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 = 'A36' 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 = 'A36' 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 2026FA0000675Rib · crackedRH FLAP INBOARD NOSE RIB CRACKED.SDR 2025FA0000760Solenoid · corrodedI MOVED THE GEAR LEVER INTO THE UP POSITION AFTER TAKEOFF IN VFR CONDITIONS. THE PANEL INDICATED A LOW VOLTAGE WARNING THEN THE GLASS PANEL (G500, GTN 750/650, EDM 900) WENT BLANK ALONG WITH OTHER ELECTRICAL DASH INDICATIONS INCLUDING THE GEAR LIGHTS. I CYCLESDR 2025FA0000662Intake Valve · damagedTHE INTAKE VALVE HAS MATERIAL MISSING IN I LOCATIONS AROUND THE PERIMETER OF THE VALVE HEAD SEAT AREA, LT APPEARS TO BE VALVE FAILURE AND NOT FOD, (OTHER INFO FOUND ON VALVE WFAA PMA719077QITALY),SDR 2025FA0000428Spark Plug · brokenNR 4 EGT WAS NOTED TO BE HIGHER THAN BASELINE AND THE ENGINE WAS RUNNING ROUGH. MECHANIC REMOVED THE #4 PLUGS AND FOUND THE CENTER ELECTRODE ON THE BOTTOM PLUG WAS MISSING. TESTED THE PLUG AND IT DID NOT FIRE. BORESCOPE OF THE CYLINDER LOOKED OK. A NEW PLUG WASDR 2025FA0000065Engine · destroyedDURING CRUISE FLIGHT AT 7500 FT. THERE WAS A SUDDEN LOUD BANG AND VIBRATION. THE COCKPIT FILLED WITH SMOKE AND THE WINDSCREEN COVERED IN OIL. UPON A VISUAL INSPECTION OF THE ENGINE THERE WAS MULTIPLE HOLES IN THE ENGINE CASE. THE LARGEST HOLE WAS BETWEEN CYLINSDR XGNA202404080002Engine · power lossDURING CLIMB A PARTIAL LOSS OF ENGINE POWER OCCURRED WITH FLUCTUATING MANIFOLD PRESSURE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. PILOT RETURNED TO THE AIRPORT. MAGNETO DROPS WERE NORMAL.SDR XGNA202404080001Engine · power lossDURING CLIMB A PARTIAL LOSS OF ENGINE POWER OCCURRED WITH FLUCTUATING MANIFOLD PRESSURE. ALL OTHER ENGINE PARAMETERS WERE NORMAL. MAGNETO DROPS WERE NORMAL. PILOT RETURNED TO AIRPORT.SDR 2024FA0000255Mount · chafedDURING ANNUAL TYPE INSPECTION, CHAFFING (FIG A) WAS NOTED ON THE RH AFT ENGINE MOUNT FITTING P/N 35-910027-3 SERVICE BULLETIN SB71-3638 ADDRESSES DAMAGE TO THE 35-910027-3 FITTING CAUSED BY CHAFFING FROM THE OPTIONAL 35-910003-85 HEAT SHIELD AND PROVIDES APPROSDR 2024FA0000067Servo · bindingPILOT REPORTED RUDDER SYSTEM WAS BINDING, AND NOISE WAS HEARD FROM REAR FUSELAGE LOCATION AFTER ENGINE SHUT DOWN WHILE RUDDER PEDALS WERE MOVED. FAULT ISOLATED TO KS271C YAW SERVO. THE YAW SERVO WAS REMOVED FROM SERVO CAPSTAN ASSEMBLY, AND CONTROLS WERE FREESDR 2022FA0000210Cylinder · separation#5 CYLINDER HEAD SEPARATED FROM THE CYLINDER BETWEEN THE 5TH AND 10TH COOLING FINS ON CLIMB OUT. THERE WAS EVIDENCE OF EXHAUST BLOWBY ON APPROXIMATELY 1/3 OF THE CIRCUMFERENCE OF THE CRACKED