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 CA120209005Distributor Blk · chafed(CAN) DISTRIBUTOR BLOCK FOUND WITH BUSHING WORN, CAUSING CHAFING ON DISTRIBUTOR BLOCK SPARK PINS. NEW DISTRIBUTOR BLOCK, PN:10-391586 INSTALLED. NEW GEAR, PN:10-349237 INSTALLED. MAGNETO RETURNED TO SERVICE.SDR CA120205001Starter · failed(CAN) LEFT ENGINE WOULD NOT TURN OVER. STARTER REPLACED.SDR CA120105003Starter · loose(CAN) DURING A SCHEDULED INSPECTION, THE RT STARTER AFT CASE WAS FOUND LOOSE. THE CASE ATTACH BOLT LOCK TABS WERE STILL ENGAGED, BUT THE BOLTS WERE LOOSE. STARTER WAS REMOVED AND REPLACED WITH A SERVICEABLE SPARE.SDR CA120209003Points · failed(CAN) BREAKER POINT POPPED MAGNETO.SDR CA120205002Starter · intermittent(CAN) RIGHT HAND STARTER INTERMITTENT. REPLACED STARTER.SDR CA111123014Control Cable · damaged(CAN) UPON RIGGING PROP CONTROLS AFTER CABLE REPLACEMENT ON RT ENGINE, FOUND SUSPICIOUS LT PROP CONTROL ATTACHMENT. JOINT ASSEMBLY PN 469-153 WAS RUSTED, BUT MOST UNUSUAL WAS THAT A FIBRE LOCK NUT WAS USED AS SECURING DEVICE AND THAT THREADS WERE WELL BELOW FSDR CA111117011Mount · cracked(CAN) DURING SCHEDULED INSPECTION OF RT ENGINE, THE LT UPPER TURBO MOUNT TUBE WAS FOUND CRACKED. TURBO MOUNT REPLACED WITH PN: LW15952. TSN OF REMOVED PART COULD NOT BE DETERMINED.SDR CA120209002Bushing · worn(CAN) DISTRIBUTOR BLOCK FOUND WITH BUSHING WORN, CAUSING CHAFING ON DISTRIBUTOR BLOCK SPARK PINS. NEW MAGNETO INSTALLED (SN: F09CA093) (TC# 20120209002)SDR CA110826009Tire · deflated(CAN) ON TAXI PILOT REPORTED HEARING A LOUD NOISE AND DIFICULTY TAXING. UPON FURTHER INVESTIGATION FOUND RT TIRE WAS FLAT. ACFT WAS TAKEN TO HANGAR AMO 60-99 AND TIRE WAS REMOVED. THE CAUSE OF THE FLAT TIRE WAS THE INBD RIM WAS SPLIT ALONG THE BEAD.SDR CA110818005Cylinder · failed(CAN) AT APPROX 2115 UTC ON 15 AUG 11, IN CRUISE FLIGHT, ENROUTE, EXPERIENCED DROP IN MANIFOLD PRESSURE ON LT ENGINE, FOLLOWED BY VIBRATION. PILOT FEATHERED PROP, SECURED ENGINE, DECLARED EMERGENCY, DIVERTED, AND LANDED WITHOUT FURTHER INCIDENT. SUBSEQUENT ISDR CA110606016Bushing · wornRT ENGINE, CAN`T RESTART ENGINE ON GROUND. LT MAGNETO REMOVED, INSPECTED AND FOUND BUSHING WORN OUT ON GEAR. SENT TO O/H.SDR CA110512004Pump · failedACFT EXPERIENCED RT PNEUMATIC FAILURE DURING GROUND RUN. RT DRY AIR PUMP REPLACED.SDR CA110216003Hose · rupturedGEAR WOULD NOT LOCK DOWN WHEN SELECTED BY PILOT. IT HAD TO BE LOCKED MANUALLY THROUGH HAND PUMP. FOUND HYD SYS FLUID DEPLEATED FROM BURST LT MAIN GEAR UP LOCK HOSE. FOUND HYD SYS HOSES IN LANDING GEAR SYS APPEARED TO BE ORIGINAL, INSTALLED AT TIME OF ACFT MFGSDR CA110208027Tube · deflated(CAN) AFTER NORMAL LANDING AND TAXI TO SKYWINGS HANGAR - TIRE