Garrett TPE331-8
Service difficulty reports · 89
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 engine_model_key = 'TPE3318' 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 engine_model_key = 'TPE3318' 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 AUS20020027Hose · restricted(AUS) RT ENGINE OIL COOLER SCAVENGE HOSE INTERNALLY RESTRICTED. SUSPECT HOSE COULD HAVE BEEN KINKED DURING ENGINE INSTALLATION.SDR AUS20011439Housing · cracked(AUS) ENGINE OIL PUMP HOUSING CRACKED.SDR AUS20011384Exhaust Stack · cracked(AUS) ENGINE EXHAUST DUCT CRACKED AT AFT FLANGE ATTACHMENT WELD.SDR AUS20011224Housing · cracked(AUS) ENGINE OIL PUMP HOUSING CRACKED.SDR 2001FA0000543Rib · crackedDURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE LEFT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-1 (LCWS 26.85) HAD A VISUALLY SUSPECT AREA ALONG THE BEND RADIUS BETWEEN THE CENTER WING MAIN SPAR (FS 177.45) AND FS 188.95. FURTHER INSPECTION USING FLUSDR AUS20011135Bearing · failed(AUS) STARTER-GENERATOR BEARINGS FAILED.SDR CA010830007Starter Gen · failed(CAN) PILOT WAS TAXING WHEN HE LOST TOTAL POWER TO NO. 2 BUS. INVESTIGATION FOUND THAT THE R/H GENERATOR COOLING FAN BLADES TOTALLY CRACKED OFF AND FLEW INTO THE GENERATOR WINDINGS, DESTROYING ALL WORKING CAPABLITY OF STARTER GENERATOR. THIS CAUSED A GCU FAILSDR AUS20010858Switch · out of adj(AUS) NOSE LANDING GEAR ACTUATOR POSITION SWITCH INCORRECTLY ADJUSTED.PERSONNEL/MAINTENANCE ERROR.SDR AUS20010746Wheel · worn(AUS) MAIN LANDING GEAR WHEEL INNER HALF WORN IN BEARING BORE. BEARING SPINNING IN HUB.SDR AUS20010699Wire · broken(AUS) FLAP SELECTOR LOOM WIRE BROKEN FROM CRIMP TO FLAP MICROSWITCH.SDR AU010363Tire · leaking(AUS) LT MAIN WHEEL TYRE CONTAINED A SLOW LEAK FROM ONE OF THE SIDEWALL VENT HOLES.SDR AU010040Pin · cracked(AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED.SDR AU010020Pin · cracked(AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED. FOUND DURING INSPECTION IAW CESSNA SB CQB00-3.SDR AU001240Mount · broken(AUS) RT ENGINE INBOARD MOUNT BROKEN. ENGINE HAD DROPPED APPROXIMATELY38.1MM (1.5IN).SDR AU001258Wheel · broken(AUS) ELEVATOR TRIM WHEEL POINTER GROOVE BROKEN.SDR 20001011SH002Governor · malfunctionedPILOT REPORTED THAT AFTER ENGINE SHUT-DOWN OF A NORMAL FLIGHT, OIL WAS NOTICED LEAKING PROFUSELY FROM THE RIGHT COWLING. FURTHER INVESTIGATION REVEALED THE OIL LEAK WAS ORIGINATING FROM THE PROP GOVERNOR BASE FLANGE SEAM. IT WAS VERIFIED BY A MECHANIC THATSDR 20001011SH003Governor · malfunctionedA MECHANIC INSTALLED A NEW PROP GOVERNOR, P/N 897160-9, ON THE RIGHT ENGINE OF A CESSNA 441. WHILE PERFORMING ROUTINE GROUND RUNS AND LEAK CHECKS IT WAS NOTED THAT OIL WAS LEAKING FROM THE TORQUE MOTOR, SPECIFICALLY THE EXIT POINT FOR THE WIRES. GOVERNOR TIMESDR AU000984Turbine · overheated(AUS) LEFT ENGINE UNCOMMANDED TORQUE REDUCTION COUPLED WITH HIGH EGT INDICATION. HOT SECTION OVERTEMP DAMAGE. (X)SDR AU000462Seal · leaking(AUS) LEFT ENGINE CARBON SEAL ALLOWING OIL TO