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 = '182T' 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 = '182T' 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 2017FA0000028Pushrod · unserviceablePUSHRODS INSPECTED PER SA-167A AND FOUND THAT ALL PUSHROD ENDS EXCEED THE LIMITATIONS OF THE SA AND ARE ORDERED AOG TO REPLACE ALL PUSHRODS AND ROCKER ARMS.SDR 2016FA0000672Pushrod · scored7 PUSHRODS AND 7 ROCKERS REQUIRE REPLACEMENT DUE TO INSPECTION CRITERIA FROM SA-167A. SCORING IS BEYOND LIMITS.SDR 2016FA0000634Pushrod · scoredNR 3 CYLINDER PUSHRODS AND ROCKER REPLACED DUE TO INSPECTION IAW SA-167A. THERE WAS ALSO REPORTED STUCK VALVES AT THE NR 3 AND 6 EXHAUST VALVE ASSEMBLY.SDR 2016FA0000630Pushrod · scoredTWO PUSHRODS AND ROCKER MATES SCORED, REPLACING PARTS IAW SA-167A.SDR 2016FA0000629Pushrod · scoredTWO PUSHRODS AND MATING ROCKER ARMS HAVE SCORING THAT IS BEYOND THE LIMITS OF THE IAW SA-167A. PARTS REPLACED IN ACCORDANCE WITH SA.SDR 2016FA0000604Pushrod · scoredNR 2 INTAKE AND NR 3 EXHAUST PUSHRODS HAVE SEVER SCORING ON THE ROCKER ARM END. REPLACING IN ACCORDANCE WITH SA-167A.SDR 2016FA0000603Pushrod · scoredALL PUSHRODS AND ROCKER ARMS REQUIRE REPLACEMENT DUE TO INSPECTION IAW SA-167A.SDR 2016FA0000593Pushrod · scoredPUSHROD SCORING ON THE ROCKER END SIDE WITH THE ROCKER SHOWING SIGNS OF SCORING AS WELL, REPLACED IAW SA-167A.SDR 2016FA0000578Pushrod · scoredPUSHRODS SHOW SIGNS OF SCORING AFTER OVERHAUL ON MULTIPLE ROCKER AND PUSHROD MATING SURFACES. THIS INSTANCE THE ENGINE HAS 25 HOURS TSO WITH NEW PUSHRODS AND ROCKERS, AFTER INSPECTING ONE CYLINDER AND EVIDENCES SHOWS SCORING, WE REQUESTED MAINTENANCE PERFORM SDR 2016FA0000574Hose · damagedPILOT REPORTED FUEL ODOR IN CABIN. FOUND SEVERAL FUEL HOSES CRACKED AND SPLIT IN THE WING ROOT.SDR 2016FA0000455Flap Track · brokenRIGHT FLAP OUTBOARD FLAP TRACK ASSEMBLY BROKEN. FLAPS WERE MOVED FROM 20 DEGREES TO FULL EXTENSION. MOMENTS UPON REACHING AND STOPPING AT FULL EXTENSION, A LOUD "BANG" WAS HEARD (APPROX 200FT AGL). PILOT LOOKED RIGHT AND SAW BROKEN PART PROTRUDING FROM WING. ASDR 2016FA0000148Valve · stuckOWNER REPORTED LOSS OF POWER, EXTREMELY ROUGH RUNNING ENGINE, UNABLE TO MAINTAIN ALTITUDE, FORCED LANDING. ENGINE INSPECTION FOUND NR 4 CYLINDER EXHAUST VALVE STUCK OPEN, BENT PUSH-ROD AND ROD HOUSING. BORESCOPE INSPECTION OF THE CAMSHAFT LOBE, LIFTER FACE, RSDR 2015FA0000503Alternator · failedALTERNATOR FAILED TO CHARGE DURING CROSS COUNTRY FLIGHT. INSPECTION SHOWS SEPARATION OF ALTERNATOR CASE HALVES. CASE HALF THROUGH BOLTS HELD COMPONENT INTACT BUT RESULTED IN LOSE OR SLOPPY TOLERANCE ON DRIVE SHAFT MAIN BEARING AND FAILURE TO PRODUCE CURRENT.SDR CA151013009Magneto · out of adjust(CAN) MAGNETO TIMING DRIFTED 7 DEGREES WITH ONLY 55 HRS SINCE 500HR INSPECTION.SDR CA151013008Magneto · out of adjust(CAN) MAGNETO TIMING DRIFTED 5 DEGREES WITH ONLY 55 HOURS SINCE 500HR INSPECTION.SDR 2015FA0000206Cylinder · crackedUPON REMOVAL OF