WENT FLAT WHILE UN LOADING PASSENGERS. UPON FURTHER INSPECTION - TUBE SPLIT AT THE SEAM. OTHER THAN SPLIT SEAM - TUBE WAS IN GOOD CONDITION. TUBE WAS INSTALLED NEW MARCH 5TH, 2010.SDR CA110131009Spar · cracked(CAN) CRACK ON SPAR COMPLETE ACROSS LOCATED AT APPROX 4 INCHES IB OF OB HINGE AT THE INSPECTION HOLE THE SURFACE SKIN HAD A SMALL CRACK WHICH PROMPTED US TO LOOK FURTHER. THIS INSPECTION IS LONGER DONE AS PER AD 99-12-05. THIS VISUAL INSPECTION SHOULD BE DONESDR CA110125003Engine · fluctuatesIFSD CREW REPORTS STATE THAT DURING CLIMB, PASSING 11000 FT AT HIGH POWER, WHILE MONITORING TORQUE AND OIL PRESSURE FLUCTUATIONS THE ENGINE LOST OIL PRESSURE, WHICH COINCIDED WITH A LOUD NOISE AND AUTOFEATHER.SDR CA110113001Housing · crackedDURING 100 HRS INSP, WE FOUND THE NLG HSG CRACK.SDR CA101122013Hose · ruptured(CAN) DURING APPROACH PILOT SELECTED GEAR DOWN AND THE LANDING GEAR FAILED TO EXTEND. PILOT SELECTED LANDING GEAR HANDLE TO THE UP POSITION THEN CYCLED THE GEAR HANDLE BACK TO THE DOWN POSITION AGAIN WITH A FAILURE OF THE GEAR TO EXTEND. APPROACH CANCELLED ASDR CA110103011Alternator · warning lightRT ALTERNATOR INOP LIGHT ILLUMINATED. REPLACED ALTERNATOR.SDR CA101115026Cylinder Head · separated(CAN) PILOTS REPORT CHT HIGH, THEN CHT TEMP FELL OFF TO BOTTOM OF GREEN ARC. ENGINE LOST SOME MANIFOLD PRESSURE. ON INSPECTION AFTER LANDING, IT DISCOVERED THAT CYLINDER NR 6, CYLINDER HEAD HAD COMPLETELY SEPARATED FROM THE BARREL. NO OTHER DAMAGE. CYLINDESDR CA101210005Altimeter · inaccurate(CAN) ALTIMETER INDICATING 150 FEET LOW AT ALTITUDES BETWEEN 2,000 AND 10,000 FEET. ALTIMETER WAS PREVIOUSLY REPAIRED AND RECERTIFIED IN AUGUST 2010. ALTIMETER REPLACED.SDR CA101108010Altimeter · reads low(CAN) ENCODING ALTIMETER REPORTING 150 FEET LOW AT ALL ALTITUDES BETWEEN 2000 AND 10,000 FEET. UNIT WAS REPAIRED AND RECERTIFIED JULY 30, 2010. NEXT DUE FOR RECERTIFICATION JULY 30, 2012.SDR CA101022001Pump · cracked(CAN) HYD PUMP ON LT ENGINE FAILED TO RESPOND DURING OPS TEST ON GROUND. ACFT RETURNED TO BASE WHERE THE HYD PUMP WAS FOUND CRACKED AND LEAKING. CRACK WAS RADIATING FROM THE CTR RING OF THE PUMP WHERE THE BOLTS GO THROUGH TO HOLD THE PUMP TOGETHER. PUMP WAS SDR CA101007010Magneto · intermittentINTERMITTENT IGNITION FAILURE AT CRUISE POWER SETTING, CAUSING PARTIAL LOSS OF POWER AND OVERHEAT.SDR CA100730001Gyro · failedTHE GYRO HORIZON FAILED ON FIRST FLIGHT AFTER INSTALLATION. IT TOPPLES TO 90 DEGREES DURING A 20 DEGREE BANK.SDR CA100720001O-Ring · leaking(CAN) COWLS REMOVED FOR SCHEDULED OIL CHANGE, BOTH UPPER AND LOWER COWLS OIL SOAKED WITH STREAKING DOWN NACELLE. ENGINE IS 109.3 HOURS OUT OF OVERHAUL AND AS THIS IS THE THIRD