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 = 'J3C65' 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 = 'J3C65' 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 2026FA0000052Spark Plug · crackedLEVELED AT 4000FT, ENGINE POWER WAS REDUCED TO 80% WITH FUEL CONSUMPTION LEANED TO 17GAL/HR. AFTER BEING SET IN THIS CRUISE PROFILE FOR APPROXIMATELY 2 MINUTES, THE ENGINE BEGAN TO RUN ROUGH. THE PILOT THEN RICHENED THE MIXTURE WHICH DID NOT FIX THE ISSUE, HE SDR YV3R2021042700451Warning System · defectiveCUSTOMER REPORTED WARNING UNIT - LOW RPM P/N: A569-9 WAS FAULTY, HORN SOUNDS INTERMITTENTLY @ 102%.SDR 2020FA0000403Tab · brokenRUDDER CABLE ATTACHMENT TAB BROKE OFF DURING LANDING ROLLOUT LEFT REAR RUDDER TAB.SDR 2015FA0000359Housing · crackedDUE TO A "STUCK" EXHAUST VALVE IN 1 CYLINDER, THE ROCKER ARM BROKE, AND THE PUSHROD ASSOCIATED WITH THAT ROCKER ARM DAMAGED AND CRACKED THE FLANGE-PUSHROD HOUSING. THE CRACKED FLANGE-PUSHROD HOUSING CREATED AN OIL LEAK. THE "STUCK" EXHAUST VALVE WAS CAUSED BSDR BPGR20140313001Strut · failedACFT WAS FLOWN FOR 45 HRS ON SNOW SKIES BEFORE THE RT SHOCK STRUT BROKE AT LOW SPEED TAXI. THE RT LONG SHOCK STRUT BROKE HALF WAY DOWN THE TUBE WITH NO SIGNS OF PREVIOUS CRACKING. BRAKE OCCURRED DURING COMPRESSION OF THE SHOCK STRUT DUE TO HIGH SIDE LOADS FRSDR 2013FA0000382Bracket · crackedTHE AILERON HINGE REINFORCING BRACKET FOUND SEVERELY CORRODED AND CRACKED.SDR CA130831001Hinge Bracket · corroded(CAN) ON ACCOMPLISHING ANNUAL INSPECTION, FOUND DIS-COLOURED SPOT ON BOTTOM OF HINGE BRACKET PIVOT. ON APPLYING "MAULE TESTER" FOR STRENGTH TEST. TUBE COLLAPSED. INSPECTION FOUND THE SUPPORT TUBE WAS NOT DRILLED FOR DRAINAGE. THE NEW REPLACEMENT BRACKET WASSDR 2012FA0000110Axle · corrodedDURING CLEANING IN PREPARATION FOR RECOVERING OF THE RT LANDING GEAR IT WAS NOTED THAT WOOD PLUG, PN 30941, WAS MISSING. SEVERE CORROSION WAS NOTICED INSIDE LOWER RADIUS OF THE AXLE TUBE. ESTIMATE THE LOWER PORTION OF TUBE WAS CORRODED MORE THEN 50 PERCENT OSDR FPI2012F00001Cylinder · crackedDURING A 100 HR INSPECTION COMPRESSION TEST FOUND NR 1 CYLINDER CRACKED FROM BEHIND FIRST FIN TO SPARK PLUG HOLE (UPPER) ABOVE EXHAUST PORT. REPLACED WITH NEW CYLINDER ASSY.SDR CA110803009Oil System · leaking(CAN) DURING CRUISE, THE PILOT NOTICED THE LOW OIL PRESSURE WARNING LIGHT AND SAW PRESSURE WAS FLUCTUATING. WHEN THE PRESSURE FLUCTUATED DOWN TO 10 PSI THE ENGINE WAS SHUTDOWN. AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. INITIAL REPORTS OBSERVED LARGE QUANTISDR 2010FA0000481Spar · corrodedSEVERE CORROSION ON SPAR BETWEEN