ROCKER COVER FOR GASKET REPLACEMENT, THE OTBD ROCKER SHAFT ON THE EXHAUST WAS FOUND TO BE CRACKED. ON REMOVAL OF THE ROCKER SHAFT, THE BOSS CAME COMPLETELY OFF. THIS CYLINDER HAS NEVER HAD ANY WORK DONE TO IT AND MUST HAVE LEFT THE FACTORY CRSDR NJ5R2015FA0000198Baffle · warpedFORWARD MUFFLER BAFFLE ON MUFFLER SYSTEM IS WARPED AND DISTORTED AFTER 199 HRS IN SERVICE. BAFFLE MATERIAL IS TOO THIN FOR APPLICATION.SDR CA141223006Ignition Switch · broken(CAN) IGNITION SWITCH COULD BE ROTATED COUNTER CLOCKWISE PAST THE "OFF" POSITION AND ENGAGE THE STARTER.SDR KC2R2014110300049Impulse Coupling · crackedDURING INSPECTION OF IMPULSE COUPLINGS AT "500 HR INSPECTION" , IT WAS DISCOVERED THAT BOTH IMPULSE FLYWEIGHT BASE PLATES SHOWED CRACKS NEAT FLYWEIGHT AXLES. CRACKS WERE DISCOVERED USING MAGNETIC PARTICLE NDT METHOD. BOTH IMPULSE COUPLINGS REPLACED WITH NEW.SDR KC2R1029201449484Impulse Coupling · crackedDURING A ROUTINE 500 HR INSPECTION OF THE MAGNETOS, FOUND BOTH IMPULSE COUPLINGS CRACKED AT HUB PLATE, NEAR FULL ADVANCE STOP NOTCH.SDR YN8R201410170001Bracket · out of positionDURING INSPECTION, FOUND FLAP FOLLOW UP CABLE, SAWING INTO IT'S HOUSING AT THE UPPER ATTACHMENT BRACKET, THAT IS RIVETED IN PLACE ON THE RT UPPER AFT FACE OF THE REAR DOOR POST BULKHEAD ASSY . THE POSITIONING OF THE BRACKET RESULTS IN THE CABLE BEING MISALIGSDR JRUR2014FA0000510Points · looseOWNER REPORTED HAVING TROUBLE WITH STARTING THE ACFT ENGINE WHILE IT WAS HOT. ACFT WAS JUST RETURNING FROM SERVICE AND WAS DUE A PHASE 1 INSPECTION. REMOVED BOTH THE LT AND RT MAGNETOS TO CHECK THE PRIMARY POINTS FOR DRIFTING. INSPECTION OF THE LT MAGNETOSDR CA140714017Doubler · failed(CAN) RIGHT MAIN LANDING GEAR WHEEL FAIRING OUTBOARD DOUBLER FAILED AT THE ATTACH BOLT HOLE. THIS ALLOWED THE FAIRING TO CONTACT THE TIRE WHICH ON LANDING CAUSED THE FAIRING TO BE DRAWN UP UNDER THE TIRE AND DESTROYED.SDR 2014FA0000417Setscrew · leakingINSTALLED O/H FUEL SERVO AND RAN IT TO SET THE IDLE MIXTURE SETTING. ACFT SAT OVER THE WEEKEND AND WENT TO COWL THE ENGINE AND NOTICED A SET SCREW AT THE FRONT OF THE SERVO WAS LEAKING FUEL. SCREW IS NOT USED TO ADJUST IDLE MIXTURE AND WAS LOCK WIRED AT THE OSDR 2014FA0000405Servo · failedENGINE HAS BEEN RUNNING ROUGH AND VERY RICH AT IDLE. IDLE MIXTURE WAS ADJUSTED DUE TO A RISE OF OVER 100 RPM WHEN CHECKING. ACFT FLEW FOR A FEW MORE HOURS, BUT MIXTURE WAS RICH AGAIN. ALSO WHEN ACFT WAS PARKED OVERNIGHT, FUEL STAIN WAS ON THE GROUND UNDERNEATSDR 2014FA0000396Snap Ring · corrodedPROPELLER WAS OVERHAULED 5 MONTHS, 96 HOURS AGO, AND IS IN FOR INSPECTION. SNAP RING AROUND BASE OF A BLADE AND THE GROOVE IN THE BLADE HAS CORROSION. PROPELLER WAS REMOVED AND BEING SENT BACK FOR REPAIR. NO CORROSION PREVENTATIVE WAS OBSERVED ON THE SNAP SDR 2013FA0000722Guide · out of toleranceDURING THE PERFORMANCE OF SB 388C, THE EXHAUST VALVE GUIDE CLEARANCE ON NR 4 CYLINDER WAS FOUND TO BE .030". THIS IS THE MAXIMUM CLEARANCE ALLOWED.SDR 2013FA0000716Seat