Garrett TPE-331-10UG
Service difficulty reports · 100
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 = 'TPE33110UG' 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 = 'TPE33110UG' 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 BMAC040015Warning Light · illuminatedLANDING GEAR INDICATE DOWN AFTER THE LANDING GEAR HANDLE GOES UP- LT SIDE. PERFORMED LANDING GEAR EXTENSION AND RETRACTION FUNCTION CHECK IAW MM. OPS CHECKED OK. (K)SDR BMAC040013Connector · looseSMOKE PRESENT IN COCKPIT WITH FLOWS ON. FOUND CONNECTOR ON LT OVERTEMP SWITCH TO BE LOOSE. RECONNECTED AND SECURED IAW MM. FUNCTIONAL CHECK GOOD.SDR CA041214005Bearing · leaking(CAN) OIL WAS FOUND LEAKING FROM THE AFT BEARING COVER, ENOUGH OIL WAS LEAKING WHICH ALLOWED A 4 INCH DIAMETER POOL OF OIL IN THE STUB PIPE.ENGINE TEAR DOWN STRIP REPORT WILL BE SENT IN.SDR BMAC040010Wire · brokenLT MLG IN TRANSITION LIGHT REMAINED ILLUMINATED IN FLIGHT. REPAIRED BROKEN WIRE ON LT MLG DOWNLOCK SWITCH. PERFORMED FUNCTIONAL TEST OF POSITION AND WARNING SYSTEM IAW J-31 MM 32-60-00, CHECKS GOOD.SDR CA041209010Shutoff Valve · failed(CAN) DURING START SEQUENCE THE ENGINE APPEARED TO START NORMALLY UNTIL STARTER DIS-ENGAGED THEN SHUT ITSELF DOWN. TESTING FOUND FUEL SHUTOFF VIBRATING LOUDLY WHEN POWER APPLIED WITH ENGINE STOP BUTTON. SUSPECT THE VALVE WAS TRYING TO BE OPEN ANDCLOSED AT THE SDR CA041015006Bulb · shorted(CAN) UPON COMPLETION OF ENG START & TURNING ON AVIONICS IN PREPARATION FOR DEPARTURE ON A CHARTER TRIP, CREW OBSERVED SMOKE COMING FROM THE RT AVIONICS. CREW SHUTDOWN ENGINES & MASTER SWITCH & DEPLANED ALONG WITH PAX. MX RESPONDED & AFTER LOCATING SOURCE OF SSDR CA041209009Wire · chafed(CAN) DURING CLIMB, POWER LOSS ON RT ENG AT A FREQ OF 1-2 MINS, A TOTAL OF 4 TIMES. DURING FINAL , LANDING & TAXI TO SHUTDOWN, ENG NORM. CHIP DETECTOR & FILTERS INSPD, NO FAULTS FOUND. FUEL PRESSURE OK. COMPLETE GROUND RUN PERFORMED WITH NO FAULTS. TEST FLT PSDR ZJ62004F00000Indicator · malfunctionedRT ENG TORQUE AND RPM DROPPED. TORQ FELL TO APPROX 10 PERCENT REGARDLESS OF PWR LEVER POSITION. EGT WAS FLUCTUATING BETWEEN 450 DEGREES AND 650 DEGREES C. ENG RPM THEN STABILIZED AT 96 PERCENT WHILE TORQ REMAINED AT 10 TO 20 PERCENT REGARDLESS OF PWR LEVER SDR CA040521003Transducer · malfunctioned(CAN) CREW REPORTED THAT ON TAXI FOR TAKE-OFF FOR THE SECOND FLIGHT OF THE MORNING THAT THE RT STALL SYSTEM WAS ACTUATED ON GROUND WITH STALL IDENT LIGHT RT ON AND CONTINUOUS STICK SHAKER IN FLIGHT CONTROL SYSTEM. UNABLE TO