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 = 'O235' 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 = 'O235' 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 2003FA0001130Bracket · crackedFOUND LT REAR VERTICAL FIN BRACKET CRACKED AT BASE (FITTING).SDR 2003FA0000853Attach Fitting · crackedON ANNUAL INSPECTION FOUND LEFT VERTICAL FIN ATTACH POINT OUTBOARD EAR BROKEN OFF. ALSO FOUND A STEEL TAPERED SHIM (.018 TO .065) UNDER THE RIGHT THREE OF THE FOUR AFT FIN ATTACH FITTING BOLTS. TECH SUPPORT FOUND NO REF TO ANY SUCH PART. REMOVED SHIM AND RESDR 2003FA0000691Spar · crackedCRACK UNDER PLYWOOD PLATE, BOTH CRACKS FLOW THE GRAIN.SDR 2003FA0000616Circuit Breaker · defectiveCHANGED 2 CIRCUIT BREAKERS. PN 454707 HIGH VOLTAGE DROP AND WOULD NOT TRIP AT 200 PERCENT RATING. PN 454706 HIGH VOLTAGE DROP AND TERMINALS WERE HOT ENOUGH TO BLISTER A FINGER AFTER 5 MINUTES OF OPERATION.SDR 2003FA0000419Structure · crackedDURING INSPECTION THE UPPER HORITONTAL (Z) ON THE FIREWALL WAS FOUND CRACKED. THIS IS THE LATER REINFORCED VERSION REV. 4. THE CRACK WAS LOCATED FROM THE HOLE WHERE THE NOSE GEAR STRUT COMES THROUGH TO THE OUTSIDE FORWARD EDGE.THE PLASTIC STOP UNDER THE (Z) WASDR 2003FA0000420Structure · crackedDURING INSPECTION THE UPPER HORITONTAL (Z) ON THE FIREWALL WAS FOUND CRACKED. THIS IS THE LATER REINFORCED VERSION REV. 4. THE CRACK WAS LOCATED FROM THE HOLE WHERE THE NOSE GEAR STRUT COMES THROUGH TO THE OUTSIDE FORWARD EDGE.THE PLASTIC STOP UNDER THE (Z) WASDR 2003FA0000469Gear · wornTHE KEEPER FOR THE MAGNETO TIMING GEAR WAS FOUND LOOSE IN THE MAG CASE. THE KEEPER, TIMING GEAR KEY WAY AND SHAFT KEY WAY SLOT WERE ALL FOUND WORN. THIS WAS A 1961 ENGINE, WITH 1876 HOURS TT. NO RECORD OF MAG MAINTENANCE COULD BE LOCATED. KEY PN 10-907-88-SDR 2003FA0000385Exhaust Pipe · defectiveTHIS IS THE SECOND REPORT OF FINDING THE ABOVE COMPONENT DEFECTIVE. THEY ARE CRACKING BEHIND THE MUFFLER SHROUD AND CANNOT BE SEEN WITHOUT REMOVAL OF THE SHROUD. THIS ALLOWS EXHAUST GASES TO ENTER THE COCKPIT WHEN THE HEATER IS UTILIZED. THE CRACK LENGTH ISSDR 2003FA0000209Nut · failedON BOTH STABILATOR HNGE BOLTS THE NYLON LOCKNUTS BACKED OFF DUE TO THE NYLON PART OF THE NUT BECOMING DETACHED FROM THE NUT ITSELF. THIS HAPPENED IN APPROXIMATELY 100 HOURS TSNSDR 2003FA0000095Bracket · crackedDURING AN INSPECTION FOR AD (CRACKED NUT PLATES) THE BRACKET WHICH HOLDS THE NUT PLATES WAS FOUND CRACKED ON THE UPPER RIGHT HAND SIDE FROM THE CORNER RELIEF HOLE, INBOARD FOR APPROXIMATELY ONE INCH ALONG THE TOP BEND. THIS CRACK IS DIRECTLY ADJACENT TO AND JSDR LER2002F00000Bolt · failedIN CRUISE FLIGHT. 