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 HKG2011F00001Bearing · failedDURING APPROACH, NR 1 ENGINE SHUTDOWN, INSPECTION DETERMINED LOSS OF DEDICATED DRIVE FOR OIL AND FUEL COMPONENTS. ENGINE DISASSEMBLY DETERMINED SPUR GEAR SHEARED FROM FAILED BEARINGS.SDR HKG2011F00002Bearing · failedDURING APPROACH, NR 1 ENGINE SHUTDOWN. INSP DETERMINED LOSS OF DEDICATED DRIVE FOR OIL AND FUEL COMPONENTS. ENGINE DISASSEMBLY DETERMINED SPUR GEAR SHEARED FROM FAILED BEARINGS.SDR 2011FA0000345Seal · cutTHE PROP DOME PISTON SEAL RUPTURED AND PUMPED OIL OUT OF THE LT ENGINE AND INTO THE ENGINE INLET CAUSING FUMES TO ENTER THE COCKPIT. THIS CAUSED AN INFLIGHT ENGINE SHUTDOWN, AND THE PILOT DIVERTED BACK TO DEPARTURE. ON 5-11-2011, DEPARTE WITH CARGO ABOARD THSDR 2011FA0000381Seal · rupturedTHE PROP DOME PISTON SEAL RUPTURED AND PUMPED OIL OUT OF THE LT ENGINE AND INTO THE ENGINE INLET CAUSING FUMES TO ENTER THE COCKPIT. THIS CAUSED AN INFLIGHT ENGINE SHUTDOWN, AND THE PILOT DIVERTED BACK TO DEPARTURE. ON 05/11/2011 DEPARTED WITH CARGO ABOARD, SDR CA110418010Bearing · failed(CAN) NR 1 GENERATOR WENT OFF LINE WHILE AIRBORNE. AFTER LANDING AND SHUTDOWN, STARTING ATTEMPT WAS UNSUCCESSFUL, ENGINE TURNED OVER VERY SLOWLY. GEN REPLACED. AMO FOR ST-GEN MAINTENANCE FOUND THE BEARING AT THE ANTI-DRIVE END HAD FAILED, ALLOWING THE ARMATSDR CA110412002Door Seal · contaminated(CAN) WHEN DE-ICE BOOTS WERE ACTIVATED DURING CRUISE AT 16,000 FT THE ACFT LOST PRESSURIZATION AND THE PRESSURE DIFFERENTIAL WENT TO "0". THE REMAINDER OF THE FLIGHT WAS CARRIED OUT AT 10,000 FT AND BELOW UNPRESSURIZED WITH THE DUMP SWITCH SET TO "DUMP" PASSSDR CA110407008Starter Gen · failed(CAN) THE LT GEN LIGHT FAIL LIGHT CAME ON DURING TAKEOFF ALONG WITH THE BATTERY FAULT & LT & RT BATTERY DISCONNECT LIGHTS. TROUBLESHOOTING IS BEING CARRIED OUT MORE TO REPORT AS FACTS ARRIVE. FOUND 2 SMALL E LEADS ON LT GEN HAVING RESISTANCE READING TO GND. SDR KY7A20110203Engine · failedE2 INDICATIONS WERE NORMAL DURING TAXIING OUT. AFTER ACFT GOT TO ABOUT 30 PERCENT TORQUE, HEARD A POP FROM THE RT SIDE OF THE AIRPLANE AND NOTICED THE RT SRL OFF LIGHT ILLUMINATE, SAW ENGINE SPOOLING DOWN. PULLED STOP & FEATHER, REDUCED POWER ON LT ENGINESDR CA110307002Windshield · cracked(CAN) AT 21000 FT DURING CRUISE, 20 MINUTES INTO FLIGHT DEPARTING BS RT WINDSHIELD OUTER GLASS PANE SHATTERED. ACFT DESCENDED, DEPRESSURIZED, TURNED AROUND AND CAME BACK TO BS.SDR LY02011F00000Packing · leakingACFT DURING ASCENT WITH ALTITUDE OF 6500 FT WAS EVIDENCE THE LOW OIL PRESSURE LIGHT ENG RT "TURN ON", AND THE OIL QTY INDICATOR TO ZERO. CABIN CREW AGREES TO SHUTDOWN THE RT ENGINE IAW THE PROVISIONS OF THE CHECKLIST " ENGINE FAILURE DURING FLIGHT". THE CONTSDR YLX2011F00000Cowling · departedAFTER TAKEOFF, ACFT LEVELED OUT AT APPROX 1800 FT, THE RT ENG UPPER COWLING DEPARTED THE ACFT DUE TO UNKNOWN CAUSE. LOWER COWLING REMAINED IN PLACE.SDR CA101206018Retainer · cracked(CAN) OIL LEAKING OUT OF NOSE CASE - UPON INSPECTION FOUND TO HAVE INITIATED FROM THE BOLT HOLE BOSS ON THE INSIDE DIAMETER. THE BOSS`S USUALLY HAVE RADIUS-ED CORNERS, HOWEVER, ON THIS EXAMPLE THE CORNERS ARE SHARP AND NOT RADIUS-ED. (TC# 20101206018)SDR CA101202004Windshield · crackedIN CRUISE THE CREW HEARD A LOUD BANG AND IMMEDIATELY NOTICED THE LEFT WINDSHIELD OUTER PANE HAD COMPLETELY CRACKED. THEY REQUESTED DESCENT, SLOWED THE AIRSPEED AND BEGAN TO DIAL UP THE CABIN TO REDUCE THE PRESSURE ON THE GLASS. THEY THEN REQUESTED A DIVERSIONSDR CA101116014Spar · cracked(CAN) AILERON REMOVED FOR SKIN CRACKING ON UPPER AFT SKIN OF OTBD HINGE. FURTHER INVESTIGATION REVEALED SEVERE CRACK IN THE SPAR WEB AS WELL ON THE UPPER HINGE BRACKET. THE RIB DIRECTLY BEHIND THE HINGE POINT WAS ALSO FOUND CRACKED. THE CRACK IN THE STRINGESDR KY7A16725Door Frame · crackedPILOT REPORTED ACFT NOT PRESSURIZING IN FLIGHT. THE LOWER FWD DOOR CORNER FRAME WAS FOUND TO BE CRACKED ALONG FWD END OF DOOR HINGE ATTACH RIVETS. THIS WAS THE THIRD FAILURE OF THIS THIS TYPE FOUND IN OUR FLEET. THE DOOR FRAME CORNER AND INTERCOSTAL WERE RESDR KY7AR4480Line · crackedON APPROACH FOR LANDING, THE RT ENGINE FLAMED OUT. AFTER INSP, A FUEL LINE PN 894568-1 BETWEEN THE FCU AND THE FUEL FLOW TRANSDUCER WAS FOUND CRACKED AT THE ATTACHMENT TO THE FUEL CONTROL. THIS IS THE SECOND FAILURE OF THIS LINE IN OUR FLEET. THE FUEL FLOW SDR CA101122014Gasket · failed(CAN) DATE OF OCCURRENCE: NOV 5, 2010 TOOK OFF ON A FREIGHT FLIGHT WITH A STOP TO DROP OFF TWO MECHANICS. (THE MECHANICS WERE GOING TO YRS TO DO SOME WORK DUE TO SOME HYDRAULICS ISSUES.) SHORTLY AFTER TAKEOFF, THE RIGHT WING OVERHEAT LIGHT CAME ON STEADY. PERSDR CA101022002Strut · fracturedLT MAIN GEAR LOWER STRUT TORQUE KNEE ATTACH BOSS FRACTURED AND SEPARATED FROM MAIN LOWER ASSY DURING TAXI CAUSING SEVERE SHIMMY.SDR CA101019009Screen · blockedDURING INTERNAL INSP OF ENG, A PIECE OF PLASTIC WAS FOUND IN THE OIL GALLEY BORE UNDER A NOZZLE. THIS PIECE OF PLASTIC WAS LARGE ENOUGH TO COMPLETELY BLOCK OIL PASSAGE AT THE NOZZLE SCREEN. THIS IS THE ONLY OIL SUPPLY TO THE MAIN PROPELLER SHAFT BEARING PN 3SDR CA101019008Actuator · seizedFLIGHT CREW REPORTED RUDDER TRIM WOULD NOT MOVE LT OF NEUTRAL. ACTUATOR REMOVED AND FOUND SEIZED. ACTUATOR REPLACED AND ACFT RETURNED TO SERVICE.SDR CA101019012Switch · burnedON APPROACH ALL PASSENGER READING LIGHTS CAME ON, DEADHEADING FLIGHT CREW IN REAR SEATS SMELLED SMOKE. SHORTLY AFTER LAV FIRE LIGHT CAME ON AND STAYED ON FOR 15 MINUTES. ACFT CONTINUED