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 = 'PA31' 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 = 'PA31' 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 CA990318022Trunnion · cracked(CAN) NOSE GEAR WAS OVER-STEERED WITH SCISSORS HOOKED TOGETHER.SDR CA990125006Blade · corroded(CAN) DURING OVERHAUL, CORROSION WAS FOUND IN THE BLADE BALANCE HOLES. INSPECTED AND CORROSION WAS REMOVED PER HARTZELL SB 136.SDR CA990115015Seal · leaking(CAN) OIL LEAK REPORTED BY PILOT. INSPECTION FOUND THE FRONT CRANKSHAFT SEAL LEAKING. IT HAD SLIPPED OUT APPROXIMATELY .0625 INCH AND WAS LOOSE. THE POSSIBLE CAUSE WAS A COLD START AND THE ENGINE RPM TOO HIGH DURING ENGINE WARM UP CAUSING HIGH OIL PRESSURE.SDR CA981230014Switch · failed(CAN) COMPLIANCE WITH AD 96-20-07 FOUND THE PRESSURE SWITCH UNSERVICEABLE.SDR CA981230041Spar · cracked(CAN) INSPECTION PER SB 998A. LEFT HAND SPAR FOUND CRACKED AT THE VERY TIP, OUTBOARD RIB CONNECTION. NEW SPAR, NR 40075-020 INSTALLLED.SDR CA990310033Switch · intermittent(CAN) DURING APPROACH, THE CREW WERE UNABLE TO GET A 'DOWN AND LOCKED GREEN LIGHT' ON THE NOSE GEAR. THEY CYCLED THE GEAR SEVERALTIMES AS WELL AS TRYING THE HAND PUMP. INVESTIGATION REVEALED AN INTERMITTENT CIRCUIT IN THE 'DOWN AND LOCKED' CLOSED SIDE OF THE SDR CA990310032Switch · failed(CAN) DURING APPROACH,THE CREW SELECTED GEAR DOWN AND DID NOT GET A GREEN NOSE LOCKED INDICATION. THEY FLEW FOR ABOUT 20 MINUTES WHILE CYCLING THE GEAR TO TRY TO GET AN INDICATION. INSPECTION REVEALED THE NOSE GEAR DOWN AND LOCKED MICROSWITCH P/N 1CH21-4 WAS SDR CA990318020Slip Ring · shorted(CAN) SLIP RING (TRACKS) WERE SHORTED OUT.SDR CA981209010Crankcase · cracked(CAN) DURING INSPECTION, THE PRESENCE OF AN OIL LEAK AT THE LOWER FORWARD STUD AT NR 2 CYLINDER LED TO FINDING A CRACK 1.50 INCHES LONG IN THE CRANKCASE, WHICH WAS VERIFIED BY A FLUORESCENT PENETRANT INSPECTION. THE ENGINE WAS REPLACED.SDR CA990318019Tee · cracked(CAN) HYDRAULIC MANIFOLD CRACKED.SDR CA981207026Regulator · intermittent(CAN) PILOTS REPORTED LEFT WING DE-ICER BOOT NOT VERY EFFICIENT WHEN NEEDED. TESTING EVENTUALLY FOUND HOSE P/N 82371-106 FROM FIREWALL TO DUAL REGULATOR LEAKING IF AIRCRAFT ROCKED DURING TEST. THE HOSE WAS HARDENED. THE LOW PRESSURE VALVE WAS NOT OPERATING SDR CA981202015Magneto · failed(CAN) PILOT REPORTED NR 2 ENGINE HARD TO START. SPARK PLUGS WERE REPLACED AND MAINTENANCE FOUND ALL MAGNETO SWITCHES IN THE ON POSITION, MAGS WERE TURNED OFF. IT IS ASSUMED THE SHUT-DOWN PROCEDURES WERE CUT SHORT. AIR CREWS WERE CAUTIONED ON DANGER OF LEAVISDR CA981130019Support · broken(CAN) ENGINE RECEIVED FROM OVERHAUL ON EXCHANGE. INSPECTION FOUND THE BOLT