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 = 'M20F' 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 = 'M20F' 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 2026FA0000634Servo · failedDURING DESCENT FROM BIG BEAR, THE GARMIN AUTOPILOT ABRUPTLY DISCONNECTED FOLLOWING FAILURE OF THE GSA 28 PITCH SERVO. IMMEDIATELY PRIOR TO THE FAILURE, I OBSERVED A MOMENTARY PITCH-TRIM-DOWN INDICATION. THE AIRCRAFT USES MANUAL PITCH TRIM. UPON SERVO/AUTOPILOTSDR 2025FA0000507Mount · crackedDURING ENGINE OVERHAUL AND ANNUAL INSPECTION, THE R/H LOWER ENGINE MOUNT WAS FOUND CRACKED. THIS WAS HIDDEN UNTIL THE ENGINE MOUNT WAS REMOVED. RECOMMEND THAT MECHANICS VISUALLY INSPECT THE LOWER ENGINE MOUNT AREA WHERE IT AFFIXES TO THE FIREWAL, WITH A BORESCSDR 2025FA0000278Leg Assy · shearedNOSE/FRONT LANDING GEAR SHEARED AFTER ENCOUNTERING 2-DEGREE DRAINAGE INDENTURE/DIP WHEN TAXING FROM PARKING. EXAMINATION OF NOSE GEAR ASSEMBLY REVEALED THAT FRONT GEAR FORK/GEAR LEG OF THE NOSE GEAR ASSEMBLY (PN: 54004-505) AT WELDING POINT, JUST ABOVE THE SHSDR 2024FA0000629Fuel Line · broken#1 FUEL INJECTION LINE CAME APART AT SOLDER JOINT BY INJECTOR B-NUT. CYLINDER SHUT DOWN IN FLIGHT AND CAUSED A FUEL LEAK. AIRCRAFT MADE EMERGENCY LANDING AT MILITARY INSTALLATION. PART IS 1029.9 HOURS SINCE NEW FROM FACTORY. REPETITIVE INSPECTION UNDER AD I1SDR 2025FA0000471Support · crackedLUG SUPPORT CRACKED AT LANDING GEAR ACTUATOR AFT ATTACH TO FUSELAGE ALLOWING FORE AND AFT MOVEMENT OF ACTUATOR. LUG MOUNTING HOLES ELONGATED IN BRACKET ASSEMBLY.SDR 2023FA0000797Landing Gear · failed inspEXCESSIVE CORROSION FOUND IN THE MLG SPINDLE, UPPER TORQUE TUBE. CORROSION WAS HIDDEN BY PAINT AND DIRT. PAINT WAS REMOVED FROM THE GEAR SPINDLES IN PREPARATION FOR REPAIR AND REPAINT. IT WAS ONLY THEN THE DAMAGE WAS LOCATED. TWO OTHER SERVICEABLE SPINDLES WERSDR 2023FA0000039Shaft · shearedDURING LANDING FLARE, PILOT'S CONTROL YOKE SEPARATED FROM THE CONTROL SHAFT. INSPECTION REVEALED THE SHAFT HAD SHEARED OFF AT THE HOLES FOR THE TAPER PIN HOLDING THE YOKE TO THE SHAFT. CONDITION IS THE SUBJECT OF AD 77-17-04. AIRCRAFT WAS IN COMPLIANCE WITHSDR 2019FA0000179Rod End · separatedDURING CRUISE FLIGHT, THE MIXTURE CONTROL ROD END SEPARATED FROM THE PRESSURE CARBURETOR CONTROL ARM, WHICH RESULTED IN POWER LOSS.SDR 2015FA0000506Truss · separatedDURING TAXI NLG TRUSS SEPARATED FROM ACFT. DISCOVERED DURING RECORDS INSPECTION, IN 1999 THE TRUSS WAS R & R WITH A TRUSS WITH STOPS INSTALLED. THE ENTRY READS, REPLACED TRUSS WITH PN L540041-501. THE TAG READS REPLACED BENT TUBES, ADD STOPS, HEAT TREAT. TSDR 2015FA0000443Lever · separatedWHILE TAXING FOR T/O, THE NLG COLLAPSED, FOLLOWED BY BOTH MAIN GEARS. INSPECTION REVEALED THE LANDING GEAR RETRACTION LEVER ASSEMBLY SEPARATED AT THE WELD. THE WELD SHOWED SIGNS OF AN OLDER CRACK BEING PRESENT AT WELD, PRIOR TO COMPLETE FAILURE.SDR 2014FA0000522Filler · crackedREPLACED SPINNER AND ADAPTER PLATE WITH PN 103585F2 WHEN PROPELLER HAD 29.96 TSMOH AND SINCE NEW THAT WAS INSTALLED IAW THE MM. DURING A RECENT ANNUAL INSPECTION, REMOVED THE SPINNER FOR INSPECTION AND LUBRICATION OF THE PROPELLER. FOUND CRACK EMANATING FROMSDR CA120103022Spinner · cracked(CAN) PROPELLER SPINNER CRACKED FROM A ATTACHEMENT SCREW TO THE BLADE CUTOUT AND A 3 INCH PIECE SEPERATED IN FLIGHT. AIRCRAFT WAS GROUNDED AND A NEW SPINNER INSTALLED PER HARTZELL ALERT SERVICE BULLETIN HC-ASB-61-332.SDR 2012FA0000004Adapter · crackedINSTALLED A NEW STC PROPELLER WITH A NEW SPINNER AND ADAPTER PLATE SUPPLIED IAW STC SA02414CH-D. AFTER 30 HOURS OF OPERATION, WHILE DOING A WALK AROUND INSP, NOTICED THE SPINNER WAS CRACKED AT A SCREW HOLE. REMOVED SPINNER AND FOUND ADAPTER PLATE CRACKED. TSDR 2012FA0000003Spinner · crackedINSTALLED A NEW STC PROPELLER WITH A NEW SPINNER AND ADAPTER PLATE SUPPLIED IAW STC SA02414CH-D. AFTER 30 HOURS OF OPERATION, WHILE DOING A WALK AROUND INSPECTION, NOTICED THE SPINNER WAS CRACKED AT A SCREW HOLE. REMOVED SPINNER AND FOUND ADAPTER PLATE CRACKSDR 2011FA0000627Cylinder Bore · peelingCLIMBING THROUGH 7000 FELT A SLIGHT SHUDDER. WHILE LEVELING AT 9500, NOTICED OIL PRESSURE GOING DOWN. PROP WENT TO FLAT PITCH. OIL PRESSURE NOW IN YELLOW ARC. DECLARED AN EMERGENCY. PULLED ENGINE TO IDLE AND BEGAN A DESCENT TO AIRPORT. LANDED LONG AND BLSDR CA110829008Selector Switch · broken(CAN) FLAPS T/O, FULL FLAP AND FLAPS UP SELECTED ON RUN UP. FLAPS STOPPED AT T/O POSITION AND WOULD NOT MOVE WHEN SELECTED UP OR DOWN. FOUND THE FLAP SELECTOR SWITCH BROKEN AT THE PIVOT POINT OF THE SWITCH. NO REPORTED PROBLEMS WITH THIS SWITCH SINCE ACFT WASDR 2011FA0000464Torque Tube · brokenRUDDER TORQUE TUBE ASSY BROKE AT POINT WHERE BELCRANK IS ATTACHED TO TORQUE TUBE CAUSING LOSS OF STEERING CONTROL.SDR CA110517002Camshaft · making metalINSPECTION OF OIL FILTER DURING ROUTINE MX REVEALED SMALL FERROUS METAL PARTICLES THAT WARRANTED FURTHER INVESTIGATION RESULTING IN THE REMOVAL OF NR 1 CYLINDER. IT WAS DISCOVERED THAT THE NR1 INTAKE TAPPET WAS SEVERELY GALLED. THE ENGINE WAS REMOVED FOR REPASDR 2010FA0000228Mount · brokenHAVE HAD MULTIPLE PROBLEMS WITH THE MOUNTING KIT FOR THE ALTERNATOR THROUGH STC SA334SW. A NEW ALTERNATOR WAS INSTALLED ON 9/8/2006. AFTER 64 FLIGHT HOURS, THE ALUMINUM MOUNTING