FLIGHT PLAN AND LANDED. MX FOUND INTERMITTENT READING LIGHT SWITCH WHEN SDR CA101014002Turbine Blades · cracked3101520-3 NR1 T-WHEEL COOLING HOLE CRACKS. REMOVED, WAS FORWARDED TO THE TURBINE SHOP FOR A SCHEDULED INSP. UPON TEARING THE ENG DOWN FOR INSP AND FORWARDING THE NR1 T-WHEEL TO THE NDT DEPARTMENT FOR THE FPI INSP. IT WAS NOTICED THAT ON THE VERY TIP OF THE RSDR CA100915003Switch · shortedCAWI SYS ACTIVATED IN FLIGHT UN-COMMANDED. FLIGHT CREW PULLED SYS CIRCUIT BREAKERS AND ENGINE PARAMETERS RETURNED TO NORMAL. CAWI CONTROL SWITCH FOUND SHORTING INTERNALLY-SWITCH REPLACED AND ACFT RETURNED TO SERVICE.SDR CA100811010Duct · crackedDURING MX FOR A HYD LEAK, THE LT COOLING TURBINE AND ASSOCIATED PLUMBING WAS REMOVED TO GAIN ACCESS TO THE FAILED HYD COMPONENT. UPON INSP OF THE BLEED AIR TUBE PRIOR TO INSTALLATION IT WAS NOTED THAT THERE WAS A CIRCUMFRENTIAL CRACK IN THE FLANGE WELD. THE CSDR CA100714004Retainer · crackedTHIS ACFT IS CURRENTLY UNDERGOING IMPORT INSPECTION. THE PART CYCLES AND TSO ARE BASED ON THE ASSUMPTION THAT THIS IS THE ORIGINAL PART FROM MFG. WHILE CARRYING OUT CABIN WINDOW FRAME FASTENER CORROSION INSPECTION, DURING ZONE 4, INSPECTION FOUND CRACK IN RTSDR 2010FA0000594Bearing · missingENGINE WAS REMOVED FROM ACFT FOR POSSIBLE OVERTEMP OPERATION. CUSTOMER REQUESTED TEST RUN TO NOTE CONDITION PRIOR TO DISASSEMBLY. HIGHT VIBRATION WAS NOTED FROM GEARBOX THAT INDICATED THE HIGH SPEED PINION. ENGINE GEAR BOX WAS DISASSEMBLED AND HIGH SPEED PSDR CA100528007Circuit Breaker · fod(CAN) ACFT TOOK OFF AND AFTER A SHORT PERIOD OBSERVED PROBLEMS WITH THE PRESSURIZATION, NOT PRESSURIZING, AND ELECTED TO SWITCH TO MANUAL AND NOTED THERE WERE NO PROBLEMS AFTER THAT. A SHORT TIME LATER DURING SOME TURBULENCE A LT AC BUS LIGHT ON THE ANNUNCIATSDR DUFA20100006Fuel Control · defectiveWHILE ON APPROACH, THE PILOT WAS INSTRUCTED BY ATC TO REDUCE POWER AND SLOW THE ACFT IN ORDER TO MAINTAIN SEPARATION. IN THIS ATTEMPT, HE WAS UNABLE TO GET THE RT ENGINE TO REDUCE POWER BELOW 54 PERCENT TORQUE INDICATION. HE DECLARED A MISSED APPROACH AND INITSDR CA100217002Indicator · inoperative(CAN) WHILE IN CRUISE FLIGHT THE CAPTAIN`S ATTITUDE INDICATOR FLAGGED. SHORTLY THEREAFTER AN ELECTRICAL SMELL WAS NOTED BY THE CREW FOLLOWED BY THE FACE OF THE INDICATOR FILLING WITH SMOKE. THE INDICATOR WAS ISOLATED BY PULLING THE CONTROL CIRCUIT BREAKER AND SDR CA100201004Actuator · binding(CAN) PITCH TRIM ACTUATOR FOUND TO BE BINDING AT THE FULL NOSE UP POSITION WHEN GOING FROM FULL NOSE UP TO NOSE DOWN AND MAKING A CLUNKING NOISE. NEW ACTUATOR IN SLATTED AND OLD ACTUATOR REMOVED FROM SERVICE AND ACFT RETURNED TO SERVICE (TC 20100201004).SDR HKGA01272010729CController · faultySINGLE PILOT, FAR 135 ON DEMAND CARGO