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 = '210L' 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 = '210L' 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 96ZZZX4070Wheel · failedWHEEL ASSY BLEW APART ON TAXI, DISC SIDE OF WHEEL. SUSPECT CAUSE, THREADS WEAK ON 12-BOLT, 3-PIECE, MCCAULEY WHEEL ASSY. REPLACED WHEEL ASSY, 3-PIECE, WITH 2-PIECE CLEVELAND AFTER 2,500 HOURS TIS.SDR 96ZZZX3766Nozzle · threads strippedWHEN REMOVING FUEL INJECTOR NOZZLE FOR CLEANING AT FIRST 91-HOUR TSMOH, FACTORY REMANUFACTURE, NOZZLE CAME OUT OF CYLINDER HEAD WITH ALUMINUM, STRIPPED THREADS IN CLYINDER HEAD.SDR 96ZZZX3802Rectifier Assy · failedTHE PILOT EXPERIENCED AN ALTERNATOR FAILURE DURING AN IFR FLIGHT. A SUCCESSFUL EMERGENCY LANDING WAS MADE. AN INVESTIGATION AS TO WHY THE ALTERNATOR FAILED REVEALED THAT ONE NEGATIVE RECTIFIER GROUND STUD HAD FAILED AND THE OTHER GROUND STUD WAS LOOSE. THISSDR 96ZZZX4086Wheel · threads failedWHEEL ASSY BLEW APART ON LANDING, RT BRAKE DISC SIDE OF WHEEL. SUSPECT CAUSE, THREADS WEAK ON 12-BOLT, 3-PIECE MCCAULEY WHEEL ASSY. REPLACED WHEEL ASSY, 3-PIECE, WITH 2-PIECE, CLEVELAND.SDR 96ZZZX3378Fuel Cap · defectiveCOMPLIANCE WITH AD 94-12-08. AD NO LONGER APPLIES TO THIS AIRCRAFT.SDR AU960568Cable · frayed(AUS) RH AILERON/RUDDER INTERCONNECT CABLE FRAYED DUE TO CHAFING ON EACH END OF THE STEEL TUBE COVERING THE CABLESDR AU960534Microswitch · faulty(AUS) LANDING GEAR MICROSWITCH ACTUATING ARM BROKEN OFF - WARNING HORN FAILED TO OPERATE AND AIRCRAFT LANDED WITH GEAR RETRACTEDSDR AU960555Switch · faulty(AUS) LANDING GEAR MOTOR PRESSURE SWITCH WIRE BROKEN AT SOLDERED JOINT - FAILURE WAS COVERED BY HEAT SHRINK MAKING IT DIFFICULT TODETECTSDR EY2R9600529Retain Bearing · corrodedRETAIN BEARING FOUND CORRODED.SDR 96ZZZX2408Cylinder · crackedFIVE OF SIX CYLINDERS HAVE CRACKS IN ROCKER BOSS AREA UP TO THE ROCKER SHAFT RETAINING BOLTS. TWO OF THESE FIVE HAVE CRACKS ON INTAKE AND EXHAUST BOSSES. THIS ENGINE DOES NOT INCORPORATE LONG BOLTS AND SOLID SHAFTS.SDR AU960932Solenoid · faulty(AUS) LANDING GEAR CONTROL SOLENOID PNO 9881202-1 HAD INSULATION BREAKDOWN - LANDING GEAR FAILED TO EXTEND ELECTRICALLY - EXTENDED SAFELY WITH MECHANICAL HYDRAULIC HAND PUMPSDR AU960308Dowel · worn(AUS) WING TO FUSELAGE LOCATING DOWEL PINS WORN ALLOWING MOVEMENT AT ATTACHMENT POINTS - SUSPECT CAUSED BY USE OF ACF 50 MATERIAL WORKING BETWEEN MATING SURFACES AND CAUSING MOVEMENTSDR 96ZZZX2553Fuel Cap · water leakFUEL CAPS LEAKING WATER INTO FUEL TANKS WHEN EXPOSED TO INCLEMENT WEATHER. CORRECTED BY INSTALLING CESSNA T210L, (WW OVAL PLATES) FROM MONARCH AIR AND DEVELOPMENT, INC.SDR AU960314Switch · faulty(AUS) LH MAIN LANDING GEAR DOWNLOCK MICROSWITCH FAULTY - NLG MICROSWITCH SUSPECT FAULTYSDR AU960185Bracket · cracked(AUS) HORIZONTAL STABILISER REAR CENTRE SPAR REINFORCEMENT BRACKET CRACKED IN AREA OF LOWER LH FLANGE - INITIAL POINT OF CRACKAPPEARS TO BE AT THE BOLT HOLE WITH SECONDARY CRACKING IN BRACKETRADIUS - SUSPECT CAUSED BY PUSHING DOWN ON STABILISER DURING GROUND HSDR 96ZZZX765Fuel Flow Line · chafedAIRCRAFT EXPERIENCED ELECTRICAL FAILURE ON 1-26-96. MX FOUND FUEL FLOW LINE CHAFED THROUGH, SPRAYING A FUEL MIST