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 = 'M20J' 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 = 'M20J' 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 99ZZZX3962Baggage Door · separatedBAGGAGE DOOR CAME OPEN IN-FLIGHT. CAUSE UNKNOWN. DOOR LATCH AD HAD BEEN C/W. NO ACCIDENT OCCURRED. DOOR WAS REPLACED WITH NEW DOOR.SDR 99ZZZX3824Fuel Cell · leakingFUEL LEAK UNDER FORWARD WING WALK TWO INBOARD SCREWS.SDR 99ZZZX2989Tube · misinstalledTHE PITOT TUBING IN THE CABIN WAS IMPROPERLY ROUTED CAUSING THE TUBING TO BE CRUSHED BETWEEN THE CABIN STEEL FRAME AND THE LEFT SIDE SKIN. THIS CAUSED A RESTRICTION OF PRESSURE TO THE AIRSPEED INDICATOR RESULTING IN INCORRECT INDICATIONS TO THE PILOT. THIS ASDR 99ZZZX4197Muffler · separatedFOUND RISER FROM NR 2 CYLINDER HAD DEPARTED FROM MUFFLER WHILE TROUBLESHOOING ROUGH RUNNING ENGINE. MUFFLER HAD BEEN REPAIRED 10 HOURS PRIOR TO THIS FLIGHT.SDR 99ZZZX2925Truss · wornCURING NLG INSPECTION, FOUND STEERING TRUSS BOLT HOLES ELONGATED WHERE OVERCENTER LINK BOLTS ONTO TRUSS; MFG SPECS FOR ALLOWABLE WEAR AT THIS LOCATION IS .375 INCH - .379 INCH. MEASURED WEAR WAS .392 INCH. REPLACED TRUSS WITH SERVICEABLE UNIT. SUSPECT WEAR SDR 99ZZZX2402Magneto · looseFOUND MAGNETO SEPARATED FROM ENGINE. HOLD DOWN BLOCKS WORE FLANGE DOWN. NEW LOCKING HARDWARE WAS INSTALLED PREVIOUSLY. SUBMITTER STATED THIS HAS BEEN FOUND ON 3 OTHER INSTALLATIONS OVER PAST 2 YEARS.SDR 20000713SH002Clutch · brokenAIRCRAFT OWNER REPORTED GEAR WILL NOT RETRACT, TRIPS CIRCUIT BREAKER. REMOVED JAMMED GEAR MOTOR ASSY, AND FOUND CLUTCH SPRING TAB BROKEN. SPRING WAS REPLACED 763 HOURS AGO IAW MOONEY SI M20-92 PER RECOMMENED REPLACEMENT SCHEDULE OF EVERY 1,000 HRS TIS. CAUSESDR 99ZZZX2025Fitting · crackedNOSE GEAR STARTED TO SHIMMY SEVERELY ON TAKEOFF ROLL. FOUND STEERING T-FITTING BROKEN OFF. FRACTURE OCCURRED NEXT TO WELD.SDR 99ZZZX1389Push Rod · failedTWO SEPARATE ENGINE FAILURES BEFORE CYLINDER REPLACED UNDER WARRANTY BY LYCOMING. SIGNIFICANT ALUMINUM FILINGS IN OIL SINCE REPLACEMENT.SDR 99ZZZX1079Blade · separatedPROPELLER BLADE SEPARATED AT APPROXIMATELY 2 INCHES FROM BUTT. AIRPLANE DAMAGE WAS SUBSTANTIAL. PILOT MADE A SUCCESSFUL OFF-AIRPORT LANDING. NTSB INVESTIGATION UNDERWAY.SDR AU990091Filter · failed(AUS) ENGINE AIR FILTER ASSEMBLY SCREEN BREAKING UP AROUND THE ATTACHMENT RIVETS. FILTER GASKET ALSO BROKEN WITH SMALL PARTS OF THE GASKET MISSING.SDR AU990054Frame · corroded(AUS) FUSELAGE TUBULAR FRAMES CORRODED EXTERNALLY. FOUND DURING INSPECTION IAW SB M20-208B. PART