BLOCK BROKE DURING FLIGHT ON 6/5/07, AND WAS REPLACED ON 6/13/07. AFTER 127 FLISDR 2008FA0000879Leg Assy · brokenPILOT STATED THAT HE HEARD A LOUD NOISE DURING TAKE-OFF AND THAT THE AIRCRAFT BEGAN TO "HANDLE DIFFERENTLY." HE CONTINUED TO ACCELERATE BRIEFLY, LIFTED OFF AND THEN DECIDED TO ABORT THE TAKEOFF. THE ACFT CAME TO REST ON ITS NOSE WITH THE NOSE L/G FOLDED BACK SDR 2008FA0000878Tube · brokenPILOT STATED THAT HE HEARD A LOUD SOUND DURING THE TAKE OFF ROLL OFF OF A GRASS STRIP AND THE ACFT BEGAN TO "HANDLE DIFFERENTLY". HE CONTINUED TO ACCELERATE BRIEFLY AND THEN DECIDED TO ABORT THE TAKE-OFF. INCIDENT INVESTIGATION FOUND ACFT ON ITS NOSE WITH TSDR CA081003007Actuator · failed(CAN) LANDING GEAR FAILED TO EXTEND ELECTRICALLY. ACTUATOR TEAR DOWN REVEALED THE MOTOR HAD FAILED.SDR 2008FA0000203Starter · failedTHIS STARTER WAS PURCHASED NEW FROM A LOCAL VENDOR. THE STARTER FAILED TO OPERATE AFTER LESS THAN A YEAR AND LESS THAN 100 HOURS OF SERVICE. THE OWNER\OPERATOR WANTED TO HAVE THE OLDER, HEAVIER STARTER INSTALLED HOWEVER NONE WERE AVAILABLE, AFTER CONTACTING SSDR 2005FA0000232Warning Switch · looseLANDING GEAR WARNING SWITCH FOUND LOOSE ON THE ATTACH AREA OF THROTTLE CABLE CAUSING INTERMITTENT OPERATION OF HORN. SCREWS WERE TIGHTENED AND SYSTEM OPERATES NORMALLY.(K)SDR 07092004Landing Gear · collapsedLANDING GEAR CIRCUIT BREAKER POPPED, ATTEMPTED TO RESET IT AND SAW SPARKS. PILOT ATTEMPTED MANUAL EXTENSION OF GEAR BUT WAS UNABLE TO GET DOWN AND LOCKED INDICATION. PILOT REPORTED GEAR PROBLEM TO TOWER. GEAR APPEARED TO BE DOWN AND THE PILOT FLEW BY TOWERSDR 2003FA0000848Camshaft · spalledCAMSHAFT, FOUND EVIDENCE OF SEVERE SPALLING ON SEVERAL CAM LOBES. ENGINE HAD APPROX 750 HOURS ON A FACTORY OVERHAUL.SDR 2003FA0000195Shaft · shearedNEW VACUUM PUMP SHAFT SHEARED WITH ONLY 3 HOURS OF OPERATION INSTALLED ON 04/25/2002. BROKE ON 02/19/2003.SDR AUS20021005Bearing · failed(AUS) ENGINE OIL FILTERS CONTAMINATED WITH METAL. SUSPECT CAUSED BY FAILURE OF EITHER MAIN BEARING OR BIGEND BEARING.SDR 2002FA0000864Structure · corrodedHEADLINER EACH LOCATION THE HEADLINER MATERIAL CAME INTO CONTACT WITH ALUMINUM ATTACH POINTS THE AREA CORRODED THE INTERIOR WAS REPLACED IN THE SUBJECT AIRCRAFT ON MAY 1, 1998 THE CORROSION WAS DISCOVERED DURING MAINTENANCE MAY 17, 2002.SDR 2002FA0000625Actuator · failedWHEN PILOT SELECTED GEAR DOWN INCOMPLETE EXTENSION OCCURRED. ATTEMPTS TO EXTEND THE GEAR MANUALLY ALSO FAILED. AFTER THE AIRCRAFT WAS RETREIVED, PLACED ON JACKS AND BELLY PANELS REMOVED, IT WAS DISCOVERED THE MAIN LANDING GEAR ACTUATOR (DUKES) COUPLING BETWSDR 2002FA0000624Coupling · failedWHEN