ON CHAFED ELECTRICAL WIRES. ON 2-1-96, FLIGHT EXPRESS (FPIA) REPORTED THAT AN INSPECTION ON THE FUEL PRESSURE LINE TO THE FUEL FLOW INDICATOR BEHSDR 96ZZZX2927Fuel Flow Line · chafedON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMMER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS ON REMAINING FLEET OFSDR 96ZZZX2926Fuel Flow Line · chafedON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMMER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS ON REMAINING FLEET OFSDR 96ZZZX2925Fuel Flow Line · chafedON JANUARY 26, 1996, PILOT REPORTED ELECTRICAL FAILURE GLOW BEHIND INSTRUMENT PANEL. MAINTENANCE FOUND TRANSPONDER DIMMER WIRE SHORTED AGAINST PRESSURE LINE. REPLACED FUEL PRESSURE LINE WITH STRATOFLEX III HOSE AND FITTING. INSPECTIONS ON REMAINING FLEET OFSDR AU960018Bulkhead · cracked(AUS) FUSELAGE REAR BULKHEAD CRACKED IN AREA OF RH HORIZONTAL STABILISER FORWARD ATTACHMENT FITTINGSDR EY2R9600282Blade · corrodedBLADE SN K95331YS IS CORRODEDSDR EY2R9600281Blade · corrodedBLADE SN K94806YS IS CORRODEDSDR EY2R9600280Blade · corrodedBLADE SN K95680YS IS CORRODEDSDR EY2R9600278Cylinder · corrodedPROP ASSY CYLINDER IS CORRODEDSDR EY2R9600277Nut · corrodedPROP ASSY NUT PN C4902 IS CORRODEDSDR EY2R9600276Retain Bearing · corrodedPROP ASSY RETAINING BEARING IS CORRODEDSDR 96ZZZX1543Adapter · oil leakUPON INSPECTION OF OIL FILTER ADAPTER IAW CESSNA SEB 93-1-R1, FOUND FILTER ADAPTER THREADS HAD PIECES MISSING. INSPECTION WAS PROMPTED BY LOOSE RETAINING NUT AND OIL LEAK. THREADS ON THE ENGINE WERE INTACT. REPLACED FILTER ASSY WITH NEW CESSNA ASSY.SDR 96ZZZX1121Collar · looseDURING ANNUAL INSPECTION, FOUND LOWER COLLAR ON NLG LOOSE. DISASSEMBLED STRUT AND INSPECTED PARTS. REASSEMBLED STRUT AND RE-SHIMMED COLLAR. FUNCTIONAL CHECK OK.SDR 96ZZZX1120Support · looseDURING ANNUAL INSPECTION, FOUND MAIN GEAR DOWNLOCK SUPPORT ASSEMBLY LOOSE AND ALLOWING SHIM TO MIGRATE. ALL 4 BOLTS WHICH SECURE SUPPORT WERE LOOSE. MM CALLS FOR THESE BOLTS TO BE LOCTITED AND SECURED WITH A SHAKEPROOF WASHER. ASSUMING THAT VIBRATION OVER TSDR 95ZZZX5995Blade Pin · brokenDISASSEMBLED PROPELLER, FOUND ONE BLADE PIN BROKEN. BROKEN PIN WAS FOUND TO HAVE BEEN GROUND SHORT ON STONE AND NOT MACHINED AS SB NR 99 SECTION C STATES. REMAINING TWO BLADE PINS WERE FOUND OVERTORQUED BY AT LEAST 5 POUNDS PER MANUAL 720415.SDR 95ZZZX5650Trim Tab · corrodedELEVATOR TRIM TAB CORRODED AT PUSH/PULL ROD ATTACHMENT. SAME CONDITION AS MENTIONED ON AC 43-16, ALERT NR 200, PAGE 6.SDR 95ZZZX2889Cylinder · crackedENGINE OPERATION BECAME ROUGH IN-FLIGHT. AIRCRAFT WAS LANDED TO INVESTIGATE THE PROBLEM. FOUND CYLINDER NR 4 HAD CRACKED AND THE HEAD HAD SEPARATED.SDR 95ZZZX1701Link Assy · bentTOP SCISSOR LINK FOUND BOWED DOWNWARD. SUSPECT CAUSE AS REPEATED NOSE STRUT EXTENSIONS EXERTING PULL-DOWN PRESSURE ON UPPER LINK, WHICH HAS A STOP BLOCK PN 1243038-1, ATTACHED TO IT, PREVENTING OVER EXTENSION.SDR 95ZZZX1700Link Assy · crackedTOP SCISSOR LINK FOUND CRACKED ON BOTTOM SIDE. SUSPECT REPEATED NOSE STRUT EXTENSIONS EXERTING PULL-DOWN PRESSURE ON UPPER LINK, WHICH INCORPORATES A STOP BLOCK, PREVENTING OVER EXTENSION.
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