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 = 'A100' 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 = 'A100' 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 CA010628047Harness · mismanufactured(CAN) AFTER A FALSE FIRE WARNING. ENGINE WAS SHUTDOWN. WHILE TROUBLESHOOTING. FOUND POWER FOR AUTO IGNITION SYSTEM WAS BLEEDING THROUGH WET WIRE INSULATION & INTO FIRE DETECT SYSTEM THROUGH IT'S WIRE INSULATION. THIS TOOK PLACE IN MAIN WIRE BUNDLE FOR RT ENG.SDR CA010629019Fuel Control · failed(CAN) RT POWER LEVER IS VERY DIFFICULT TO SCHEDULE SUBTLE POWER CHANGES. IE. WHEN ATTEPTING TO SELECT A CHANGE OF 100 FT/LBS RESULTING TORQUE CHANGE COULD BE AS MUCH AS 400FT/LBS. THIS RESULTS IN AN OSCILLATION OF POWER LEVER MOVEMENT TO GET DESIRED POWER OUTPSDR CA010508007Fire Detector · shorted(CAN) DURING DESCENT NR 1 ENG FIRE INDICATION ILLUMINATED. ENGINE WAS SHUT DOWN. INSPECTION DETERMINED NO ACTUAL FIRE. THE ERRONEOUS FIRE INDICATION COULD NOT BE DUPLICATED ON GROUND. BASED ON PREVIOUS TROUBLE SHOOTING ALL THE WIRING FOR THE FIRE DETECTIONS WASDR 20010419CW015Tube · puncturedINSTALL BLEED AIR TUBE IN LEFT WING CENTER SECTION. USING ICE PICK ON SUSPECT COROSION BLISTERS, TUBE COULD BE PUNCTURED EASILY. TUBE REMOVED FOR REPLACEMENT, 1 PIN HOLE ON TOP OF TUBE. HOLES LOCATED 8 TO 9 INCHES INBOARD OF COUPLING HOSE END OF TUBE.SDR CA010323019Wheel · cracked(CAN) RT INBOARD WHEEL WAS REMOVED FOR A ROUTINE TIRE CHANGE. UPON DISASSEMBLY IT WAS NOTICED THAT THERE WAS A 4 - 5 INCH CRACK IN THE BEAD AREA. THE RIM WAS BENT AND DEFORMED IN THIS AREA. THERE ARE NO INDICATIONS OF A STRIKE WITH A GROUND OBJECT YET THE CRACSDR CA010402002Bearing · corroded(CAN) DURING ROUTINE INSPECTION IT WAS NOTICED THAT THE LANDING GEAR WAS SLOW TO RETRACT. UPON FURTHER INSPECTION THE BEARING SUPPORTING THE RT DRIVE SHAFT WAS FOUND CORRODED AND STIFF. THIS BEARING ALSO CAUSED THE GEAR MOTOR TO BECOME WEAK AND NEEDED TO BE SDR CA001228021Downlock Switch · failed(CAN) ON APPROACH, GEAR SELECTED DOWN, NOSE WHEEL LIGHT DID NOT ILLUMINATE. CHECKED BULB AND CYCLED GEAR AGAIN WITH NO SUCCESS. LIGHT EVENTUALLY ILLUMINATED BY ITSELF. MAINTENANCE REPLACED WIRES AND TERMINAL LUGS ON NOSE LIGHT SOCKET, CLEANED DOWN LOCK SWITCH,SDR CA001030006Fitting · cracked(CAN) CRACK IS FROM THE FORWARD I/B SPAR CAP TO FITTING RIVET AND GOES TO THE EDGE OF THE FITTING. THE CRACK WAS DISCOVERED DURING A SCHEDULED WING INSPECTION. CRACK WAS VERIFIED USING LEVEL 2 PENETRANT.SDR CA001017008Wheel · cracked(CAN) DURING A ROUTINE INSPECTION MAINTENANCE NOTICED A CRACK IN THE PAINT IN THE BEAD AREA. AREA WAS CLEANED WITH A LIQUID DYE PEN INSPECTION FOUND A 2.5 INCH CRACK FOLLOWING THE CIRCUMFERENCE. WHEEL ASSEMBLY WAS