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 = '1900D' 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 = '1900D' 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 CA051130008Starter Gen · failedATTEMPTED TO START THE LEFT ENGINE BUT NO SUCCESS. MAINTENANCE WAS NOTIFIED AND AIRCRAFT BROUGHT BACK INTO HANGAR. SYSTEM INSPECTED AND FOUND THAT STARTER GENERATOR AT FAULT. REPLACED STARTER GENERATOR AND ENGINE RUN PERFORMED. SYSTEM CHECKED SATISFACTORY SDR S2YA05078Windshield · crackedDURING FLIGHT, THE RT WINDSHIELD DEVELOPED A CRACK FROM TOP TO BOTTOM. THE CREW LANDED SAFELY AND THE AC WAS FERRIED BACK. MX REPLACED TH RT WINDSHIELD AND RETURNED TO AC TO SERVICE. (K)SDR CA051129002Spring · fracturedDURING TAXI, THE FLIGHT CREW NOTICED A FULL LEFT BIAS DEFLECTION IN THE AILERON SYSTEM. MAINTENANCE FOUND ONE OF THE AILERON INTERCONNECT SPRINGS HAD FRACTURED AT THE END RING THAT PROVIDES CONNECTION TO THE BRIDLE. IT IS FELT THAT THE ISSUE MAY HAVE BEEN INSDR S2YA05075Altimeter · malfunctionedON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE CAPTAIN`S ALTIMETER FLAGGED SHORTLY AFTER ROTATION AND STAYED FLAGGED. THE CREW PERFORMED AND AIR-TURN-BACK. UPON ARRIVAL BACK, THE ALTIMETER BEGAN TO WORK AGAIN. MX REPLACED THE AITIMETER AND RETURNED THE AC TOSDR 11042005ACircuit Breaker · trippedGEAR WOULD NOT COME UP AFTER TAKEOFF. RESET LANDING GEAR CONTROL CIRCUIT BREAKER. CYCLED LANDING GEAR FOUR TIMES, OPS CHECK GOOD.SDR 73843Brake · weakUPON LANDING, CAPT'S NOTED BOTH BRAKES WEAK WHEN APPLIED. CREW TAXIED TO THE GATE WITH NO FURTHER INCIDENT. PHONED MAINTENANCE CONTROL, OUTSIDE MAINTENANCE WAS CALLED AND BRAKES WERE BLED. OPS CHECK NORMAL. THEREFORE NO PARTS WERE USED.SDR S2YA05071Uplock Switch · inoperativeON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE RED IN TRANSIT LIGHT STAYED ILLUMINATED AFTER THE GEAR WAS SELECTED UP AND APPARENTLY DID FULLY RETRACT. THE RELEASE WAS AMENDED AND THE AC CONTINUED WITHOUT STOPPING. MX REPLACED THE NOSE GEAR UPLOCK SWITCH AND SDR S2YA05072Pressure Switch · inoperativeON TAKEOFF OF FLIGHT, THE CREW REPORTED THE RT ENVIRONMENTAL BLEED AIR SYSTEM FAILED AND ABORTED THE TAKEOFF. THE SYSTEM WAS PUT ON MEL AND THE AC WAS RETURNED TO SERVICE. REPLACED A BAD PRESSURE SWITCH AND WITH NO FURTHER DISCREPANCIES RETURNED THE AC TO SESDR 11022005ARelay · failedFLAPS STUCK AT 17 DEGREES. REMOVED AND REPLACED FLAP CONTROL RELAY OPS CHECK NORMAL, P/N SM50D7.SDR 11012005AAutofeather Sys · malfunctionedIN FLIGHT, LEFT ENGINE AUTOFEATHER LIGHTS LIGHTS EXTINGUISHED WITH POWER AT 3750 TORQUE. REMOVED AND REPLACED LT ENGINE AUTOFEATHER PRESSURE SWITCH