Belt · misinstalledDURING ANNUAL INSPECTION, FOUND PILOT SEAT BELT INFLATABLE RESTRAINT SYSTEM INSTALLED UPSIDE DOWN WITH THE NATURAL LAY OF THE BELT WOULD CAUSE THE DEPLOYMENT OF THE AIRBAG TO BE DIRECTED INTO THE PILOTS BODY.SDR CA131129002Adapter · clogged(CAN) RESTRICTOR ORIFICE IN MANIFOLD PRESSURE INDICATOR LINE ADAPTOR AT CYLINDER NR 3 FOUND PLUGGED. ORIFICE CLEANED.SDR 2013FA0000693Pump · leakingUPON FIRST START SINCE ENGINE OVERHAUL, FUEL BEGAN LEAKING FROM THE FUEL PUMP OVERBOARD DRAIN. FUEL PUMP WAS A NEW, PN AF-15473. REPLACED THAT FUEL PUMP WITH ANOTHER NEW FUEL PUMP, PN AF-15473. THIS SECOND NEW FUEL PUMP BEGAN LEAKING AFTER APPROXIMATELY 8 HSDR 2013FA0000570Guard · missingFACTORY ELECTRICAL WIRING ON PILOT SIDE PANEL, FWD OF INSTRUMENT PANEL, BETWEEN FUSELAGE STATIONS FS 0.00 AND FS 17.0. THE LT AILERON CABLE IS RUBBING AGAINST VERTICAL WIRE HARNESS. THE WIRE HARNESS IS TIED OFF ABOVE AND BELOW THE AILERON CABLE. THE GUARD SDR JRUR201308090012Exhaust Valve · out of toleranceDURING PERFORMANCE OF SB 388C, FOUND NR 4 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED .031". EXCEEDS MAXIMUM ALLOWABLE CLEARANCE OF .030". NR 4 CYLINDER WAS REPAIRED.SDR JRUR201303060011Exhaust Valve · out of toleranceWHILE PERFORMING SB 388C, NR 6 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE WAS FOUND TO BE .010". BELOW ACCEPTABLE MINIMUM TOLERANCE OF .015". HAD 201 HOURS TIS SINCE SB 388C HAD PREVIOUSLY BEEN PERFORMED. VALVE DRIVEN OUT TO REMOVE IT FOR REAMING OF THE GUISDR JRUR201303060010Exhaust Valve · out of toleranceNR 3 EXHAUST VALVE TO GUIDE CLEARANCE WAS FOUND TO BE .012". BELOW ACCEPTABLE MINIMUM TOLERANCE OF .015". 201 HOURS TIS SINCE SB 388C HAD PREVIOUSLY BEEN PERFORMED. VALVE CLEARANCE MEASUREMENT HAD BEEN .020". VALVE HAD TO BE DRIVEN OUT TO REMOVE IT FOR RESDR 2013FA0000071Engine · fodSHIPPING PLUG WAS REMOVED PRIOR TO INSTALLATION OF PROPELLER ON A ZERO TIME FACTORY REBUILT ENGINE. INSIDE OF THE CRANKSHAFT BORE, A SLIVER OF METAL WAS FOUND. ENGINE INSTALLATION WAS STOPPED. ENGINE MFG WAS CONTACTED FOR FURTHER EVALUATION AND RECOMMENDATISDR YN8R2012111501Line · leakingFUEL SYSTEM LEAKING AT FLARE ON LINE UNDER PILOT SEAT. LINE MFG WITH A SEAM IN THE TUBING. WHEN FLARED, THE SEAM CAN BE FELT WITH THUMBNAIL. EVIDENTLY CREATING LEAK PATH. B-NUT WAS TORQUED WHEN PROBLEM WAS FOUND. REPLACED LINE WITH NEW PART.SDR 2012FA0000609Tube · splitAIRCRAFT EXPERIENCED A FAILED LT MAIN TIRE INNER-TUBE ON TOUCHDOWN AND EXITED THE RUNWAY. ACFT STOPPED IN THE GRASS WITH NO DAMAGE TO AIRCRAFT. THIS WAS THE 15TH INNER TUBE FAILURE ON OUR FLEET OF AFT IN THE PAST 18 MONTHS. IN AUGUST 2012 1 OF OUR ACFT, EXPSDR JRUR201208140006Exhaust Valve · stuckDURING START, PILOT NOTICED THE ENGINE RAN VERY ROUGH. SHUTDOWN ENGINE AND RESTARTED IT. ENGINE RUNNING SMOOTHER, BUT A VIBRATION WAS NOTED. ENGINE SHUTDOWN AND MECHANIC INVESTIGATED. A COMPRESSION CHECK WAS TAKEN AND NR 3 CYLINDER COMPRESSION WAS 0/80 