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 = 'K35' 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 = 'K35' 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 2014FA0000642Adapter · damagedTHE OIL FILTER ADAPTER HAD SEPARATED, PULLED OUT OF OIL PUMP HOUSING, DUE TO THE FAILURE/SHEARING OF THE ATTACHMENT THREADS. THIS FAILURE ALLOWED ALL ENGINE OIL TO BE PUMPED OVERBOARD AND CAUSING AN OFF AIRPORT LANDING. THIS PART IS THE SUBJECT OF AD 96-12-2SDR 2014FA0000660Piston · destroyedSEVERE ENGINE DAMAGE FOUND DURING SCHEDULED 50 HR INSPECTION: DURING OIL AND FILTER CHANGE, CHIPS AND LARGE METAL PIECES WERE FOUND IN THE OIL, OIL SCREEN, OIL FILTER AND OIL SUMP. AFTER REMOVAL OF THE OIL SUMP IT TURNED OUT THAT THE PISTON SKIRT OF PISTON SDR 2014FA0000513Landing Gear · failedON DOWNWIND, GEAR HORN SOUNDED AND OBSERVED NO GREEN GEAR INDICATION, CYCLED GEAR, NO HELP. PERFORMED MANUAL GEAR EXTENSION PROCEDURES, NO HELP. FELT A BINDING OR PREMATURE STOP WHILE CRANKING DOWN GEAR FOR MANUAL EXTENSION. GEAR HORN AND UNSAFE INDICATION SDR 2014FA0000543Drag Brace · shearedGEAR WARNING LIGHT AND HORN, CYCLED GEAR, NO HELP, PERFORMED MANUAL EXTENSION AND LANDED. ON LANDING THE ACFT SETTLED ON THE GEAR DOORS AND GROUND TO A HALT ON CENTER LINE. FOUND NOSE GEAR DRAG BRACE/RETRACT TRIANGLE ASSEMBLY BROKEN AT WELD. IPC SHOWS PN 95SDR W59R2012043031326Hub · crackedPROPELLER SUBMITTED FOR OIL LEAK. DURING REPAIR, THE HUB WAS MAGNETIC PARTICLE INSPECTED IAW AD 62-17-01. HUB WAS FOUND CRACKED IN THE WELD AREA, WHICH IS THE SUBJECT OF AN AD.SDR 2011FA0000325Drive Shaft · shearedPUMP DRIVE SHAFT SHEARED RENDERING PUMP INOPERATIVE. THIS IS A SINGLE DRIVE, DUAL VACUUM PUMP. BOTH PUMPS INOPERATIVE.SDR 2007FA0000483Unknown · unknownLOST ELECTRICAL POWER.SDR 2005FA0000710Brace · corrodedCORROSION PITS APPROXIMATELY 30 TO 50 PERCENT OF WALL THICKNESS. THIS PART ONLY 10 PERCENT OF WALL THICKNESS ALLOWED BY MFG. THIS PART IS MAGNESIUM. THE PIRTING IS UNDER THE FEL 35, ABOVE THE LOWER BUSHING, THE FELT IS SATURATED WITH MOISTURE AND GREASE WHISDR 20000619SH026Roll Pin · missingFUEL STARVATION, OFF AIRPORT LANDING. PILOT REPORTED THAT WHEN HE SWITCHED TANKS HE DID NOT FEEL POSITIVE DETENT. APPROX 12 MINUTES LATER, ENGINE QUIT. AGAIN ATTEMPTED TO SWITCH TANKS AND SELECTOR HANDLE CAME DETACHED FROM SELECTOR VALVE SHAFT. EMERG LANDISDR 99ZZZX1018Bracket · misinstalledALTERNATOR LOWER ATTACH BOLT PULLED FROM BRACKET CAUSING LOSS OF BELT TENSION AND SUBSEQUENT BATTERY DRAIN AND INTERRUPTION OF RADIO CONTACT. BOLT HAD ONLY ENGAGED TWO OR THREE THREADS IN MOUNTING BRACKET BECAUSE OF TOO MANY WASHERS UNDER BOLT HEAD. WITHOUSDR 99ZZZX1070Breaker Assy · defectiveDURING PERFORMANCE OF 100-HOUR INSPECTION, LT POSITION MAGNETO, BENDIX (TCM) PN 10-79020-10, RE-MANUFACTURED BY AIRBORNE ELECTROSYSTEMS, INC., AND INSTALLED AT ENGINE OVERHAUL BY CRS 764-88 IN MARCH 1984. TT 1,228.8 BREAKER ASSY PN ES10-357174 CHANGED WHEN SUSDR 98ZZZX3030Control Cable · frayedALL AILERON CABLES (4 EACH) WERE FOUND WORN AND FRAYED AT THE FAIRLEADS AT THE OUTBOARD END OF THE MAIN WHEEL WELLS. RECOMMEND AD NOTE REQUIRING CABLE REPLACEMENT AT REGULAR INTERVALS POSSIBLY 4,000 HOURS OR 20 YEARS WHICHEVER COMES FIRST.SDR 98ZZZX3029Control Cable · frayedALL AILERON CABLES (4 EACH) WERE FOUND WORN AND FRAYED AT THE FAIRLEADS AT THE OUTBOARD END OF THE MAIN WHEEL WELLS. RECOMMEND AD NOTE REQUIRING CABLE REPLACEMENT AT REGULAR INTERVALS POSSIBLY 4,000 HOURS OR 20 YEARS WHICHEVER COMES FIRST.SDR 97ZZZX3899Pushrod · corrodedWHILE C/W AD 97-06-11, LEFT PUSH ROD WAS FOUND FULL OF WATER. UPON PAINT REMOVAL IN PREPARATION FOR DYE/PEN INSPECTION, AN APPROXIMATE .25 INCH HOLE WAS FOUND CORRODED THROUGH THE WALL THICKNESS AT THE LOWER FORWARD END OF THE ROD. THIS AREA WAS NOT VISIBLE SDR 97ZZZX2627Brace · corrodedABOVE THE LOWER BEARING IN THIS CASTING, THERE IS CORROSION ALL THE WAY THROUGH THE NOSE WHEEL BRACE ASSY. THE CORROSION IS ON THE INSIDE AND HARD TO SEE WITHOUT DISASSEMBLING. TOTAL TIME ON THIS AIRCRAFT IS 3,315 HRS.SDR 97ZZZX2020Cam Assy · rivet failedDURING ACCOMPLISHING SB MSB645, NR 639, AND AD 96-12-07, FOUND MAG SNAP RING CAM ASSY HAD RIVET FAILURE.SDR 96ZZZX5803Tube · brokenDISASSEMBLING ENG FOR OVERHAUL FOUND THE OIL SUCTION TUBE WAS BROKEN IN 2 PLACES. TUBE WAS BROKE OFF FROM SCREEN AND ONE OF THE ATTACHING ANGLES WAS BROKEN BY BOLT HOLE. TT ENG 4306.44. SMOH 1448.84.SDR 96ZZZX5006Rheostat · overheatedALL FOUR LIGHTING DIMMER RHEOSTAT/TRANSISTOR ASSEMBLIES WERE SUBJECTED TO EXCESSIVE HEAT DURING NORMAL OPERATION. THERE WAS NOT A SHORTED WIRE CONDITION CAUSING THIS HEAT. THE POTTING COMPOUND FORMING THE UNIT MELTED (DRIPPING DOWN ONTO THE FLOOR) EVENTUALLY
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