HOLDING THE TOP TURBO ROD TO THE ENGINE BENT. THE BOLT WAS BENT DUE TO IT BEING FORCED TO MOUNT A SUPPORT PLATE WITH INCORRECT DIMENSIONS. THE FORCING OF THE SUPPORT PLATE LED TO ITSSDR CA981123008Heater Can · cracked(CAN) EXHAUST FUMES IN CABIN. MAINTENANCE CHECK OF FORWARD CABIN HEATER FOUND A 1.5 INCH CRACK AT THE BOTTOM OF THE CAN BY THE EXHAUST STACK. ALSO, CAN WAS BUCKLED AT CRACK AREA. HEATER REPLACED.SDR CA981007007Switch · corroded(CAN) WHEN FLAPS SELECTED TO 15 DEGREES, THEY STUCK. AIRCRAFT LANDED OK. INVESTGATION FOUND CORROSION ON THE UPPER LIMIT SWITCH.SDR CA980922020Skin · cracked(CAN) BEACON CIRCUIT BREAKER TRIPPED. WATER INFILTRATING THE FRONT TOP END OF THE VERTICAL STABILIZER, AND RUNNING INTO POWER PACK IN THE BEACON. THE BEACON IS MOUNTED ON THE FIN TIP. THIS WAS ORIGINALLY USED FOR AN ADF ANTENNA INSTALLATION ALSO BUT WAS NO LSDR CA990310035Fitting · restricted(CAN) DURING CRUISE,THE NR 2 ENGINE LOST THE TURBO AND WENT NORMALLY ASPIRATED. SMOKE WAS OBSERVED COMING FROM THE EXHAUST, SO A PRECAUTIONARY SHUTDOWN WAS CARRIED OUT, DUE TO THE POSSIBILITY OF OIL LOSS FROM THE TURBO. POST-FLIGHT INSPECTION REVEALED NO LOSSDR AU981295Nlg · lack of lube(AUS) NOSE LANDING GEAR FAILED TO OPERATE CORRECTLY DUE TO LACK OF LUBRICATION. INVESTIGATION FOUND THAT THE AIRCRAFT HAD FLOWN THROUGH HEAVY RAIN WITH THE LANDING GEAR DOWN FOR APPROXIMATELY 20 MINUTES ON THE PREVIOUS FLIGHT THREE DAYS EARLIER.SDR CA980915018Wire · broken(CAN) ON APPROACH, DURING LANDING GEAR LOWERING, NO LIGHT INDICATION OR FLAG FOR THE RIGHT MAIN LANDING GEAR. EMERGENCY DECLARED AND AIRCRAFT LANDED SAFELY. MAINTENANCE INVESTIGATION FOUND A BROKEN WIRE.SDR 98ZZZX3458Control Cable · brokenPILOT REPORTED HAVING NO CONTROL OF MIXTURE. INSPECTION FOUND MIX IN FULL RICH POSITION ON FUEL SERVO AND CONTROL CABLE BROKEN. BREAK WAS DETERMINED TO BE INSIDE CABLE HOUSING AT CONSOLE END. NO RECORD OF CABLE REPLACEMENT FOUND. AIRCRAFT HAS 10,600 HOURS.SDR CA980827007Hinge · failed(CAN) RIGHT OUTBOARD GEAR DOOR APPEARED LOOSE. FORWARD HINGE BROKEN. A CRACK HAD ORIGINATED IN THE INNER RADIUS OF THE ELBOW SECTION. CRACK APPEARED TO HAVE RUN 3/4 WAY THROUGH BEFORE IT FAILED.SDR CA980915012Switch · loose(CAN) NO GREEN LIGHT INDICATION FOR DOWN AND LOCKED LANDING GEAR. MAINTENANCE FOUND MICROSWITCH ON RIGHT LANDING GEAR LOOSE. MICROSWITCH ADJUSTED AND SECURED. RETRACTION TESTS CHECKS SERVICEABLE.SDR CA980916016Head · cracked(CAN) DURING CLIMB-OUT, THE NR 1 ENGINE BEGAN TO RUN ROUGH. A SHORT TIME LATER, OIL STARTED TO APPEAR ON THE ENGINE COWLING. THE CREW DID A PRECAUTIONARY SHUTDOWN AND RETURNED TO THE POINT OF DEPARTURE. POST-FLIGHT INSPECTION FOUND THE NR 3 