Garrett TPE331-10R
Service difficulty reports · 88
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 = 'TPE33110R' 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 = 'TPE33110R' 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 JTAA20260821001Engine · making metalNR 2 ENGINE FAILED IN FLIGHT. ON INSPECTION FOUND METAL PARTICLES IN OIL FILTER BOWL.SDR UATA2650406267901Oil Cooler · failedLEFT ENGINE OIL TEMPERATURE INCREASED TO REDLINE, PERFORMED PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED #1 OIL COOLER REF CASA MM 79-20-00 LEAK CHECK GOOD.SDR BIGA20260205001Flex Coupling · contaminatedTHE CREW WAS CONDUCTING A MAINTENANCE ACCEPTANCE FLIGHT ON AIRCRAFT FOR THE REPLACEMENT OF LEFT AND RIGHT PROPELLERS. THE NTS SHUTDOWN PROCEDURE WAS BEING PERFORMED IN-FLIGHT AS REQUIRED ON THE RT ENG. DURING THE NTS SHUTDOWN, THE RT PROPELLER DID NOT FULLY SDR 2025FA0000088Nut · failedTORQUE SENSOR ASSEMBLY [PN: 3101726-3, SN: P-8423, TSO: 3,059.5] HEXAGON PLAIN NUT [PN: 867349-1] BACKED OFF DURING FLIGHT.SDR 2025F00018Engine · flamed outDURING DESCENT, ENGINE FLAMED OUT @ 7000 FT MSL. THROTTLES @ FLIGHT IDLE, ENGINE NTS SURGING, EGT 428, RPM DROPPED TO 38%, INITIATED FEATHER OF ENGINE. SINGLE ENGINE LANDING UNEVENTFUL. CAUSE TBD.SDR JTAA202504290107Engine · flamed outDURING DESCENT, #2 ENGINE FLAMED OUT @ 7000 FOOT MSL, THROTTLES @ F.I. ENGINE NTS SURGING, EGT 428, RPM 38%, FEATHERED ENGINE. SINGLE ENGINE LDG UNEVENTFUL. CAUSE TBDSDR 2022F00329Engine · failedUNCOMMANDED RH ENGINE SHUTDOWN.SDR UATA202101073315Firewall · crackedNR 1 AND 2 ENGINE AFT SIDE OF FIREWALL LOWER DOUBLERS FOUND CRACKED NEAR OUTER EDGE OF BOTH LEFT AND RIGHT LOWER MOUNT FITTINGS. REPAIRED BOTH LT AND RT CRACKED DOUBLERS ON BOTH ENGINE FIREWALLS BY INSERTION OF NEW DOUBLER SECTIONS OF SIMILAR THICKNESS AND SISDR JTAA202007270001Engine · inoperativeDURING CRUISE FLIGHT, 50 MILES FROM HK01, #1 ENGINE FAILED. CREW PERFORMED APPROPRIATE EMERGENCY PROCEDURE, ANALYZED PERFORMANCE OF AIRCRAFT WITH ONE ENGINE AND ENTERED DESCENT, APPROACH, AND LANDING PHASES FOR SINGLE ENGINE LANDING. AIR RESTART WAS ATTEMPTED SDR BIGA20190721001Engine · malfunctionedRIGHT ENGINE SURGED, UP TO 100% AND COULD NOT BE REDUCED. CHIP DETECTOR LIGHT CAME ONE AND OIL PRESSURE WENT TO ZERO. PILOT FOLLOWED EMERGENCY PROCEDURES SHUT DOWN ENGINE AND RETURNED TO THE NEARBY AIRPORT. AFTER LANDING THE ENGINE PROPELLER COULD NOT BE ROSDR BIGA20170821001Line · crackedTHE PILOT REPORTED AN OIL LEAK AND FLUCTUATING OIL PRESSURE ON THE RIGHT ENGINE. MAINTENANCE FOUND THE ENGINE 4 QTS LOW ON OIL, CLEANED ENGINE AND COWLINGS, AND SERVICED ENGINE OIL. THE ENGINE WAS MOTORED AND A THE OIL LEAK WAS LOCATED ON THE .125 INCH STAINSDR 8EKA20170425001Compensator · failedCLIMBING THROUGH 4,500MSL, PILOT FELT NOTICEABLE YAW TO THE LEFT. PILOT NOTICED EGT HAD DROPPED TO 231 DEGREES. LOOKED OUTSIDE TO SEE IF THERE WAS ANY INDICATION OF FIRE, WHEN HE LOOKED BACK IN THE GAUGE, THE EGT HAD SPIKED TO 870. ANNOUNCED THE MALFUNCTION ANSDR BIGA20161206001Mount · crackedA VIBRATION WAS NOTED ON THE RIGHT PROPELLER DURING ENGINE RUN UP DURING MAINTENANCE, PROP DYNAMIC BALANCE WAS FOUND OUT OF LIMITS (2.5 IPS). THE PROPELLER WAS FOUND TO HAVE 3 BLADES SLIP IN THE CLAMPS CAUSING 2 BLADES TO BE OVER 1.5 DEGREES