Piper PA46R-350T
Service difficulty reports · 19
Newest first. General aviation reporting is voluntary.
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 = 'PA46R350T' 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 = 'PA46R350T' 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 LF1RAUG26580MMTurbocharger · wornDURING THE ANNUAL INSPECTION, IT WAS NOTED THAT THE RT TURBOCHARGER HAD A LOOSE TURBINE HOUSING. THE TURBINE HOUSING EXHIBITED SIGNIFICANT PLAY WHERE IT MEETS THE CENTER BEARING HOUSING. IT APPEARS THAT THIS HAD BEEN GOING ON FOR SOME TIME. THE TURBINE HOUSSDR 2020FA0000384Landing Gear · failedMECHANICAL FAILURE OF THE NOSE GEAR ASSEMBLY, WHICH RESULTED IN AIRCRAFT NOT RESPONDING TO PILOT INPUTS UPON LANDING. THE LACK OF AIRCRAFT RESPONSE CAUSED THE AIRCRAFT TO EXIT THE PAVED RUNWAY SURFACE AND SKID TO A STOP APPROXIMATELY 100 YARDS IN THE GRASS. SDR V94R20200309001Tire · defectiveTIRE LOST AIR PRESSURE IN RUN-UP AREA, FOUND TIRE INTERIOR TO HAVE A DEFECT THAT CONTINUED TO CAUSE INNER TUBES TO SLOW LEAK. REPLACED TIER AND TUBE.SDR 6GTA201812110009Software · incorrectAIRCRAFT G1000 SYSTEM SHOWED VERSION 17, BUT THERE WAS NO LOG ENTRY FOR APPLICATION OF SERVICE LETTER 1194. A SOFTWARE MISMATCH ERROR WAS NOTED ON A GFC COMPONENT AT 3299 HOURS AND THAT ONE COMPONENT SOFTWARE WAS RELOADED AND ALL SYSTEMS APPEARED TO OPERATE NOSDR FE4R201801250001Skin · crackedFUSELAGE SKIN CRACKS BOTH SIDES OF COMMUNICATION ANTENNA MOUNTED ON TOP OF FUSELAGE BETWEEN FS 198.25-207.00, CRACKS THREE INCHES LONG. ANTENNA DOUBLER MULTIPLE CRACKS RADIATING FROM ANTENNA ATTACH HOLES.SDR 2017F00028Wastegate Valve · crackedMANIFOLD PRESSURE OSCILLATED UNCONTROLLABLY FOR 30 SECONDS. REDUCING POWER MAY HAVE STOPPED OSCILLATION. OCCURRED DURING CLIMB AFTER INITIAL POWER REDUCTION. NO FURTHER PRECAUTIONARY PROCEDURES REQUIRED DURING FLIGHT, EXCEPT TO HAVE THE ENGINE INSPECTED AS SDR LC1R20150414920Circuit Board · damagedWHEN SETTING UP FOR A LANDING APPROACH, THE PILOT NOTED THAT THE LG CB HAD POPPED & FURTHER NOTED THAT THERE WERE NO GREEN DOWN LIGHTS ILLUMINATED. THE PILOT PERFORMED AN EMER GEAR EXTENSION & DID A TOWER FLY BY TO VERIFY THE GEAR APPEARED TO BE DOWN. THE LASDR CA150508003Mount · broken(CAN) IT WAS NOTED WHEN APPROACHING THE AIRCRAFT IN ITS HANGAR PARKING SPOT. THE NOSE LANDING GEAR TRUNNION AND STRUT ASSEMBLY HAD A AFT FACING RAKE ANGLE (LESS THAN 90 DEGREES) AS NOTED FROM A DISTANCE. INVESTIGATION FOUND THE NOSE LANDING GEAR ACTUATOR RIGHTSDR 6GTA2015FA0000002Cylinder · separatedNR 2 CYLINDER SEPARATED FROM CRANKCASE AT THE MOUNTING BOLTS. ENGINE CONTINUED