REPLACED.SDR CA001018003Spring · broken(CAN) DURING UNSCHEDULED MAINTENANCE, BOTH LT AND RT RUDDER RETURN SPRINGS WERE FOUND BROKEN. NO FLIGHT CONTROL PROBLEMS WERE REPORTED FROM THE FLIGHT CREW. THE SPRINGS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. THESE RETURN SPRINGS ARE AN IMPROVED SDR CA000927012Washer · failed(CAN) WHILE REASSEMBLING THE WING FOLLOWING INSPECTION IN ACCORDANCE WITH CF-81-25R5, A NEW PRELOAD INDICATING WASHER ASSY INSTALLED ON THE LT LOWER FORWARD WING BOLT INDICATED THE BOLT WAS TORQUED AT AN ABNORMALLY LOW TORQUE. THE BOLT WAS UNDONE AND THE WASHESDR CA000928028Connector · loose(CAN) AIRCRAFT WAS UNABLE TO TRANSMIT ON ANY OF THE 3 COMMS. MAINTENANCE DISCOVERED THE CONNECTOR TO BACK OF THE RADIO RACK LOOSE. THE CONNECTOR WAS CONNECTED, COMMS TESTED, AND THE AIRCRAFT RETURNED TO SERVICE. AVIONICS HAS ADVISED THAT THESE CONNECTORS CAN BSDR CA000928027Line · broken(CAN) DURING CLIMB LT BLEED AIR LIGHT ILLUMINTED INDICATING BLEED AIR FAILURE. THE AIRCRAFT RETURNED TO BASE AND LANDED UNEVENTFULLY. MAINTENANCE DISCOVERED THE SENSE LINE HAD BROKEN OFF A CONNECTION. THE SENSE LINE WAS RE-ATTACHED A GROUND RUN WAS CONDUCTED ASDR CA000907011Connector · dirty(CAN) AIRCRAFT RETURNED BACK TO BASE DUE TO HIGH OIL TEMP ON R/H ENGINE. OIL TEMP BULB CONNECTOR FOUND TO BE DIRTY. CONNECTOR CLEANED AND SYSTEM CHECKED SERVICEABLE.SDR 20000712SH001Vent Line · failedOPERATIONAL CHECKS AT INSPECTION INTERVALS TYPICALLY FIND THE VENT HEATS INOPERATIVE DUE TO THE ELECTRICAL CONNECTION ON THE TUBE ITSELF. USING A PROBE AND INSERTING IN THE HOLE WHERE THE HEATING COIL TERMINATES PRODUCES A SPARK AND THEN THE COIL WILL HEAT PRSDR CA000712024Fitting · cracked(CAN) CRACKED AT RADIUS OF WING ROOT ATTACH FLANGE ON FORWARD SIDE OF FITTING. SLOT AREA.SDR CA000614036Wire · broken(CAN) AIRCRAFT DEPARTED AND SHORTLY AFTER TAKEOFF, THE MAIN STABILIZER TRIM FAILED. AIRCRAFT RETURNED TO BASE. A WIRE WAS FOUND BROKEN ON THE COPILOT''''S SIDE WHERE THE WIRE GOES THROUGH THE DASH. WIRE REPAIRED AND AIRCRAFT RELEASED TO SERVICE.SDR CA000719030Clamp · failed(CAN) DURING A COMPANY TRAINING FLIGHT, THE LT BLEED AIR FAIL ANNUNCIATOR LIGHT (RED) ILLUMINATED. A S PER PROCEDURES, THE LT BLEED AIR SWITCH WAS SELECTED TO THE OFF POSITION. A VISUAL MEANS TO ASCERTAIN THE VALVE IS WORKING IS WHEN SELECTED TO OFF, A SLIGHTSDR CA000530043Wire · loose(CAN) GEAR WAS SELECTED UP AND THE GEAR WOULD NOT RETRACT. THE SELECTION WAS TRIED SEVERAL TIMES AND FINALLY RETRACTED.A LOOSE WIRE WAS FOUND ON THE EMERGENCY EXTENSION MICROSWITCH LOCATED BY THE GEAR TRANSMISSION. THE CONNECTION WAS RESECURED.SDR CA000530032Tach Generator · failed(CAN) WHILE IN CRUISE, THE RT PROPELLER INDICATION WENT TO ZERO. NO