CANCEL. AIRCRAFT RETURNED TO BLOCKSDR CA040304011Maxaret · broken(CAN) AFTER A FLIGHT THE AIRCRAFT WAS BEING PULLED INTO THE HANGAR. AN AME WAS WALKING PAST THE AIRCRAFT AND NOTICED THE LT ANTI-SKID COVER WAS MISSING THE THREE RIVETS ON THE CASE. ON REMOVAL OF THE COVER THE COMPOSITE BLOCKS DESIGNED TO HOLD THE DRIVE PORTSDR CA040217013Combustion Liner · cracked(CAN) THE LT ENGINE WOULD NOT PRODUCE RATED POWER, IN FACT IT ONLY WENT TO 80 PERCENT. THE CREW ABORTED THE TAKEOFF ROLL AND RETURNED TO THE HANGAR. ON INVESTIGATION, A CRACK WAS FOUND ON THE LOWER CENTER OF THE COMBUSTION CASE. THE CRACK GOES AROUND AN UNUSESDR 54140Plenum · crackedFOUND CRACKED AT THE PRIMARY FUEL NOZZLE BOSS.SDR 54148Plenum · crackedFOUND CRACKED AT DRAIN BOSS.SDR 54140APlenum · crackedFOUND CRACKED AT DRAIN.SDR CA040121002Window · cracked(CAN) AC WAS IN LEVEL FLIGHT AT FL190. CABIN ALTITUDE WAS 5500 FT, NEAR MAX DIFFERENTIAL OF ABOUT 5.5 PSID. SLIGHT THUD WAS HEARD FROM PASSENGER COMPARTMENT. NO DECREASE IN PRESSURIZATION OR ANY OTHER WARNINGS. FLIGHT CONTINUED WITH NO PROBLEMS. PASSENGER SDR CA040109005Brushes · failed(CAN) AFTER PREVIOUS STARTER GEN FAILED. IT WAS REMOVED BECAUSE IT FAILED TO ROTATE ENGINE DURING START. REMOVED BRUSH COVER AND FOUND ONE OF BRUSH LEADS MELTED AND SMALL PIECES OF METAL FALLING OUT OF THE UNIT. TOOK PICTURES, SENT IT TO A THIRD PARTY FOR EVSDR 2004F00290Shutoff Valve · failedCREW REPORTED ON REPOSITION FLIGHT FROM MIV TO ACY, WHILE BEING VECTORED TO APPROACH IN HEAVY TURBULENCE AND RAIN THE LEFT ENGINE EXPERIENCED A LOSS OF POWER. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. UPON INVESTIGATION MAINTENANCE PERSONNEL REPLACED THE ENGINSDR CA040108001Brushes · damaged(CAN) BRUSH PIGTAILS WERE FOUND TO BE BADLY FRAYED, BRUSHES WERE DAMAGED. RETURNED UNIT FOR EVALUATION. ARMATURE FAILED, COMMUTATOR BARS LIFTED CAUSING DESTRUCTION OF BRUSHES AND DAMAGE TO 4 BRUSH SPRINGS. ARMATURE WAS SERVICEABLE AT TIME OF PREVIOUS O/H. CAUSDR CA040105003Door Frame · cracked(CAN) DURING ROUTINE INSPECTION, A .1250 INCH CRACK WAS FOUND IN THE CABIN DOOR FRAME AT THE UPPER FORWARD DRAW BOLT. THROUGH CONTACT WITH MFG AND OTHER LOCAL VENDORS, IT WAS DETERMINED TO BE MORE COST EFFECTIVE TO REPLACE THE ENTIRE DOOR ASSEMBLY RATHER THAN SDR CA031020011Case · cracked(CAN) A/C WAS APPROACHING AIRPORT WITH INTENTIONS TO LAND. RT ENG BETA LIGHT ON WITH OTHER ABNORMAL ENG INDICATIONS. A MISSED APPROACH INITIATED. RT ENGINE WOULD ONLY GENERATE 70 PERCENT TORQUE AND TEMPS AND FUEL FLOW