CYLINDER WITH ASDR AU981092Plate · cracked(AUS) RIGHT ENGINE INBOARD ENGINE MOUNT PLATE LOOSE AND RIVETS MISSING. PART TC: 9,754.SDR 98ZZZX3420Clamp · looseEXHAUST CLAMP CAME LOOSE IN-FLIGHT ALLOWING EXHAUST STACK TO COME LOOSE FROM THE TURBOCHARGER EXIT PORT ON THE LEFT ENGINE. HOT EXHAUST GASSES BLISTERED THE PAINT ON THE AFT CENTER OF THE COWLING. ENGINE WAS SECURED/FEATHERED AND UNEVENTFUL LANDING ACCOMPLISSDR 98ZZZX3196Wheel · corrodedMAIN WHEEL WAS DISASSEMBLED FOR BRAKE DISC REPLACEMENT. THE INBOARD HALF WAS SEVERELY PITTED FROM CORROSION AND HAD TO BE REPLACED. THIS AREA CANNOT BE SEEN UNLESS THE DISC IS REMOVED. THE AREA SHOULD BE LOOKED AT EVERY TIRE CHANGE.SDR 98ZZZX3026Bracket · crackedFOUND TURBO UPPER AFT MOUNT BRACKET CRACKED AT WELD. THIS WAS A HARD AREA TO SEE AND SHOULD BE LOOKED AT EVERY INSPECTION.SDR AU981006Rod · cracked(AUS) NR 3 CYLINDER CONNECTING ROD CRACKED. FOUND USING FLUORESCENT MAGNETIC PARTICLE TECHNIQUE.SDR CA981006008Turbocharger · leaking(CAN) ON TAKEOFF ROLL, THE TURBO CHARGER OIL SEAL FAILED CAUSING A LOSS OF POWER (MANIFOLD PRESSURE) AND SMOKE FROM THE EXHAUST. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE RAMP. TURBOCHARGER WAS REPLACED. NO OTHER FAULTS WERE FOUND.SDR CA980706023Seal · leaking(CAN) PILOT SIDE WINDOW SEAL LEAKING PERMITTING WATER TO ENTER CIRCUIT BREAKER PANEL DIRECTLY BELOW WINDOW. PANEL FULL OF WATER. BAD RADIO COMMUNICATION, INSTRUMENTS LIGHTS FLUCTUATING, WARNING LIGHTS AND LANDING GEAR LIGHTS GOING OUT. REPAIRED.SDR CA980706022Beacon · failed(CAN) STROBE BEACON FAILED AFTER 98 HOUR, THEN 3 HOURS, THEN TRIPPED CIRCUIT BREAKER AFTER 61 HOURS AND THEN AT 25 HOURS. UNIT RETURNED. REPLACED.SDR AU980808Pipe · corroded(AUS) HYDRAULIC PIPE LOCATED IN THE LOWER FUSELAGE ADJACENT TO THE SPAR CONTAINED A CORROSION PIN HOLE IN THE AREA BELOW THE PIPE IDENTIFICATION TAG. PART TOTAL CYCLES: 19,729.SDR AU980640Pump · seized(AUS) RT ENGINE DRIVEN FUEL PUMP FAILED INTERNALLY.SDR CA980615005Brake · locked(CAN) INSPECTION REVEALED FLAT SPOT ON LT WHEEL. BRAKE GRINDING WHEN TOWED, DISCS WARPED. BRAKES AND WHEELS REPLACED.SDR CA980603004Pump · leaking(CAN) DURING FLIGHT, THE PILOT NOTICED THE NR 2 ENGINE FUEL GAUGE DROPPING RAPIDLY WITH A CORRESPONDING DROP IN FUEL PRESSURE. THE EMERGENCY FUEL PUMP WAS SELECTED ON AND THE FUEL LOSS INCREASED. THE ENGINE COUGHED AND THE FUEL CROSS FEED WAS SELECTED, STILL FSDR CA980603003Bolt · failed(CAN) LOSS OF POWER ON NR 1 ENGINE FOLLOWED BY OIL LOSS. ENGINE WAS SHUTDOWN. INSPECTION FOUND THE STUDS AND THRU BOLT ON THE ENGINE CASING BROKEN.SDR AU980562Bolt · failed(AUS) LT ENGINE NR 6 CYLINDER HOLD-DOWN BOLTS/STUDS (6OFF) BROKEN.SDR CA980529003Hinge · cracked(CAN) LANDING GEAR DOOR HINGE BRACKET CRACKED IN INNER RADIUS. REPLACED.SDR AU980542Coil · failed(AUS) MAGNETO COIL CASE SHORT CIRCUITING TO MAGNETO FRAME.SDR AU980514Bracket · corroded(AUS) RUDDER CORRODED. WHEN THE RUDDER WAS REMOVED, THE TOP AND CENTER HINGE BRACKETS WERE FOUND TO BE CRACKED ON THE SPARS AND DOUBLERS.SDR 98ZZZX2167Pump · failedPILOT REPORT - GEAR SLOW TO RETRACT. FOUND HYDRAULIC PUMP INOPERATIVE RT ENGINE. HYDRAULIC PUMP DRIVE GEAR SEPARATED INTO TWO PARTS. GEAR KEYWAY AND SECTION OF GEAR FOUND IN OUTLET SECTION OF PUMP HEAD. THERE WAS NO SIGN OF SEIZURE TO CAUSE THIS FAILURE.SDR 98ZZZX2053Alternator · shortedPILOT REPORTED BOTH ALTERNATORS FAILED. PILOT TRIED AUXILIARY REGULATOR, ALTERNATOR CAME ON-LINE FOR SHORT TIME, THEN FAILED. INVESTIGATION REVEALED THE FIELD OF THE RT GENERATOR WAS INTERMITTENTLY SHORTING TO GROUND. SUBMITTER SUSPECTED INSULATION BREAKDOWSDR CA980506010Transition · cracked(CAN) TURBOCHARGED TRANSITION HEADER LOOSING POWER. TRANSITION REMOVED, FOUND CRACKED INSIDE AND HAD BEEN PREVIOUSLY REPAIRED, WELD LIFTING AND CRACKING. REPAIRED.SDR CA971006007Relay · corroded(CAN) FLAP MOTOR INTERMITTENT ON TAKEOFF AND LANDING. MAINTENANCE FOUND RELAY OF MOTOR PITTED. FLAP MOTOR WAS REPLACED.SDR CA980430039Windshield · cracked(CAN) IN CRUISE, THE PILOT HEARD A LOUD BANG AND NOTED THAT THE LT WINDSHIELD HAD A 6 INCH CRACK IN THE CENTER. AIRSPEED WAS REDUCED AND THE CRACK PROGRESSED ACROSS THE WINDSHIELD. ON APPROACH, HEAT WAS APPLIED AND A U-SHAPE CRACK APPEARED AT THE ELEMENT. RSDR AU980378Pipe · fractured(AUS) RT ENGINE NR 4 INJECTOR LINE FRACTURED ADJACENT TO THE INJECTOR NOZZLE.SDR CA980407012Fuel Pump · leaking(CAN) AFTER OVERHAULED ENGINE WAS INSTALLED, A LEAK CHECK WAS CARRIED OUT. WHEN AIRCRAFT BOOSTER PUMPS WERE TURNED ON, FUEL POURED FROM THE ENGINE DRIVEN FUEL PUMP THROUGH THE BASE DRAIN LINE. THE FUEL PUMP WAS REPLACED AND THE FAILED PUMP WAS RETURNED TO THSDR AU981359Lug · separated(AUS) ROCKER SHAFT RETAINING LUG BROKE OFF THE ROCKER HAT ALLOWING THE INLET VALVE ROCKER SHAFT TO MIGRATE AND THE ROCKER TO DISLODGE. THE LUG IS NORMALLY SILVER SOLDERED TO THE ROCKER HAT. SUBMITTER SUSPECTED CAUSE AS POORLY SOLDERED JOINT.SDR CA971021003Housing · cracked(CAN) AFTER LANDING, PILOT REPORTED LT LANDING STRUT WAS FLAT AND LEAKING FLUID. MAINTENANCE INSPECTION REVEALED STRUT HOUSING HAD A 16 INCH VERTICAL CRACK. HOUSING REPLACED.SDR CA980402021Spar · cracked(CAN) AILERON FRONT SPAR FOUND CRACKED. FOUND DURING REBUILD. AD 96-21-03 MANDATED SB 974 THE INSTALLATION OF BRACKET WHICH TERMINATED REPEAT INSPECTION. REPAIRED.
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