6 HOURS AFTER ENGINE START WHEN PILOT NOTICED SLIGHT ROUGHNESS FOLLOWED BY LOSS OF OIL PRESSURE. FOLLOWED IMMEDIATELY BY EXTREME VIBRATION, SMOKE AND OIL FROM ENGINE COMPARTMENT AND ENGINE STOPPAGE. PILOT COMPLETED A SUCCESSFUL EMERGENCY LSDR 2002FA0000866Bolt · damagedMLG ATTACH BOLTS WERE REMOVED FOR INSPECTION DUE TO AN INCIDENT THAT OCCURED ON 6/17/02 WITH A SAME MODEL AIRCRAFT. FOUND THE INBOARD GEAR ATTACH BOLTS FOR BOTH MAIN LANDING GEAR BENT IN THE SHANK AREA. ONE BOLT HAD ITS SHANK DISPLACED APPROX. .012 OF AN INCSDR 2002FA0000472Torque Tube · brokenPILOT LEFT RUDDER PEDAL TORQUE TUBE BROKE AT WELD FOR PEDAL ARM. RESULTING IN PILOT HAVING REDUCED OR NO LEFT RUDDER OR NOSE STEERING. POSSIBLY CAUSED BY A DEFECTIVE WELD.SDR 2003FA0000219Exhaust Pipe · crackedASSEMBLIES ARE CRACKING WITH LESS THAN 100 HOURS IN SERVICE SINCE NEW. THE CRACKS ARE UNDER THE CABIN HEAT SHROUD AND CAN NOT BE SEEN UNLESS THE SHROUD IS REMOVED. NUMEROUS CRACKS HAVE ALSO BEEN FOUND IN OTHER AREAS OF THESE ASSEMBLIES. IT IS SUGGESTED THATSDR 2002FA0000671Bracket · crackedWHILE INSPECTING THE NUTPLATES IAW AD, WE FOUND THAT THE FORWARD UPPER WELD JOINT HAD CRACKED ADJACENT TO THE NUTPLATES THEMSELVES. THIS AIRCRAFT IS OPERATED IN A TRAINING ENVIRONMENT AND IS SUBJECTED TO A LOT OF ABRUPT MANEUVERS INCLUDING SPINS. DUE TO THE SDR 2002FA0000668Bracket · crackedWHILE INSPECTING THE NUTPLATES IAW AD. WE FOUND THAT THE FORWARD UPPER WELD JOINT HAD CRACKED ADJACENT TO THE NUTPLATES THEMSELVES. THIS AIRCRAFT IS OPERATED IN A TRAINING ENVIRONMENT AND IS SUBJECTED TO A LOT OF ABRUPT MANEUVERS INCLUDING SPINS. DUE TO THESDR TVM2002F00000Spar · crackedWHILE COMPLYING WITH AD, A LONGITUDINAL CRACK IN THE RIGHT FORWARD WOODEN WING SPAR APPROXIMATELY 30 INCHES LONG.SDR 2002FA0000157Transformer · shortedTRANSFORMER SHORTED.SDR 2002FA0000052Float · failedON LANDING THE ENGINE QUIT. FUEL WAS OBSERVED LEAKING FROM THE AIRCRAFT. DURING DISASSEMBLY OF THE CARBURETOR IT WAS NOTED BOTH FLOATS WERE FILLED WITH FUEL CAUSING FUEL TO POUR THRU THE VENT. THE MANUFACTURE DATE OF THE FLOAT WAS 4/92.SDR 2001FA0000554Fuel Cap · improper part(2) PILOTS HAD FUEL STARVATION. BOTH PILOTS, ON LANDING, CHECK RIGHT WING TANKS AND HEARD HISSING SOUND. EXAMINED CAPS AND FOUND NOW VENT HOLES. BOTH CAPS SEEMED NEW AND MADE OF ALUMINUM. CHANGED CAPS TO VENTED STYLE, HAD NO FURTHER TROUBLE.SDR 2001FA0000599Spar · crackedREMOVED ELEVATOR TO REPAIR WORN OUTBOARD HINGE BUSHINGS, AFTER ELEVATOR WAS REMOVED FOUND THE ELEVATOR SPAR CRACKED UNDER THE OUTBOARD HINGE WHERE IT ATTACHES TO THE SPAR, REPLACED SPAR WITH NEW.SDR 2002FA0000255Fastener · missingNUMEROUS RIB NAILS MISSING OR BACKED OUT FARTHER THAN .1250 ON FORWARD AND AFT WING SPARS, LEFT AND RIGHT