HINGES AND SPAR. AIRCRAFT WAS NOT HANGARED. WATER SEEPAGE BETWEEN STEEL HINGE BRACKET AND ALUMINUM SPAR DEVELOPED TO CAUSE CORROSION TO BLISTER AROUND RIVETS FASTENING HINGE TO SPAR. THIS CONDITION WAS FOUND DURING THE FABRIC RSDR 2010FA0000087Spar · corrodedSEVERE CORROSION ON LT AND RT AILERON MAIN SPARS BETWEEN SPAR AND BRACKETS. SPAR BULGES AROUND RIVETS ATTACHING THE BRACKETS TO THE SPAR. THIS CONDITION WAS FOUND WHEN INSPECTING AILERONS PRIOR TO RECOVERING. SUSPECT THEY MAY HAVE BEEN ON SEA PLANE OPERATED ONSDR 2008FA0000702Torque Link · crackedCRACK FOUND DURING 100 HR INSPECTION. LAST INSPECTION FOR AD 72-08-06. DONE AT 5214.07 HR, PRESENT TIME 5440.53 (225.76 HR). SUGGEST PART BE LIFE LIMITED. THIS IS 2ND SET CRACK. THIS FLEET WITH OVER 5000 HR. TIME IN SERVICE. (K)SDR 2008FA0000908Connecting Rod · failedNR 1 CONNECTING ROD FAILED IN FLT, OFF-AIRPORT LANDING AND SUBSTANTIAL DAMAGE. CONNECTING ROD FAILED SLIGHTLY ABOVE CRANKSHAFT; ROD CAP STILL BOLTED & SAFETIED TO DAMAGED & SEPARATED LOWER PORTION OF CONNECTING ROD. DAMAGE TO CRANKCASE, CRANKSHAFT, & ADDITISDR 2007FA0000168Spar · crackedDURING REMOVAL OF LT WING FOR INSTALLATION OF WING FUEL TANK, A QUESTIONABLE PREVIOUS REPAIR WAS FOUND AT THE FRONT WOOD SPAR ROOT. FURTHER INVESTIGATION FOUND LONGNATUDINAL CRACKS OF THE LT AND RT, FOR AND AFT WOOD WING SPARS. THESE CRACKS WERE VISIBLE WITHSDR 2004FA0000275Brake Assy · brokenAFTER DISASSEMBLY OF THE RT WHEEL AND BRAKE COMPONENTS FOR INSPECTION, ONE OF SIX BRAKE BLOCK (NR B27-59-D) WAS FOUND TO BE BROKEN, AND ONE OF SIX SPRING RETAINERS (NR R21-35) WAS FOUND TO BE BROKEN, AND LOOSE. THIS CLIP (RETAINER) MAY HAVE JAMMED UNDER A BRASDR 2002FA0001265Shutoff Valve · failedDURING AN INVESTIGATION OF AN AIRCRAFT INCIDENT IN WHICH THE AIRCRAFT CRASHED INTO A POND DUE TO FUEL STARVATION. IT WAS DETERMINED THAT AN ALTERATION TO FUEL SHUT OFF VALVE HAD BEEN PERFORMED AND WAS NOT APPROVED. AN EXTENSION TO THE VALVE WAS INSTALLED ANDSDR CA001229006Contactor · failed(CAN) SOLDER CONNECTIONS ON SPRING STEEL BATTERY TERMINAL BREAK OFF.IT IS NOT POSSIBLE TO GET A GOOD SOLDER JOINT, TRYING TO SOLDER TO STEEL. CONTACTED MANUFACTURER WHO HAS NO ANSWER EXCEPT TO RETURN TO FACTORY.SDR 20000714SH021Plug · looseFOLLOWING MAJOR OVERHAUL, ALUM PARTICLES WERE FOUND IN THE OIL SCREEN AT 30, 55, AND 75 HOURS. CYLINDERS WERE REMOVED AND THE PISTON PIN PLUGS WERE FOUND WORN ON THE SHANK IN THE FORM OF A TAPER. THE PINS AND PLUGS WERE NEW AND CAME FROM A SET. THE OVERHAULSDR 98ZZZX4254Lift Strut · corrodedTHIS WAS THE FRONT WING LIFT STRUT. WHILE C/W AD 98-10-06 