N3527U
Service difficulty reports · 24
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N3527U' AND registry_match = 'registration' 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 n_number = 'N3527U' AND registry_match = 'registration' 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 2010FA0000852Camshaft · corrodedEXCESSIVE CAM LOBE WEAR IS CAUSING POWER LOSS AND EARLY REMOVAL OF SEVERAL OF OUR ENGINES. THIS ENGINE WAS THE EARLIEST REMOVAL SO FAR, WITH 744 HOURS REMAINING UNTIL O/H. HAVE BEEN IN CONTACT WITH MFG TECH SUPPORT FOR AN EXTENDED PERIOD OF TIME NOW AND HAVE YSDR WVB2006F00002Oil System · unknownPILOT NOTICED RT ENGINE OIL PRESSURE DROP AFTER CLIMBING THRU 24000 FT. HE SHUT THE ENGINE DOWN AS A PRECAUTIONARY MEASURE. THE PILOT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE COMPLIED WITH A VISUAL CHECK OF THE ENGINE AND DID A FULL ENGINE RUN UP. THE SDR WVBA2002005Valve · leakingDURING SOME LINE MAINTENANCE, THE TECHNICIAN NOTICED FUEL STAIN FROM THE HEATER DRAIN. THE SOURCE WAS FOUND TO BE THE FUEL PRESSURE REGULATOR WHICH WAS LEAKING FROM THE LOWER PARTING SURFACE. THE UNIT WAS REMOVED AND REPLACED.SDR WVBA2001033Pump · leakingDURING INSPECTION IT WAS NOTICED THAT FUEL STAIN WAS ON THE BODY OF THE FUEL PUMP NEAR THE DRAIN COMING FROM THE PARTING SURFACE (LOWER) NOTE THIS IS A NEW STYLE PUMP DESIGNED TO RELIEVE THE LEAKING PROBLEM THE OLDER PUMPS HAD IN THIS AREA. THE PUMP WAS REPLSDR WVBA2001026Motor · failedPILOT REPORTED FLAPS STUCK IN DOWN POSITION, IT WAS DISCOVERED THAT THE FLAPS HAD STOPPED PRIOR TO HITTING THE DOWN LIMIT SWITCH AND WAS DETERMINED THAT THE MOTOR HAD BURNED OUT. THE UNIT WAS REMOVED AND REPLACED AND FLAP OPERATION APPEARED NORMAL.SDR WVBA2001016Camshaft · damagedDURING INSPECTION METAL CONTAMINATION WAS DISCOVERED IN THE OIL FILTER. A CHECK OF VALVELIFT WAS DONE AND IT WAS DISCOVERED THAT NR1 AND NR2 INTAKE LOBES WERE EXCESSIVE. NR1 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON THE CAM LOBES AND TAPPET FOLLOWERS. NOSDR WVBA2001008Regulator · leakingDURING ROUTINE INSPECTION REGULATOR WAS FOUND TO BE LEAKING FROM THE PARTING SURFACE. THE UNIT WAS REMOVED AND REPLACED.SDR 20010125CW004Valve · leakingDURING ROUTINE INSPECTION, FUEL WAS OBSERVED LEAKING FROM FUEL SOLENOID SHUT OFF VALVE. PART WAS REMOVED FROM SERVICE.SDR 20001016SH024Camshaft · damagedDURING INSPECTION, LOW CYLINDER COMPRESSION WAS DETECTED DURING THE COMPRESSION CHECK. THE CYLINDER WAS REMOVED AND A VISUAL INSPECTION PEFORMED ON THE CAMSHAFT. DETERMINED BOTH NR 3 AND NR 4 INTAKE LOBES AND TAPPET FACES WERE DAMAGED. SUBMITTER STATED THISSDR 20001016SH023Heater · leakingDURING ROUTINE INSPECTION, FUEL WAS OBSERVED DRIPPING OUT OF THE DRAIN OF THE FRONT JANITROL HEATER AND FUEL PRESSURE REGULATOR DRAIN. THE REGULATOR WAS REMOVED AND FUEL WAS NOTED LEAKING FROM WHERE THE POWER WIRE ENTERS THE UNIT.SDR WVBAO1399Seal · leakingDURING INSPECTION OF PROPELLER, RED HUB OIL WAS FOUND LEAKING FROM THE BASES OF ALL 