WERE HIGH. PILOT IN COMMAND RETURNED TSDR 2003F00549Torque Ring · failedFLT 3525 - BGR - PILOT REPORTED AFTER TAKEOFF, NR 1 ENGINE TORQUE GAUGE BEGAN TO FLUCTUATE FROM 120 PERCENT OT 0 PERCENT. ENGINE BEGAN TO TTL DUE TO TORQUE READING. TTL WAS TURNED OFF AND ENGINE CONTINUED AND STABILIZED. THEN TORQUE GAUGE DROPPED TO 0 PERCESDR CA030618008Bypass Valve · intermittent(CAN) ON TAKE OFF, BOTH ENGS PRODUCED NORM TAKE OFF PWR AT 400 FT AGL, CAPT CALLED FOR CLIMB PWR, RT ENG POWER REDUCED TO 30 PERCENT TORQUE. A/C RETURNED TO LAND WITH RT ENG SHUTDOWN & RT PROP FEATHERED. MAINT RECEIVED A/C WITH RT PROP FEATHERED. PROP WASDR CA030407003Starter Gen · failed(CAN) AFTER START THE GENERATOR WOULD NOT COME ON LINE. TESTING REVEALED A FAILED TERMINAL END ON THE FIELD WIRE INSIDE THE GENERATOR.SDR BMAC030006SEngine · malfunctionedBWI - FLT 3103 - PILOT REPORTED LEFT ENGINE PRODUCES FULL POWER WHEN POWER LEVER IS AT STOP. RIGHT POWER LEVER AT STOP PRODUCES 92 PERCENT TORQUE, 530 DEGREES EGT AT 6,000 FEET, TEMP FOR ALT AND TEMP IS 560C. MAINTENANCE FOUND AIRCRAFT FUEL TANKS TO BE CONTASDR CA030708006Turbine Wheel · failed(CAN) ENG SUSPECT INTERNAL VIBRATION. SOURCE OF VIBRATION WAS 6, BROKEN BY STRESS RUPTURE, P/N 3101512-6 BLADES ON FIRST STAGE T-WHEEL ASSY. P/N 3101512-6 BLADES ARE NO LONGER BEING INSTALLED. IT IS NOTED THAT 6 P/N 3101512-6 BLADES WERE REPLACED DURING A PSDR CA030110004Bearing · seized(CAN) DEPARTURE FROM CYXD WAS NORMAL APART FROM LIGHT VIBRATIONS FROM NR 2 ENGINE. APPROXIMATELY 10 MIN. AFTER DEPARTURE NR 2 GEN INOPERATIVE LIGHT ILLUMINATED. RESET GEN SWITCH, IT DID NOT COME ON LINE, SO IT WAS TURNED OFF. THE VIBRATION GOT WORSE, ERRATIC SDR CA021223003O-Ring · broken(CAN) PROPELLER WAS LEAKING OIL OUT OF CYLINDER. TRAVELLED TO AIRCRAFT, FOUND PISTON TO CYLINDER SEAL, ITEM 40, IPL FIG 3, APPEARED TO BE TWISTED AND SPLIT. IT FELL OFF OF PISTON WHEN CYLINDER WAS REMOVED. REPLACED SEAL, REINSTALLED CYLINDER, NO LEAKAGE EVIDSDR CA030407002Seal · broken(CAN) AT DEPARTURE, CLIMBING TROUGH 2000 FT, SMOKE WAS NOTICED IN COCKPIT. RECIRCULATION FAN WAS CONFIRMED OFF, BOTH PRESSURIZATION FLOWS WERE TURNED OFF WHICH REDUCED SMOKE ENTERING COCKPIT. ON LANDING, REVERSE THRUST WAS ASSYMETRIC. AFTER SHUT-DOWN, LT ENGINSDR CA030103008Bearing · spalled(CAN) ON PREFLIGHT CHECK PILOT PULLED PROPELLER THROUGH BY HAND & NOTED UNUSUAL NOISE. THE PILOT THEN NOTIFIED MAINTENANCE ABOUT AFFECTED ENGINE. MAINTENANCE AME PULLED PROPELLER THROUGH BY HAND VERIFYING UNUSUAL NOISE AND