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 engine_model_key = 'O360A1A' 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 engine_model_key = 'O360A1A' 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 AU001197Bracket · corroded(AUS) STABILISER ATTACHMENT BRACKET CONTAINED EXFOLIATION CORROSION INTHE OUTBOARD VERTICAL FACE.SDR CA001102007Spring · broken(CAN) DURING LANDING ON A GRAVEL STRIP THE TAIL WHEEL SPRING BROKE. PILOT KEPT CONTROL OF THE PLANE AND HAD NO OTHER DAMAGE. THE LOWER SPRING LEAF (P.N. O542106) HAS BEEN FOUND BROKEN AT TWO PLACES. ALL (4) SPRING LEAVES HAVE BEEN REPLACED WITH NEW UNITS.SDR EY2R56679Blade · brokenTIP OF NR 2 BLADE SNAPPED OFF 3.50 INCHES.SDR 20000516SH010Buckle · damagedNOSE GEAR BUCKLE OFF AT UPPER TRUSS. POSSIBLY WEAKENED BY OVERTURNING WITH TOW TRACTOR. SUBMITTER SUGGESTED HEAVIER METAL, BETTER SUPERVISION AND TRAINING. (X)SDR AU991028Bracket · cracked(AUS) NOSE LANDING GEAR LEFT (P/N 880-21-456-1) AND RIGHT (P/N 880-21-456-2) ATTACHMENT BRACKETS CRACKED.SDR AU990978Rib · corroded(AUS) WING RIB CONTAINED SEVERE EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE. THE RIB IS THE ONE TO WHICH THE LANDING GEAR OLEO STRUT IS ATTACHED.SDR AU990979Rib · corroded(AUS) WING RIB CONTAINED SEVERE EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE. CORROSION ALSO EVIDENT IN OTHER AREAS OF THE RIB.SDR AU990993Mount · cracked(AUS) NOSE LANDING GEAR RIGHT TOP OLEO MOUNT CRACKED ON THE TOP WELD ADJACENT TO THE STEERING STOP. THE CRACK EXTENDS FOR APPROXIMATELY 66 PERCENT OF THE TUBE CIRCUMFERENCE.SDR AU990994Mount · corroded(AUS) REAR RIGHT TAILPLANE HINGE MOUNT CONTAINS SLIGHT INTERGRANULAR CORROSION.SDR AU990995Rib · corroded(AUS) WING RIB CONTAINS EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE AND AT OTHER LOCATIONS ON THE RIB.SDR CA991028013Crank Case · cracked(CAN) CRACK FOUND IN VICINITY OF STARTER PAD.SDR AU990884Hinge · cracked(AUS) RIGHT ELEVATOR HINGE CRACKED THROUGH FROM THE ATTACHMENT BOLT HOLE.SDR AU990835Hinge · cracked(AUS) LEFT ELEVATOR HINGE CRACKED FROM ATTACHMENT BOLT HOLES.SDR AU990438Bracket · broken(AUS) LEFT CONTROL COLUMN SUPPORT BRACKET BROKEN THROUGH THE RADIUS AFT END ATTACHMENT.SDR 99ZZZX2181Shaft · shearedWHILE PERFORMING OPERATIONAL CHECK OF MAGNETO SYSTEM, NOTED THAT NORMAL DROP OCCURRED AT 1,800 RPM'S, BUT WAS ROUGH AT LOWER RPM'S. AFTER ELIMINATING PLUGS AND IGNITION HARNESS FOR DEFECTS, PULLED AND INSPECTED MAGNETO. UPON OPENING THE POINT/CAPACITOR AREA,SDR AU990430033Fork · worn(AU) PROPELLER RECEIVED FOR CORROSION INSPECTION. FORK WAS FOUND WORN BEYOND LIMITS, PROPELLER HAD NOT BEEN GREASED.SDR AU990867Hinge · cracked(AUS) RIGHT ELEVATOR HINGE CRACKED FROM ATTACHMENT BOLT HOLE.SDR AU990315Exhaust Pipe · fractured(AUS) NR 2 CYLINDER EXHAUST PIPE FRACTURED AT FLANGE.SDR AU990081Support · corroded(AUS) HORIZONTAL STABILIZER LEFT HINGE SUPPORT BRACKET CONTAINED EXFOLIATION CORROSION. FURTHER INVESTIGATION FOUND THAT THE HORIZONTAL STABILIZER P/N TB1034020100 CONTAINED MINOR EXFOLIATION CORROSION. PART TC: 4,880.SDR 