CASTING, PRIOR TO THE COMPLETE FAILURE OF THE CYLINDER. THE AIRCRAFTSDR 2022F00006Door Frame · loosePILOT'S DOOR POPPED OPEN IN FLIGHT, PILOT DIVERTED TO THE NEAREST AIRPORT, LANDED AND RE-LATCHED THE DOOR. THEN CONTINUED ON TO DESTINATION. ONCE THERE, THE UPPER DOOR LATCH CHANNEL (AIRFRAME SIDE) WAS FOUND TO BE LOOSE AND WAS TIGHTENED AND RETURNED TO SERVICSDR 2021FA0000368Exhaust Duct · leakingELECTRICAL WIRES ON FORWARD SIDE OF FIREWALL WERE COMPROMISED DUE TO EXHAUST LEAK AT TURBO/DOWN PIPE INTERFACE, AND SHORTED OUT ON EACH OTHER. CAUSING A TEMPORARY, SMALL SMOKE PLUME. NOT EVIDENCE OF SUSTAINED FIRE WAS FOUND.SDR XGNA2021062400013Bladder · collapsedPERFORMED THE INITIAL POWER REDUCTION, THE AIRCRAFT EXPERIENCED AN UNEXPECTED DECREASE IN ENGINE POWER AND ENGINE ROUGHNESS. PERFORMED THE "ENGINE FAILURE AFTER LIFTOFF" CHECKLIST ITEMS. AT THIS POINT THERE WAS NO IMPROVEMENT IN THE ENGINE PERFORMANCE. DECLARSDR 2020F00479Lamp · inoperativeOVERHEAD EMERGENCY AREA LIGHT ADJUSTED TO SEAT 7H INOPERABLE.SDR XGNA2020062600008Cap · leakingLEFT FUEL CAP LEAKING - ABORTED TAKE OFF- RETURNED TO BASE - SERVICEABLE FUEL CAP INSTALLED - FLIGHT PROCEEDED WITHOUT FURTHER INCIDENT.SDR XGNA2020030900000Frame Splice · corrodedCORROSION FOUND ON UPPER FRAME SPLICE BEHIND HAT SHELF,FUSELAGE STATION 179.00. CORROSION FOUND ON 2 UPPER SKINS (LEFT & RIGHT) AFT OF HAT SHELF, FUSELAGE STATION 179.00-207.00.SDR 2019FA0000098Door · openTHE DOOR INADVERTENTLY OPENED ON TAKEOFF RIGHT AT ROTATION. THE OPEN DOOR CAUSED THE ANGLE OF ATTACK INDICATOR TO INDICATE AN IMMINENT STALL ON TAKEOFF DESPITE INITIATING A CLIMB AT VY. THE AOA CONTINUED TO INDICATE AN IMMINENT STALL DESPITE SAFE AIR SPEEDS.SDR 2019FA0000238Crankcase · crackedDEPARTED (MEZ) TO (JBR) ON A VFR FLIGHT, EXPERIENCED ROUGH RUNNING ENGINE, LOSS OF OIL PRESSURE, AND SUBSEQUENT ENGINE FAILURE APPROXIMATELY 40 MINUTES INTO THE FLIGHT. THE PILOT LANDED IN AN OPEN FIELD. INVESTIGATION REVEALED THE ENGINE FAILED TO A MAIN BEARISDR 2018FA0000347Alternator · failedDURING DESCENT, LOSS OF ELECTRIC POWER. SELECTED STANDBY ALTERNATOR. UNABLE TO EXTEND GEAR ELECTRICALLY. MANUALLY EXTENDED GEAR AND LANDED UNEVENTFULLY. TROUBLESHOT TO ALTERNATOR WHICH WAS SENT TO REPAIR STATION WHICH REPLACED THE STATOR AND RECTIFIER.SDR 2017FA0000547Nut · backed outDURING FLIGHT, NOTICED THE THROTTLE WAS NOT RESPONDING CORRECTLY. IT HAD ADVANCED TO FULL POWER. TRIED TO TROUBLESHOOT AND EVENTUALLY FOUND THE THROTTLE STUCK AT FULL POWER. DIVERTED AND WAS ABLE TO LAND WITHOUT ANY PROBLEMS. THE ENGINE HAD BEEN REPLACED ASDR 2017F00042Rod · bentRIGHT GEAR RETRACT ROD BENT, ON A WET WINTER DAY THE PILOT PUT THE GEAR HANDLE DOWN AND THE BREAKER POPPED. HE MANUALLY EXTENDED THE GEAR WITH THE HAND CRANK AND GOT 2 GREEN LIGHTS. 