PN 50-389121-21, SN ON 10015, SN OFF UNKNOWN.SDR S2YA05070Altimeter · stickingON CLIMB OUT OF FLIGHT, THE CREW REPORTED THE CAPTAIN`S ALTIMETER FROZE UP (STOPPED CLIMBING) WERE PERFORMEING AN AIR-TURN-BACK. UPON ARRIVAL BACK, THE ALTIMETER BEGAN TO WORK AGAIN. MX REPLACED THE ALTIMETER AND RETURNED THE AC TO SERVICE. (K)SDR S2YA05069Bracket · inoperativeDURING FLIGHT, THE CREW REPORTED THE CARGO DOOR ANNUCIATOR ILLUMINATED AND WERE PERFORMING AN AIR-TURN-BACK. THE ANNUCIATOR WAS MEL`D AND THE AC WAS RETURNED TO SERVICE. MX REPLACED THE ACTUATOR BRACKET AND CLEARED THE MEL. (K)SDR 105092102690Stringer · crackedFOUND STRINGER 3R AT FS 163.9. CRACKED. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE. THEREFORE NO PARTS WERE USED.SDR 105092102666Frame · crackedFOUND CRACKED INNERSKIN AND FRAME (ASD) STA 150.6. MAINTENANCE REPAIRED THE PROBLEM.SDR 1050921026131Splice Plate · crackedFOUND FS 434 CRACKED SPLICE PLATE SIDEWALL. MAINTENANCE REPAIRED THE SPLICE PLATE SIDEWALL.SDR 1050921026160Stringer · crackedFOUND STRINGER 3R AT FS 163.9 CRACKED. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.SDR 1050921026090Stringer · corrodedCORRSION FOUND ON FASTENERS FS 150-183 AND STRINGER 1-3R. MAINTENANCE REMOVED CORROSION AND TREATED FASTENERS WITH ALODINE.SDR 1050921026120Angle · crackedFOUND LEFT FS 400 1 FT ABOVE FLOOR CRACKED. MAINTENANCE FABRICATED REPAIR ANGLE AND INSTALLED.SDR 1050921026072Frame · crackedFOUND FRAME ANGLE AT FS 456 CRACKED. MAINTENANCE INSPECTED AND NO CRACKS WERE NOTED. THEREFORE NO PARTS WERE USED.SDR 1050921026071Stringer · crackedSTRINGER 12 AT FS 456 RT CRACKED. MAINTENANCE REPAIRED STRINGER WHILE AIRCRAFT WAS IN STRUCTURAL REPAIR.SDR 1050921026Frame · crackedCRACKED INNER SKIN AND FRAME. MAINTENANCE REPAIRED IAW SRM 51-70-00 AND 51-70-15. MORE INFORMATION WILL BE AVAILABLE AT A LATER TIME.SDR S2YA05067Pressure Switch · inoperativeDURING FLIGHT, THE CREW REPORTED THE RT AUX PUMP AUTO FUNCTION DID NOT STOP THE PUMP, RT NO AUX TRANSFER ILLUMINATED WHEN PUMP WAS IN AUTO FUNCTION. BETWEEN MX AND OPS, IT WAS DECIDED AN AIR-TURN-BACK WAS THE BEST OPTION. MX INSPECTED THE SYSTEM BUT COULD NOSDR 73619Bolt · unknownAFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED BOLT IN RIGHT SQUAT SWITCH.SDR AMWA73619Landing Gear · malfunctionedAFTER TAKEOFF, CREW UNABLE TO RETRACT LANDING GEAR. RETURNED TO FIELD WITH NO FURTHER INCIDENT. MORE INFORMATION WILL BE AVAILABLE AT A LATER DATE.SDR 10212005AFire Detector · malfunctionedRT FIRE LOOP ANNUNCIATOR ILLUMINATED DURING RUNUP AND REMAINS ON. INSPECTED FIRE LOOPS, CANNON PLUGS AND A319 NO DEFECTS NOTED. REMOVED AND REPLACED