PILOT SELECTED GEAR DOWN, INCOMPLETE EXTENSION OCCURRED. ATTEMPTS TO EXTEND THE GEAR MANUALLY ALSO FAILED. GEAR COLLAPSED ON LANDING. Z AN INSPECTION FOUND THAT THE COUPLING BETWEEN THE GEAR MOTOR AND ACTUATOR WAS SEPARATED. THE MOTOR WAS FOUND NOT TO SDR 20010604CW012Fuel Cell · contaminatedENGINE LOST POWER, THEN QUIT, DURING TAKEOFF CLIMB. AIRCRAFT MADE OFF AIRPORT LANDING. INVESTIGATION FOUND WATER IN THE RIGHT HAND FUEL SUMP. AIRCRAFT HAD BEEN PARKED OUTSIDE THROUGH HEAVY RAIN.SDR CA010518010Plate · cracked(CAN) CRACK & FAILURE OF FLANGE OF BACKING PLATE THAT HAS BLADE ROOT CLOSING FAIRING ATTACHED.A PORTION OF FAIRING REMAINED ATTACHED TO SPINNER WHICH SEVERELY DAMAGED NOSE BOWL FAIING LEAVING BACKING PLATE&FAIRING DEBRIS INSIDE ENGINE COWL.THERE WAS SOME MINORSDR 20010518CW001Gyro · contaminatedDURING ANNUAL INSPECTION, FOUND LIQUID IN WINDOW OF GYRO, DISCONNECTED LINE TO HAVE WATER FLOW OUT, REMOVED INSTRUMENT. OPENDED CASE AND FOUND LONG-TERM CORROSION ON ALL INTERNAL PARTS. REPLACED WITH OVERHAULED INSTRUMENT. NO OTHER INSTRUMENTS CONTAINED WATSDR 20000516SH010Buckle · damagedNOSE GEAR BUCKLE OFF AT UPPER TRUSS. POSSIBLY WEAKENED BY OVERTURNING WITH TOW TRACTOR. SUBMITTER SUGGESTED HEAVIER METAL, BETTER SUPERVISION AND TRAINING. (X)SDR 2000ZZZX409Nut · looseLANDING GEAR COLLAPSED ON LANDING. AFTER AIRCRAFT WAS TOWED TO HANGAR AND PLACED ON JACKS, FOUND THE GEAR ACTUATOR JACKSCREW HAD BECOME SEPARATED FROM THE MOTOR/GEAR PORTION OF THE GEAR ACTUATOR. AFTER REMOVAL OF THE ACTUATOR FROM AIRCRAFT AND DISASSEMBLY, DSDR 99ZZZX2427Vibrator · mismarkedPILOT REPORTED AIRCRAFT HARD TO START. TROUBLESHOT PROBLEM TO INTERMITTENT STARTING VIBRATOR, TCM SYSTEM SUPPORT MANUAL INDICATOR, PN 10-176485-121, TO BE USED WITH S-200 SERIES MAGS. HOWEVER, WHEN UNIT PULLED FROM STOCK PRINTED ON UNIT IN 'RED', USE WITH 12SDR 99ZZZX1642Regulator · contaminatedENGINE QUIT WHILE AIRCRAFT WAS FLYING.SDR 98ZZZX3926Alternator · failedPILOT LOST ALL ELECTRICAL POWER. ON INSPECTION, THE ALTERNATOR FAN WAS FOUND DESTROYED AND LODGED IN THE ALTERNATOR BRACKET AND ENGINE BAFFELS. SUBMITTER STATED POSSIBLE CAUSE SEEMS TO BE FRAME CRACKS OR DAMAGE DONE PREVIOUSLY TO CAUSE A FAN SEPARATION UNDERSDR 98ZZZX3928Crankshaft · failedENGINE VIBRATED 5-10 SECONDS BEFORE SEIZING, NO OTHER INDICATIONS OF PENDING FAILURE WERE NOTED. AT ENGINE TEARDOWN, THE CRANKSHAFT WAS FOUND BROKEN AT THE FORWARD END OF THE NR 4 CONNECTING ROD JOURNAL. MAINTENANCE RECORDS ONLY WENT BACK TO LAST OVERHAUL ANSDR 98ZZZX886Battery · poor groundTROUBLESHOOTING FOR POOR BATTERY CHARGING, INTERMITTENT CRANKING, AND INTERMITTENT