CHECKED CHIP DETECTOR LIGHT WHICH WASSDR CA020404002Wire · broken(CAN) ON APPROACH THE PILOT NOTICED THAT THE NOSE GEAR WAS NOT INDICATING DOWN AND LOCKED. AFTER CYCLING THE GEAR WITH NO CHANGE IN THE INDICATION, A FLY PAST WAS CARRIED OUT TO DETERMINE THE GEAR STATUS. AFTER DECIDING THAT THE GEAR WAS LIKELY DOWN AND LOCKSDR CA011121007Line · broken(CAN) SHORTLY AFTER DEPARTURE FROM LA RONGE, SK, THE CREW NOTICED A HIGH ITT, A REDUCTION IN ENGINE POWER, FOLLOWED BY A BETA LIGHT AND LOW OIL PRESSURE LIGHT WARNING. THE CREW SHUT DOWN AND SECURED NR 2 ENGINE AND RETURNED TO LA RONGE. MAINTENANCE FOUND THAT SDR CA011210019Wire · broken(CAN) AFTER THE GEAR WAS SELECTED DOWN IT WAS NOTED THAT THE NOSE GEAR WAS NOT INDICATING DOWN AND LOCKED. THE LANDING WAS ABORTED AND A FLY-BY OF THE TOWER WAS CARRIED OUT OF FOR VISUAL CONFIRMATION THAT THE GEAR WAS DOWN. THE EMERGENCY SERVICES WERE REQUESTESDR CA011030006Housing · scored(CAN) WHILE IN CRUISE AT 18,000 FT, CREW EXPERIENCED LOSS OF POWER ON LT ENGINE. PRIOR TO LOSS OF POWER CREW DID NOT RPT ANY UNUSUAL IND.S. CREW FEATHERED & SECURED ENGINE & LANDED AT NEAREST AVAILABLE FACILITIES. MAINTENANCE REPORTED THAT ENGINE NOT SEIZED, SDR CA010822013Engine · damaged(CAN) ON LANDING IN FORT MCMURRAY ON THE MORNING OF 30 JULY, 01 AN UNCOMMANDED ENGINE SHUTDOWN OCCURRED. THE PILOT REPORTED THAT THE ENGINE SHUT DOWN WHEN THE WHEEL TOUCHED THE GROUND, OR SHORTLY THEREAFTER. HE PULLED THE STOP FEATHER LEVER FOR THAT ENGINE ANDSDR CA010711008Check Valve · cracked(CAN) PILOTS WERE NOT ABLE TO EXTEND LANDING GEAR. GEAR WAS PUMPED DOWN (EMERGENCY EXTENSION). AIRCRAFT LANDED WITHOUT INCIDENT. CHECK VALVE WAS FOUND CRACKED, ALLOWING FLUID TO EXCAPE SYSTEM. NO PHYSICAL DAMAGE THAT COULD CAUSE CRACK WAS EVIDENT. PART REPLACESDR CA010622035Door · bent(CAN) THE GEAR WAS SELECTED DOWN FOR LANDING. A VIBRATION WAS FELT AND THE AIRCRAFT DELVELOPED A SLIGHT YAW TO THE RIGHT. THE YAW WAS TRIMMED OUTAND THE LA NDING CONTINUED. AFTER LANDING IT WAS DISCOVERED THAT THE RT GEAR DOOR WAS HANGING LOOSE. ON INSPECTION SDR CA010219018Smoke Detector · failed(CAN) JUST AFTER TAKEOFF OUT OF LA RONGE HEADING NORTH APPROXIMATELY 80 MILES, THE BAGGAGE POD SMOKE ALARM WENT OFF. THE AIRSCREW TURNED AROUND, & DECLARED AN EMERGENCY TO LANDED BACK IN YVC. MAINTENANCE FOUND NO SMOKE OR FIRE IN THE POD. THE SMOKE DETECTOR WASDR CHQA20000019Fire Loop · malfunctionedLEFT FIRE DETECTOR INDICATION SYSTEM WOULD NOT TURN OFF. THE FIRE LOOP WAS REPLACED AND ALL INDICATIONS NORMAL.SDR