FIRE DETECTION CONTROL UNIT. OPS CHECK GOOD, PN 477-90005, SN 9036-005.SDR 10172005AFire Detector · malfunctionedRT FIRE LOOP STUCK IN TEST MODE. INSPECTED FIRE LOOP NO DEFECTS FOUND, INSPECTED CONTROLLER AND C/B, NO DEFECTS NOTED, DISCONNECTED LOOP AT FIREWALL, FIRE LOOP LIGHT REMAINED ON, RECONNECTED LOOP AT FIREWALL LIGHT REMAINED ON. FOUND FIRE DETECTION CONTROL BOSDR S2YA05066CFlex Drive · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING SDR S2YA05066BFlex Drive · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEARBOX STRUGGLING SDR S2YA05066AGearbox · damagedSHORTLY AFTER TAKEOFF THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WHERE RAISED USING THE OVER RIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. MX DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLISDR S2YA05066Motor · damagedSHORTLY AFTER TAKEOFF, THE CREW REPORTED THE FLAPS WERE AT 17 DEGREES AND WILL NOT RETRACT. THE AC CONTINUED WITH THE FLAPS AT 17. THE FLAPS WERE RAISED USING THE OVERRIDE SWITCH AND THE SYSTEM WAS PUT ON MEL. DISCOVERED THE FLAP MOTOR/GEAR BOX STRUGGLING TSDR GUU2005F00058O-Ring · wornNO BRAKES AFTER PRESSING THE RT BRAKE PEDAL. REPLACED NR 3 AND 4 BRAKE ASSEMBLIES. UPON BRAKE REMOVAL, DETERMINED NR 3 BRAKE SWIVEL FITTING O-RING TO BE LEAKING. (K)SDR S2YA05065BRelay · failedFLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INS SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE AT 17 DEGREES AND WILL NSDR S2YA05065AGearbox · failedFLAPS FIALED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR, FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CRWE REPORTED FLAPS WERE A T 17 DEGREES AND WOULD NSDR S2YA05065Motor · malfunctionedFLAPS FAILED TO EXTEND, SYS WAS MEL`D. MEL WAS CLEARED WHEN MX INSP SYS, OPS CHECKED IT, COULD NOT DUPLICATE DISCREPANCY. TROUBLESHOOTING REPLACED FLAP MOTOR AND FLAP POSITION RELAY (K105). SHORTLY AFTER TAKEOFF CREW REPORTED FLAPS WERE A 17 DEGREES AND WILSDR 1051101026Spring · brokenFLIGHT CREW REPORTED THAT WHILE ON THE GROUND WHEN THE CONTROL YOKE WAS LET LOOSE IT WOULD FLOP OVER TO THE RIGHT. MAINTENANCE PERSONNEL FOUND THE AFT AILERON/RUDDER INTERCONNECT SPRING HAD BROKEN NEAR THE HOOK END. MAINTENANCE INSTALLED NEW SPRING. INSPECTSDR GUU2005F00050Wire · chafedRT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. REPAIRED CHAFED WIRE BENEATH FORWARD FLOORBOARD 131AT. (K)SDR S2YA05061Wire · damagedDURING APPROACH, THE CREW REPORTED THEY WERE UNABLE TO EXTEND THE GEAR AND FOUND THE CIRCUIT BREAKER (CB) POPPED. THE CREW RESET THE CB ONLY TO HAVE IT POP WHEN SELECTING GEAR DOWN. THE CREW MANUALLY EXTENDED THE GEAR, ACHIEVED 3 GREEN