ACTION WAS TAKEN, AIRCRAFT WAS RETURNING TO BASE. MAINTENANCE REMOVED TACH GENERATOR AND FOUND DRIVESHAFT ROUNDED OFF. NEW TACH GENERATOR INSTALLED.SDR CA000518015Switch · loose(CAN) DURING CLIMB, THE GEAR WAS SELECTED UP AND THE GEAR DID NOT RETRACT. THE SELECTION WAS ATTEMPTED SEVERAL TIMES WITH THE GEAR RETRACTING ON THE LAST SELECTION. MAINTENANCE FOUND A LOOSE WIRE ON THE EMERGENCY EXTENSION MICROSWITCH LOCATED BY THE GEAR TRANSDR CA000511019Bracket · cracked(CAN) CRACK FOUND DURING INSPECTION IN WEBBING. SUBMITTER STATED THIS IS A COMMON AREA FOR CRACKING WITH THE UNITS.SDR CA000511018Wire · loose(CAN) AIRCRAFT RETURNED WITH GEAR IN-TRANSIT LIGHT. AFTER NUMEROUS GEAR SWINGS IT WAS DISCOVERED THAT THE WIRE WAS LOOSE WHERE IT IS ATTACHED TO THE EMERGENCY GEAR EXTENTION MICRO-SWITCH.THIS SWITCH CUTS POWER SO THAT WHEN THE EMERGENCY SYSTEM IS USED THERE ISDR CA000427017Panel · corroded(CAN) DURING THE COMPLETION OF THE DEPARTMENTS CAMPAIGN NOTICE FOR CORROSION INSPECTION OF INTEGRAL FUEL TANKS, FASTENERS & THREAD INSERTS IN THE ACCESS PANELS IT WAS DISCOVERED THAT SOME WERE BADLY CORRODED. CORROSION WAS ALSO DISCOVERED ON THE ACCESS PANELS SDR CA000410022Switch · intermittent(CAN) FLAP DOWN SWITCH INTERMITTANT.WHEN SWITCH WAS SHAKEN YOU COULD HEAR LOOSE PART(S) IN SWITCH.SWITCH REPLACED.SDR CA000329012Switch · faulty(CAN) PILOT REPORTED LANDING GEAR UNSAFE LIGHT ON HANDLE WOULD NOT EXTINGUISH. LANDING GEAR POSITION SWITCH ON MOTOR ADJUSTED. PROBLEM RECURRED WITH INDICATION LIGHT NOW BEING INTERMITTANT. DISCOVERED MICROSWITCH INTERNALLY FAULTY.SDR CA000323006Snap Ring · loose(CAN) DURING REPLACEMENT OF THE VENT BLOWER ASSY, THE AME LIGHTLY PULLED ON THE PILOT''S LT RUDDER PEDAL. THE LT BRAKE MASTER CYLINDER SNAP RING LET GO AND THE CYLINDER CAME APART DRAINING ALL THE BRAKE FLUID AND LEAVING THE BRAKE SYSTEM INOPERATIVE. THE SUBMSDR CA000317010Bearing · failed(CAN) BLADE BEARING FAILED CAUSING DAMAGE TO BEARING BORE.SDR CA000301036Actuator · noisy(CAN) FOLLOWING TAKE-OFF THE PILOT COULD NOT GET THE LANDING GEAR TO FULLY RETRACT OR EXTEND. MANUAL EXTENSION WAS REQUIRED. DURING RETRACTION TEST, MAINTENANCE OBSERVED THE GEARBOX WAS NOISY AND THE NOSEGEAR ACTUATOR WAS AT MAX LIMITS END PLAY. THE NOSE GESDR CA000314006Bracket · wrong part(CAN) BEECH SERVICE INSTRUCTION 0464-213 PROVIDES FOR IMPROVED SWITCHES ON THE LANDING GEAR GEARBOX. THE GEARBOX IN QUESTION HAS THE NEW SWITCHES BUT ONE SWITCH WOULD DEFLECT IN ITS BRACKET AND MAKE CONTACT LATE WHEN ACTUATED BY A CAM. A NEW KIT WAS ORDERED SDR CA000301032Uplock Switch · failed(CAN) TROUBLESHOOTING LANDING GEAR RETRACTION PROBLEMS REVEALED THE RT MLG UPLOCK SWITCH WAS IN A POSITION TO INDICATE A GEAR INTRANSIT SITUATION BUT