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 = 'D95A' 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 = 'D95A' 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 2025FA0000100Relay · defectiveSUSPECTED LANDING GEAR DYNAMIC BRAKING RELAY MALFUNCTIONED GIVING THE PILOTS A GREEN LIGHT INDICATING THE LANDING GEAR IS DOWN AND LOCKED AND STOPPED THE LANDING GEAR MOTOR BEFORE THE LANDING GEAR WAS DOWN AND LOCKED. UPON AIRCRAFT TOUCHING DOWN THE AIRCRAFT SDR 2015FA0000612Leg Assy · brokenWHILE EXECUTING A LANDING, PILOT STATED THE MAIN WHEELS TOUCHDOWN FIRST, AS SOON AS NOSE WHEEL TOUCHED DOWN THE NOSE GEAR COLLAPSED CAUSING THE PROPELLERS TO STRIKE THE GROUND AND ACFT SKIDDED TO A STOP WITH PILOT AND 1 PASSENGER EXITING THE AIRCRAFT WITH NO ISDR 2015FA0000438Arm · brokenWHILE ON APPROACH, THE LANDING GEAR WAS SELECTED TO DOWN POSITION, THE NOSE GEAR DID NOT EXTENDED TO DOWN AND LOCKED. EMERGENCY PROCEDURES PERFORMED WITH NO RESULTS. ACFT MADE EMERGENCY LANDING WITH MINOR DAMAGE TO NOSE CONE. PILOT AND PASSENGER EGRESSED ACSDR 2015FA0000287Circuit Breaker · brokenWE HAD JUST COMPLETED PATTERN WORK AND RECEIVED RADAR VECTORS. WHILE ON THE APPROACH BOTH PILOTS NOTICED FUMES FROM WHAT SEEMED LIKE THE INSTRUMENTS, WE BEGAN TROUBLESHOOTING AND NOTICED THE ONLY GAUGE THAT WAS OUT OF THE NORM WAS THE RT ENGINE OIL TEMP WITH NSDR CA140205005Tube · defective(CAN) DISCOVERED A PIN HOLE IN THE SIDE WALL OF THE INNER TUBE.SDR 2012FA0000668Tube · splitFAILURE OF TUBE WHILE ACFT SAT ON RAMP. FOUND SMALL SPLIT IN SIDE OF TUBE. 5TH FAILURE OF RUBBER TUBES EXPERIENCED WITH NO EVIDENCE OF UNDER OR OVER INFLATION.SDR CA101108014Disk · cracked(CAN) DURING REPLACEMENT OF A BLOWN WHEEL AND OVERHAUL OF A WHEEL ASSEMBLY, THE DISK WAS REMOVED, MEASURED FOR WEAR AND INSPECTED FOR DEFECTS. AT THIS TIME A CRACK WAS NOTICED ON THE INNER SIDE OF THE DISK. THIS SIDE IS NOT EASILY VISIBLE DURING SERVICE. THESDR CA080116022Mount · mismanufactured(CAN) AFTER ENGINE REPLACEMENT FOR OVERHAUL A PRELIMINARY GROUND RUN WAS CARRIED OUT. IT WAS FOUND THAT THE PROPELLER WOULD NOT FEATHER WHEN PERFORMING A GOVERNOR CHECK. THE PROBLEM WAS TRACED TO THE GOVERNOR MOUNT PAD WHICH HAD NOT HAD AN OIL GALLERY COMPLETESDR FAA061214001Motor · shortedLANDING GEAR MOTOR CIRCUIT BREAKER BLEW WHEN GEAR WAS RETRACTED ON TAKEOFF. AT THE SAME TIME THE ALTERNATORS DROPPED OFFLINE. PILOT SWITCHED TO THE OTHER VOLTAGE REGULATOR AND THE ALTERNATORS CAME BACK ONLINE. AIRCRAFT WAS FLOWN FOR AN HOUR OR MORE TO BURN OSDR CA050127002Control Horn · cracked(CAN) DURING SHEET METAL REPAIR OF THE RT ELEVATOR ASSY IT WAS NOTED THAT THE ELEVATOR SKIN AT THE CONTROL HORN ATTACH POINT WAS CRACKED. FURTHER INSPECTION OF THE CONTROL HORN ASSY REVEALED A