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.

SDR AUS20040175Switch · faulty(AUS) NOSE LANDING GEAR SQUAT SWITCH FAULTY. INVESTIGATION FOUND THE CONTACTS HAD HIGH RESISTANCE.Mar 11, 2004 · Bag JETSTM3201 · Landing Gear Position and WarningSDR 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.Mar 10, 2004 · Swrngn SA227* · Pitot/Static SystemSDR AUS20040124Actuator · cracked(AUS) LT WING TRAILING EDGE FLAP ACTUATOR HOUSING CRACKED AND LEAKING FROM A HAIRLINE FRACTURE AT THE END OF THE HOUSING.Feb 24, 2004 · Swrngn SA227* · Trailing Edge Flap ActuatorSDR 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 THFeb 19, 2004 · Swrngn SA227* · Propeller GovernorSDR AUS20040089Propeller · faulty(AUS) LT AND RT PROPELLERS FAULTY. BOTH ENGINES OVERTEMPED.Feb 6, 2004 · Swrngn SA227* · Propeller AssemblySDR AUS20031323Skin · cracked(AUS) RT ENGINE IB NACELLE SKIN CRACKED. STRINGER AND FORMER ALSO CRACKED.Nov 26, 2003 · Swrngn SA227* · Nacelle/Pylon, Plate/SkinSDR AUS20031186Blade · unserviceable(AUS) LT ENGINE PROPELLER BLADE FAULTY. LIMITED INFORMATION PROVIDED.Nov 16, 2003 · Swrngn SA227* · Propeller Blade SectionSDR AUS20031173Hose · burst(AUS) RT HYDRAULIC PUMP MAIN PRESSURE LINE FAILED. LOSS OF HYDRAULIC FLUID. BOTH HYDRAULIC PUMPS UNSERVICEABLE DUE TO LACK OF FLUID.Nov 12, 2003 · Swrngn SA227* · Hydraulic System, MainSDR AUS20031192Case · cracked(AUS) LT FLAP ACTUATOR CASE CRACKED AND LEAKING.Nov 10, 2003 · Swrngn SA227* · Trailing Edge Flap ActuatorSDR AUS20031127Windshield · cracked(AUS) RT WINDSHIELD CRACKED.Nov 1, 2003 · Bag JETSTM3201 · Flight Compartment WindowsSDR AUS20031103Tire · punctured(AUS) RT MLG TIRE PUNCTURED ON LANDING.Oct 29, 2003 · Bag JETSTM3201 · TireSDR AUS20031087Controller · faulty(AUS) CABIN PRESSURE CONTROLLER FAULTY.Oct 25, 2003 · Swrngn SA227* · Cabin Pressure ControllerSDR AUS20031088Frame · cracked(AUS) CABIN BELT FRAME CRACKED. FOUND DURING INSPECTION IAW SERVICE LETTER CC7-SL-036.Oct 22, 2003 · Swrngn SA227* · Fuselage Main, FrameSDR 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.Oct 10, 2003 · Bag JETSTM3201 · Windshield/Door Rain/Ice RemovalSDR AUS20030941Current Limiter · mismanufactured(AUS) CURRENT LIMITER INCORRECTLY ASSEMBLED CAUSING ARCING AT THE CONNECTION POINT. PERSONNEL/MAINTENANCE ERROR.Sep 15, 2003 · Swrngn SA227* · DC Power Distribution SystemSDR AUS20030920Altimeter · failed(AUS) PILOTS ALTIMETER FAILED. ALTIMETER HAD BEEN INSTALLED FOR 5.4 HOURS SINCE REPAIR.Sep 11, 2003 · Swrngn SA227* · Altimeter, Barometric/EncoderSDR AUS20030919Switch · faulty(AUS) LT HYD SYS LOW PRESSURE WARNING SWITCH FAULTY.Sep 10, 2003 · Swrngn SA227* · Hydraulic Pressure SensorSDR AUS20030928Plunger · fractured(AUS) RUDDER GUST LOCK PLUNGER BROKEN INTO TWO PARTS.Sep 10, 2003 · Swrngn SA227* · Gust Lock Damper SystemSDR 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 REPAIRAug 20, 2003 · Swrngn SA227* · Turbine Engine Accessory DriveSDR 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.Aug 20, 2003 · Swrngn SA227* · Turbine Engine Accessory DriveSDR 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.Aug 19, 2003 · Bag JETSTM3201 · Engine Indicating System WiringSDR AUS20030831Cylinder · failed(AUS) RT MAIN LANDING GEAR OLEO FLAT. INVESTIGATION FOUND A FAILURE IN THE CIRCLIP GROOVE LOCATED IN THE LOWER CYLINDER ASSEMBLY.Aug 18, 2003 · Swrngn SA227* · Main Landing Gear Strut/Axle/TruckSDR 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 GROUNAug 18, 2003 · Frchld SA227DC · Electrical Power System WiringSDR 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 ENJul 22, 2003 · Swrngn SA227* · Engine Anti-Icing SystemSDR AUS20030628Current Limiter · damaged(AUS) RT GENERATOR CURRENT LIMITER TERMINAL LOOSE. POOR CONNECTION CAUSED LOCALISED HEATING OF THE CURRENT