WITHSDR 2012FA0000450Magneto · out of toleranceMAGNETO FOUND TO BE OUT OF TIME AT RUN UP. MAGNETO WAS REPLACED.SDR 2012FA0000438Antenna · separatedHAD SEVERAL (FOUR PLUS) FAILURES OF THE WHIP ELT ANTENNA FOR THE ELT. THESE ANTENNA'S WERE INSTALLED BY STC, BY MANUFACTURER. ONE FAILURE SEPARATED AND BECAME LODGED BETWEEN THE LT HORIZONTAL STABILIZER AND ELEVATOR. NO CONTROL ISSUES WERE NOTED.SDR 2012FA0000449Magneto · failedMAGNETO COIL FAILED AND POINTS LOOSE.SDR JRUR201205160005Exhaust Valve · leakingENGINE MISSING & VIBRATION ON TAKEOFF. PILOT STATED THAT THE VIBRATION WAS SEVERE AND THOUGHT THE ENGINE WAS GOING TO QUIT. LANDED. ON INSPECTION, NR 4 CYLINDER COMPRESSION WAS MEASURED AT 78/80. PERFORMED SB 388C. VALVE TO GUIDE CLEARANCE WAS MEASURED AT .0SDR JRUR201205160004Exhaust Valve · stuckENGINE MISSING & VIBRATION ON TAKEOFF. PILOT STATED THAT THE VIBRATION WAS SEVERE AND THOUGHT THE ENGINE WAS GOING TO QUIT. PILOT MADE A 180 DEGREE TURN AND LANDED. UPON INSPECTION, THE NR 2 CYLINDER FAILED A COMPRESSION CHECK. COMPRESSION WAS MEASURED AT 5/SDR 2012FA0000216Bulkhead · crackedCRACKS FOUND IN FLANGE OF BOTH THE LT AND RT FUSELAGE BULKHEAD AT STATION 17. CRACKS RADIATING FROM THE UPPER BOLT HOLE WHERE THE FUELING STEP ATTACHES. BOLT HOLE IS TOO CLOSE TO BEND RADIUS OF BULKHEAD, CAUSING DISTRESS WHEN BOLT IS TIGHTENED.SDR 2012FA0000215Bulkhead · crackedCRACKS FOUND IN FLANGE OF BOTH THE LEFT AND RIGHT FUSELAGE BULKHEADS AT STATION 17. CRACKS RADIATING FROM UPPER BOLT HOLE WHERE FUELING STEP ATTACHES. BOLT HOLE IS TOO CLOSE TO BEND RADIUS OF BULKHEAD, CAUSING DISTRESS WHEN BOLT IS TIGHTENED. SECOND INSTANCSDR JRUR20120515003Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING RPM. AIRCRAFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON THE ENGINE AND FOUND THE NR 2 CYLINDER HAD AN ACSDR JRUR201205150002Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING RPM. ACFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON ENGINE AND FOUND NR 4 CYLINDER HAD AN ACCEPTABLE COSDR JRUR201205150001Exhaust Valve · leakingPROPELLER AND ENGINE PULSE CAVITATION IN FLIGHT. SIGNIFICANT OIL LEAK ON GROUND. HAD 19 INCHES MANIFOLD PRESSURE, 2100 RPM WHEN SLOWLY ADVANCING THE RPM. ACFT GROUNDED. MECHANIC PERFORMED A COMPRESSION CHECK ON ENGINE AND FOUND THE NR 6 CYLINDER HAD A COMPSDR CA120316006Bulkhead · dented(CAN) 3 DENTS, GOING FORWARD ON LOWER PORTION OF FS 209.0 BULKHEAD. ESTIMATED DENT DEPTH APPROXIMATE 0.185". APPEARS TO HAVE BEEN THIS WAY DURING MFG AS THERE ARE BUCKING BAR MARKS ON FORWARD FACE OF THE BULKHEAD WHICH ARE CONSISTENT WITH SURROUNDING STRUCTURSDR 2011FA0000447Resistor · burned outDURING CRUSE, HAD A RESISTOR AND A ZENER DIODE (WHICH IS PART OF THE RADIO DIMMER SWITCHING CIRCUIT) FAILED IN FLIGHT. THIS FAILURE CAUSED A LARGE AMOUNT OF SMOKE IN THE CABIN THE PILOT LANDED THE ACFT AT THE AIRPORT. THIS SWITCH IS PART OF STC SA01216WI. TH
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