LARGE CRACK PROGRESSSING FROM 1 OF 4 ELEVATOR TO CONTROL HORN MOUNTSDR CA040624006Motor · failed(CAN) UPON REPLACEMENT, TESTING OF LANDING GEAR MOTOR RECEIVED FROM AN APPROVED OH FACILITY IT WAS DETERMINED MOTOR WAS SPINNING IN REVERSE DIRECTION. MOTOR WAS REMOVED AND BENCH TESTED TO ELIMINATE AN AC WIRING PROBLEM. MOTOR ROTATED IN WRONG DIRECTION AGAISDR CA030908004Alternator · failed(CAN) NOTICED NO CHARGE, MINIMIZED ELECTRICAL LOAD TURNED OFF ALTERNATORS RESET ON CHANGED RELAY LT TO RT. NO CHARGE TURNED MASTER OFF, 25 MILES FROM AIRPORT, TURNED MASTER ON AND 1 RADIO GOT ATIS AND CALLED TOWER LOST ALL POWER, CALLED TOWER ON CELL DID A MSDR CA030321004Shaft · cracked(CAN) RT ENGINE WOULD NOT START. DURING TROUBLESHOOTING THE MAGNETO WAS REPLACED. DURING THE INSPECTION OF THE MAGNETO, IT WAS NOTICED THAT THE MAGNETO SHAFT WAS CRACKED AT THE POINT WHERE THE PHENOLIC CAM FOR THE POINTS IS INSERTED INTO THE SHAFT. ALSO EXCESSDR CA020418004Rib · cracked(CAN) THE RIB WAS CRACKED AND BROKEN IN THE NOSE AREA AND THE FORWARD ANCHOR NUT FOR THE FLAP ACTUATOR ATTACH BRACKET WAS BROKEN. WITH THE FLAPS UP THE AME STEPED ON THE FLAP WALKWAY AND A LOUD NOISE WAS HEARD. HE APPLIED UP AND DOWN LOADS TO THE FLAP AT THE TSDR AU001032Blade · separated(AUS) LEFT PROPELLER BLADE SECTION SEPARATED APPROXIMATELY 200 MM (7.87 INCHES) FROM THE BLADE TIP. FAILURE ORIGINATED FROM A PREVIOUS STONE STRIKE THAT HAD NOT BEEN ADEQUATELY BLENDED OUT. (X)SDR CA000328005Pin · missing(CAN) THE LT MAGNETO SWITCH WAS FOUND WITH THE KNOB AND ACTUATOR SEPARATED FROM THE SWITCH. IT APPEARS THE INTERFERENCE FIT PIN INSIDE THE SWITCH THAT HOLDS THE ACTUATOR IN PLACE WAS MISSING. NO EVIDENCE OF THE MISSING PIN WAS FOUND INSIDE THE SWITCH.SDR CA000203016Actuator · failed(CAN) AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT.THE AIRCRAFT RETURNED AND A SUBSEQUENT INSPECTION REVEALED THAT THE LANDING GEAR MOTOR HAD FAILED.THE MOTOR WAS REPLACED. THE SUBMITTER STATES THAT THE AIRCRAFT IS PRIMARILY USED FOR FLIGHT TRAINING SO ISDR AU000203016Actuator · failed(AU) AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED AND A SUBSEQUENT INSPECTION REVEALED THAT THE LANDING GEAR MOTOR HAD FAILED THE MOTOR WAS REPLACED. THE SUBMITTER STATES THAT THE AIRCRAFT IS PRIMARILY USED FOR FLIGHT TRAINING SO SDR CA000118001Brace · cracked(CAN) THE AIRCRAFT WAS IN FOR A 100 HR. INSPECTION. WHEN THE COWLS WERE REMOVED FROM THE RT ENGINE IT WAS NOTICED THAT AN O/B DIAGONAL BRACE WAS BROKEN. THE MOUNT WAS REMOVED AND SHIPPED TO AN APPROVED AMO FOR WELDING REPAIRS AND TUBE REPLACEMENT.SDR AU990459Strut · cracked(AUS) LEFT AND RIGHT MAIN LANDING GEAR CYLINDERS P/N 35815246-1 (LT) AND P/N 35815246-3 (RT) CRACKED IN THE RADIUS OF THE LOWER BRACE ATTACHMENT