DID NOT INDICATE IT. THE SWITCH WAS REPLACED.SDR CA000215025Clevis · seized(CAN) THE AIRCRAFT WAS ON APPROACH WITHOUT NOSE GEAR LOCK INDICATION. GEAR CYCLED WITH NO INDICATION. ON CLIMBOUT THE NOSE GEAR LIGHT CAME ON. DURING INSPECTION THE NOSE GEAR ACTUATOR CLEVIS WAS FOUND STUCK IN THE ACTUATOR AND COULD NOT EXTEND WITH THE SPRINGSDR CA000218002Bellcrank · failed(CAN) WHILE ASCENDING, THE PASSENGERS HEARD A LARGE BANG AROUND THE DOOR AREA. CREW MEMBER INSPECTED THE DOOR IN FLIGHT, DID NOT PERCEIVE TO HAVE A PROBLEM. UPON LANDING, IT WAS DISCOVERED THE FORWARD PIN WAS NOT PROPERLY SEATED. UPON FURTHER INVESTIGATION, SDR CA000203013Windshield · failed(CAN) AFTER DEPARTING, ON CLIMB OUT, INNER PANE OF WINDSHIELD SHATTERED ON CAPTAINS SIDE.AIRCRAFT RETURNED WHERE WINDSHIELD WAS REPLACED.THE WINDSHIELD WHICH FAILED HAD PREVIOUSLY EXHIBITED SIGNS OF DELAMINATION BUT THE BEECH 100 MAINTENANCE MANUAL ATA CHAPTERSDR AU000203013Windshield · failed(AU) AFTER DEPARTING, ON CLIMB OUT, INNER PANE OF WINDSHIELD SHATTERED ON CAPTAIN'S SIDE. AIRCRAFT RETURNED WHERE WINDSHIELD WAS REPLACED. THE WINDSHIELD WHICH FAILED HAD PREVIOUSLY EXHIBITED SIGNS OF DELAMINATION, BUT THE BEECH 100 MAINTENANCE MANUAL ATA CHSDR CA991230040Cable · stuck(CAN) AFTER COMPLETING THE DECENT CHECKS, THE CREW ATTEMPTED TO REDUCE POWER ON BOTH ENGINES. THE POWER LEVER FOR THE RT ENGINE WOULD NOT MOVE. ALL ATTEMPTS TO MOVE THE POWER LEVER WERE UNSUCESSFUL SO THECREW ELECTED TO SHUT THE RT ENGINE DOWN. ON THE GROUND,SDR CA991230038Wire · failed(CAN) WHEN PILOT SELECTED GEAR DOWN AIRCRAFT EXPERIENCED MULTIPLE FAILURES OF MLG & FLT INSTRUMENTS, ALSO THERE WAS SMOKE IN COCKPIT. PILOT EXTENDED THE MLG MANUALLY & LANDED W/O INCIDENT. MAINT DISCOVERED 2 PROBLEMS: THE WIRE GOING TO BUS FEEDER DIODE WASDR CA991209059Wire · broken(CAN) AIRCRAFT WAS ON APPROACH WHEN AFTER SELECTING GEAR DOWN , THE LEFT MAIN GEAR DOWN AND LOCKED INDICATION LIGHT FAILED TO ILLUMINATE. THE GEAR WAS CYCLED SEVERAL TIMES, BUT DID NOT HELP. THE GEAR INTRANSIT LIGHTS WERE EXTINGUISHED AFTER THE COMPLETION OFSDR CA991103051Torque Knee · cracked(CAN) WHILE MOVING AXLE TO CHECK FOR EXCESSIVE PLAY, MOVEMENT WAS NOTICED IN THE TORQUE KNEE UPPER AND LOWER BUSHINGS (BOTH MAIN GEAR). LEFT AND RIGHT LANDING GEAR TORQUE KNEES REMOVED TO INSTALL NEW BUSHINGS. DURING BUSHING REPLACEMENT, A SMALL CRACK WAS NOSDR CA991209058Motor · overheated(CAN) THE AIRCRAFT WAS PARKED AND THE ENGINES SHUT DOWN, WHEN, WITH THE BATTERY STILL ON, THE CABIN FILLED WITH SMOKE. INVESTIGATION REVEALED THE FLAP MOTOR HAD OVERHEATED, SEIZED AND BEGAN TO SMOKE. THE CAUSE WAS THE UPLIMIT SWITCH NOT MAKING CONTACT WHEN THSDR CA991209057Tire · failed(CAN) ON TAKEOFF, THE LEFT INBOARD