98ZZZX4776Bearing · failedPILOT REPORTED NORMAL MAG CHECK PRIOR TO 10-MINUTE FLIGHT. AFTER LANDING NOTICED OIL DRIPPING FROM COWL. FOUND LT MAGNETO WITH LOWER MOUNTING EAR BROKEN OFF AND MAG PULLED AWAY FROM ACCESSORY CASE. THE MAGNETO CASE WAS GAPPED OPEN AND ONLY 2 SCREWS REMAINEDSDR CA990115007Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. SEVERE STONE DAMAGE WAS FOUND ON THE PROPELLER BLADES LEADING EDGES.SDR AU981404Spring · broken(AUS) NR 2 CYLINDER INLET VALVE PUSH ROD TUBE COVER RETAINING SPRING BROKEN. PART TC: 1,711.SDR AU981143Bearing · cracked(AUS) STABILATOR RIGHT HINGE BEARING CRACKED FROM THE BORE HOLE TO THE BOTTOM FLANGE OF THE HINGE. CRACK LENGTH 9 MM (0.35 INCH). PART TC: 6,109.SDR AU981041Door · malfunctioned(AUS) RIGHT DOOR OPENED IN-FLIGHT. INVESTIGATION COULD FIND NO FAULTS WITH THE LATCHES OR LOCKING MECHANISM.SDR 99ZZZX337Engine · mismanufacturedTHIS ENGINE WAS INSTALLED NEW ON A HOMEBUILT KIT VAN RV-6 AIRCRAFT. DUIRNG CRUISE FLIGHT, THE PROPELLER BECAME LOOSE CAUSING A VIBRATION. THE FRONT CRANKSHAFT COMPRESSION PLUG OPENED AND OIL WAS ALLOWED TO FLOW OUT AROUND THE BACK OF THE PROPELLER. SUBMITTESDR CA980811008Bearing · broken(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. PROPELLER BLADE BEARING WAS FOUND BROKEN.SDR 98ZZZX2559Crankshaft · failedAIRCRAFT SUFFERED CATASTROPHIC ENGINE SEIZURE. MADE SUCCESSFUL GOLF COURSE LANDING. ENGINE DISASSEMBLY RECEIVED BROKEN CRANKSHAFT AT THE FORWARD SIDE OF NR 4 ROD JOURNAL.SDR AU980680Spring · broken(AUS) NR 2 AND NR 3 CYLINDER PUSHROD RETAINING SPRINGS BROKEN. PART TC: 532.SDR 98ZZZX2044Spring Seat · failedENGINE SUCTION SCREEN REMOVED DURING ANNUAL INSP AND SEVERAL LARGE PIECES OF FERROUS METAL WERE FOUND. RECORDS INDICATED THE ENG HAD NEW CYLINDERS INSTALLED DURING OVERHAUL 272.7 HOURS PREVIOUSLY. THE PIECES OF METAL WERE FROM THE LOWER INTAKE VALVE SPRING SSDR AU980472Nut · loose(AUS) ENGINE THERMOSTATIC OIL COOLER BYPASS VALVE (VERNATHERM) CRIMP NUT LOOSE. NOTE: VALVE P/N 53E22144 IS NOT MENTIONED IN SB 318A AS A PROBLEM.SDR 98ZZZX528Impulse Coupling · wornPILOT FOUND 250 RPM MAG DROP, LT MAG. TROUBLESHOT IGNITION SYSTEM. REMOVED MAG AND FOUND EXCESS PLAY IN IMPULSE COUPLING AND MAG DRIVE. SENT OUT FOR REPAIR, SPRING WAS BROKEN. SUSPECT IMPROPER INSTALLATION OR DEFECTIVE METALLURGY PRIOR TO INSTALLATION.SDR AU980003Bracket · cracked(AUS) LH WING REAR ATTACHMENT BRACKET BROKEN THROUGH LOWER BOLT HOLE. SUSPECT CAUSED BY UNREPORTED HEAVY LANDING.SDR 97ZZZX4627Shaft · wornPILOT REPORTED ENGINE RUNNING ROUGH. PERFORMED TROUBLESHOOTING, FOUND RT MAGNETO ROTOR SHAFT AND ROTOR GEAR WORN BEYOND LIMITS. GEAR WAS FOUND LOOSE ON SHAFT. THIS IS THE SECOND SUCH 4300 SERIES TYPE MAGNETO WITH APPROXIMATELY 500 HOURS TT WITH THE SAME PROSDR 97ZZZX4628Gear · wornPILOT REPORTED ENGINE RUNNING ROUGH. PERFORMED TROUBLESHOOTING, FOUND RT MAGNETO ROTOR SHAFT AND ROTOR GEAR WORN BEYOND LIMITS. GEAR WAS FOUND LOOSE ON SHAFT. THIS IS THE SECOND SUCH 4300 SERIES TYPE MAGNETO WITH APPROXIMATELY 500 HOURS TT WITH THE SAME PROSDR AU970795Frame · cracked(AUS) FUSELAGE FRAME NO9 CRACKED AT TOP RH RADIUS IN AREA ABOVE STABILATOR ATTACHMENT FITTING - FOUND DURING INSPECTION IAW AD/TB10/11/01SDR CA970626019Door Hinge · cracked(CAN) ON INSPECTION THE AFT DOOR HINGE WAS FOUND CRACKED ON THE INSIDE OF THE RADIUS OF THE CURVE. SUBMITTER STATES THAT THIS PARTICULAR HINGE IS NOT PART OF PIPER SERVICE BULLETIN 682 AND AD 80-26-05.SDR CA970612004Blade Bearing · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTIOIN. BLADE BEARINGS, BALLS, BLADE CLAMPS AND CYLINDER WERE FOUND CORRODED. PARTS WERE REPLACED.SDR AU970613Throttle · wrong part(AUS) SUSPECT INCORRECT THROTTLE CONTROL FITTED - NO MICROSWITCH IS FITTED FOR THE UNDERCARRIAGE WARNING SYSTEM AND THE WIRING IS SECURED BEHIND THE INSTRUMENT PANEL - PERSONNEL/MAINTENANCE ERROR - UNAPPROVED PARTSDR CA970527013Bearing Balls · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADE BEARING BALLS WERE FOUND CORRODED AND REMOVED FROM SERVICE.SDR AU970293Balance Weight · loose(AUS) LH AILERON BALANCE WEIGHT LOOSE - `POP' RIVETS MOVINGSDR AU970298Rib · corroded(AUS) RH WING ROOT RIB LOWER FLANGE CORRODED IN AREA OF RIB TO LOWER WING SKIN ATTACHMENT RIVETS - AIRCRAFT OPERATES IN A SALT LADENENVIRONMENT AND IS NOT HANGAREDSDR AU970172Spinner · cracked(AUS) PROPELLER SPINNER CRACKED FROM ATTACHMENT SCREW HOLES - INVESTIGATION FOUND THAT THE SPINNER WAS NOT A FIRM FIT ON THE PROPELLER HUBSDR AU970169Plunger · sticking(AUS) ENGINE DRIVEN FUEL PUMP PLUNGER STICKING - INVESTIGATION FOUND THAT THE PLUNGER WAS JAMMED BY A SLIVER OF ALUMINIUM ALLOY APPROXIMATELY 5MM (0.196IN) IN LENGTH - METAL SLIVER APPEARS TO BE A SECTION OF THE REAR COVER RESULTING FROM THE MACHINING OFTHE FUSDR CA961105004Discs · defective(CAN) AFTER DISC REPLACEMENT, AND WHILE TAXIING A PULSATING WAS FELT IN THE RUDDER PEDALS. BRAKE DISC THICKNESS MEASURED AND FOUND TO HAVE .006 TO .007 INCH DIFFERENCE FROM ONE SIDE TO THE OTHER. DISCS REPLACED AGAIN.SDR CA961018008Skin · corroded(CAN) INTERIOR OF FUSELAGE SKIN AND BULKHEADS FOUND CORRODED WHERE GLUE IS USED TO SECURE INSULATION TO COMPONENTS INSIDE THE CABIN.SDR AU960848Switch · seized(AUS) LANDING GEAR WARNING MICROSWITCH SEIZED IN 'SAFE' POSITIONSDR 96ZZZX3340P-Lead · deterioratedENGINE INTERMITTENT, ROUGHNESS, WAS BELIEVED CAUSED BY LEFT MAGNETO P-LEAD SHORTING OUT AGAINST OUTSIDE SHIELDING. BOTH LT AND RT P-LEADS INTERNAL INSULATION HAD DETERIORATED TO POWDER. THIS CONTRIBUTED TO ACCIDENT. P-LEADS APPEARED TO BE ORIGINAL EQUIPMENTSDR AU960567Stiffener · cracked(AUS) FUSELAGE STIFFENER LH CRACKED IN AREA OF TORQUE TUBE SUPPORT REAR ANCHOR NUT HOLE - FOUND DURING INSPECTION IAW SOCATA 10-77-53SDR AU960501Fitting · damaged(AUS) LH FRONT WING ATTACHMENT FITTING AT FUSELAGE DAMAGED - FUSELAGE PANELS LH AND RH SIDE ABOVE MAIN SPARS DISTORTEDSDR CA960509202Ribs · bent(CAN) RIGHT WING RIBS AT W.S. 94.864, 108.281 AND 122.500 FOUND BENT AND BUCKLED UNDER THE UPPER WING SKIN. POSSIBLY CAUSED BY OVERPRESSURE OF FUEL IN AUXILIARY TANK (THERMAL EXPANSION ).
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