMATELY 1.5 INCHES AND RAN CHORD WISE WITH WING. IT WAS LOCATED IN THE AFT OF THE CAP WSDR OIK2003F00000Wire · inoperativeDURING GEAR EXTENSION, UPON LANDING, PILOT NOTICED THE RIGHT GREEN LIGHT WAS NOT ILLUMINATED. EMERGENCY LANDING ASSISTANCE WAS REQUESTED ON INSPECTION OF THE LANDING GEAR. A BROKEN WIRE WAS FOUND ON THE GEAR SWITCH DOWN LOCK SYSTEM. REPAIR WAS MADE GEAR GROSDR CSS2003F00000Engine · surgesENGINE SURGED, POWER LOSS, AND WAS SHUT DOWN IN FLIGHT.SDR 2002FA0001392Wire · brokenON TAKEOFF PILOT OBSERVED SMOKE AND SPARK FROM BEHIND INSTRUMENT PANEL. BROKEN WIRE WAS FOUND FROM POST LIGHT SOCKET CONNECTOR. REPLACED CONNECTOR. OPS CHECK OF DASHBOARD LIGHTING FOUND, OK.SDR QTVA901UControl Cable · brokenON SHORT FINAL, HEARD A THUD IN FLOORBOARDS. JUST AFTER PUTTING GEAR DOWN. AIRCRAFT HAD A SLIGHT YAW AND ROLL AND LANDED UNEVENTFULLY. TAXIED IN, SELECTED FLAPS UP AND SHUTDOWN AIRCRAFT. DURING POSTFLIGHT NOTICED FLAPS WERE STILL FULLDOWN. MAINTENANCE INSSDR 2002FA0001060Switch · faultyLANDING GEAR WILL NOT RETRACT. DURING NORMAL TAKEOFF, FAULTY SWITCH FOUND ON. SAFETY SWITCH ASSEMBLY ON LT MLG ASSEMBLY. REPLACED SWITCH AND CHECK OPS OK. AIRCRAFT RETURNED TO SERVICE.SDR 081620027947QEscape Hatch · separatedBETWEEN SLC & TWF PILOT REPORTED A LOUD BOOMING/STRIKING NOISE, AS IF HE HAD HIT A BIRD. UPON INVESTIGATION HE NOTICED THE ESCAPE HATCH WAS MISSING. HE NOTIFIED SALT LAKE CENTER OF THE SITUATION. NO OTHER DAMAGE WAS NOTICED. THE PILOT SLOWED THE AIRCRAFT AND CSDR AUS20020788Barrel · broken(AUS) NOSE LANDING GEAR SHIMMY DAMPER BODY BROKEN AWAY FROM ATTACHMENTLUG.SDR MHJ2002F00004Transfer Pump · inoperativeTHESE PUMPS ARE A CONTINUAL PROBLEM WITH MFG. IN THIS CASE BOTH PUMPS WERE INOPERATIVE. SOMETHING NEEDS TO BE DONE DIFFERENT.SDR 2002FA0000785Gear · wornDURING LANDING GEAR RETRACTION PILOT REPORTED LAND GRINDING NOISE. CAUSED BY WORN OUT GEAR BOX INTERNAL SYSTEM. INSPECTED WORN OUT GEARS TOOTH.SDR CA020607011Trunnion · cracked(CAN) WHILE PERFORMING AN NDT INSPECTION ON THE NOSE GEAR TRUNNION LUGS. IT WAS DISCOVERED THAT ONE OF TWO LUGS HAD A CRACK OF APPROXIMATELY 1 1/2 INCHES AROUND THE CIRCUMFERENCE. THIS WAS BEYOND ANY SERVICEABLE LIMIT, CAUSING THE UPPER TRUNNION ASSEMBLY TO BESDR 2002F00429Bolt · brokenUPON REACHING DESTINATION THE PILOT SELECTED GEAR DOWN AND THERE WAS NO GREEN LIGHT FOR THE NOSE GEAR. THE GEAR WAS CYCLED AND MANUAL EXTENSION TRIED TO NO AVAIL. RETURNED TO HOME BASE AND MANEUVERED THE AIRCRAFT IN AN ATTEMPT TO SWING THE GEAR OVER CENTER, SDR 2002F00360Control Cable · brokenWHILE ON APPROACH THE PILOT SELECTED HIS APPROACH FLAP SETTING OF 15 DEGREES. UPON DOING SO HE HEARD A BANG AND THE AIRCRAFT BEGAN A SLIGHT ROLL TO THE RIGHT. HE THEN RETRACTED THE FLAPS, WHICH CORRECTED THE SITUATION. HE CONTINUED HIS APPROACH AND MADE AN UNESDR 2002FA0000958Igniter · overheatedNITE IMC HAD SUDDEN ELECTRIAL SMELL AND SMOKE IN COCKPIT. PILOT SHUT DOWN TOTAL ELECTRICAL SYSTEM SMELL AND SMOKE CLEARED. WHILE TROUBLESHOOTING FOUND INGNITION UNIT ON HEATER HAD OVERHEATED AND STARTED TO MELT DOWN CHANGED UNIT SYSTEM OPS CHECKED GOOD.SDR AUS20020048Connecting Rod · failed(AUS) RH ENGINE INTERNAL FAILURE. INSPECTION FOUND HOLES IN THE FORWARD END OF THE CRANKCASE IN THE AREA OF NO5 AND NO6 CYLINDERS. ON DISASSEMBLY MASSIVE INTERNAL DAMAGE FOUND. CONNECTING ROD FOUND IN SUMP. CAMSHAFT BROKEN. SUSPECT CONNECTING ROD OR CONNECTINGSDR 2002FA0000032Bushing · corrodedBEARING PART OF BUSHING, NOT TAKING GREASE. DISASSEMBLE AND PHYSICALLY INSPECT BOTH. FOUND CORRODEDSDR 2002FA0000009Gearbox · wornDURING GEAR EXTENSION, PILOT REPORTED A LOUD NOISE. REPORTED 3 GREEN LIGHTS FOR DOWN AND LOCK GEAR INDICATION, AND EMERGENCY LANDING ASSISTANCE WAS REQUESTED, AIRCRAFT LANDED SAFELY AND TAXIED TO THE MAINTENANCE FACILITY, UPON INSPECTION OF THE LANDING GEAR
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