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 2026FA0000573Light · brokenPULSE LIGHT WAS FIRST REPLACED 9-30-2025 DUE TO LT WIG WAG NOT WORKING, SOLID ON WORKED. AFTER A MONTH OF OPERATION LT WIG WAG FAILED AGAIN, DIDNT GET TO TROUBLESHOOT AGAIN UNTIL 4-20-2026 AND NOTED THAT AT THAT TIME EVEN SOLID ON DID NOT WORK, SUSPECTED FAULSDR 2026FA0000250Cable · frayedWHILE TROUBLESHOOTING A FUEL LEAK THE MECHANIC NOTICED THAT THE AILERON CARRY THROUGH CABLE WAS FRAYED.SDR 2026FA0000094Doubler · crackedDURING FIREWALL CLEANING/INSPECTION DURING ANNUAL/100HR INSPECTION, A CRACK, APPROXIMATELY 1.0" IN LENGTH WAS DISCOVERED IN THE UPPER RADIUS OF THE LEFT HAND SIDE OF THE LOWER FIREWALL DOUBLER DIRECTLY THROUGH THE TOP RIVET THAT HOLDS THE PARKING BRAKE BRACKETSDR 2026FA0000074Doubler · crackedDURING FIREWALL CLEANING/INSPECTION DURING ANNUAL/100HR INSPECTION, A CRACK, APPROXIMATELY 2.3 IN LENGTH WAS DISCOVERED IN THE UPPER RADIUS OF THE LEFT HAND SIDE OF THE LOWER FIREWALL DOUBLER DIRECTLY THROUGH THE TOP RIVET THAT HOLDS THE PARKING BRAKE BRACKET SDR 2026FA0000001Strut · crackedCRACK ON WING SIDE OF RH STRUT. AIRFRAME TOTAL TIME IS 10298.9. CRACK WAS FOUND DURING ROUTINE 100/HR INSPECTION. AIRPLANE DOES PIPELINE PATROL.SDR 2026FA0000073Doubler · crackedDURING FIREWALL CLEANING IN PREPARATION OF INSTALLATION OF NEWLY OVERHAULED ENGINE, A CRACK, APPROXIMATELY 2.3 IN LENGTH WAS DISCOVERED IN THE UPPER RADIUS OF THE LEFT HAND SIDE OF THE LOWER FIREWALL DOUBLER DIRECTLY THROUGH THE TOP RIVET THAT HOLDS THE PARKINSDR ODAR2025080600001Skin · crackedDURING 100HR / ANNUAL INSPECTION FOUND RH INBOARD FLAP COVE SKIN CRACKED ALONG WITH FLAP TRACK RIVETS WORKING OUT. INSPECTED AREA AROUND FLAP AND FOUND THE INBD FLAP TRACK/RIB ASSEMBLY TO BE CRACKED THROUGH.SDR 2024FA0000717Attach Fitting · crackedDURING A 50-HOUR OIL CHANGE / INSPECTION EVENT THE NOSE LANDING GEAR LOWER STRUT FITTING WAS DISCOVERED TO BE CRACKED IN TWO ON THE RIGHT-HAND WEB SECTION. AFTER REMOVAL OF BROKEN MOUNT, EVIDENCE SHOWED THE CRACK HAD OCCURRED PRIOR TO THE FINAL FAILURE OF THE SDR 2024FA0000515Fitting · crackedNOSE GEAR LOWER ATTACH FITTING CRACKED. DISCOVERED DURING ANNUAL INSPECTION.SDR 2024FA0000512Fitting · crackedNOSE GEAR, LOWER ATTACH STRUT FITTING CRACKED IN RADIUS.SDR 2024FA0000520Fitting · crackedNOSE STRUT LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION, CONFIRMED VIA DYE PENETRANT INSPECTION.SDR 2024FA0000519Fitting · crackedNOSE STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. CRACK DISCOVERED DURING ANNUAL INSPECTION. CONFIRMED WITH DYE PENETRANT.SDR 2024FA0000518Fitting · crackedNOSE STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. CRACK DISCOVERED DURING ANNUAL INSPECTION.SDR 2023FA0000671Tube · deflatedON THE 5TH