3 GEAR COULD BE SEEN FROM THE GROUND AND HE LANDED. LANDING WAS OK, BUT ON ROLSDR 2016FA0000197Check Valve · cloggedACFT MADE AN OFF AIRPORT LANDING DUE TO THE ENGINE LOSING OIL PRESSURE AND THEN QUITTING. A CONNECTING ROD WAS FOUND PROTRUDING THROUGH THE CASE UPON LANDING. THIS ACFT HAD A NORMALIZING SYSTEM INSTALLED APPROXIMATELY 4 YEARS AND 400 HRS AGO. DURING INVESTISDR FAA201609280001Landing Gear · collapsedTHE AIRCRAFT CONTINUED TO ROLL OUT ABOUT 2000 FT. WHILE STILL ON THE RUNWAY THE NOSE GEAR COLLAPSED RESULTING IN A PROPELLER STRIKE AT IDLE POWER, THE AIRCRAFT CONTINUED TO MOVING FORWARD ON THE MAINS WITH THE NOSE OF THE AIRCRAFT ON THE RUNWAY SURFACE. AS TSDR 2016FA0000074Camshaft · crackedDURING CLIMB OUT, PIC HEARD ENGINE NOISE. AT 6000 AGL ENGINE SHUTDOWN AND PILOT LANDED AT NEAREST AIRPORT. A SUBSEQUENT ENGINE TEARDOWN REVEALED APPROXIMATELY 12 CAM GEAR TEETH DAMAGED ON PN 655516A.SDR 2015FA0000354Manifold · crackedTHE ACFT WAS INVOLVED IN AN INFLIGHT EMERGENCY AND WAS VECTORED TO LAND WITH NO FURTHER INCIDENT. SHORTLY AFTER THE PILOT DECLARED THE EMERGENCY FOR AN ELECTRICAL SYSTEM FAILURE, SMOKE ENTERED THE COCKPIT. THE SMOKE MOST LIKELY ENTERED THROUGH THE FLOOR VENTSDR XGN2015F00001Circuit Breaker · failedRESULT OF AD 2008-13-17, THE NEW CB`S THAT ARE REQUIRED TO REPLACE THE OLD SWITCHES ARE FAILING. THE NEW PN SWITCHES ARE OF POOR QUALITY & ARE FAILING AT A FASTER RATE.SDR XGN2015F00002Circuit Breaker · failedAS A RESULT OF AD 2008-13-17, THE NEW CB REPLACEMENTS ARE FAILING AT A REGULAR RATE, COMPARED TO THE ORIGINAL PN SWITCHES. THESE REPLACEMENT SWITCHES ARE OF POOR QUALITY & DO NOT LAST LONG. WE ARE HAVING A HIGH FAILURE RATE.SDR 2015FA0000257Bevel Gear · separatedREMOVED AND REINSTALLED NEWLY O/H PROPELLER GOVENOR BECAUSE OF SLUGGISH ACTION. TECH SUPPORT RECOMMENDED FLIGHT CHECK. DURING TAKEOFF CLIMB PORTION OF CHECK FLIGHT, ENGINE RPM INCREASED TO 2855 RPM, REDLINE IS 2700 RPM. GOVERNING ACTION WAS LOST. ENGINE SUSDR KC2R2015020549760Impulse Coupling · crackedIMPULSE COUPLING FOUND TO BE CRACKED AT ADVANCE STOP NOTCHES OF BASE PLATE. DEFECT WAS DISCOVERED USING MAGNETIC PARTICLE INSPECTION OF PART DURING PERFORMANCE OF MFG RECOMMENDED-500 HOUR INSPECTION. BOTH MAGS ON THIS ENGINE SHOW SAME DEFECT.SDR 2015FA0000053Nut · splitDURING ANNUAL INSPECTION, FOUND NUT MISSING FROM NR 6 CYLINDER THROUGH STUD, UPPER FORWARD STUD. FOUND NUT IN BOTTOM OF COWLING. NUT WAS SPLIT. REMOVED ENGINE FOR INTERNAL INSPECTION DUE TO LOSS OF CRANKSHAFT BEARING PRELOAD. 