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 = '152' 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 = '152' 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 95ZZZX4342Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4341Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4340Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4339Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4338Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4337Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4336Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4335Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4334Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4333Hub · crackedFOLLOWING THE DISCOVERY OF A PROPELLER WITH A HUB CRACK AT THE LEADING EDGE BOLT HOLE OF NR 1 BLADE, INSPECTION OF SAME PROPELLER MODEL ON OTHER 'N' NUMBERED AIRCRAFT WAS MADE. THE OTHER PROPELLERS' TIMES RANGED FROM 3,950 HRS TO 6,171 HRS, TT. ALL OF THE OLSDR 95ZZZX4428Push Rod · defectiveENGINE LOW STATIC. FOUND PUSH ROD WITH BOTH ENDS LOOSE AND TUBE MUSHROOMED. REPLACED PUSH ROD. INSPECTED ALL OTHER FOR PROPER ADJUSTMENT - OK.SDR BIER950018Seat Track · corrosionDURING COMPLIANCE WITH AD87-20-03 R2, FOUND SEVERE CORROSION IN/ON COPILOT RT OB SEAT TRACK TO APPROX HALF THICKNESS OF TRACK. CORROSION WAS PROGRESSING INTO FLOOR PAN.SDR 95ZZZX4181Pushrod · mushroomedCYLINDER NR 3 REMOVED FOR LOW COMPRESSION, FOUND EXCESSIVE CLEARANCE BETWEEN EXHAUST VALVE AND ROCKER ARM CAUSED BY PUSHROD THAT HAD MUSHROOMED UNDER BALL END.SDR 95ZZZX4332Hub · crackedA CRACK WAS FOUND IN THE HUB AREA. CRACK RADIATED FROM INSIDE THE HUB THROUGH THE FACE OF THE HUB TO THE MOUNTING SURFACE ENDING IN THE BOLT HOLE ADJACENT TO THE NR 1 BLADE. COMPLIANCE WITH MCCAULEY SB 169C AND AD 89-26-10 WAS ACCOMPLISHED AT 3229.7 TOTAL HOSDR 95ZZZX4314Resistor · not requiredMALFUNCTION OR DEFECT REPORT, FAA FORM 8010-4, WAS SUBMITTED TO FSDO WITH FOLLOWING STATEMENT: 'AFTER INSTALLING REPLACEMENT FUEL QUANTITY GAUGES AND TRANSMITTERS PER SK152-21A, THE TRANSMITTERS COULD NOT BE CALIBRATED, THE GAUGES READ FULL WITH TANKS LESS THSDR 95ZZZX3627Indicator · will not calibAFTER INSTALLING REPLACEMENT FUEL QUANTITY GAUGES AND TRANSMITTERS PER SK152-21A, THE TRANSMITTERS COULD NOT BE CALIBRATED, THE GAUGES READ FULL WITH TANKS LESS THAN HALF FULL. THERE IS A RESISTOR, PN 20 OHM 5W, INSTALLED BY THE FACTORY, AT THE TRANSMITTER, OSDR 95ZZZX4327Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4326Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4325Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4324Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4323Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4322Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4321Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4320Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4319Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4318Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4317Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4316Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR 95ZZZX4315Arm · wornDURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.SDR BIER950013Spring · brokenFOUND BROKEN RUDDER PEDAL RETURN SPRING (P/N 0310196-13), ON RT PEDAL, WHICH CAUSED PEDAL TO FALL TO FLOOR. SUBMITTER STATES BOTH SPRINGS SHOULD BE INSPECTED CLOSELY, ANNUALLY AND REPLACED AT 5 YEAR INTERVALS.SDR 95ZZZX3478Rib · crackedHORIZONTAL STABILIZER LEADING EDGE INBOARD. RIBS ARE BEING FOUND WITH CRACKS OR BROKEN TABS. DEFECT IS PRIMARILY FOUND ON RT SIDE PROBABLY DUE TO ELEVATOR TRIM BEING ON THAT SIDE. THIS IS A HIGH TIME AIRCRAFT USED IN A TRAINING FLEET.SDR 95ZZZX3477Rib · crackedHORIZONTAL STABILIZER LEADING EDGE INBOARD. RIBS ARE BEING FOUND WITH CRACKS OR BROKEN TABS. DEFECT IS PRIMARILY FOUND ON RT SIDE PROBABLY DUE TO ELEVATOR TRIM BEING ON THAT SIDE. THIS IS A HIGH TIME AIRCRAFT USED IN A TRAINING FLEET.SDR 