WINGS. INSPECTED SPARS AND REPLACED SUCH NAILS.SDR 2002FA0000239Spar · crackedDURING ANNUAL INSPECTION, WING SPAR INSPECTION IAW AD., FOUND LONGITUDINAL CRACKS IN THE AREA OF WING STRUT ATTACH POINTS. RIGHT FORWARD SPAR LONGITUDINAL CRACK OBSERVED FROM MISSING CENTER RIB NAIL, INBOARD FROM THE STRUT ATTACH DOUBLER APPROXIMATELY 2 INCH SDR 2001FA0000041Sump · failedINDUCTION TUBE ATTACHED TO OIL SUMP BECAME LOOSE CAUSING ROUGH RUNNING ENGINE. ENGINE OIL SUMP REPLACED TO CORRECT PROBLEM.SDR 2001FA0000586Mount · crackedPILOTS RIGHT HAND LOW RUDDER PEDAL ASSEMBLY MOUNT CRACKED AROUND WELD CAUSING ON GROUND LOSS OF DIRECTIONAL CONTROL AND MADE BRAKING DIFFICULT.SDR 2002FA0000253Spar · crackedWHILE COMPLYING WITH AD, A LONGITUDINAL CRACK IN THE RIGHT FOREWARD WOODEN WING SPAR APPROXIMATELY 30 INCHES LONG.SDR 20010419CW012Spar · crackedA LONGITUDINAL CRACK IN THE RIGHT FORWARD WOODEN WING SPAR, APPROXIMATELY 30 INCHES LONG.SDR 20010430CW001Control Cable · brokenDURING 100 HOUR INSPECTION, IT WAS DISCOVERED THAT THE LEFT AILERON CROSSOVER CABLE HAD A BROKEN STRAND AT A POINT 63.5 INCHES FROM THE TURNBUCKLE END. BROKEN STRAND WAS WHERE CABLE PARTED OVER A RUB BLOCK ATTACHED TO RIB AT WING STA. 56.875.SDR 20010301CW010Oil Filter · defectiveSEALANT USED IN MANUFACTURE OF FILTER TO SEAL THE INLET AND OUTLET TO THE FILTER APPEARS TO BE FLAKING OFF. PIECES ARE BEING FOUND INSIDE THE FILTER ON THE PLEATS AND ON THE OIL SUMP SUCTION SCREEN. THESE PIECES COULD GET INTO THE PRESSURE SYSTEM AND STARVE SDR 99ZZZX2030Carburetor · misoverhauledCARBURETOR LISTED IN NR 6 WAS REPAIRED AND TESTED. 23.1 HOURS AFTER INSTALLATION OF THIS CARBURETOR, ENGINE WOULD ONLY PRODUCE 2,000 RPM. TEAR DOWN OF CARBURETOR REVEALED NEEDLE VALVE AND SEAT WORN, FLOAT LEVEL SET TOO HIGH, AND A THUMB SIZED BALL OF LINE INSDR 98ZZZX2092Engine · failedTHIRTY MINUTES INTO LOCAL FLIGHT, ENGINE FAILED. PILOT MADE A FORCED LANDING IN A PLOWED FARM FIELD. NO VISIBLE DAMAGE INCURRED TO AIRPLANE. ON TEARDOWN, DEEP SCORING WAS FOUND IN THE OIL PUMP GEAR HOUSING. ALUMINUM AND PISTON RING PIECES WERE FOUND IN THESDR 98ZZZX766Crankshaft · crackedCRANKSHAFT WAS REMOVED FROM INVENTORY FOR PRECAUTIONARY MPI. RANK WAS PROCESSED BY AIR AGENCY AND WAS FOUND CRACKED AT THE JOURNAL RADII.SDR 98ZZZX769Crankshaft · crackedPART WAS REMOVED FROM INVENTORY FOR PRECAUTIONARY MPI. CRANKSHAFT WAS GROUND AND POLISHED BY AIR AGENCY AND WAS FOUND TO HAVE CRACKS IN THE JOURNAL AREAS.SDR 98ZZZX930Crankshaft · crackedCRANKSHAFT WAS REMOVED FROM INVENTORY FOR PRECAUTIONARY MPI. CRANKSHAFT WAS PROCESSED BY AIR AGENCY AND WAS FOUND CRACKED AT THE JOURNAL RADII.
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