CHQA20000014Master Cylinder · lowCAPTAIN REPORTED THE RT CAPTAINS BRAKE PEDAL HAD NO PRESSURE. MAINTENANCE INSPECTED THE SYSTEM, SERVICED THE BRAKE MASTER CYLINDER, BLED THE SYSTEM. OPS CHECKED OK.SDR CHQA20000012Connector · dirtyCREW RETURNED TO THE FIELD AFTER RIGHT ENGINE TORQUE AND FUEL FLOW FLUCTUATED DURING TAKEOFF. MAINTENANCE CLEANED THE CANNON PLUG TO THE STRAIN GAUGE, GROUND RAN AND TEST FLEW WITH NO FLUCTUATIONS NOTED.SDR CHQA20000013Harness · brokenCREW RETURNED TO THE FIELD AFTER THE LEFT ENGINE EGT STARTED TO FLUCTUATE. MAINTENANCE GROUND RAN WITH SRL OFF, NO FLUX NOTED. THE SYSTEM WAS DEFERRED. THE SYSTEM WAS INSPECTED AND FOUND A WIRE BROKEN AT THE ENGINE EGT SHORT LEAD. THE WIRE WAS REPLACED, ENSDR CHQA20000009Controller · failedEMERGENCY LIGHT OVER PASSENGER DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY POWER CONTROL. OPERATIONAL CHECKED NORMAL.SDR CHQA20000003Gauge · failedFLIGHT CREW RETURNED TO THE FIELD AFTER THE LEFT ENGINE EGT GAUGE INDICATION DROPPED TO ZERO. THE LEFT EGT GAUGE WAS REPLACED, GROUND RAN WITH ALL INDICATIONS NORMAL.SDR CA991208078Wire · broken(CAN) WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH, THE INTRANSIT AND GEAR DOWN LIGHTS FAILED TO ILLUMINATE. THE CREW FOUND THE GEAR INDICATION CIRCUIT BREAKER TRIPPED AND RESET IT, AT WHICH TIME THE LIGHTS OPERATED NORMALLY. MAINTENANCE TRACED THESDR CA991103023Switch · failed(CAN) GEAR WAS SLECTED DOWN ON APPROACH AND THE CREW FAILED TO GET A NOSE GEAR DOWN AND LOCKED (GREEN) LIGHT. GEAR IN TRANSIT (RED ) LIGHT REMAINED ILLUMINATED. AFTER A LOW PASS FOR GROUND OBSERVATION, THE AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE NOSE SDR CA991027072Fcu · failed(CAN) POWER SETTING COULD NOT BE ALTERED USING POWER LEVER. FCU CHANGED.SDR CA991007074Valve · cracked(CAN) ON APPROACH, FLAPS WERE SELECTED AND THE CREW NOTICED HYDRAULIC PRESSURE AT ZERO PSI. EMERGENCY GEAR EXTENSION WAS CARRIED OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE INVESTIGATED AND FOUND FLUID IN BELLY POD AREA AND DETERMINED IT TO BE COMING FROM THSDR AU990716Sensor · faulty(AUS) LEFT ENGINE T2/P2 SENSOR SUPECT FAULTY.SDR CA990719007Exhaust Stub · cracked(CAN) EXHAUST STUB WAS FOUND TO BE CRACKED 75 PERCENT AROUND CIRCUMFERENCE OF THE EXHAUST FLANGE. RECTIFIED BY IMPLEMENTATION OF SB 78-JM7799.SDR AU990266Bearing · failed(AUS) ENGINE ACCESSORY GEARBOX BEARING FAILED ALLOWING LOSS OF DRIVE TO THE FCU FUEL PUMP AND THE ENGINE OIL PUMP. PART TC: 18,523.
Back to Garrett TPE-331-10UG