TC: 2,208.SDR 99ZZZX509Valve · failedDURING FLIGHT, OBSERVED HIGH OIL TEMPERATURE OF 230 DEGREES FAHRENHEIT, OAT MINUS 10 DEGREES CELCIUS. CHT NORMAL, OIL PRESSURE NORMAL. AFTER FLIGHT, OIL LEVEL 6-1/2 QUARTS, NORMAL. OIL COOLER APPEARED CLEAN, BUT COLD. REMOVED THERMOSTATIC BYPASS VALVE. CHSDR 99ZZZX592Magneto · wornTHE AIRCRAFT WAS FORCED TO MAKE AN OFF-AIRPORT GEAR UP LANDING IN A FIELD DUE TO A LOSS OF ENGINE POWER. SUBSEQUENT INVESTIGATION REVEALED THE ENGINE MAGNETO HAD EXCESSIVE WEAR ON THE CAM. THIS CAUSED IMPROPER POINT GAP CAUSING MAGNETO TO MALFUNCTION AND CRESDR 99ZZZX945Magneto · failedDURING CRUISE FLIGHT, THE ENGINE FAILED TO PRODUCE POWER DUE TO A TOTAL FAILURE OF THE DUAL MAGNETO. POST-ACCIDENT INVESTIGATION REVEALED BOTH THE LEFT AND RIGHT IGNITION POINTS OF THE BENDIX D4LN-300 DUAL MAGNETO WERE NOT OPENING. THE PLASTIC CAM FOLLOWERS SDR 98ZZZX4231Exhaust Valve · failedCYLINDER NR 4 EXHAUST VALVE STUCK OPEN ON TAKEOFF. AIRCRAFT RETURNED TO AIRPORT AND MADE A SAFE LANDING. UPON INSPECTION, THE CYLINDER'S NR 4 EXHAUST ROTATER CAP WAS FOUND IN THE BOTTOM OF THE ROCKER BOX. INSPECTED VALVE PER LYC SB 388B. CLEARANCE FOUND TOSDR 98ZZZX3879Vacuum Line · failedTHESE LINES ARE MADE OF SURGICAL TUBING AND CRACK AND ROLL AFTER A FEW YEARS. IN THIS CASE, OWNER STARTED AIRCRAFT AND NO VACUUM WAS AVAILABLE.SDR 98ZZZX3678Spark Plug · failedDURING THE COURSE OF AN ANNUAL INSPECTION, ALL BOTTOM PLUGS WERE FOUND TO HAVE CENTER ELECTRODE FAILURE. ALL CENTER ELECTRODES WERE FOUND WEAKENED AT THE CERAMIC AND BENT OVER TOWARD THE GROUND. SUBMITTER STATED CAUSE IS UNDETERMINED.SDR 99ZZZX68Actuator Arm · brokenDURING ANNUAL INSPECTION, THE ACTUATOR ARM FOR THE ALTERNATE AIR DOOR SWITCH WAS FOUND BROKEN. SIX HOURS AFTER THE NEW SWITCH ACTUATOR WAS INSTALLED, THE PILOT REPORTED THE ALTERNATE AIR LIGHT WAS ON. AFTER INVESTIGATING THE CAUSE OF THE LIGHT, DISCOVERED THSDR 98ZZZX3888Exhaust Valve · stuckCYLINDER NR 4 EXHAUST VALVE STUCK OPEN ON TAKEOFF. AIRCRAFT RETURNED TO AIRPORT, MADE SAFE LANDING. UPON INSPECTION, CYLINDER NR 4 EXHAUST ROTATER CAP WAS FOUND IN THE BOTTOM OF THE ROCKER BOX. INSPECTED VALVE PER LYC SB 388B. CLEARANCE FOUND TO BE SATISFASDR 98ZZZX3748Skin · looseDURING FLIGHT, FLAPS WERE MOVED FROM FULL DOWN TO APPROACH THEN TO FULL UP AT WHICH TIME A SPLIT FLAP CONDITION OCCURRED. UPON INSPECTION, IT WAS DETERMINED A SKIN SEAM WAS HANGING DOWN AND CATCHING ON THE FLAP SKIN PREVENTING IT FROM GOING FULL UP.SDR AU981116Suppressor · failed(AUS) ALTERNATOR NOISE SUPPRESSOR RFI (RADIO FREQUENCY INTERFERENCE) UNIT FAULTY.SDR CA980421022Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE FOUND WITH EXTENSIVE STONE/ROCK DAMAGE. THE BLADES WERE NOT REPAIRED.SDR 98ZZZX1590Tube Assy · brokenTHE PILOT REPORTED A ROUGH ENGINE AND MADE A PRECAUTIONARY LANDING. THE NR 1 CYLINDER FUEL INJECTOR LINE WAS BROKEN AT THE CYLINDER END. RAW FUEL WAS BEING SPRAYED ON THE ENGINE AS IT WAS RUNNING. THERE WAS NO FIRE. THIS IS A COMMON PROBLEM ON THIS INSTALLSDR 99ZZZX636Line · brokenTHE PILOT REPORTED A ROUGH ENGINE THAT RESULTED IN A PRECAUTIONARY LANDING. THE INITIAL INSPECTION REVEALED THE NR 1 CYLINDER FUEL INJECTOR LINE WAS BROKEN IN TWO AT THE NOZZLE END. THE FLIGHT SCHOOL OPERATES A FLEET OF 8 M20J AIRCRAFT. AD 93-02-05 IS ALWAYSSDR 98ZZZX1001Servo · corrodedCORROSION FOUND INSIDE FUEL INJECTOR SERVO DIAPHRAGM SECTION WAS IMPEDING MOVEMENT OF DIAPHRAGM RESTRICTING FUEL FLOW. SUBMITTER SUSPECTED WATER LAYING IN THIS AREA CORRODING SMALL SECTION OF INJECTOR HOUSING CAUSED GROWTH OF CORROSION DEPOSIT. LAB REPORT ON SDR 97ZZZX5211Control Link · brokenIN-FLIGHT FAILURE. OWNER-PILOT NOTICED SLOPPY AILERON RESPONSE, SAW RT AILERON 'VIBRATING', NOT RESPONDING TO CONTROL INPUT. RIGHT CONTROL LINK ROD ASSEMBLY LOCATED AT BELLCRANK BELOW CABIN FLOOR HAD BROKEN ALONG FACTORY WELD THEN THROUGH THE TUBING WALL. TSDR 98ZZZX2118Piston Pin · failedPISTON PIN BROKE IN-FLIGHT CAUSING MASSIVE DAMAGE INTERNALLY IN ENGINE. THE CRACKSHAFT AND ONE CYLINDER WERE THE ONLY ITEMS SALVAGEABLE. PILOT NOTICED ENGINE ROUGNESS AND LOSS OF OIL PRESSURE. AIRPLANE LANDED WITHOUT DAMAGE TO AIRCRAFT OR PILOT. ENGINE QUISDR CA971112003Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. STONE DAMAGE FOUND ON THE LEADING EDGES AND THE FACE OF THE BLADES. THE BLADES WERE REPAIRED AND ANODIZED.SDR 97ZZZX4672Push/Pull Tube · brokenDURING CONTROL CHECK JUST PRIOR TO TAKEOFF, NOTED THE RIGHT AILERON DID NOT MOVE. INVESTIGATION REVEALED THE PUSH ROD LOCATED IN THE BELLY OF THE AIRCRAFT WAS BROKEN AT A WELD WHERE PART HAS A 90 DEGREE BEND. THE BREAK WAS JUST AT THE EDGE OF THE WELD. IT ASDR CA970609029Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECITON. BLADE(S) FOUND CORRODED, BLADES WERE MACHINED TO REMOVE CORROSION. BLADE AND HUB WERE ANODIZED. ACTUATING PIN FOUND WORN, PIN WAS REPLACED.SDR 97ZZZX2794Starter · bolts looseTHE .3125 INCH HEAD MACHINE HARDWARE HOLDING THE STARTER MOTOR FORWARD CASE TO THE BODY HAS COME LOOSE LEAVING THE MOTOR ARMATURE IN FAILURE. THE LOC-TITE APPLIED TO THE THREADED HARDWARE