GPS/COMM FAILURES, FOUND PAINT ON AIR FRAME STRUCTURE CAUSING POOR BATTERY GROUND. SUBMITTER SUGGESTS REMOVING PAINT UNDER BOLTS AND NUT AND ADD A HEAVY GROUND STRAP.SDR 98ZZZX840Hose · leakingPILOT COMPLAINED THAT FOLLOWING THE LAST SEVERAL FLIGHTS, HE HAD NOTICED FUEL DRIPPING FROM THE RT SIDE OF THE COWLING. MECHANICS THEN PRESSURIZED THE FUEL SYS WITH THE PUMP AND SAW A FAN-SHAPED SPRAY PATTERN EMITTING FROM THE FUEL LINE WHICH LEADS TO THE COCSDR 97ZZZX4212Cover Plate · displacedENGINE BEGAN TO RUN ROUGH IN FLIGHT, PRECAUTIONARY LANDING. FOUND INTAKE ROCKER SHAFT ON NR 1 CYLINDER HAD MOVED OUT OF POSITION DUE TO LOSS OF COVER PLATE, 7510. CAUSE OF COVER PLATE LOSS UNDETERMINED. SUBMITTER RECOMMENDS PERIODICAL RE-CHECK OF COVER PLATSDR 97ZZZX3695Valve · stuckENGINE RAN ROUGH AT TAKEOFF, AIRCRAFT LOST POWER. AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE DURING A FORCED LANDING. EXAMINATION FOR THE ENGINE REVEALED AN OPEN EXHAUST VALVE, CYLINDER NR 4. ENGINE HAD A CYLINDER, NR 4 EXHAUST VALVE STUCK.SDR 97ZZZX1058Pump · failedOPERATOR REPORTED THAT EMERGENCY ELECTRIC FUEL PUMP NO LONGER WORKED. UPON REMOVAL AND REPLACMENT OF PUMP, DISCOVERED THE FAILED PUMP HAD BEEN IN SERVICE ON THE AIRCRAFT FOR 23 YEARS. THESE PUMPS ARE STAMPED ON THE PUMP HOUSING TO REPLACE EVERY TEN YEARS. TSDR 96ZZZX2083Actuator · failedLANDING GEAR FAILED TO EXTEND ELECTRICALLY. MANUAL EXTENSION WAS ATTEMPTED WITH NO EXTENSION. AIRCRAFT LANDED WITH WHEELS UP. INVESTIGATION REVEALED DUKES ACTUATOR (PN 3214-00) PINION GEAR (ADDRESSED IN AD 75-23-04) WORN BEYOND LIMITS CAUSING PINION AND DRISDR AU960561Rivet · sheared(AUS) HORIZONTAL STABILISER RH ATTACHMENT BRACKET RIVETS (8OFF) SHEAREDSDR 95ZZZX5952Air Control · wrong partINSTALLED CONTROL AND FOUND THREADED BULKHEAD SLEEVE TO BE 6 INCHES SHORT OF FIREWALL. INSPECTED MOONEY DWG 940088 DATED 8-28-95 AND FOUND DIMENSIONALLY WRONG FOR MODEL AIRCRAFT. THIS PART IS LISTED AS A RETROFIT WITH A MOVEABLE THREADED SLEEVE (SLEEVE IS CRSDR 95ZZZX4521Skin · crackedTHE RT WING SKIN AREA THAT IS FORWARD OF THE FLAP, WHERE THE FLAP FITS THE WING CONTOUR WHEN RETRACTED, WAS FOUND CRACKED. THE CRACK IS LOCATED NEXT TO THE INBOARD FLAP ATTACH SUPPORT ON THE UNDERSIDE OF THE RT WING SKIN. THE SUPPORT IS PRIMARILY ATTACHED TOSDR 95ZZZX6141Through-Bolt · brokenSUBJECT NR 1 CYLINDER UPPER THROUGH-BOLT FOUND BROKEN DURING PREFLIGHT. DETECTED AS THE MAJOR REMAINING PORTION AND HOLD-DOWN NUT FOUND BACKED OUT OF POSITION AND LODGED AGAINST CYL FINS. INSTALLED NEW BOLT, SPACER, AND NUT. TORQUED PER LYC SERVICE LETTER 1
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