42.9 HOURS SINCE LAST ANNUAL.SDR 2015FA0000052Nut · splitDURING ANNUAL INSPECTION FOUND NUT MISSING FROM NR 6 CYLINDER THROUGH STUD, UPPER FORWARD STUD. FOUND NUT IN BOTTOM OF COWLING. NUT WAS SPLIT. REMOVED ENGINE FOR INTERNAL INSPECTION DUE TO LOSS OF CRANKSHAFT BEARING PRELOAD. 42.9 HOURS SINCE LAST ANNUAL.SDR KC2R0130201549748Impulse Coupling · crackedIMPULSE COUPLING FOUND TO BE CRACKED AT ADVANCE STOP NOTCHES OF BASE PLATE. DEFECT WAS DISCOVERED USING MAGNETIC PARTICLE INSPECTION OF PART DURING PERFORMANCE OF MANUFACTURERS RECOMMENDED-500 HOUR INSPECTION. WE HAVE SEEN THIS SAME DEFECT ON A VERY LARGE PESDR IEYR2014102100001Wire · shortedDURING TROUBLESHOOTING A NAVIGATION LIGHT ISSUE, FOUND SMALL MINOR BURN MARKS ON MULTIPLE RIBS IN BOTH WINGS WHERE THE WIRING HAD CAME OUT OF THE STRINGER FROM AN STC. THE EFFECTED STC WOULD BE EITHER STC SA03913AT OF THE WING NAVIGATION LIGHTS OR STC SA02723SDR KC2R2014100249404Impulse Coupling · crackedDURING A 500 HOUR INSPECTION OF MAGNETO, A CRACK WAS DISCOVERED IN THE IMPULSE COUPLING BASE PLATE. CRACK ORIGINATES AT THE ADVANCE STOP NOTCH OF THE FLYWEIGHT BASE PLATE. CRACK DISCOVERED USING MAGNETIC PARTICLE INSPECTION NDT. IMPULSE REPLACED WITH NEW. HSDR CA141024001Engine · power loss(CAN) DURING TAKEOFF CLIMB, AT AROUND 9000 FT, ENGINE ROLLED BACK AND ALL PARAMETERS WENT DOWN. CREW ELECTED TO SHUTDOWN THE AFFECTED ENGINE AND PERFORMED AN UNEVENTFUL LANDING WITH THE REMAINING ENGINES.SDR KC2R0821201449286Impulse Coupling · crackedDURING A 500 HOUR INSPECTION OF MAGNETOS, IMPULSE COUPLING ON EACH MAG WAS FOUND TO HAVE CRACKS IN THE HUB BASE PLATE, LOCATED AT THE FULL ADVANCE STOP NOTCH. CRACKS RADIATE FROM THE SHARP-CORNERED FEATURE OF THE NOTCH OF THE PLATE. DEFECT DETECTED USING MAGSDR WS9R2014080400456Armature · damagedENGINE WOULD NOT TURN OVER DURING START ATTEMPT. STARTER COULD BE HEARD TURNING. STARTER REMOVED AND DISASSEMBLED. ARMATURE COIL FOUND LOOSE AND SPINNING ON SPLINED SHAFT.SDR BWVR20140708001Spline · wornPILOT DECLARED AN IN-FLIGHT EMERGENCY, THROTTLE STUCK OPEN, ON FINAL APPROACH PILOT SHUTDOWN THE ENGINE AND LANDED SAFELY. PILOT REPORTED NO THROTTLE CONTROL BUT PROP AND MIXTURE CONTROLS WORKED. HAD NO ABNORMAL EXHAUST GAS TEMPERATURES OR CYLINDER HEAD TEMPSDR J4YR201406149901Cylinder · crackedDURING AN ANNUAL INSPECTION, DISCOVERED THE NR 2 AND NR 6 CYLINDERS WERE CRACKED AND LEAKING ON THE EXHAUST SIDE AT AROUND THE 17TH FIN FROM THE BOTTOM.SDR AU3R20140515001Heater · dislodgedDURING REMOVAL OF THE LT LOWER SIDE ENGINE COMPARTMENT INSPECTION PANEL, THE LT SUMP HEATER WAS FOUND DISLOGGED AND WRAPPED AROUND