IAW SB 528D, SKETCH 'A', CORROSION WAS FOUND AT 5 INCH-7 INCH, AND 10 INCH-12 INCH FROM THE END OF THE STRUT. AT 12 INCHES, THIS IS 1 INCH OUTSIDE THE INSPECTION AREA PER SKETCH 'A'. THE STRUT WAS RESDR 99ZZZX1055Fittings · crackedDURING A ROUTINE INSPECTION, FOUND CRACK ON THE BASE OF THE MOUNTING LUG ON THE AFT RT WING STRUT/GEAR ATTACH FITTING, PN 20401-01. AFTER PEELING OFF THE REMAINING DOPE FINISH ON THE FITTING, DISCOVERED A SECOND CRACK. AT LT FITTING, PN 20401-00, AND AFTER SSDR 99ZZZX1054Fittings · crackedDURING A ROUTINE INSPECTION, FOUND CRACK ON THE BASE OF THE MOUNTING LUG ON THE AFT RT WING STRUT/GEAR ATTACH FITTING, PN 20401-01. AFTER PEELING OFF THE REMAINING DOPE FINISH ON THE FITTING, DISCOVERED A SECOND CRACK. AT LT FITTING, PN 20401-00, AND AFTER SSDR 98ZZZX3423Gear · wornGEAR TEETH WORN IN MAGNETO.SDR CA980504018Turnbuckle · cracked(CAN) ONE INCH CRACK IN TURNBUCKLE BARREL STARTING FROM LT THREAD END. REPLACED.SDR 98ZZZX2050Battery · failedBATTERY WAS BOOST CHARGED EVERY FLIGHT AND/OR 90 DAYS WHEN IN STORAGE. BATTERY WAS USED FOR NAV LIGHTS AND HOUR METER ONLY (NO STARTER OR GENERATOR ON AIRCRAFT). BATTERY WAS REMOVED FROM AIRCRAFT AND CHARGED AT HOME WITH CONSTANT VOLTAGE CHARGER.SDR 97ZZZX3937Propeller · departedTHIRTY MINUTES AFTER TAKEOFF, PILOT REPORTS VIBRATION AND THEN PROPELLER SEPARATED FROM ENGINE. PILOT SAYS NOT SURE IF BIRD STRIKE OR PART FAILURE. AIRCRAFT LANDED WITHOUT INJURY TO PILOT OR FURTHER DAMAGE TO AIRCRAFT.SDR 97ZZZX3689Exhaust Stack · crackedEXHAUST STACK CRACKED AT NR 1 CYLINDER. CRACK WELDED WITH STAINLESS STEEL.SDR 97ZZZX3483Muffler · crackedINSPECTION FOUND MUFFLER CRACKED. WELDED WITH STAINLESS STEEL.SDR 96ZZZX177Coil · crackedWHILE DETERMINING C/W TELEDYNE AD 94-01-03R2, FOUND RIGHT MAGNETO TO HAVE AN UNAIRWORTHY COIL. UPON REMOVAL, COIL WAS FOUND CRACKED IN TWO PLACES ORIGINATING FROM THE CORE ON THE GROUND LEAD END. LOG ENTRY OF 2-20-88 INDICATES THIS MAGNETO COIL WAS CHANGED TSDR 96ZZZX172Cable Assy · wrong lengthWITH RUDDER PEDAL IN NEUTRAL POSITION, RUDDER WAS AT ALMOST FULL LEFT DEFLECTION. UPON INVESTIGATION, FOUND THAT RUDDER CABLES HAD BEEN REPLACED AND WERE OF DIFFERENT LENGTHS. SUBMITTER STATED FAILURE TO FOLLOW AIRWORTHY PRACTICES WAS THE OBVIOUS CAUSE. REPSDR 95ZZZX505Engine · malfunctionedENGINE POWER FAILURE DURING TAKEOFF. MAINTENANCE INVESTIGATION AND POST-ENGINE RUN WAS CONDUCTED. ENGINE RAN SATISFACTORY. MAINTENANCE ADVISED, SUSPECT FUEL STARVATION DUE TO FREEZING OF WATER CONTAMINATION IN LOW SECTION OF FUEL LINE.
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