CHARTER OPERATION, EMPTY LEG FROM SDF. DURING CLIMB THE LEFT ENG FIRE WARNING LIGHT ILLUMINATED STEADY. PILOT SHUT DOWN AND SECURED ENGINE, FIRE WARNING LIGHT WENT OUT, PILOT ELECTED TO FIRE THE LEFT ENG FIRE EXTINGUISHESDR CA100202003Actuator · malfunctioned(CAN) DURING INSP IT WAS NOTED THAT THE HORIZ STAB HAD EXCESSIVE PLAY AT THE L/E. WHEN THE FREE PLAY CHECK WAS CARRIED OUT ON THE ACTUATOR IT WAS NOTED THAT THE MEASUREMENT WAS .027 WHICH IS ABOVE THE MAXIMUM ALLOWED. UNIT REPLACED AND ACFT RETURNED TO SERVICESDR 2010FA0000073Valve · stuckDURING TESTING OF ENGINE P-44720 AFTER REPAIR DUE TO BIRD INGESTION, IT WAS NOTED THAT THE NTS SYSTEM WOULD NOT SET IAW MM 72-00-25 REV 13, DATED FEB. 13 2003. AFTER TROUBLESHOOTING, HAD FOUND THAT THE NTS VALVE WOULD NOT SET (STUCK CLOSED) CAUSING THE NTS SYSDR CA100126005Valve · unserviceable(CAN) PART FAILED DURING NTS SYS CHECK. AFTER ENG REPAIR DUE TO BIRD INGESTION, DURING ENGINE TEST, AN NTS SYS CHECK WAS ACCOMPLISHED AND THE NTS SYS DID NOT TRIP. THE NTS VALVE WAS REPLACED WITH A NEW UNIT AND THE NTS SYS WORKED PROPERLY. TTSN=1018.7 HRS.SDR CA100108003Windshield · delaminated(CAN) IN CRUISE THE CREW NOTICED SPARKS AND HOT GLOWING SPOTS ON THE F/O HEATED WINDSHIELD. MX NOTED A LARGE AREA OF DELAMINATION PRIOR TO REPLACING THE WINDOW.SDR CA091229001Windshield · cracked(CAN) IN MID-CRUISE AT FL220, THE CAPTAIN`S WINDSHIELD CRACKED. THE CREW DECENDED TO A100, SLOWED TO 190 AND DECREASED THE CABIN DIFF WINDSHIELD HEAT WAS ON HIGH AT THE TIME OF THE OCCURANCE. THIS WINDOW WAS IN SERVICE FOR A TOTAL OF 14 MONTHS.SDR CA100105001Circuit Breaker · overheated(CAN) ENGINE INSTRUMENTS FLICKERING ON/OFF WITH AN ARCING SOUND FROM LT ESSENTIAL BUSS TIE SWITCH UPON INSP FOUND THE PLASTIC BASE CRACKED AND ALSO EVIDENCE OF OVERHEATING WAS NOTED.SDR CA091216009Accumulator · low(CAN) AIRCRAFT RETURNED TO BASE AS THE LANDING GEAR WOULD NOT REMAIN UP AND LOCKED. MAINTENANCE INSPECTED AIRCRAFT AND ACCOMPLISHED GEAR SWINGS AND THE GEAR OPERATED NORMALLY. HYDRAULIC ACCUMULATOR WAS FOUND TO BE LOW AND THE PRESSURE WAS ADJUSTED TO MANUFACSDR CA091211010Switch · burned(CAN) BURNING SMELL COMING FROM BEHIND THE CAPT CHAIR THE LT ESSENTIAL BUSS TIE SWITCH WAS EXTREMELY HOT TO TOUCH. BURNING SMELL AND HOT, SWITCH REMAINED ON FOR DURATION OF THE FLIGHT. ON TAXI FROM APRON TO HANGER THE LT ESSENTIAL BUS TIE SWITCH WAS TURNED OFSDR CA091125004Turbine Blades · failed(CAN) A/C CAME IN FOR A ROUTINE FUEL NOZZLE CHANGE ON THE RT ENGINE. THE MECHANIC AT THAT TIME WAS DOING A SCHEDULED BOROSCOPE AND BEFORE PUTTING THE NEW FUEL NOZZLES IN HAD FOUND SOME DISCREPANCIES INSIDE THE ENGINE. THE MECHANIC THEN NOTIFIED THE TURBINE SSDR CA091113011Windshield · failed(CAN) ACFT TOOKOFF AND