OFF FROM THE RESTSDR 2016F00121Bearing · migratedCOPILOT AILERON CONTROL ROD FOUND DISCONNECTED FROM INTERCONNECT BELLCRANK, DUE TO BEARING MIGRATION FROM ROD END. INSTALLATION DID NOT HAVE LARGE DIAMETER WASHER INSTALLED, WHICH ACTS AS A FAIL-SAFE TO THIS OCCURRENCE. OPPOSITE SIDE WAS INSPECTED & SOME PLASDR 39LA20151117147Landing Light · shortedON DEPARTURE, SMOKE NOTICED IN THE COCKPIT. DECLARED EMER & RETURNED. R & R LT LANDING LIGHT IAW MM 33-40-10.SDR 39LA20151015146Unknown · smokeDURING APPROACH, THE FLIGHT CREW SMELLED & OBSERVED A PUFF OF SMOKE THAT CAME FROM THE BOTTOM LT SIDE OF THE INSTRUMENT PANEL. NO ACTION WAS TAKEN AS LANDING WAS IMMINENT & A NORMAL LANDING WAS PERFORMED WITHOUT INCIDENT.SDR 39LA20150629137Skin · crackedLOWER WING SKIN CRACKED AT 2 PLACES, RT WING STATION 3500 & REAR SPAR. THE CRACKS ARE FROM FASTENERS TO EDGE OF SKIN. INSTALLED NEW PARTS IAW EO 15002-2001 REV V.SDR 39LA20150629138Skin · damagedHEAT CORROSION AFT OF NR 1 ENG EXHAUST AREA BOTTOM SKIN. REPAIRED IAW TECHNICAL INSTRUCTION NO 017 REV.SDR CA150416004Control Rod · bent(CAN) ANNUAL INSPECTION, LT WING, FOUND THE ACTUATING CONTROL ROD FOR FLAP SYSTEM, PN C3CF105-7 WAS BENT, DEFLECT .5", INSIDE WING, NEAR FUSELAGE, JUST BEHIND THE FIBER ROLLER APPROXIMATE 2", IN NORMAL OPERATION THIS SECTION DOESN`T TOUCH THE FIBER ROLLER, NO SDR 39LA20150326113Floorbeam · corrodedFLOORBEAM UPPER T CAP SHOWED EXFOLIATION CORROSION AT LT SEAT TRACK, FS 6250. REPLACED UPPER T CAP WITH SERVICEABLE IAW EO 14022-300 & DWG 14022-2008.SDR 39LA20150326114Threshold · corrodedLEFT AFT ENTRANCE DOOR THRESHOLD FOUND CORRODED. REPLACED WITH SERVICEABLE IAW EO14022-300 & DWG 14022-2017.SDR 39LA20150326115Skin · dentedMULTIPLE DENTS FOUND IN ACFT SKIN ON BOTTOM OF FUSELAGE. REPAIRED IAW EO 14022-300.SDR 39LA20150326116Stringer · corrodedLEFT WING CTR SECTION STRINGER FOUND CORRODED AT WING STATION 3296, THIRD STRINGER FWD. REPAIRED IAW EO 14022-300 SECTION 8 14.SDR 39LA20150326117Skin · corrodedLEFT LOWER WING SKIN EXFOLIATED AT WING STATION 2485. REPAIRED IAW EO 14022-300 SECTION 8 15.SDR 39LA20150326118Door Frame · puncturedAIRFRAME SIDE OF EMER ESCAPE HATCH FOUND PUNCTURED 1" FWD OF LOCK MOUNT HOLE. REPAIRED IAW EO 14022-300 & DWGS 14022-2004, 14022-2005, 14022-2006 & 14022-2007.SDR 39LA20150326119Skin · corrodedLEFT HORIZONTAL STABILIZER LE CORRODED UNDER DE-ICE BOOT. REPAIRED IAW EO14022-300 & DWG 14022-2009.SDR 39LA20150326120Skin · corrodedRIGHT HORIZONTAL STAB LE CORRODED UNDER DE-ICE BOOT. REPAIRED IAW DWG 14022-2010 & EO14022-300.SDR 39LA20150326121Skin · damagedAIRFRAME SKIN AT LT FWD ENTRY DOOR, FS 3150, STRINGER 16L, FOUND DAMAGED UPON INSPECTION. REPAIRED IAW DWG 14022-2001 & EO 14022-300.SDR 39LA20150326122Bushing · corrodedRIGHT ENG LOWER ATTACH FITTING BUSHING CORRODED. REPAIRED IAW DWG 14022-2013 & EO 14022-300.SDR 39LA20150326123Skin · crackedLEFT OTBD WING LE CRACKED AT WS 7700. REPAIRED IAW DWG 14022-2011 & EO 14022-300.SDR 39LA20150326124Mount · chafedNUMBER 1 ENG EXHAUST DUCT AFT INBD MOUNT FOUND CHAFED ABOVE & BELOW BASE OF MOUNT STUD. REPLACED WITH SERVICEABLE UNIT IAW MM.SDR 39LA20150326125Skin · crackedINSPECTION OF LT ELEVATOR REVEALED TWO SMALL CRACKS ON LE OF ELEVATOR. REPAIRED IAW DWG 14022-2016 & EO 14022-300.SDR 39LA20150326128Angle · crackedCRACK ABOUT 1/2 INCH ON ANGLE, INSIDE OF LT AILERON ABOVE ACCESS PANEL 540 EB.SDR 39LA20150326129Flap · dentedRIGHT INBD FLAP LE DENTED. REPAIRED IAW EO 14022-2018.SDR 39LA20150326130Flap · chafedRIGHT WING OTBD FLAP FOUND CHAFED & CRACKED UPON INSPECTION. REPAIRED IAW EO 14022-300 & DWG 14022-2002.SDR 39LA20150326131Frame · damagedFOUND OVERSIZED HOLE IN FRAME 18F, STRINGER 08, ON INSPECTION. REPAIRED IAW EO 14022-300 & DWG 14022-2012.SDR BIGA20150211001Fuel Control · failedTHE FUEL CONTROL UNIT , FCU, WAS SENT OUT FOR BENCH CHECK & REPAIR DUE TO A SUSPECTED FUEL FLOW PROBLEM. THE FCU WAS BENCH CHECKED & THE PROBLEM COULD IT WAS SLIGHTLY OUT OF RIG THAT MAY HAVE BEEN CAUSING A GOVERNOR INTERFERENCE PROBLEM. IT ALSO HAD THE DRIVSDR 39LA20140917100Frame · damagedDURING INSPECTION FOUND NR 6 LT & NR 6 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2013 & 14019-2014 INSTRUCTIONS.SDR 39LA20140917101Frame · damagedDURING INSPECTION FOUND NR 11 LT & NR 11 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2018 & 14019-2019 INSTRUCTIONS.SDR 39LA20140917102Mount Fitting · corrodedDURING NDT OF LT ENG MOUNT FITTING INSPECTION, FOUND AFT UPPER LT ENG MOUNT FITTING TO BE CORRODED. REMOVED UPPER ENG MOUNT FITTING PN 212-13116-01.2 & SENT OUT TO BE LOCALLY FABRICATED. WORK DONE IAW DWG 14019-2026.SDR 39LA2014090599Mount Fitting · corrodedFOUND CRACK INDICATION ON NR 1 ENG UPPER MOUNT FITTING ON LT WING FWD SPAR NEAR GROUNDING LUG. FURTHER INSPECTION FOUND TO BE LEVEL 2 CORROSION. PART TO BE REPLACED WITH SERVICEABLE.SDR 39LA2014082797Skin · crackedCRACK FOUND AT STATION 3950 RT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14019-2049 REV V1. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082798Skin · crackedCRACK FOUND AT STATION 3950 LT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14019-2049 REV V1. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082689Mount Bracket · corrodedDURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT UPPER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2027 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082690Mount Bracket · corrodedDURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT LOWER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2028 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082691Skin · dentedDURING INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER OTBD SKIN TO HAVE A DENT BEYOND LIMITS. FABRICATED SECTION OF SKIN USING ORIGINAL SKIN AS SAMPLE. MATERIAL USED .025 X 2024-T3 LOT 267230. ALL WORK DONE IAW EO 14019-300, REV V8 PAR 8 112. NO FURTHER ASDR 39LA2014082692Channel · corrodedLEFT SEAT TRACK SUPPORT HAT CHANNEL & SEAT TRACK FROM FS 3150 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT.SDR 39LA2014082693Channel · corrodedRIGHT SEAT TRACK HAT CHANNEL SUPPORT & SEAT TRACK FROM FS 2400 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT.SDR 39LA2014082694Skin · corrodedLEFT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED, REPAIR OF EXHAUST AREA THROUGH SKIN REPLACEMENT & DOUBLER PATCH.SDR 39LA2014082695Skin · corrodedRIGHT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED REPAIR OF EXHAUST AREA THROUGH SKIN REPLACEMENT & DOUBLER PATCH.
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