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 = '95C55' 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 = '95C55' 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 20001214SH011Crankcase · failedCRANKCASE FAILED AROUND NR 6 CYLINDER CAUSING CYLINDER TO DEPART ENGINE IN-FLIGHT. THE AIRCRAFT WAS IN LEVEL FLIGHT AT TIME OF FAILURE. (X)SDR AU000040Bracket · corroded(AUS) LEFT MAIN LANDING GEAR UPLOCK BRACKET CORRODED IN THE AREA OF THE MOUNTING BOLT HOLE.SDR 99ZZZX3397Autopilot · malfunctionedWHILE IN HEADING MODE, AUTOPILOT WENT INTO A 30 DEGREE RIGHT TURN, UN-COMMANDED. ALSO, THE DISCONNECT BUTTON HAD NO EFFECT (IT WOULD NOT DISCONNECT). IT WAS NECESSARY TO SHUT OFF POWER TO APPROACH TO DISCONNECT CONTROL LOAD.SDR 99ZZZX1082Switch · malfunctionedLANDING GEAR FAILED TO EXTEND. DURING TROUBLESHOOTING, FOUND SELECTOR SWITCH FAILED. CLEANED SWITCH AND GEAR OPERATED NORMALLY. INSTALLED NEW SWITCH AND PERFORMED OPERATIONAL CHECK OF LANDING GEAR WITH SATISFACTORY RESULTS.SDR CA981207001Crankcase · cracked(CAN) ENGINE LEAKING OIL. INSPECTION FOUND TWO THROUGH BOLTS BROKEN. THIS CAUSED NR 4 CYLINDER TO BECOME LOOSE. THE LOOSE CYLINDER CREATED PULL ON THE CYLINDER HOLD-DOWN STUDS AND CRACKED THE CRANKCASE, WHERE THE STUD WAS PULLED.SDR AU981396Arm · worn(AUS) AILERON TRIM TAB ARM WORN. INVESTIGATION FOUND THE ARM WAS MANUFACTURED FROM ALUMINIUM INSTEAD OF STEEL AND A BUSHING HAD BEEN FITTED TO REMOVE PREVIOUS WEAR. UNAPPROVED PART.SDR 98ZZZX19Bearing · failedENGINE RPM FLUCTUATING IN-FLIGHT. PRECAUTIONARY ENGINE SHUT DOWN AND FEATHERING ACCOMPLISHED. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION DISCLOSED THE STARTER ADAPTER FAILED DUE TO LACK OF OIL. THIS OCCURRED AFTER .5 HOURS OF OPERATION. DISASSEMBLY OFSDR AU971536Bolt · broken(AUS) LH NO6 CYLINDER UPPER THROUGH BOLT BROKEN IN LINE WITH THECYLINDER BASE FLANGE.SDR 97ZZZX4764Spring · brokenENGINE RAN ROUGH. INSPECTION FOUND NR 2 EXHAUST OUTER VALVE SPRING BROKEN.SDR 97ZZZX1711Hub · crackedDURING INSPECTION, HUB FOUND CRACKED IN BLADE SOCKET NR 2. HUB HAS BEEN SCRAPPED.SDR AU970317Bracket · cracked(AUS) RH FLAP ACTUATOR ATTACHMENT BRACKET CRACKED AND SEPARATED FROM FLAP AT THE CENTRE ATTACHMENT SCREW. WHEN DOWNWARDS PRESSURE WAS APPLIED TO THE TRAILING EDGE OF THE FLAP - INVESTIGATION FOUND APREVIOUS REPAIR UNDER THE BRACKET ALSO CRACKED AND THE RIB BESDR 96ZZZX5003Filter · mismanufacturedDURING A ROUTINE OIL CHANGE, EXAMINATION OF THE OIL FILTER REVEALED THE RUBBER