3 BLADES. THE INSIDE OF THE SPINNER AND SPINNER BULKHEAD ALSO HAD A NOTICEABLE AMOUNT OF RED OIL ON THEM. THE PROP WAS WASHED DOWN AND THE ENGINE RAN FOR 5 MINUTES AND SHUT DOSDR WVBAD1499Seal · leakingDURING INSPECTION OF PROPELLER, RED HUB OIL WAS FOUND LEAKING FROM THE BASES OF ALL 3 BLADES. THE INSIDE OF THE SPINNER AND SPINNER BULKHEAD ALSO HAD A NOTICEABLE AMOUNT OF RED OIL ON THEM. THE PROP WAS WASHED DOWN AND THE ENGINE RAN FOR 5 MINUTES AND SHUT DOSDR 99ZZZX3485Regulator · leakingDURING ROUTINE INSPECTION, REGULATOR WAS FOUND LEAKING AT UPPER GASKET.SDR 99ZZZX2568Regulator · leakingPILOT REPORTED A DROP IN RIGHT FUEL PRESSURE WHEN HEATER WAS STARTED. FURTHER INVESTIGATION REVEALED FUEL LEAKAGE FROM HEATER FUEL PRESSURE REGULATOR AT UPPER SEAL.SDR 99ZZZX2320Camshaft · wornAT 100-HOUR INSPECTION, DISCOVERED FERROUS METAL CONTAMINATION IN FILTER ELEMENT. PERFORMED VALVE CLEARANCE CHECK AND FOUND NR 5, NR 6 INTAKE LOBBS WITH EXCESSIVE CLELARANCE BASED ON A SIMILAR CIRCUMSTANCE. IT WAS DECIDED TO REMOVE THE ENGINE FROM SERVICE FOSDR WVBA00799Regulator · leakingOIL WAS OBSERVED ON SIDE OF COWLING ON POST-FLIGHT AND IN THE BOTTOM OF COWL. ALSO, AFTER REMOVING COWL, OIL WAS OBSERVED COMING FROM AROUND THE THREADS OF OIL PRESSURE REGULATOR. REGULATOR WAS REPLACED. (X)SDR 99ZZZX1210Fitting · brokenON TAKEOFF, PILOT SELECTED GEAR UP. RED UNSAFE LIGHT REMAINED ILLUMINATED. PILOT RETURNED TO BASE, PUMPED GEAR DOWN BY HAND. LANDED WITHOUT INCIDENT. RIGHT MAIN INNER GEAR DOOR ACTUATOR UP-LINE FITTING WAS SNAPPED IN HALF. DURING GEAR INSPECTION, OBSERVATSDR 99ZZZX1398Flange · brokenTHE FLANGE SECTION OF THE HOUSING DESIGNED TO BE SECURED BY THE BOTTOM CLAMP, BROKE OFF DURING FLIGHT. MAGNETO CONTINUED TO FUNCTION NORMALLY, BUT PILOT REPORTED AN OIL LEAK IN THE RIGHT ENGINE, OBSERVED DURING WALK-AROUND AFTER LANDING. HOUSING SHOULD HAUL A SDR 98ZZZX4766Switch · failedWILL NOT TEST UP OR DOWN. AUTOPILOT WILL NOT ENGAGE.SDR 98ZZZX4764Switch · failedSWITCH INTERMITTENT, WILL TEST SUCCESSFULLY. REMOVED UNIT AND BENCH TESTED. DUPLICATED MALFUNCTION ON BENCH, BUT ONLY AFTER SUBJECTING UNIT TO A TEMPERATURE OF MINUS 12 DEGREES FAHRENHEIT FOR 3.75 HOURS.SDR 98ZZZX1052Switch · intermittentACCELERATOR SWITCH TESTS INERMITTENTLY IN AUTOPILOT SYSTEM ESPECIALLY IN COLD WEATHER.SDR 98ZZZX227Valves · pittedINSPECTION OF 6 NEW VALVES FOUND TWO OF THE VALVE STEMS WERE GENERALLY IN POOR CONDITION. FURTHER INSPECTION FOUND DEEP PITS AND SCRATCHES THAT APPEARED TO BE INCLUSIONS OR OTHER IMPURITIES.SDR 98ZZZX228Dist Block · wornINSPECTION OF MAGNETO DISTRIBUTOR BLOCK FOUND BUSHING WEAR AND WEAR DAMAGE TO LARGE DISTRIBUTOR GEAR.SDR 97ZZZX2875Spar · crackedAIRCRAFT ELEVATORS WERE OPENED UP IN C/W PIPER MANDATORY SB 998. THE LEFT ELEVATOR SPAR WAS FOUND CRACKED AT THE TIP AND FOUND CRACKED HALF WAY THROUGH THE SPAR JUST INBOARD OF THE VERY OUTBOARD ATTACH POINT. ELEVATOR SPARS NEED TO BE STRENGTHENED UP AT THES
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