Garrett TPE331-11U
Service difficulty reports · 625
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 = 'TPE33111U' 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 = 'TPE33111U' 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 CA970226069Bolt · sheared(CAN) DURING LEFT ENGINE MAINTENANCE THE BOLT FOR REAR ENGINE MOUNT WAS FOUND SHEARED OFF WITH WEAR TO ELASTOMER MOUNT SHANK. DELAMINATION OF ELASTOMER MOUNT ALSO FOUND.SDR CA970219006Control Cable · frayed(CAN) WHILE COMPLYING WITH FAIRCHILD 'B' INSPECTION, LEFT AILERON CONTROL CABLE WAS FOUND WITH THREE BROKEN STRANDS WHERE THE CABLE RUNS THROUGH THE PHENOLIC GUIDE BLOCK ATTACHED TO THE FUSELAGE BULKHEAD AT STATION 227-271. FAA AD 87-02-02 CALLS FOR CHECKS EVESDR CA970121011Bearing · rollers missing(CAN) OUTSIDE BEARING ON #2 MAIN WHEEL ASSEMBLY FAILED AND RESULTED IN WHEEL DEPARTING THE AIRCRAFT. THE BEARING ROLLERS LEFT THE BEARING CAGE ALLOWING THE WHEEL TO EXIT THE AXLE OVER THE SPACER, WASHER AND NUT. INNER BEARING WAS EXCESSIVELY WORN, THERE WAS STSDR MALA975284Clamp · looseFLT 3262 - DURING PREFLIGHT IN MSP, LEFT ENGINE DID NOT MAKE STANDARD POWER, 88 PERCENT TORQUE, 610 DEGREE MAX, NO BYPASS LIGHT, BUT FUEL LIMITED. MAINTENANCE TIGHTENED PRIMARY BLEED TUBE UPPER CLAMP. MAINTENANCE COMPLETED POWER CHECK BLEEDS, ON/OFF. OPS CHSDR CA970327029Housing · cracked(CAN) APPARENT EXCESSIVE FORCE ON OPENING DOOR CAUSED HOUSING TO CRACK.SDR 97ZZZM178Auto Ignition Sw · crackedOTZ-ANC - DURING CLIMB, THE CREW SMELLED BURNING OIL, IN COCKPIT. CREW ISOLATED IT TO THE LT BLEED AIR SYS AND SHUT IT OFF. ALSO, NOTED THE LT OIL PRESSURE DROPPING. CREW INITIATED A PRE-PLANNED ENG SHUTDOWN USING THE ABNORM CHECKLIST. AFTER THE ENG WAS SECSDR 97ZZZM177P2t2 Sensor · frozenLT EGT SLOWLEY INCREASED 70 DEG UNTIL THE CAPT TURNED ON THE ENG INLET HEAT, DUCT AND PROP HEAT. THE EGT DROPPED TO NORM. WHEN THE EGT STARTED TO RISE AGAIN AND THE PWR LVR HAD NO EFFECT ON THE DROPPING TQ, CAPT ELECTED TO SHUTDOWN THE ENG AS A PRECAUTIONARYSDR 97ZZZM176Engine · failedFLT 4060 - ON TRAINING FLIGHT, THE PILOT REPORTED A LOSS OF OIL PRESSURE ON THE RIGHT ENGINE. THE RIGHT ENGINE WAS SHUT DOWN AND SECURED IN FLIGHT. THE FLIGHT RETURNED TO AUS AND LANDED WITHOUT INCIDENT. THE ENGINE WAS REPLACED AND OPERATIONALLY CHECKED GOOSDR CA961216034Power Cable · severed(CAN) AS THE POWER LEVERS WERE ADVANCED FOR TAXI, THE RIGHT HAND ENGINE DID NOT RESPOND. INVESTIGATION REVEALED THAT THE CABLE ASSEMBLY ATTACHED TO THE PROP PITCH CONTROL HAD DETACHED DUE TO INTERNAL FAILURE AT THE ENGINE FIREWALL.SDR SWIA95777Retract Mech · out of adjustLT MAIN GEAR WOULD NOT RETRACT. JACKED A/C AND OPS CHECKED LANDING GEAR SYSTEM. ONLY FOUND FAULT WITH THE LT MAIN LANDING GEAR NOT FULLY ENGAGING IN UPLOCK HOOK. ADJUSTED LT MAIN ACTUATORS