RUNNING AND SUBSEQUENT SHAKING BROKE EXHAUST MANIFOLD ON LT SIDE BETWEEN CYLINDERS AND TURBOCHARGER. NO HEAT DAMAGE TO SURROUNDING COMPONENTS NOTED PROBABLY BECAUSE AIRCRAFT WAS MSDR C41R201407310002Door · wornAIRCRAFT WAS UNDERGOING AN ANNUAL INSPECTION. DURING THE FUNCTIONAL CHECK OF THE ALTERNATE AIR SYSTEM THE TECH DISCOVERED LOOSE AND WORN ALTERNATE AIR COMPONENTS AT AIR BOX ASSY. NEW PARTS WERE INSTALLED AND SYSTEM RIGGED IAW MM. SYSTEM FUNCTIONED NORMAL. MASDR C41R201407310001Rod End · looseACFT WAS UNDERGOING AN ANNUAL INSPECTION. ON COMPLETING A FLIGHT CONTROL SYSTEM CHECK AND DISCOVERED THE RUDDER TRIM SYSTEM DID NOT FEEL AND FUNCTION AS NORMAL. AFTER FURTHER INVESTIGATION THE RUDDER TRIM WHEEL ACTUATOR ROD AND JAM NUT ASSY WERE FOUND LOOSE SDR C41R201402170001Coupling · looseAFTER FLIGHT, PILOT NOTICED OIL DRIPPING FROM ENGINE ASSEMBLY. AFTER FURTHER INVESTIGATION, OIL PRESSURE SWITCH SENDING UNIT LINE WAS FOUND INSTALLED FINGER TIGHT. REMOVED LINE AND EXAMINED FITTING AND LINE, REINSTALLED THE LINE AND COMPLETED ENGINE RUN PROSDR CA130318026Display · intermittent(CAN) PILOT REPORTS ON APPROACH, MULTI FUNCTION DISPLAY, MFD, FAILED WHEN PILOT CHANGED NAVIGATION MAP RANGE TO ZOOM IN ON ZONE. UNIT FROZE ON SCREEN AND REQUIRED CIRCUIT BREAKER TO BE PULLED AND RESET. UNIT REBOOT OF APPROXIMATELY 4 MINUTES WHILE IN FLIGHT.SDR 2012FA0000480Landing Gear · failedSB 1103D WAS 212 HOURS OVERDUE WHEN THE NOSE GEAR COLLAPSED AFTER LANDING CAUSING SUBSTAINTIAL DAMAGE TO THE AIRCRAFT.SDR 2011FA0000192Turbine Wheel · wornTURBOCHARGER WOULD NOT OBTAIN MANIFOLD PRESSURE AT CRITICAL ALTITUDE. TURBOCHARGER EXHIBITS NOTICEABLE RADIAL PLAY AND DRAGGING. THE COMPRESSOR OIL SEAL APPEARS TO BE DEFECTIVE. OIL IS BYPASSING THE SEAL BEING FORCED INTO ENGINE INDUCTION SYS. TURBINE WHEESDR 2010FA0000233Magneto · seizedDURING A POST MX RUNUP, THE ENG/ PROP CEASED TO ROTATE. THIS OCCURRED AT OR NEAR THE ENGINE IDLE SPEED SETTING (APPROX 850 RPM). INSPECTED ENG AND FOUND THE LT MAGNETO DISLODGED SLIGHTLY FROM ITS DRIVE PAD. REMOVED THE LT MAGNETO AND FOUND THE DRIVE ADAPTER SDR 2008FA0000295Cam · wornBREAKER CAM WORN BEYOND SERVICEABLE LIMITS, 49.9 HOURS SINCE NEW. TIMING HAD CHANGED CONSIDERABLY AND AIRCRAFT DIFFICULT TO START.SDR 2008FA0000294Cam · wornBREAKER CAM WORN BEYOND SERVICEABLE LIMITS, 49.9 HOURS SINCE NEW. TIMING HAD CHANGED CONSIDERABLY AND AIRCRAFT DIFFICULT TO START.SDR 2008FA0000293Cam · wornBREAKER CAM WORN BEYOND SERVICEABLE LIMITS, 49.9 HOURS SINCE NEW. TIMING HAD CHANGED CONSIDERABLY AND AIRCRAFT DIFFICULT TO START.
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