UPON GETTING TO THE HANGAR I FOUND THE TIRE STILL FULLY INFLATED AND AT PROPER PSI. I REMOVED THE TIRE AND REPLACED THE TUBE WITH NEW. UPON INSPECTING THE OLD TUBE I FOUND A SMALL HOLE ON THE SIDE OF THE TUBE THAT WAS NOT LEAKING WHEN FULLY INFLATEDSDR 2023FA0000395Alternator · seizedCREW REPORTED DURING GROUND RUN AND PRIOR TO TAXI, ENGINE MADE A LOUD NOISE, AND THE ENGINE WAS SHUT DOWN IMMEDIATELY. THIS HAPPENED PRIOR TO FLIGHT, WITH NO INDICATION OF A PENDING FAILURE. MAINTENANCE TECHNICIAN REPORTED THAT THE ALTERNATOR HAD SEIZED, ANSDR 2023FA0000310Points · brokenTEST, TEST, TEST: MAGNETO POINT FAILURESDR 2024FA0000517Fitting · crackedNOSE STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION.SDR 2022FA0000270Points · brokenMAGNETO POINT FAILURESDR 2022FA0000171None · looseDURING THE PREFLIGHT INSPECTION OF THE RH ELEVATOR, A CREAKING NOISE WAS HEARD FROM THE ELEVATOR PIVOTING TORQUE TUBE. AFTER AN IN DEPTH INSPECTION SMOKING RIVETS WERE FOUND ON THE RH ELEVATOR TORQUE TUBE END PLATE. WHEN THE ELEVATOR WAS REMOVED TO MAKE THE NESDR 2024FA0000516Fitting · crackedNOSE GEAR STRUT, LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION.SDR JRUR202012090014Control Rod · brokenNO HEAT FLOW INTO THE CABIN WHEN IN FLIGHT. FOUND THAT WELD THAT ATTACHED THE CONTROL ROD TO THE VALVE PLATE HINGE CRACKED & BROKEN CAUSING THE VALVE PLATE TO NOT FUNCTION AS DESIGNED TO OPEN OR CLOSE ALLOWING HOT AIR FROM ENTERING THE CABIN.SDR 2024FA0000514Fitting · crackedNOSE GEAR LOWER ATTACH FITTING CRACKED IN RADIUS. DISCOVERED DURING ANNUAL INSPECTION.SDR 2024FA0000513Fitting · crackedNOSE GEAR LOWER ATTACH FITTING CRACKED.SDR JRUR2020032560002Magneto · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
INSPECTED MAGNETO MODEL NO. 6351 P/N: SDR JRUR202003120012Impulse Coupling · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
MAGNETO INSTALLED WITH TSN 0.0 AT AN ASDR JRUR202003120011Impulse Coupling · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
MAGNETO INSTALLED WITH TSN 0.0 AT AN ASDR JRUR202003060005Magneto · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
MAGNETO INSTALLED WITH TSN 952.3 AT ANSDR JRUR202003060004Magneto · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
MAGNETO INSTALLED WITH TSN 0.0 AT AN ASDR JRUR202003060003Magneto · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
MAGNETO INSTALLED WITH TSN 493.9 AT ANSDR JRUR202003060001Magneto · unserviceableSUPPLEMENTAL INFORMATION
SLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF SDR JRUR2020030560002Magneto · unserviceableSLICK BY CHAMPION SB2-19A
MANDATORY INSPECTION OF IMPULSE COUPLING.
THE SB HAS YOU INSPECT THE IMPULSE COUPLING PER THE MAINTENANCE MANUAL. IF ANY MOVEMENT IS FOUND IN THE RIVETS, THE IMPULSE COUPLING MUST BE REJECTED.