95ZZZX3080Valve · crimp nut looseC/W SB 518C (LYC) CHECKED VERNATHERM NUT, FOUND LOOSE, NOT CRIMPED CORRECTLY. NEW PART ON ORDER. PREVIOUSLY FOUND 3 OTHER AIRCRAFT OUT OF 5 AIRCRAFT CHECKED WITH VERNATHERM NUTS LOOSE, AND THEY WERE REPLACED WITH NEW VERNATHERM VALVES AFTER INSPECTION TO C/WSDR 95ZZZX3239Pushrod · tip failedPUSHROD TIP SEPARATION. SECOND FAILURE ON THIS ENGINE. TOTAL TIME 6696. ENGINE TSMOH 366. REMOVED PN 73806. REPLACED WITH NEW PUSHROD PN 73806, REV A.SDR 95ZZZX5216Alternator · failedALTERNATOR FAILED IN-FLIGHT. ACFT LANDED AND REPLACED THE ALTERNATOR. NO OBVIOUS DAMAGE.SDR 95ZZZX3507Alternator · failedALTERNATOR FAILED IN-FLIGHT. LANDED AND REPLACED. NO OBVIOUS DAMAGE.SDR 95ZZZX2744Propeller · crackedDURING 100-HOUR INSPECTION, FOUND PROPELLER CRACKED AT MOUNTING BOLT HOLE. CRACK IS 2.50 INCHES LONG AND ON EITHER SIDE OF MOUNTING HOLE. MCCAULEY SB 169C COMPLETED JUNE 4, 1990. PROPELLER REPLACED WITH SERVICEABLE UNIT.SDR 95ZZZX3242Track · corrodedAIRCRAFT IS PRIMARILY A LINE TRAINER AND IS STORED OUTSIDE FOR MOST OF ITS SERVICE. CORROSION DEVELOPED BETWEEN FLAP ROLLER BUSHINGS AND TRACK SLOTS. SUBMITTER SUGGESTS KEEPING SLOTS CLEAN AND INSPECT REGULARLY.SDR 95ZZZX2191Cylinder · mismanufacturedNEW SUPERIOR CYLINDERS WERE INSTALLED AT ROUTINE OVERHAUL. AT FIRST OIL CHANGE, SIGNIFICANT AMOUNTS OF ALUMINUM WERE FOUND IN THE OIL FILTER. AFTER 5 MORE FLIGHT HOURS, THE FILTER WAS AGAIN INSPECTED, MORE ALUMINUM WAS FOUND. THE ENGINE WAS DISASSEMBLED ANDSDR 95ZZZX3498Elt · failedWHILE PERFORMING THE OPERATIONAL CHECK PER 91.207D, NO SIGNAL OUTPUT WAS NOTED EITHER BY USING THE G-SWITCH TEST OR IN MANUAL ACTIVATION.SDR 95ZZZX3497Elt · corrodedWHILE PERFORMING THE INSPECTION PER FAR91.207D, AN INSPECTION OF THE CASE REVEALED A CORRODED AREA AT THE END OF THE BATTERY SECTION. THIS CORROSION HAD EATEN ALMOST COMPLETELY THROUGH THE CASE.SDR 95ZZZX2186Cylinder · crackedCRACK FOUND DURING AN INSPECTION TO FIND AN OIL LEAK. LOCATION OF CRACK IS AT THE BOTTOM PORTION OF CYLINDER BARREL, 3.75 INCHES FROM BOTTOM OF FLANGE. THE CRACK IS APPROXIMATELY 2 INCHES LONG AND EXTENDS PARALLEL TO COOLING FINS.SDR 95ZZZX2109Switch · intermittentINTERMITTENT FAILURE OF IGNITION SWTICH CAUSING ENGINE TO FAIL GIVING INTERMITTENT MAGNETO DROPS UP TO 500-600 RPM.SDR 95ZZZX1982Valve · crimp nut looseCOMPLYING WITH LYCOMING SB 518A, CRIMP NUT WAS FOUND TO BE LOOSE AND NOT MEET CRIMP DEPTH SPEC.SDR 95ZZZX2551Hub · crackedPROPELLER TOTAL TIME: 5815.0. A CRACK WAS FOUND IN THE HUB AREA. CRACK RADIATED FROM INSIDE THE HUB THROUGH THE FACE OF THE HUB TO THE MOUNTING SURFACE ENDING IN THE BOLT HOLE ADJACENT TO THE NR 1 BLADE. COMPLIANCE WITH MCCAULEY SB 169C AND AD 89-26-10 WASSDR 95ZZZX1363Push Rod · brokenFOUND 1 BROKEN AND 3 OTHERS CRACKED. ALL DAMAGE ON END OF THE TUBE NEAR INSERT OPPOSITE END OF TUBE WHERE PART NUMBER IS LOCATED. AD95-03-10 PERTAINS TO ASSEMBLY NR 73806 AND 'V' OR 'W' REVISION. PART TT UNKNOWN.SDR 95ZZZX1359Valve · loose crimp nutWHILE COMPLYING WITH LYCOMING SB 518A, FOUND CRIMP NUT LOOSE AS SHOWN IN STEP 2 OF BULLETIN. SUBMITTER SUGGESTS CRIMP NUT LOOSE DUE TO POOR DESIGN.SDR 95ZZZX2068Bolt · nut missingOWNER COMPLAINED ABOUT LOOSE ALTERNATOR BELT. INSPECTED ALTERNATOR AND FOUND PIVOT BOLT NUT MISSING. REMOVED BOLT AND FOUND SEVERELY WORN. LINK AND ALTERNATOR HOUSING WORN FROM ASSY BEING LOOSE. REPLACED WITH NEW HARDWARE. MAY HAVE BEEN CAUSED BY LOCKNUT SDR 95ZZZX1463Float · filledNOTED FUEL DRIPPING FROM COWL. UNCOWLED AND FOUND FUEL LEAKING FROM CARBURETOR ENGINE RAN ROUGH AT LOW SPEEDS. PULLED CARBURETOR AND FOUND FLOAT FULL OF FUEL. REPLACED WITH NEW. HAD METAL FLOAT REPLACED 10-12-89 UNDER PRECISION SERVICE BULLETIN MSA-1.SDR 95ZZZX1280Coil · defectiveENGINE LOST 125 RPM IN-FLIGHT, LANDED WITHOUT INCIDENT, MAG CHECK REVEALED LT MAGNETO DEAD. TROUBLESHOT AND FOUND NO DEFECTS IN MAG AFTER DISASSEMBLY. REPLACED COIL AND RAN UP AND OPS CHECKED OKAY.
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