AND PROCEEDED TO LAND SDR 73127Terminal · crackedDURING A ROUTINE INSPECTION, INSPECTION PERSONNEL FOUND THE RT ENGINE BETA CABLE FRONT PUSH PULL TERMINAL CRACKED AROUND THE ENTIRE CIRCUMFERENCE. IT IS UNKNOWN HOW THIS CONDITION OCCURRED. PARTS HISTORY RESEARCH SHOWED NO RECENT USAGE. MORE INFORMATION WILL BSDR GUU2005F00051Bracket · corrodedAT SCHEDULED MAINTENANCE, RT ELEVATOR, CENTER HINGE BRACKET SHOWS SIGN OF EXFOLIATION. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K)SDR 09212005DFuel Control · failedON LEFT ENGINE START AT 44 PERCENT, ITT ROSE RAPIDLY AND ABORTED START AT 980 DEGREES CELSIUS (ENG AT 980 DEGREES FOR LESS THAN 5 SECS BEFORE SHUTDOWN). REMOVED AND REPLACED LEFT FUEL CONTROL. OPS CHECK GOOD.SDR R017794Bearing · brokenPROP WAS REMOVED FOR LOOSE BLADE. PROP WAS OVERHAULED BY MFG SERVICE CENTER ON 10/7/03 AND INSTALLED NEW D-7745 BEARINGS AT THAT TIME. HUB SIDE BEARINGS ON BLADES 2 AND 3 ARE CRACKED CIRCUMFERENTIALLY. HUB SIDE BEARING ON BLADE 4 IS BROKEN.SDR 09212005CSwitch · failedDUAL ENVIROMENTAL FAIL. T/O ABORTED AT 50 KNOTS. PERFORMED OPS CHECK OF RIGHT TEST VALVE OPS CHECKED GOOD. CLEANED LEFT PNEUMATIC BLEED TEST SWITCH E305WDM, OPS CHECK GOOD.SDR 09212005BHandle · out of rigLEFT EMERGENCY EXIT EXTERIOR HANDLE NOT FLUSHED. RIGGED DOOR HANDLE.SDR 1050902038Intercostal · crackedINTERCOSTAL ABOVE CARGO DOOR CRACKED AT FS 468, 482 AND 495. MAINTENANCE WAS DOING A STRUCTURAL REPAIR.SDR S2YA05058Gyro · inoperativeDURING FLIGHT, THE CREW REPORTED THE (D) DISCHARGE LIGHT ON THE RT PUSH TO DISCHARGE FIRE EXTINGUISHER BUTTON WAS INTERMITTENTLY ILLUMINATING. ALSO THE CREW REPORTED CAPTAIN`S DIRECTIONAL GYRO (DG) WAS INOP IN ALL MODES. THE CREW PERFORMED AN AIR-TURN-BACK. SDR 09152005BSwitch · failedLT ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY THEREAFTER. BOTTLE PRESSURE READS NORMAL. REMOVED AND REPLACED UPPER LT FIRE TEST SWITCH IAW 31-10-00, OPS CHECK GOOD.SDR GUU2005F00048Bracket · corrodedAT SCHEDULED MAINTENANCE, THE LEFT ELEVATOR, OUTBOARD HINGE BRACKET WAS DETERMINED TO HAVE EXFOLIATION CORROSION. REPLACED THE LEFT ELEVATOR OUTBOARD HINGE BRACKET. (M)SDR 09132005AGround Wire · looseFLAP WILL NOT GO DOWN WHEN SELECTED 17 DEGREES. MEL'ED FLAP SYSTEM. C/W MEL ON 9/15/2005 FOUND LOOSE GROUND, RESECURED, OPS CHECK GOOD.SDR 09122005FCircuit Breaker · inoperativePROP OVERSPEED TEST INOP. LOW PITCH TEST INOP. AUTOFEATHER INOP. RESET CB9, OPS CHECK GOOD FOR PROP OVERSPEED, LOW PITCH, AND AUTOFEATHER TEST.SDR 09122005ESkin · bird strikeBIRD STRIKE ON LEFT INBOARD LEADING EDGE. REMOVED AND REPLACED LEADING EDGE, ONLY WAITING ON A BOOT.
Back to Beech 1900D