Garrett TPE331-12UHR
Service difficulty reports · 287
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 = 'TPE33112UHR' 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 = 'TPE33112UHR' 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 AUS20040175Switch · faulty(AUS) NOSE LANDING GEAR SQUAT SWITCH FAULTY. INVESTIGATION FOUND THE CONTACTS HAD HIGH RESISTANCE.SDR AUS20040304Static Port · blocked(AUS) PITOT/STATIC INSTRUMENTS FAILED TO OPERATE FOLLOWING TAKEOFF. INVESTIGATION FOUND CLEAR PLASTIC TAPE OVER AFT STATIC VENT PORTS. TAPE HAD BEEN LEFT ON FOLLOWING PITOT/STATIC CHECK. PERSONNEL/MAINTENANCE ERROR.SDR AUS20040124Actuator · cracked(AUS) LT WING TRAILING EDGE FLAP ACTUATOR HOUSING CRACKED AND LEAKING FROM A HAIRLINE FRACTURE AT THE END OF THE HOUSING.SDR AUS20040144Governor · failed(AUS) LT ENGINE PROPELLER GOVERNOR FAILED. WORKSHOP INVESTIGATION AND DISASSEMBLY OF THE GOVERNOR FOUND A NUMBER OF FAULTS WITH THE UNIT, HOWEVER THE MAIN FAILURE MODE WAS DUE TO THE FLYWEIGHT HEAD ASSEMBLY MISSING ALL TRIGGER TEETH, CAUSED BY CONTACT WITH THSDR AUS20040089Propeller · faulty(AUS) LT AND RT PROPELLERS FAULTY. BOTH ENGINES OVERTEMPED.SDR AUS20031323Skin · cracked(AUS) RT ENGINE IB NACELLE SKIN CRACKED. STRINGER AND FORMER ALSO CRACKED.SDR AUS20031186Blade · unserviceable(AUS) LT ENGINE PROPELLER BLADE FAULTY. LIMITED INFORMATION PROVIDED.SDR AUS20031173Hose · burst(AUS) RT HYDRAULIC PUMP MAIN PRESSURE LINE FAILED. LOSS OF HYDRAULIC FLUID. BOTH HYDRAULIC PUMPS UNSERVICEABLE DUE TO LACK OF FLUID.SDR AUS20031192Case · cracked(AUS) LT FLAP ACTUATOR CASE CRACKED AND LEAKING.SDR AUS20031127Windshield · cracked(AUS) RT WINDSHIELD CRACKED.SDR AUS20031103Tire · punctured(AUS) RT MLG TIRE PUNCTURED ON LANDING.SDR AUS20031087Controller · faulty(AUS) CABIN PRESSURE CONTROLLER FAULTY.SDR AUS20031088Frame · cracked(AUS) CABIN BELT FRAME CRACKED. FOUND DURING INSPECTION IAW SERVICE LETTER CC7-SL-036.SDR AUS20031068Arm · cracked(AUS) LT WINDSHIELD WIPER PIVOT ARM LUG CRACKED FROM TOP RADIUS TO ATTACHMENT PIN HOLE. FOUND DURING INSPECTION IAW AD JETSTREAM 76AMDT1 AND SB 30-JA-95041.SDR AUS20030941Current Limiter · mismanufactured(AUS) CURRENT LIMITER INCORRECTLY ASSEMBLED CAUSING ARCING AT THE CONNECTION POINT. PERSONNEL/MAINTENANCE ERROR.SDR AUS20030920Altimeter · failed(AUS) PILOTS ALTIMETER FAILED. ALTIMETER HAD BEEN INSTALLED FOR 5.4 HOURS SINCE REPAIR.SDR AUS20030919Switch · faulty(AUS) LT HYD SYS LOW PRESSURE WARNING SWITCH FAULTY.SDR AUS20030928Plunger · fractured(AUS) RUDDER GUST LOCK PLUNGER BROKEN INTO TWO PARTS.SDR AUS20030992Gear · misrepaired(AUS) TACHOMETER GEAR HAD UNAPPROVED REPAIR CARRIED OUT IN THREADED AREA. LACK OF INTERFERENCE FIT BETWEEN GEAR AND BEARING PN 358272. PN 3103580-3 NR 2 IDLER GEAR HOUSING SUSPECT UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. UNAPPROVED REPAIRSDR AUS20030994Housing · wrong part(AUS) ENGINE IDLER GEAR HOUSING SUSPECT UNAPPROVED PART. HOUSING WAS A LOOSE FIT ONTO THE BACK OF THE DIAPHRAGM. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. SEE ALSO M OR D 03/0992 FOR ADDITIONAL INFORMATION.SDR AUS20030849Wire · chafed(AUS) EGT COMPENSATOR WIRE CHAFED ON PITOT/STATIC LINE LOCATED AT STN 145 LBL 90. CAUSED BY POOR INSTALLATION DURING COMPLIANCE WITH SB 77-JA910271. PERSONNEL/MAINTENANCE ERROR.SDR AUS20030831Cylinder · failed(AUS) RT MAIN LANDING GEAR OLEO FLAT. INVESTIGATION FOUND A FAILURE IN THE CIRCLIP GROOVE LOCATED IN THE LOWER CYLINDER ASSEMBLY.SDR CA030818002Stud · burned(CAN) DURING AN AREA INSPECT, MECHANIC NOTICED THAT GROUND STUD & WIRE FOR GROUND POWER RECEPTICLE APPEARED BURNED. ON INVEST FOUND CONNECTION LOOSE & FUSELAGE LUG, GROUND STUD & WIRE TERMINAL BURNED & OVERHEATED. ACCORDING TO PARTS LIST IN WIRING MANUAL GROUNSDR AUS20030728Nut · loose(AUS) LT ENGINE FIRE WARNING. THE ENGINE WAS SHUT DOWN AND THE FIRE EXTINGUISHER ACTIVATED. SUBSEQUENT INSPECTION COULD FIND NO EVIDENCE OF FIRE. PRELIMINARY INVESTIGATION SUGGESTS AN ENGINEANTI-ICE BLEED AIR LEAK. FURTHER INVESTIGATION FOUND THE NUT ON THE ENSDR AUS20030628Current Limiter · damaged(AUS) RT GENERATOR CURRENT LIMITER TERMINAL LOOSE. POOR CONNECTION CAUSED LOCALISED HEATING OF THE CURRENT LIMITER RESULTING IN A BURNING SMELL.SDR AUS20030563Attach Fitting · cracked(AUS) HORIZONTAL STABILIZER PITCH TRIM ACTUATOR RT ATTACHMENT FITTING OUTBOARD LUG CRACKED.SDR AUS20030675Structure · animal strike(AUS) AIRCRAFT HIT A KANGAROO DURING LANDING ROLL. INITIAL IMPACT APPEARS TO BE ON THE LT PROPELLER CAUSING SUBSTANTIAL DAMAGE TO THE PROPELLER. ANIMAL REMAINS WERE ALSO INGESTED INTO THE LT ENGINE. FOLLOWING THE IMPACT, THE KANGAROO WAS EJECTED FORWARD AND OVSDR AUS20030511Bulb · failed(AUS) LT MAIN LANDING GEAR DOWN INDICATOR BULBS BLOWN.SDR AUS20030442Impeller · damaged(AUS) LH ENGINE IMPELLER BLADES DAMAGED BY BIRDSTRIKE.SDR 03094311Connector · disconnectedDURING TAXI/GROUND HANDLING EMERGENCY TRACK LIGHTING INOPERATIVE ROW 2-4. MAINTENANCE PERSONNEL RESECURED CONNECTOR AT TRACK LIGHT. OPERATIONAL CHECK GOOD AND AIRCRAFT RETURNED TO SERVICE.SDR 03058311Light · inoperativeDURING PREFLIGHT INSPECTION THE FLIGHT CREW FOUND EMERGENCY TRACK LIGHTING BETWEEN ROWS 3A AND 4A. MAINTNANCE PERSONNEL PERFORMED OPERATIONAL CHECK OF EMERGENCY TRACK LIGHTING SYSTEM AND FOUND NO DEFECTS. AIRCRAFT RELEASED FOR CONTINUED SERVICE.SDR AUS20030217Panel · shorted(AUS) RT NON-ESSENTIAL BUS PANEL EMITTING SMOKE ODOR. INSPECTION FOUND A SHORT CIRCUIT CAUSING MELTING OF THE PLASTIC PANEL. SUSPECT SHORT CIRCUIT WAS CAUSED BY CONDENSATION ON THE PANEL DUE TO EXTREME WEATHER CONDITIONS.SDR 03049311Connector · looseEMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL RESECURED LOOSE CONNECTOR. OPERATIONAL CHECK GOOD AIRCRAFT RELEASED FOR CONTINUED OPERATION.SDR 2003F00221Line · leakingMWH - FLT 2569 - LEFT ENGINE OIL PRESSURE LIGHT CAME ON DURING CLIMB AT 18K MSL. CREW VERIFIED READING WITH OIL PRESSUE GAGE, WHICH READ 0 PSI. CREW SHUT DOWN LEFT ENGINE AT THAT TIME. LOST OIL PRESSURE DUE TO OIL LEAK. REMOVED LINE, LOOSENED ALL ATTACHINGSDR 2003F00223Line · crackedFLT 2580 - BIL - DURING DESCENT, CREW OBSERVED THE LEFT ENGINE OIL PRESSURE