SEEMS INAPPROPRIATE. SUBMITTER STATED SAFETY WIRE THE STARTER BODY HARSDR 97ZZZX2926Alternator · crackedFOUND ALTERNATOR HOUSING CRACKED AT THE FRONT MOUNTING ARM. AFTER INSPECTING LIKE AIRCRAFT, FOUND A SECOND ALTERNATOR CRACKED IN THE SAME LOCATION. THE SUSPECT CAUSE FOR THE CRACK IS INCORRECT SHIMMING OF THE ALTERNATOR TO THE MOUNT. SUBMITTER STATED CLOSE SDR 97ZZZX2941Valve · deformedAT 308 HRS SMOH, ANNUAL INSPECTION REVEALED NR 2 CYLINDER HAD NO COMPRESSION. CYLINDERS WERE ECI CERMINIL CYLINDERS. UPON REMOVAL, FOUND EXHAUST VALVE AND SEAT DEFORMED. NEW CYLINDER INSTALLED ALL OPS CHECK GOOD. 314 HRS SMOH, PILOT REPORTS AIRCRAFT SEEMS SDR 97ZZZX1973Wire · burnedWHILE TROUBLESHOOTING AND REPAIRING INOPERABLE PANEL LIGHTS, DISCOVERED NUMEROUS ELECTRICAL WIRES BURNED AND SHORTED. THE PANEL LIGHTS FAULT WAS WORN THROUGH INSULATION BY ADJACENT LIKE TYPE WIRES IN MID-HARNESS, WORN AND BURNED SEVERAL PLACES WITHIN THE HARNSDR 97ZZZX1957Wire · shortedWHILE TROUBLESHOOTING AN INTERMITTENT/UNCOMMANDED, ON OR OFF, OF THE AVIONICS MASTER RELAY - ELECTRICAL ARCING WAS HEARD. INVESTIGATION REVEALED ALTERNATOR OUTPUT 'A+' SHIELDED WIRE NR PA10A06 (BETWEEN FIRE WALL AND FORWARD END OF RF FILTER) HAD RUBBED THROUGSDR AU970281Valve · failed(AUS) NO3 CYLINDER EXHAUST VALVE HEAD FAILEDSDR 97ZZZX604Starter · bolts looseWHILE ATTEMPTING TO START A/C AFTER LANDING AND GETTING FUEL, PILOT REPORTED STARTER STOPPED WORKING AND MIXTURE CABLE WOULD NOT MOVE. FOUND STARTER HOUSING ATTACH BOLTS COMPLETELY SHEARED OFF AND MISSING ALLOWING STARTER TO REST ON MIXTURE CONTORL ARM AT FUESDR 97ZZZX437O-Ring · crackedDURING ANNUAL INSPECTION, A PRESSURE TEST OF THE ENGINE FUEL SYSTEM REVEALED A LEAK AT THE MIXTURE CONTROL SHAFT WHICH DRIPPED ON THE MUFFLER BELOW . REPLACEMENT OF O - RINGS 953516-10 AND 951401 CURED THE LEAK. SUBMITTER SUGGESTED CLOSE INSPECTION AND PRESSSDR 97ZZZX436O-Ring · crackedDURING ANNUAL INSPECTION, A PRESSURE TEST OF THE ENGINE FUEL SYSTEM REVEALED A LEAK AT THE MIXTURE CONTROL SHAFT WHICH DRIPPED ON THE MUFFLER BELOW . REPLACEMENT OF O - RINGS 953516-10 AND 951401 CURED THE LEAK. SUBMITTER SUGGESTED CLOSE INSPECTION AND PRESSSDR 97ZZZX823Crankshaft · brokenENGINE SEIZED IN-FLIGHT WITH NO WARNING (APPROX 5 SECONDS OF ROUGH OPERATION). PILOT MADE UNEVENTFUL LANDING IN THE FIELD. ENGINE WAS REMOVED AND DISASSEMBLED. CRANKSHAFT FOUND BROKEN IN TWO BETWEEN NR 3 AND NR 4 CONNECTING RODS. ENGINE INSPECTED FOR PROP SDR 97ZZZX29Mount Tube · broken tabDURING ANNUAL INSPECTION, FOUND RT HAND FORWARD