MAIN WHEEL ASSEMBLY SHED ITS ENTIRE TREAD. ALTHOUGH THIS WAS A RECAPPED TIRE, THE TREAD DID NOT SEPARATE AT THE RECAP. IN THIS CASE, THE RETREAD LAYER AND THE LAYER OF THE RUBBER FROM THE RETREAD TO THE FIRST LAYER OF CORDSDR CA991209069Strut · cracked(CAN) AFTER REMOVAL FROM AIRCRAFT FOR TIMEX ON A TIME TRIAL, IT WAS INSPECTED AND THE FOLLOWING FOUND:LPI INDICATIONS OF CRACKS ON THE TORQUE KNEE LUG. THE CRACKS WERE IN THE RADIUS OF THE LUG ON THE BOTTOM SIDE. PART WAS REJECTED.SDR CA991103048Contact · failed(CAN) AFTER TAKEOFF, THE CREW SELECTED GEAR UP BUT THE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO BASE. TROUBLESHOOTING REVEALED THAT A SET OF POINTS IN THE LANDING GEAR CONTROLLER WELDED TOGETHER. THE MOTOR WAS REPLACED. THIS IS THE FOURTH PROBLEM WSDR CA991007075Windshield · cracked(CAN) DURING CLIMB THROUGH 10,000 FEET, THE CAPTAIN'S OUTER PANE WINDSHIELD CRACKED. AIRCRAFT WINDSHIELD REPLACED.SDR CA990927070Torque Tube · cracked(CAN) DURING ACCOMPLISHMENT OF SERVICE BULLETIN 2145, CRACKS WERE DETECTED ON BOTH RIGHT AND LEFT TORQUE TUBE ASSEMBLIES (P/N 115-610015-325). LEFT FOUND AT INBOARD SUPPORT (P/N 115-610015-1), RIGHT FOUND AT CENTER SUPPORT (P/N 115-610018-1). TORQUE TUBES RESDR CA990927056Gear Chain · separated(CAN) UPON SELECTING GEAR UP, IN-TRANSIT LIGHT STAYED ON. GEAR WAS THEN SELECTED DOWN AND THE MAIN GREEN LIGHTS CAME ON. THE NOSE WAS ABOUT 15 DEGREES FROM DOWN AND LOCKED. THE AFT GEAR CHAIN WAS ACCESSED BY THE FLIGHT CREW AND WITH THE AID OF MAINTENANCE, SDR CA990812019Sprocket · worn(CAN) DURING THE UNDER FLOOR INSPECTION THE AME NOTICED THE AFT CHAIN FOR THE LANDING GEAR ACTUATION SYSTEM HAD JUMPED ONE SET OF TEETH ON A SPROCKET. FURTHER INVESTIGATION FOUND THAT THE CHAIN TENSION WAS OUT OF TOLERANCE WHICH HAS BEEN DETERMINED TO BE THE SDR CA990728080Pin · broken(CAN) DURING THE WASH AND REGREASING OF THE RIGHT MAIN LANDING GEAR, THE PIN THAT ATTACHES THE DOWNLOCK HOOK TO THE DOWNLOCK LINK WAS FOUND PROTRUDING AND BROKEN. THE BREAK WAS LOCATED AT THE HOLE FOR THE ROLL PIN. THE ROLL PIN IS USED TO RETAIN THE HOOK PINSDR CA990630057Spar · cracked(CAN) THE RUDDER WAS REMOVED TO REPAIR SOME LOOSE RIVETS ON THE TORQUE TUBE, BUT A CRACK ABOUT 1 CENTIMETER LONG WAS DISCOVERED ON THE RUDDER SPAR (P/N 96-630000-307). THE SPAR WAS ALSO FOUND TO BE CRACKED IN BEHIND. THE CRACKS ORIGINATED FROM THE NUTPLATE ISDR CA990630056Bellcrank · corroded(CAN) THE RUDDER BELLCRANK WAS REMOVED AND CORROSION WAS FOUND ON THE SURFACE WHERE THE TORQUE TUBE CONNECTS. THERE WAS ALSO CORROSION FOUND ON THE BOLT HOLES. THE BELLCRANK AND BOLTS WERE REPLACED. SUBMITTER STATED THAT THIS AREA IS HARD TO INSPECT BECAUSE
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