INSPECTED MAGNETO MODEL NO. 6351 P/N: SDR CA190723009Wheel · damaged(CAN) DURING AN OPERATION 3 INSPECTION IT WAS DISCOVERED THAT BOTH LEFT AND RIGHT MAIN LANDING GEAR TIRES HAD BEEN EXPOSED TO A SKID WHICH RENDERED THE TIRES UNSERVICEABLE. AFTER REMOVING THE TIRES THE WHEEL HALVES WERE INSPECTED AND FOUND TO HAVE INTER-GRANULSDR 2019FA0000155Switch · failedFLAPS SELECTED AND MOVED FULL DOWN FOR PREFLIGHT INSPECTION AND THEN WOULD NOT RETRACT. FOUND FLAP UP SELECTOR MICROSWITCH (S1007) BROKEN INTERNALLY.SDR JRUR201905060002Exhaust Valve · out of toleranceDURING PERFORMANCE OF SB 388C, IT WAS FOUND THAT THE NR 4 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED .031". THIS EXCEEDS THE MAXIMUM ALLOWABLE CLEARANCE OF .030". THIS ENGINE WAS OVERHAUL. THE TOTAL TIME SINCE NEW IS NOT BEING LISTED AS IT IS NOT KNOWNSDR JRUR201905060001Exhaust Valve · out of toleranceDURING PERFORMANCE OF SB 388C, IT WAS FOUND THAT THE NR 3 CYLINDER EXHAUST VALVE TO GUIDE CLEARANCE MEASURED .031". THIS EXCEEDS THE MAXIMUM ALLOWABLE CLEARANCE OF .030". THIS ENGINE WAS OVERHAUL. THE TOTAL TIME SINCE NEW IS NOT BEING LISTED AS IT IS NOT KNOWNSDR 2018FA0000339Autopilot Sys · corruptedAUTOPILOT INTEGRATED WITH G1000 REFUSED TO DISCONNECT.SDR 2017FA0000460Sprocket · brokenELEVATOR TRIM LOCKED UP IN FLIGHT. TRIM ACTUATOR SPROCKET FOUND TO BE BROKEN WHERE PIN ATTACHES IT TO ACTUATOR ASSEMBLY.SDR 2017FA0000106Pushrod · scoredDURING THE PUSHROD INSPECTION FOUND THE NR 3, 4, 5, AND 6 PUSHRODS SCORED AND REPLACED.SDR 2017FA0000105Pushrod · scoredDURING INSPECTION OF PUSHRODS FOUND THE NR 5, 4, & 1 PUSHRODS WORN OUT OF TOLERANCE, BOTH PUSHRODS AND ROCKER ARMS REPLACED WITH NEW.SDR 2017FA0000103Pushrod · scoredDURING THE INSPECTION OF PUSHRODS FOUND TWO PUSHRODS AT THE NR 2 AND 6, SCORED BEYOND LIMITS. REPLACED THE PUSHRODS AND MATING ROCKER ARMS WITH NEW.SDR 2017FA0000092Pushrod · scoredDURING INSPECTION OF PUSHRODS, FOUND NR 4 CYLINDER EXHAUST PUSHROD SCORED, REPLACED PER SA-167A.SDR 2017FA0000090Pushrod · scoredDURING INSPECTION OF SA-167A FOUND THE NR 2 CYLINDER EXHAUST PUSHROD SCORED, REPLACED THE PUSHROD AND ROCKER ARM.SDR 2017FA0000088Governor · malfunctionedPILOT STATED THAT DURIUNG DESCENT, THE ENGINE ROLLED BACK TO 1500 RPM, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE PROPELLER GOVERNOR WAS REPLACED AND NO FURTHER DEFECTS WERE NOTED.SDR 2017FA0000087Pushrod · scoredFIVE PUSHRODS FOUND TO BE SCORED ON THE NR 5, 3 AND 4 CYLINDERS, FOUND DURING THE SA-167A INSPECTION.SDR 2017FA0000086Pushrod · scoredFIVE PUSHRODS FOUND TO BE SCORED ON THE NR 5, 3 AND 4 CYLINDERS, FOUND DURING THE SA-167A INSPECTION.SDR 2017FA0000053Pushrod · scoredINSPECTION REVEALED NR 5 CYLINDER, EXHAUST AND INTAKE, NR 3 CYLINDER EXHAUST AND INTAKE AND NR 4 CYLINDER EXHAUST AND INTAKE PUSHRODS SCORED BEYOND LIMITS AND REPLACED.SDR 2017FA0000052Pushrod · wornINSPECTION SHOWS 10 OF THE PUSHRODS HAVE WEAR. THE MAINTENANCE PROVIDER SAID THE 10 PUSHRODS, ROCKER ARMS AND ALL OF THE VALVE ROCKER SHAFTS NEED TO BE REPLACED. ON 10 AUGUST 2012, TAC TIME 578.9 NR 3 CYLINDER WAS REPLACED. DURING THE CHANGE ABNORMAL WEAR WASDR 2017FA0000051Pushrod · out of limitsDURING INSPECTION OF PUSHRODS, FOUND 6 PUSHRODS AND 6 ROCKER ARMS OUT OF LIMITS IN ACCORDANCE WITH SA-167A, PARTS REPLACED UNDER WARRANTY.SDR 2017FA0000043Pushrod · scoredNR 1 INTAKE AND EXHAUST SCORED, NR 4 INTAKE AND EXHAUST SCORED, AND NR 5 EXHAUST SCORED, PARTS REPLACED PER SA-167A.SDR 2017FA0000031Pushrod · scoredNR 2 AND 6 PUSHRODS AND ROCKER ARMS REPLACED FOR EXHAUST SIDE DUE TO SA-167A INSPECTION. SCORING IS OBVIOUS AND TRANSLATED TO ROCKER ARM AS WELL. REPLACED PARTS AS NECESSARY.
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