OCCURENCE. FIRST OCCURENCE AT 63.9 HOURS NR 4 CYLINDER REMOVED AND NICKED AND TWISSDR CA100715002Pump · low pressure(CAN) FUEL PRESSURE FOUND TO BE LOW FROM THE PUMP, REPLACED WITH A SERVICABLE PUMP.SDR CA100708003Uplock Hook · out of adjustAIRCRAFT RETURNED TO HANGER AFTER HAVING THE IN TRANSIT LIGHT ON WHEN THE GEAR WAS SELECTED UP. AIRCRAFT WAS JACKED AND GEAR SWING CARRIED OUT IAW TABLE VII-1 OF PIPER MAINTENANCE MANUAL AND TROUBLE SHOOTING. FIRST GEAR SWING EVERYTHING WORKED AS PER NORMAL,SDR CA100617008Trunnion · crackedTHE NLG OLEO HAD A SMALL FLUID LEAK THUS THE OLEO WAS GETTING NEW O-RINGS INSTALLED AND BEING SERVICED. DURING THE PROCESS, A CRACK WAS NOTICED IN THE PAINT NEAR THE TURN LIMIT STOP. THE PAINT WAS STRIPPED AWAY AND THE CRACK WAS CONFIRMED VISUALLY. THERE DSDR CA100525013Pump · malfunctionedTHE PUMP ASSY WOULD NOT ALWAYS START WHEN THE SWITCH SELECTED TO ON. IF THE MOTOR WAS TAPPED WITH A SCREW DRIVER THE PUMP WOULD FUNCTION. FUEL BOOST PUMP REPLACED.SDR CA100218007Regulator · failed(CAN) THIS FUEL REGULATOR IS NEW AND FAILED TEST AFTER INSTALLATION. THIS PART IS INSPECTED EVERY 100 HOURS IAW AD 2004-25-16R1 FOR LEAKS AND IT NEVER MADE IT PAST THE TESTING STAGE. (TC 20100218007)SDR CA100202005Lifter · broken(CAN) SHORT WHILE AFTER TAKEOFF OIL PRESSURE ON THE LT ENGINE STARTED FALLING BELOW THE GREEN. RPM ALSO STARTED FALLING. WHEN OIL PRESSURE CAME CLOSE TO RED LINE, PILOT PULLED FEATHER (PROP) & SHUTDOWN THE ENGINE. AFTER INSP OF THE ENG, IT WAS FOUND THAT NR SDR CA100129007Blades · damaged(CAN) 2 PROPELLER BLADES, SN E33784 & E33694 CONTAINED TOOL MARKS/GOUGES IN THE BOTTOM OF THE BALANCE HOLES, WHICH WERE FOUND THROUGH VISUAL INSPECTION. THE BLADES HAVE BEEN SENT OUT FOR REAMING OF THE BORES AND RESHOT PEENING IAW MM 202A VOLUMES 2 REV. 28, VOSDR CA100127003Shaft · broken(CAN) GROUND TEST AFTER FLIGHT, LANDING GEAR HANDLE DIDN`T RETURN TO NEUTRAL AFTER TEST. PUMP REMOVED AND FOUND DRIVING SHAFT BROKEN, PUMP REPLACED & CHECK OK. THIS KIND OF EVENTS HAPPEN FOR THE SECOND TIME FROM THE SAME SUPPLIER.SDR CA091223012Key · broken(CAN) GROUND TEST AFTER FLY, LANDING GEAR HANDLE DIDN’T RETURN TO NEUTRAL AFTER TEST. MAINTENANCE ACTION, HYDRAULIC LEVEL CHECK OK, HYDRAULIC PUMP REMOVED AND FOUND DRIVING SHAFT KEY BROKEN. PUMP REPLACED AND CHECK OK (TC NR 20091223012)SDR CA091228001Gasket · torn(CAN) AFTER TAKEOFF, THE CREW REPORTED LOW OIL PRESSURE AND HIGH OIL TEMPERATURE ON THE LEFT ENGINE. A CIRCUIT AND LANDING WERE CARRIED OUT. THE OIL WAS DRAINED AND THE SUCTION SCREEN AND SPIN ON FILTER INSPECTED FOR CONTAMINATION. THERE WERE SEVERAL VERY SSDR CA090905002Case · crackedMAGNETOS WERE REMOVED FROM LT ENG AND SENT FOR 500 