EXHAUST MUFFLER SUPPORT TUBE BROKEN AT LOWER ATTACH TAB. THIS TUBE ASSY IS THE SAME ONE USED ON ROCKET ENGINEERING 305 - ROCKET CONVERSION ON M20K SERIES MOONEY. THIS TUBE IS OF THE NEWER HEAVY DUTY TYPE DESIGNSDR 96ZZZX5728Contact Points · failedENGINE QUIT DURING ROUTINE FLIGHT. REMOVED MAGNETO AFTER FORCED LANDING. FOUND CONTACT POINTS PITTED AN CAM FOLLOWERS WORN OUT TO THE POINT THAT THEY WOULD NO LONGER OPEN THE CONTACTS. SUBMITTER STATED MAGNETOS SHOULD BE INSPECTED ON 500-HOUR INTERVALS AND SDR 96ZZZX5567Valve · failed20 MINUTES INTO A FLT, THE OIL TEMP WENT FULL HOT. A CROSS CHECK OF INSTRUMENTS REVEALED ALL CYL TEMPERATURES NORMAL. THERE WAS NO LOSS OF ENG POWER, HOWEVER, OIL PRESS WAS LOWER THAN NORMAL. THE ONLY WAY TO LOWER THE OIL TEMP WAS TO REDUCE POWER AND PUT THESDR 96ZZZX5717Elevator · loose skinBOTH ELEVATORS ON THIS 1989 AIRCRAFT WITH ONLY 925 HRS HAVE LOOSE SKINS. THE RT ELEVATOR TOP SKIN IS LOOSE AT THE ROW OF RIVETS ALONG THE SPAR; THE LT ELEVATOR IS THE SAME EXCEPT THE BOTTOM SKIN IS LOOSE. THE BALANCE WEIGHTS AT THE ELEVATOR TIPS CAN BE FLEXESDR 96ZZZX5716Elevator · loose skinBOTH ELEVATORS ON THIS 1989 AIRCRAFT WITH ONLY 925 HRS HAVE LOOSE SKINS. THE RT ELEVATOR TOP SKIN IS LOOSE AT THE ROW OF RIVETS ALONG THE SPAR; THE LT ELEVATOR IS THE SAME EXCEPT THE BOTTOM SKIN IS LOOSE. THE BALANCE WEIGHTS AT THE ELEVATOR TIPS CAN BE FLEXESDR 96ZZZX5125Landing Light · wire chafedAN INSPECTION OF THE LANDING LIGHT CIRCUIT REVEALED THE WIRE FROM THE ENGINE COWL TO THE LIGHT CAME IN CONTACT WITH NR 1 CYLINDER EXHAUST STACK. THIS IS A RECURRING PROBLEM. THERE HAD BEEN A PREVIOUS REPAIR. THE PROBLEM AREA CAN BE VIEWED THROUGH THE RIGHT SDR 96ZZZX4065Connector · meltedDUE TO LARGE AMP DRAW, 34-PIN CONNECTOR IS MELTING. AT LANDING/TAXI, LIGHT PIN CONTACTS. SUBMITTER SUGGESTS REWIRING WIRES OUTSIDE CONNECTOR OR LARGER PINS FOR CONNECTOR. THIS IS SECOND AIRCRAFT IN FLEET TO HAVE THIS PROBLEM. M20J MODEL ACFT WITH WING MOUNSDR 96ZZZX4064Connector · meltedDUE TO LARGE AMP DRAW, 34-PIN CONNECTOR IS MELTING. AT LANDING/TAXI, LIGHT PIN CONTACTS. SUBMITTER SUGGESTS REWIRING WIRES OUTSIDE CONNECTOR OR LARGE PINS FOR CONNECTOR. THIS IS SECOND AIRCRAFT IN FLEET TO HAVE THIS PROBLEM. M20J MODEL ACFT WITH WING MOUNTSDR 96ZZZX3326Cylinder · crackedFOUR NEW LW-12993 CYLINDERS HAVE CRACKS AT THE ROCKER BOX DRAIN FITTING BOSS. THESE CRACKS OCCUR AT A CASTING FLAW. THIS MAY BE CAUSED BY THE TAPERED THREAD OF THE MS-20823-6D ELBOW FITTING.
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