AFTER APPROX 15 MINUTES THE F/O WINDSHIELD OUTER PANE SHATTERED. ACFT WAS PRESSURIZED AND WINDSHIELD HEAT WAS ON. ACFT RETURNED TO BASE WITHOUT INCIDENT AND WINDSHIELD WAS REPLACED.SDR CA091030006Terminal · burned(CAN) LEVELING AT 16000 FT ON A DIRECT TRACK . IT WAS NIGHT AND CREW WERE IN IMC SINCE CLIMBING THROUGH ABOUT 1000 AGL. ALL ICE PROTECTION AND A MAJORITY OF INTERNAL AND EXTERNAL LIGHTING WAS ON. DURING LEVEL OFF F/O NOTICED A SUBTLE STRANGE ODOR IN THE COCKPISDR CA091005003Switch · intermittent(CAN) PILOT REPORTED THAT HE HAD A RED IN TRANSIT ON THE SELECTION OF GEAR DOWN. FLIGHT CREW DID 5 GEAR SWINGS AND ON THE LAST GEAR SWING THE IN TRANSIT LIGHT WENT OUT. THIS ACCOMPANIED BY THE FACT THAT THE FLIGHT CREW COULD SEE THE GEAR SWING UP AND DOWN IN TSDR CA090813013Bearing · failedGENERATOR WOULD NOT COME ONLINE. STARTER-GEN DISASSEMBLED. ARMATURE AND STATOR RUBBED. DRIVE END BRG HAS FAILED AND HAS ONLY 2 BALLS LEFT.SDR CA090715001Wire · burned(CAN) UPON ENGINE START ON GROUND CB`S POPED UPON 10 PERCENT ENGINE SPEED WHEN AUTO IGNITION CUT IN. THE WIRING AT THE STARTER WAS INSPECTED SERVICABLE. WIRING IN THE LT WING UNDER THE FAIRING HAD MULTIPLE BURNED WIRING. COMPANY IS NOW WORKING WITH M7 FOR OSDR CA090708007Oil Jet · broken(CAN) ACFT HAD LANDED AND WAS TAXING BACK TO HANGER WHEN RT ENG HAD SHUT ITSELF DOWN WITHOUT ANY INPUT FROM THE CAPTAIN. MAINT WAS NOTIFIED OF ISSUE AND WHEN TURNING THE PROP OVER BY HAND A LOUD CLICKING NOISE WAS NOTED. AT THAT TIME TURBINE SHOP WAS NOTIFIEDSDR CA090617007Plenum · cracked(CAN) WHEN ACFT WAS DOWN FOR HEAVY MX, MECHANIC HAD NOTICED THAT THE RT ENGINE HAD A CRACK ON THE PLENUM AROUND THE BLEED AIR PORT. ENGINE WAS REMOVED AND FORWARDED TO THE COMPANY’S ENGINE SHOP FOR REPAIR. PART WAS REPLACED AND ENGINE WAS REINSTALLED ON THE SDR CA090522004Landing Gear · malfunctioned(CAN) ON DESCENT, GEAR WAS SELECTED DOWN AND THE RT GEAR DID NOT EXTEND AND LOCK DOWN ON FIRST ATTEMPT. AFTER MULTIPLE ATTEMPTS ALL 3 GEAR EXTENDED AND WERE VISUALLY CONFIRMED DOWN AND LOCKED. CREW ELECTED TO FLY TO ANOTHER BASE FOR ADDITIONAL MX INSTEAD OF LASDR CA090519007Valve · stuck(CAN) DURING THE LANDING ROLLOUT, FLIGHT CREW ATEMPTED TO STEER ACFT USING NOSE WHEEL STEERING WHICH WAS UNRESPONSIVE. NOSE STEERING SYS INDICATED NO FAULTS AND ALL REQUIRMENTS NEEDED FOR NOSE STEERING FUNCTION WERE OBTAINED (IE GEAR DOWN, NWS ARMED, ETC). NOSDR CA090512003Engine · surges(CAN) DURING THE DESCENT, APPROX 30NM FROM AIRPORT, RT ENGINE SURGED, THEN LOST POWER COMPLETELY, NTS LIGHT ILLUMINATED. CONFIRMED WITH POWER LEVER (NO TORQUE MOVEMENT, NOR YAW). COMPLETED ENGINE FAILURE CHECKLIST, DECLARED EMERGENCY (TRUCKS WERE DISPATCHED).
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