AS PER MM 32-00-00, ADJUST AND TEST OPS CKS GOOD AT THIS TIME.SDR SWIA95778Relay · failedBATT FAULT LIGHT ILLUMINATED INFLIGHT AND BOTH BATT DISC LIGHTS CAME ON. RESET BATTERIES AND SAME PROBLEM OCCURRED AGAIN. REPLACED BATT FEEDER FAULT RELAY, RAN ENGINES AND OPS CKS GOOD.SDR SWIA95773Uplock Roller · missingON GEAR RETRACTION RT MAIN INTRANSIT LIGHT WOULD NOT EXTINGUISH. FOUND UPLOCK ROLLER MISSING ON RT MAIN STRUT. INSTALLED NEW UPLOCK ROLLER AND TARGET, ADJUSTED UPLOCK SWITCHES TO TARGET, CYCLED GEAR NUMEROUS TIMES, OPS CKS GOOD MM 32-00-00.SDR COMA9620017Engine · failedRT ENGINE TORQUE ROLL BACK DURING TAKEOFF. REPLACED RT ENGINE.SDR MALA965171Compressor Seal · failedFLT 3094 - ON CLIMB-OUT FROM MSP, THE CREW NOTED A BAD ODOR FROM THE BLEED AIR SYSTEM AND A HAZE IN THE CABIN. THE AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT ENGINE COMPRESSOR SEAL. ALL CHECKS SATISFACTORY. (M)SDR QXEA9600439Bearing · failedDURING FLIGHT 19,000 FT WITH CLEAR CONDITIONS AND NO ICE, THE NR 2 ENGINE FLAMED OUT. NO ABNORMAL INDICATIONS PRIOR TO FLAME-OUT. AIRSTART WAS UNSUCCESSFUL, NO FUEL FLOW. AIRCRAFT MADE AN UNSCHEDULED LANDING IN FCA WITHOUT FURTHER PROBLEM. NR 2 ENGINE REPLSDR CA970421070Bearing · failed(CAN) AIRCRAFT HAD INTERMITTENT GENERATOR IN FLIGHT. GENERATOR REPLACED DUE TO BAD BEARINGS.SDR CA961120001Bearing · rough(CAN) DURING CLIMB AILERON SEIZED. AIRCRAFT RETURNED NO INCIDENT. BEARINGS IN ROLLER FOUND ROUGH AND REPLACED.SDR CA961216025Tube · leaking pinhole(CAN) DURING DI HYDRAULIC FLUID WAS NOTED SEEPING FROM THE LOWER OUTBOARD AREA OF THE CENTRE SECTION. THE LEFT HAND GEAR DOWN LINE WAS FOUND LEAKING FROM A SMALL PIN HOLE WHEN HYDRAULIC SYSTEM PSI WAS UP TO NORMAL OPERATING PRESSURE. TO FIND PIN HOLE THE PROTESDR SWIA95766Wire · failedLANDING GEAR WILL NOT RESPOND PROPERLY TO GEAR CONTROL INPUTS, WILL NOT FULLY RETRACT WITH SELECTOR UP. INTERMITTENTLY EXTENDED WITH GEAR CONTROL IN UP POSITION. LANDING GEAR CONTROL CIRCUIT BREAKER POPPED WHEN NOSE WHEEL STEERING SWITCH ARMED AND TESTED. RSDR COMA9620016Fuel Nozzles · malfunctionedLEFT ENGINE DOES NOT ACHIEVE REQUIRED TORQUE FOR TAKEOFF. REPLACED THE ENGINE FUEL NOZZLES.SDR SWIA95756Fire Light · shortedON CLIMBOUT, LEFT ENGINE FIRE LIGHT ILLUMINATED. FOLLOWED CHECKLIST, RETURNED TO LAX. FOUND FIRE PROBE TERMINAL ON LEFT ENGINE SHORTED AGAINST FUEL LINE. REPOSITIONED FUEL LINE AND PROBE AND INSULATED BOTH, OPS CHECK GOOD.SDR AU961116Pipe · corroded(AUS) HYDRAULIC PIPE LOCATED IN LH WHEEL BAY LEAKING AT 90 DEGREE BEND DUE TO CORROSION PITTINGSDR HKGA0012Scavenge Pump · failedAIRCRAFT WAS ON APPROACH WHEN RIGHT ENGINE OIL LIGHT CAME ON. PILOT CHECKED PRESSURE AND FOUND OIL PSI WAS LOW AND SHUT ENGINE DOWN WITH STOP AND FEATHER. LANDED WITH NO FURTHER PROBLEM. DRIVE GEAR ON THE