GASKET BETWEEN THE FILTER ELEMENT AND THE FILTER END HOUSING HAD SHIFTED, APPARENTLY DURING MANUFACTURE, AND COVERED APPROXIMATELY 75 PERCENT OF THE OIL IN HOLE AND 100 PERCENT OF TSDR 96ZZZX3200Brace Assy · fork brokeTHE FORK (FITTING) WHICH ATTACHES RETRACT ROD TO DRAG BRACE BROKE. ONE SIDE OF FORK APPEARED TO HAVE BEEN BROKEN FOR SOME TIME. THIS WAS OLDER STYLE FITTING WELDED TO BRACE. THIS IS DIFFICULT TO INSPECT WITHOUT DISCONNECTING RETRACT ROD.SDR AU960843Bolt · cracked(AUS) ENGINE MOUNT ATTACHMENT BOLT CRACKED UNDER HEAD - FOUND DURING NDT INSPECTION IAW AD/B55/74SDR 96ZZZX2572Transistor · failedTRANSMITTER MODULATOR TRANSISTOR Q3702 FAILED (SHORTED) CAUSING IC DRIVER U3701 TO FAIL. BOTH OF THESE COMPONENTS WERE BURNED CAUSING AN ELECTRICAL FIRE SMOKE ODOR TO BE PRESENT IN THE AIRCRAFT COCKPIT. SUBMITTER SUGGESTS THIS APPEARS TO BE AN ISOLATED INCIDSDR 96ZZZX2571Ic Driver · failedTRANSMITTER MODULATOR TRANSISTOR Q3702 FAILED (SHORTED) CAUSING IC DRIVER U3701 TO FAIL. BOTH OF THESE COMPONENTS WERE BURNED CAUSING AN ELECTRICAL FIRE SMOKE ODOR TO BE PRESENT IN THE AIRCRAFT COCKPIT. SUBMITTER SUGGESTS THIS APPEARS TO BE AN ISOLATED INCIDSDR 96ZZZX2166Bolt · brokenNOSE LANDING GEAR BOLTS, 2 EACH, BROKE CAUSING STEERING PROBLEMS WHICH CAUSED KNEE (SCISSORS) PN 96-820020-1 TO BREAK ON LANDING. SUSPECT CAUSE OF BOLTS TO BREAK WAS TURNING NOSE GEAR TOO MUCH TO THE LEFT OR RIGHT WHEN THE AIRCRAFT WAS TOWED PRIOR TO FLIGHT.SDR AU960311Bearing · seized(AUS) LH ELEVATOR PUSH-PULL ROD BEARING PNO NAS77-4-97 SEIZED AND WORKING IN FITTING PNO 95-610005-3 - ELONGATED HOLE WORN INFITTINGSDR 96ZZZX674Disc · chafe wheelsCLEVELAND BRAKE DISCS WERE REMOVED DUE TO WEAR. AFTER VERIFYING PART NUMBER AND INSTALLING NEW DISCS, AIRCRAFT WAS TAXI-TESTED. PILOT COMPLAINED THAT BRAKING WAS INADEQUATE. INSPECTION SHOWED MODERATE TO SEVERE CHAFE DAMAGE TO BOTH WHEELS AND TIRES FROM BRASDR 96ZZZX864Wire · shortedPILOT MADE UNEVENTFUL LANDING AFTER REPORTING SMOKE IN COCKPIT. INVESTIGATION REVEALED A WIRE SHORTED AS IT PASSED THROUGH LIGHTNING HOLE BEHIND BATTERY SWITCH. ONE SIDE OF WIRE WAS CONNECTED TO COMMON TERMINAL OF LANDING GEAR DOWN LIMIT SWITCH AND OTHER SIDSDR 95ZZZX1457Flap Motor · threads strippedA BEECHCRAFT FACTORY OVERHAULED FLAP MOTOR ASSY WAS ORDERED. UPON INSTALLATION, DISCOVERED 4 MOUNTING HOLES HAD A MAJORTIY OF ITS THREADS MISSING. SUBMITTER SUGGESTS MECHANICS SHOULD COMPLETELY INSPECT EVEN FRESHLY OVERHAULED PARTS.
Back to Beech 95-C55