THE THROTTLE ARM AND CABLE.SDR XR0R2014FA0000343Rib · crackedDURING AN ANNUAL INSPECTION, WHILE INSPECTING THE FLAPS, REFERENCING SAFETY COMMUNIQUE 313, CRACKS WERE FOUND IN THE NOSE RIB ASSY AT THE ACTUATOR ATTACHMENT BRACKET. CRACKS FOUND IN THE LT AND RT FLAP RIBS.SDR XR0R2014FA0000342Rib · crackedDURING AN ANNUAL INSPECTION, WHILE INSPECTING THE FLAPS REFERENCING SAFETY COMMUNIQUE 313, CRACKS WERE FOUND IN THE NOSE RIB ASSEMBLY AT THE ACTUATOR ATTACHMENT BRACKET. CRACKS FOUND IN BOTH LT AND RT FLAP RIBS.SDR XROR2014FA0000341Rib · crackedDURING AN ANNUAL INSPECTION, WHILE INSPECTIN THE FLAPS REFERENCING SAFETY COMMUNIQUE 313, CRACKS WERE FOUND IN THE NOSE RIB ASSEMBLY AT THE ACTUATOR ATTACHMENT BRACKET ON THE LT AND RT FLAPS.SDR CA140211011Fastener · loose(CAN) PN NAS1428-09 PIN WITH NAS1080C08 COLLAR, HUCK BOLT ASSEMBLY. LOCATION OF DEFECT SECURES PILOT OTBD SEAT TRACK TO AFT SIDE OF FWD SPAR CARRY THROUGH. UPON INSPECTION THE HUCK BOLTS THAT SECURE THE OTBD PILOT SEAT TRACK ASSEMBLY TO THE AFT SIDE OF THE FSDR 2013FA0000600Rib · crackedDURING ANNUAL INSPECTION, FOUND L/E RIB CRACKED ON RT FLAP, WHERE FLAP ACTUATOR IS ATTACHED TO FLAP. FOUND WITH BORESCOPE THRU ROLLER ACCESS HOLE. CRACK WAS AROUND FORWARD NUT PLATE ON RIB. FLAP RIGGING OR USING FLAP AS STEP GETTING IN AND OUT OF ACFT. RECSDR 2013FA0000739Battery · failedWHEN THE PILOT PUT THE LANDING GEAR HANDLE IN THE DOWN POSITION THE ACFT BATTERY FAILED, WHICH CAUSED THE ELECTRICAL SYSTEM TO DROP OFF LINE. PILOT COULD NOT DETERMINE IF THE LANDING GEAR WAS IN THE DOWN AND LOCKED POSITION AND COULD NOT COMMUNICATE WITH ANYOSDR 2013FA0000672Adapter · crackedMECHANIC WAS PERFORMING MX ON THE AIRFRAME AND NOTICED EXHAUST STAINING ON THE OUTSIDE OF THE COWLING. ON OPENING THE COWLING THE MECHANIC DISCOVERED THE EXHAUST HAS BEEN PRESSURIZED AT EVERY ANNUAL SINCE INSTALLATION. THE CRACK WAS NOT EVIDENT AT THE LAST ASDR WS9R2013FA0000568Adapter · crackedEXHAUST STAINING ON THE OUTSIDE OF COWLING. DISCOVERED EXHAUST HAS BEEN PRESSURIZED AT EVERY ANNUAL SINCE INSTALLATION. CRACK WAS NOT EVIDENT IN AT THE LAST ANNUAL APPROX 90 HRS AGO. IT WOULD APPEAR THAT THE CRACK WAS CAUSED BY EXCESSIVE STRESS ON THE EXHASDR XGNA20130621001Pressure Sensor · intermittentMANIFOLD PRESURE SENSOR BECAME INTERMITTENT.SDR 2013FA0000408Brace · crackedTHE BRACE ASSY, LT MLG CRACKED AND TWISTED TO ALLOW THE LT MAIN GEAR STRUT AND WHEEL ASSY TO COLLAPSE INWARDS AND UP THROUGH THE INNER GEAR DOOR (WHICH WAS CLOSED) INTO THE WHEEL WELL DURING ROLL OUT AFTER LANDING. ALSO DAMAGED AS A RESULT WERE THE LT FLAP, L
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