LIMITER RESULTING IN A BURNING SMELL.Jun 22, 2003 · Swrngn SA227* · DC Power Distribution SystemSDR AUS20030563Attach Fitting · cracked(AUS) HORIZONTAL STABILIZER PITCH TRIM ACTUATOR RT ATTACHMENT FITTING OUTBOARD LUG CRACKED.Jun 10, 2003 · Swrngn SA227* · Horizontal Stabilizer, Attach FittingsSDR 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 OVMay 29, 2003 · Swrngn SA227* · Fuselage Main, StructureSDR AUS20030511Bulb · failed(AUS) LT MAIN LANDING GEAR DOWN INDICATOR BULBS BLOWN.May 14, 2003 · Swrngn SA227* · Landing Gear Position and WarningSDR AUS20030442Impeller · damaged(AUS) LH ENGINE IMPELLER BLADES DAMAGED BY BIRDSTRIKE.Apr 28, 2003 · Swrngn SA227* · Turbine Engine Compressor SectionSDR 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.Apr 4, 2003 · N311UE · Jetair JETSTM4101 · Emergency LightingSDR 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.Feb 27, 2003 · N311UE · Jetair JETSTM4101 · Emergency LightingSDR 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.Feb 20, 2003 · Swrngn SA227* · AC Power Distribution SystemSDR 03049311Connector · looseEMERGENCY TRACK LIGHTING INOPERATIVE. MAINTENANCE PERSONNEL RESECURED LOOSE CONNECTOR. OPERATIONAL CHECK GOOD AIRCRAFT RELEASED FOR CONTINUED OPERATION.Feb 18, 2003 · N311UE · Jetair JETSTM4101 · Light System WiringSDR 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 ATTACHINGFeb 6, 2003 · N1119K · Frchld SA227DC · Turbine Engine Oil SystemSDR 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. REPLACEDFeb 1, 2003 · N1119K · Frchld SA227DC · Turbine Engine Oil SystemSDR 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 FAJan 7, 2003 · Bag JETSTM3212 · Rudder Control SystemSDR 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.Jan 1, 2003 · Swrngn SA227* · Engine Fuel Indicating SystemSDR 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 TODec 17, 2002 · N311UE · Jetair JETSTM4101 · Emergency LightingSDR 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.Nov 28, 2002 · Swrngn SA227* · Engine (Turbine/Turboprop)SDR AUS20021359Static Line · contaminated(AUS) STATIC LINE TO AIR DATA COMPUTER CONTAMINATED WITH WATER. EGPWS GAVE FALSE READINGS.Nov 23, 2002 · Swrngn SA227* · Pitot/Static SystemSDR 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 OFNov 2, 2002 · Swrngn SA227* · Turbine SectionSDR 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.Oct 2, 2002 · Swrngn SA227* · Hydraulic System, MainSDR AUS20021091Pipe · loose(AUS) HYDRAULIC SYSTEM PIPE FROM FIREWALL DISCONNECTED. LOSS OF HYDRAULIC FLUID. PERSONNEL/MAINTENANCE ERROR.Oct 2, 2002 · Swrngn SA227* · Hydraulic System, MainSDR AUS20021092Gcu · failed(AUS) LT GENERATOR CONTROL UNIT (GCU) FAILED. SUSPECT GCU FAILED DUE TO WATER INGRESS FOLLOWING ENGINE WASH.Oct 2, 2002 · Swrngn SA227* · AC RegulatorSDR AUS20021093Selector Valve · failed(AUS) EMERGENCY LANDING GEAR SELECTOR VALVE LEAKING. SUSPECT CAUSED BYINTERNAL SEAL FAILURE.Oct 2, 2002 · Swrngn SA227* · Landing Gear SelectorSDR AUS20021110Line · cracked(AUS) FLAP "UP" HYDRAULIC LINE FLARED END CRACKED. LINE IS LOCATED INBOARD OF THE REAR LT NACELLE.Sep 25, 2002 · Swrngn SA227* · Hydraulic System, MainSDR AUS20021023Structure · bird strike(AUS) BIRDSTRIKE ON RH HORIZONTAL STABILISER. EXTENSIVE DAMAGE CAUSED TO LEADING EDGE AND UPPER AND LOWER SKINS.Sep 11, 2002 · Swrngn SA227* · Horizontal Stabilizer StructureSDR AUS20021022Governor · faulty(AUS) RT ENGINE PROPELLER GOVERNOR SUSPECT FAULTY.Sep 6, 2002 · Swrngn SA227* · Propeller GovernorSDR 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.Aug 9, 2002 · Swrngn SA227* · Propeller Blade SectionSDR 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 TOJul 29, 2002 · Swrngn SA227* · Engine Mount Section
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