LEAK INTO THE BLEED AIR SYSTEM AND CONTAMINATE THE COALESCER BAG IN THE AIR CYCLE MACHINE. SMOKE IN THE CABIN.SDR AU000170Fcu · faulty(AUS) RT ENGINE FUEL CONTROL UNIT FAULTY.SDR PNSA000206Engine · lack of lubeDURING TAXI OIL PRESSURE INDICATED LOWER THAN NORMAL. RETURNED TO BLOCK. SERVICED OIL, OPS CHECKED OK.SDR CA991209048Relay · corroded(CAN) CREW REPORTED THAT THE LANDING GEAR WARNING SYSTEM WAS INTERMITTANT BOTH OPERATIONALLY AND DURING TEST. AFTER EXTENSIVE TROUBLESHOOTING, MAINTENANCE FOUND A FLASHER RELAY FOR THE LANDING GEAR WARNING CIRCUIT, LOCATED IN THE LEFT SIDE ELECTRICAL PANEL BESDR CA990907045Frame · cracked(CAN) FOUND LOWER DOOR FRAME CRACKED NEAR AFT HINGE ATTACHMENT.SDR AU990576Mount · cracked(AUS) LT ENGINE MOUNT ASSEMBLY CRACKED.SDR 99ZZZX2514Fuel Control · malfunctionedMANUAL MODE SOLENOID VALVE FAILED CAUSING AN UNCOMMANDED FUEL FLOW INCREASE TO THE RIGHT ENGINE. THE RESULTANT TORQUE INCREASE CAUSED THE AIRCRAFT TO VEER SLIGHTLY.SDR AU990849Vortex Generator · misinstalled(AUS) VORTEX GENERATOR KIT INCORRECTLY INSTALLED.SDR AU981189Truss · cracked(AUS) ENGINE MOUNT HORIZONTAL TUBE CRACKED AT UPPER LEFT ATTACHMENT POINT. CRACKING CONFIRMED USING DYE PENETRANT AND MAGNETIC PARTICLE INSPECTION. CRACK LENGTH APPROXIMATELY 9.525 MM (0.375 INCH). PART TC: 8,052.SDR AU981237Truss · cracked(AUS) ENGINE MOUNT DIAGONAL TUBE CRACKED AT LEFT UPPER ATTACHMENT POINT. CRACK CONFIRMED USING DYE PENETRANT AND MAGNETIC PARTICLE INSPECTION. CRACK LENGTH 9.525 MM (0.375 INCHES).SDR AU981204Wire · worn(AUS) LEFT ENGINE OIL PRESSURE LIGHT SIGNAL WIRE E120A20 INSULATION WORN THROUGH IN AN AREA LOCATED UNDER THE FLOOR BELOW THE PILOT'S SEAT.SDR AU980766Filter · contaminated(AUS) ENGINE OIL SYSTEM CONTAMINATED WITH METAL PARTICLES.SDR AU980902Filter · contaminated(AUS) RIGHT ENGINE OIL FILTER CONTAMINATED WITH METAL.SDR AU970710Computer · failed(AUS) ENGINE FUEL COMPUTER ELECTRONIC FAILURESDR AU970445Compensator · loose(AUS) LH ENGINE EGT COMPENSATOR CONNECTOR PLUG LOOSE AND CORRODEDSDR AU970379Fcu · malfunctioned(AUS) ENGINE FUEL CONTROL UNIT SUSPECT FAULTY - ENGINE SURGED AND EGT REACHED APPROXIMATELY 520 DEGREES C (OVERTEMP) - AN HOT END INSPECTION WAS CARRIED OUT WITH NO MAJOR DAMAGE FOUNDSDR AU970065Nozzle · leaking(AUS) FUEL NOZZLE BODY LEAKING - INVESTIGATION FOUND TWO PIN HOLES IN THE BODY BASE - NOZZLES WERE A NEW ITEMSDR AU961063Diffuser · bird strike(AUS) LH ENGINE SUFFERED BIRDSTRIKE - COMPRESSOR DIFFUSER VANE LEADING EDGES ROLLED BACK - BIRD REMAINS FOUND IN DIFFUSER, FUEL NOZZLES AND TURBINE EXHAUST PATHSDR AU961062Valve · faulty(AUS) RH ENGINE ANTI-ICE VALVE AND PLENUM DRAIN VALVE FAULTYSDR AU960206Blade · damaged(AUS) LH ENGINE 1ST STAGE IMPELLER DAMAGED - SECONDARY DAMAGE CAUSED TO 2ND STAGE IMPELLERSDR CA960304003Flash Tube · shorted(CAN) STROBE LIGHT FLASH TUBE INSTALLED, OVERHAULED AND FAILED WITHIN 7 HOURS OF USE. A SECOND FLASH TUBE ALSO FAILED WITHIN 39 HOURS OF USE.
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