FITTINGS.SDR AU990416026Switch · failed(AU) ON APPROACH, THE LANDING GEAR FAILED TO EXTEND ELECTRICALLY. THE LANDING GEAR MOTOR WAS REPLACED. SEVERAL FLIGHTS LATER THE SAME FAULT OCCURRED AGAIN. ON A SUBSEQUENT TEST, THE SELECTOR SWITCH WAS FOUND TO BE THE CAUSE.SDR 98ZZZX3312Skin · damagedDURING A ROUTINE ANNUAL INSPECTION, THE LOWER AFT RT NACELLE SKIN WAS FOUND CHAFING INTO THE WING SKIN DIRECTLY AFT OF THE FORWARD LOWER SPAR CAP. IT HAD ALSO CHAFED A LINE INTO THE SPAR CAP TO A DEPTH OF .008 INCH. BEECHCRAFT TECHNICAL SUPPORT WAS CONTACTEDSDR 98ZZZX2159Hose · failedOIL LINES RUNNING FROM FRONT MOUNTED OIL COOLER CONTACTED EXHAUST PIPES. OIL LINES WERE MOUNTED TO COWLING, WHEN UPPER COWL HALF WAS CLOSED AND LATCHED THE COWLING WAS PULLED INWARD CAUSING THE OIL LINES TO CONTACT EXHAUST, BURNING THROUGH AND CAUSING COMPLETSDR CA980407006Drag Brace · cracked(CAN) NOSE LANDING GEAR UPPER DRAG BRACE FOUND CRACKED ON INSPECTION.SDR CA970421061Dry Air Pump · loose(CAN) DURING TRAINING THE RIGHT HAND ENGINE OIL PRESSURE BEGAN TO DROP. ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED SAFELY. INSPECTION FOUND THE DRY AIR PUMP LOWER ATTACHING HARDWARE WAS NOT TIGHT, CAUSING A SUBSTANTIAL OIL LEAK. THE HARDWARE WAS SECURED AND SDR CA960924025Magneto · shaft sheared(CAN) THE RIGHT ENGINE WOULD NOT START. INSPECTION REVEALED THE #2 ENGINE LEFT HAND MAGNETO HAD SEPARATED FROM THE CASE BREAKING THE MAG CASTING AT THE MOUNTING FLANGES & THE MAGNETO SHAFT WAS BENT. FURTHER INVESTIGATION FOUND THE FUEL PUMP, CAMSHAFT, VACUUM PSDR CA960723009Distributor Gear · loose electrode(CAN) THE MAGNETO WAS SENT IN FOR WARRANTY REPAIR. A TEST FOUND THAT THE UNIT WAS FIRING ON ONE CYLINDER. INSPECTION FOUND THAT THE ELECTRODE HAD BROKEN FREE OF ITS MOUNTING. THE UNIT WAS GIVEN A 500 HOUR SERVICE AND THE DEFECTIVE PART REPLACED AND THE UNIT RESDR 96ZZZX3700Rotor · shaft failedENGINE NO START. TROUBLESHOOTING ISOLATED TO MAGNETO. OPENED MAGNETO HOUSING TO INSPECT. REMOVED DISTRIBUTOR BLOCK AND GEAR ASSEMBLY. NOTICED ROTOR GEAR APPEARED DETACHED. REMOVED GEAR AND FOUND SHAFT HAD BROKEN AT AREA BELOW POINT CAM SLOT. SLOTTED PORTSDR CA960626002Crankcase · cracked(CAN) WHILE REMOVING THE #2 ENGINE TO FACILITATE REPLACEMENT OF A CRACKED ENGINE MOUNT, A 6" CRACK WAS FOUND ON THE CRANKCASE, JUST AFT OF THE PROP UNDER THE FORWARD BAFFLE. THE ENGINE WAS REPLACED.SDR CA960502006Distributor Gear · loose electrode(CAN)THE MAGNETO WAS SENT IN FOR OVERHAUL, 215 HOURS AFTER A 500 HOUR INSPECTION. THE CUSTOMER HAD SNAGGED IT FOR NOT FIRING. INTERNAL INSPECTION FOUND THAT THE ELECTRODE AND AXLE ASSEMBLY HAD COME LOOSE F ROM THE GEAR ITSELF. THE GEAR IS OF THE NEWEST TYPE AN
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