HR INSP. INSP REVEALED A CRACK IN THE MAGNETO HSG. MAG MAY HAVE BEEN CRACKED FROM MFG. MAGNETO WAS SCRAPED.SDR CA090812002Altimeter · unserviceableALTIMETER UNSERVICABLE.SDR CA090710005Wedge · loose(CAN) MAG WAS RECEIVED FOR 500 HR INSP BUT NO HOURS WERE PROVIDED. WHEN MAG WAS DISASSEMBLED ONE OF ALUMINUM COIL WEDGES WAS FOUND LOOSE AND HAD TRAVELLED AROUND INSIDE MAG CAUSING DAMAGE TO DISTRIBUTOR GEAR. APPROX 5 GEAR TEETH WERE BROKEN OFF AND WERE FOUND SDR CA090430006Drive Shaft · broken(CAN) PUMP FAILED AT RUN-UP, MECHANICS REPLACED THE PUMP AND FOUND THE DRIVE SHAFT BROKEN.SDR CA090317003Line · fractured(CAN) FUEL INJECTOR LINE BETWEEN MANIFOLD AND NR 1 CYLINDER FAILED AT BEND ABOVE CYLINDER, CAUSING PARTIAL LOSS OF POWER. RESULTING VIBRATION LIKELY CAUSED SUBSEQUENT FAILURE OF 3 CYLINDER ATTACH STUDS, 50-15 AND 38-13.SDR CA090303001Tube · cracked(CAN) PILOT REPORTED BLACK DIRT IN WINDSHIELD AFTER FLIGHT, MECHANIC PERFORM PRESSURE DECAY TEST AND FOUND CRACKED BETWEEN CHAMBERS, THIS AREA WAS NOT ACCESSIBLE ENOUGH TO SEE THE DAMAGE.SDR CA090107004Rib · cracked(CAN) DURING MX, RIB P/N 40423-06, WHICH RUNS THROUGH THE LT WW, WAS FOUND CRACKED THROUGH AT THE NARROWEST PART OF THE RIB AT THE TOP CENTER OF THE WW. THE WING SKIN IMMEDIATELY ABOVE AND ATTACHED TO THE RIB ALSO HAD A SMALL CRACK WHICH COINCIDED WITH THE RIBSDR CA081128006Valve Seat · worn(CAN) INTAKE VALVE STAYING OPEN, INTAKE VALVE AND SEAT WORN.SDR CA081029002Probe · malfunctioned(CAN) PILOT OBSERVED LT ENG CYLINDER HEAD TEMP OVER RED-LINE. OTHER ENG PERIMETERS WERE NORMAL. PILOT CHOSE TO SHUTDOWN THE ENG AND FEATHER THE PROPELLER. LANDED WITHOUT INCIDENT. MAINT TROUBLESHOT AND FOUND LT ENGINE CHT READ 150 DEGREES WHEN ENGINE WAS COLD.SDR CA080904006Coil · damaged(CAN) MAG WAS RECEIVED FOR 500 HOUR INSPECTION. WHEN DISASSEMBLED THE COIL TAB WAS FOUND TO BE BENT DOWN AND ALMOST TOUCHING THE INSULATION COVERING THE COIL (APPROX. 10 DEGREES). THE CARBON BRUSH HAD WORN THE EXTERNAL EDGE ONLY. THIS TAB IS SUPPOSED TO BE LEVSDR CA080822011Pump · seized(CAN) DURING INSPECTION THE LT ENGINE VACUUM PUMP FOUND SEIZED, REPLACED.SDR CA080711012Starter · inoperative(CAN) THE STARTER WOULD NOT WORK AT ALL, REPLACED WITH A SERVICEABLE STARTER.SDR CA080708009Starter · unserviceable(CAN) THE STARTER WOULD NOT ENGAGE, REPLACED WITH A SERVICABLE STARTER.SDR CA080618009Bolt · missing(CAN) DURING INSP IT WAS DISCOVERED THAT BOTH BOLTS SECURING THE TURBO TO THE UPPER TURBO SUPPORT HAD COME OUT. THE TURBO WAS LEAKING EXHAUST GASES FROM THE SEAM BETWEEN THE TURBINE HOUSING AND THE BEARING HOUSING. WILL SUPPLY HOURS OF THE TURBO THE NEXT FEW D
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