LIGHT CAME ON, THIS WAS VERIFIED BY LEFT OIL PRESSURE INDICATION LOW, CREW THEN SHUT DOWN LEFT ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. OIL LEAK IN PROP GOVERNOR AREA. REPLACEDSDR CA030108010Shaft · loose(CAN) DURING BRIDGING INSPECTION, FOUND THAT THE CO-PILOTS LT RUDDER PEDAL TORQUE SHAFT, TORQUE LEVER ASSY. VERY LOOSE. FASTENERS ATTACHING BOTH ASSY'S LOOSE AND ELONGATIN G TORQUE TUBE HOLES. VISUALLY INSPECTED AND REPAIRED ASSY'S AS REQUIRED. NEW OVERSIZE FASDR AUS20030002Line · broken(AUS) RT ENGINE FUEL BYPASS WARNING LIGHT ILLUMINATED. INVESTIGATION FOUND THAT THE FUEL LINE TO THE DIFFERENTIAL PRESSURE TRANSMITTER WAS BROKEN AT THE CONNECTOR END FITTING.SDR 02351311Light · looseDURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY FLOOR TRACK LIGHTING WAS INOPERATIVE AT SEAT ROWS 8 TO 10. MAINTENANCE PERSONNEL SECURED THE EMERGENCY FLOOR LIGHT STRIP. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TOSDR AUS20021381Engine · leaking(AUS) NR 1 ENGINE OIL LEAK FROM PROPELLER AREA. OIL FUMES IN CABIN. INVESTIGATION COULD NOT FIND THE SOURCE OF THE LEAKAGE AND AFTER CLEANING OF THE AREA NO FURTHER OIL LEAKS WERE EVIDENT.SDR AUS20021359Static Line · contaminated(AUS) STATIC LINE TO AIR DATA COMPUTER CONTAMINATED WITH WATER. EGPWS GAVE FALSE READINGS.SDR AUS20021264Seal · failed(AUS) LT ENGINE LOW OIL PRESSURE. INSPECTION FOUND AN OIL LEAK IN THE AREA OF THE TURBINE. INVESTIGATION FOUND THE CAUSE OF THE OIL LOSS TO BE TURBINE SEAL FAILURE. THE CARBON FACE OF THE SEAL HAD DISINTEGRATED AND THE BELLOWS RUPTURED RESULTING IN THE LOSS OFSDR AUS20021090Pipe · chafed(AUS) LT ENGINE DRIVEN HYDRAULIC PUMP ALUMINIUM SUPPLY LINE CHAFING ON A STAINLESS STEEL FUEL LINE. THE HYDRAULIC LINE CHAFED THROUGH RESULTING IN LOSS OF HYDRAULIC FLUID.SDR AUS20021091Pipe · loose(AUS) HYDRAULIC SYSTEM PIPE FROM FIREWALL DISCONNECTED. LOSS OF HYDRAULIC FLUID. PERSONNEL/MAINTENANCE ERROR.SDR AUS20021092Gcu · failed(AUS) LT GENERATOR CONTROL UNIT (GCU) FAILED. SUSPECT GCU FAILED DUE TO WATER INGRESS FOLLOWING ENGINE WASH.SDR AUS20021093Selector Valve · failed(AUS) EMERGENCY LANDING GEAR SELECTOR VALVE LEAKING. SUSPECT CAUSED BYINTERNAL SEAL FAILURE.SDR AUS20021110Line · cracked(AUS) FLAP "UP" HYDRAULIC LINE FLARED END CRACKED. LINE IS LOCATED INBOARD OF THE REAR LT NACELLE.SDR AUS20021023Structure · bird strike(AUS) BIRDSTRIKE ON RH HORIZONTAL STABILISER. EXTENSIVE DAMAGE CAUSED TO LEADING EDGE AND UPPER AND LOWER SKINS.SDR AUS20021022Governor · faulty(AUS) RT ENGINE PROPELLER GOVERNOR SUSPECT FAULTY.SDR AUS20020897O-Ring · leaking(AUS) RT PROPELLER BLADE O-RING SEAL STICKING. OIL LEAKING PAST THE SEAL ENTERED THE ENGINE AIR INTAKE AND FLOWED THROUGH THE RT BLEED AIR SYSTEM INTO THE CABIN.SDR AUS20020793Mount · burned(AUS) RT ENGINE UPPER MOUNT HEAT DAMAGED. HEAT DAMAGE ALSO FOUND ON HOSES PN SS1001K000312 AND PN SS1001F0000100. NO CAUSE OF DAMAGE WAS FOUND BUT IT IS SUSPECTED THAT A FUEL LEAK HAD OCCURRED AT THE NR 10 FUEL NOZZLE FITTING ALTHOUGH THE FITTING WAS FOUND TO
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