TURBINE SCAVENGE PUMP SEARED APPROX 3 TEETH, CAUSINGSDR PNSA960728Engine · flamed outENGINE INLET BUILT UP ICE, INLET HEAT TURNED ON, ENGINE FLAMED OUT. AIR RESTART ACCOMPLISHED. LANDING UNEVENTFUL.SDR SWIA95752Strut · wornLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. INSPECTION OF AIRCRAFT DETECTED A FAULTY OUTBOARD GEAR SWITCH. REPLACED AND ADJUSTED PER 32-00-00, THE LEFT MAIN LANDING GEAR STRUT WAS IN NEED OF REBUILDING. REPLACED THE STRUT SEALS AND INSPECTED AIRCRAFT LANDSDR PNSA960718Fuel Control · out of adjustLOW POWER ON TAKEOFF. ADJUSTED MAX POWER, GROUND RUN AND FLT CHECK OK.SDR COMA9620010Fuel Nozzle · malfunctionedTAKEOFF ABORTED BECAUSE OF TORQUE ROLL BACK LT ENGINE. REPLACED THE LEFT ENGINE FUEL NOZZLES.SDR MALA965056Engine · failedFLT 3253 - EN ROUTE FROM GFK, THE RIGHT ENGINE FAILED. THE AIRCRAFT RETURNED TO GFK AND LANDED WITHOUT FURTHER INCIDENT. DURING THE POST FLIGHT, PROP AND FUSELAGE DAMAGE WAS ALSO NOTED. THE ENGINE WAS REPLACED. AN INVESTIGATION IS CONTINUING. (M)SDR AU960830Seat · broken(AUS) PASSENGER SEAT BACK BROKENSDR AU960833Indicator · fluctuates(AUS) LH ENGINE TORQUE INDICATOR FLUCTUATINGSDR AU960832Pipe · cracked(AUS) ENGINE EXHAUST SYSTEM SHORT PIPE CRACKED - HOT EXHAUST GASSES ACTIVATED FIRE WARNING SYSTEM AND FIRE BOTTLE WAS DISCHARGEDSDR SWHA96003Compressor Seal · cokedPILOT REPORTED ON SCHEDULED FLIGHT 432, FROM CRP TO AUS, APPROXIMATELY 20 MINUTES PRIOR TO LANDING 'EXHAUST FUMES IN CABIN AND COCKPIT, COMPLAINTS FROM CREW AND PAX'. INVESTIGATION REVEALED THE NR 2 ENGINE COMPRESSOR SEAL TO BE LEAKING. THE COMPRESSOR SEAL WSDR AU960964Cvr System · incorrect wired(AUS) COCKPIT VOICE RECORDER INCORRECTLY WIRED - RECORDS ONLY AREA MICROPHONE CHANNEL - PERSONNEL/MAINTENANCE ERRORSDR SWIA95739Propeller · malfunctionedHAD SMOKE IN CABIN AND COCKPIT SHORTLY AFTER TAKEOFF. COULD NOT ISOLATE. RETURNED TO SAN. REPLACED RIGHT ENGINE PROPELLER ASSEMBLY.SDR SWIA95733Lighting Panel · out of positionLANDING GEAR WOULD NOT RETRACT. CHECKED CIRCUIT BREAKERS, TRIED OVER RIDE, STILL WOULD NOT RETRACT. EMERGENCY VALVE WAS PINNED AFT. FOUND OVER RIDE BUTTON FOR GEAR HANDLE BINDING ON FROM LIGHTING PANEL CAUSING HANDLE NOT TO MOVE. REPOSITIONED FRONT PANEL, SDR MALA964977Engine · failedTOL/DTW - FLT 3328 - IN CRUISE FLIGHT, THE LEFT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFERENCE PROCEDURES. (X)SDR MEJA960302Fuel Control · defectiveABORTED TAKEOFF DUE TO LOSS OF POWER TO THE RIGHT ENGINE. REMOVED AND REPLACED THE RIGHT ENGINE FUEL CONTROL. GROUND RUNUP CHECK SHOWED ALL ENGINE PARAMETERS NORMAL, NO DISCREPANCIES. AIRCRAFT WAS RELEASED FOR A FUNCTIONAL CHECK FLIGHT, ALL PARAMETERS NORMASDR CA960328007Fcu · surging(CAN) POWER SURGING WHEN POWER LEVERS ADJUSTED. AIRCRAFT RETURNED TO BASE, SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT. FCU BELLOWS FOUND DAMAGED.SDR AU960465Switch · faulty(AUS) LH ENGINE BEGAN TO ROTATE RAPIDLY WHEN AIRCRAFT BATTERY SWITCHES SELECTED ON - SUSPECT INTERNAL SHORT ACROSS THE STARTER SWITCH CONTACTS CAUSED CONTACTS TO STICKSDR AU960327Plenum · cracked(AUS) RH ENGINE PLENUM CHAMBER CRACKED AROUND DRAIN FITTING TAKEOFF FLANGE - CRACK LENGTH 50.8MM (2IN) - RH ENGINE BLEED AIR TUBECHAFED AND LEAKING - PERSONNEL/MAINTENANCE ERRORSDR COMA9620004Nozzle · dirtyRT ENGINE WILL NOT ACHIEVE CHARTED TAKEOFF TORQUE. REPLACED THE ENGINE FUEL NOZZLES. POWER ASSURANCE RUNS NORMAL AND ACFT RETURNED TO SERVICE.SDR SWIA95721Control Cable · failedON TAXI IN FELT POP IN RUDDER PEDALS. ON FURTHER INSPECTION, FOUND THE RUDDER PEDALS NO LONGER MOVE THE RUDDER. REPLACED RIGHT AFT RUDDER CABLE. ADJUSTED TENSION, CHECKED RIGGING. OPS CHECKS GOOD.SDR COMA9620003Egt Compensator · out of adjustRT ENGINE TORQUE ROLLBACK FROM 87 PERCENT TO 82 PERCENT DURING TAKEOFF. RECALIBRATED THE EGT COMPENSATOR.SDR SWIA95718Line · failedCOMPLETE HYDRAULIC FAILURE, LEFT SYSTEM FIRST THEN COMPLETE PRESSURE LOSS. REPLACED DEFECTIVE HYDRAULIC PRESSURE LINE AT LEFT ENGINE FIREWALL AND SERVICED SYSTEM. SPRAYED DOWN SURROUNDING AREA AND RAN LEFT ENGINE TWICE, NO LEAKS NOTED. RESERVICED RESERVOIR SDR SWIA95715Red Gear Box · failedLEFT ENGINE FAILED IN FLIGHT, NO ABNORMAL INDICATIONS NOTED PRIOR TO EVENT. HOOKED UP FUEL GAUGE TO LEFT FUEL PUMP OUTPUT AND MONITORED ENGINE, NO FUEL PRESSURE REGISTERED. PULLED CHIP DETECTOR PLUG AND FOUND METAL ON PLUG. REMOVED OIL FILTER AND FOUND SUBSSDR CA960320020Diaphragm · broken(CAN)ON APPROACH WITH #1 POWER LEVER RETARDED TO FLIGHT IDLE, #1 ENGINE INDICATED 40 PERCENT TORQUE. IT TOOK ABOUT ONE MINUTE TO SLOWLY REDUCE TO ABOUT 20 PERCENT TORQUE. LEFT HAND FCU P3 DIAPHRAGM REPLACE D.SDR SWHA96001Wheel · defectiveSUMMARY REPORT OF FINDINGS OF TEAR DOWN REPORT OF SEIZED ENGINE, TEARDOWN OF HOT SECTION REVEALED FIRST STAGE TURBINE SHROUDS WERE WARPED AND ONE SHROUD HAD TIP CURL CAUSING THE SHROUD TO COME IN CONTACT WITH TURBINE WHEEL. SECOND STAGE TURBINE WHEEL COOLING SDR SWIA95712Hyd Line · failedTOTAL HYDRAULIC FAILURE OVER SMO. REPLACED NR 6 FLEX LINE FOR LEFT ENGINE HYDRAULIC PRESSURE WITH PRE-FABRICATED STAINLESS STEEL LINE. SERVICED RESERVOIR BLEED AIR FROM SYSTEM. RUN-UP AND LEAK CHECKS GOOD.SDR 96ZZZM638Bearing · failedDURING CRUISE FLIGHT, LEFT ENGINE FUEL CONTROL DRIVE GEARBOX BEARING FAILED.SDR CA960123015Lever Arm · loose nut(CAN)LOST ENGINE CONTROL WITH POWER LEVER. WHEN RETARDING POWER FOR LANDING, ENGINE REMAINED AT CRUISE POWER. ENGINE SHUTDOWN AND SINGLE ENGINE LANDING MADE. FOUND ARM SEPARATED FROM PROPELLER PITCH CONTRO L. NUT AND BOLT HAD COME LOOSE.
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