Garrett TPE331-12UAR
Service difficulty reports · 71
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 = 'TPE33112UAR' 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 = 'TPE33112UAR' 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 95ZZZM723Fcu · failedON APPROACH INTO CLT, THE LEFT ENGINE TORQUE, EGT, AND RPM DROPPED. CREW SHUT DOWN THE ENGINE WITH THE STOP AND FEATHER. AIRCRAFT LANDED WITHOUT INCIDENT. CHANGED LEFT FCU. THIS FCU HAS BEEN ON THIS ENGINE FOR 375.4 HOURS. (M)SDR 96ZZZX3725Blade · crackedENGINE DISASSEMBLY TO INVESTIGATE AND REPAIR TURBINE SECTION FAILURE REVEALED CAUSE TO BE FIRST STAGE ROTOR BLADE FAILURE. BLADE SEPARATED AT FIR TREE AIR PASSAGE. TURBINE SECTION COMPONENTS IN DOWNSTREAM GAS PATH EXPERIENCED SEVERE UNREPAIRABLE DAMAGE DUE TSDR WWMA9500075Fcu · defectivePILOT REPORTED IN CRUISE, THE RIGHT ENGINE HAD AN INTERMITTENT TORQUE FLUX OF 10 PERCENT AT 60 PERCENT TORQUE WITH A YAW AND CHANGES IN FUEL FLOW. ALL OTHER INDICATIONS WERE NORMAL. WHILE DESCENDING INTO LAX, TORQUE WAS BROUGHT BACK TO 20 PERCENT. THE RIGHTSDR WWMA9500067Monopole · intermittentDURING EN ROUTE PORTION OF FLIGHT, THE LEFT ENGINE TORQUE AND EGT DROPPED RADICALLY WITH THE POWER LEVERS MATCHED. CREW PERFORMED A PRECAUTIONARY LANDING IN SBP WITHOUT INCIDENT. DURING DEBRIEF THE CREW REPORTED THAT THE LEFT TORQUE HAD DROPPED 20 PERCENT. SDR 95ZZZX5842Seal · crackedPART REMOVED AT SCHEDULED INSPECTION, FOUND CRACKED AT FLANGE. SB TPE331-72-0840 AUTHORIZES INSTALLATION OF THIS PART TO INCREASE SEAL PLATE FLANGE PRESSURE AGAINST FIRST STAGE ROTOR. INCREASED PRESSURE CAUSES CRACKING AT SEAL FLANGE. THIS IS A CRITICAL LIFSDR 95ZZZX5844Seal · crackedDURING SCHEDULED INSPECTION, FOUND SEAL FLANGE CRACKED. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART WITH A SHIM TO INCREASE TENSION AGAINST 1ST STAGE ROTOR. INCREASE TENSION CAUSES CRACKING AT THE SEAL FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. SDR 95ZZZX5843Seal · crackedDURING SCHEDULED INSPECTION, FOUND SEAL CRACKED AT FLANGE. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO PROVIDE INCREASED TENSION AGAINST THE FIRST STAGE ROTOR. THIS INCREASED TENSION RESULTS IN CRACKING AT THE SEAL FLANGE. THIS IS A CRITICAL LIFE-LIMSDR 95ZZZX5859Seal · crackedDURING SCHEDULED INSPECTION, FOUND SEAL CRACKED AT FLANGE. SB TPE331-72-0840, AUTHORIZES INSTALLATION OF THIS PART TO INCREASE SEAL PLATE TENSION AGAINST 1ST STAGE ROTOR ASSEMBLY. INCREASED TENSION ON THE SEAL FLANGE RESULTS IN CRACKING AT THE FLANGE EDGE. SDR 95ZZZX4607Seal Plate · crackedDURING INSPECTION/REPAIR FOR LOW POWER, FOUND SEAL PLATE CRACKED. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO INCREASE SEAL PLATE TENSION AGAINST FIRST STAGE ROTOR ASSEMBLY. INCREASED TENSION ON THE SEAL FLANGE RESULTS IN CRACKING AT THE EDGE PROPOGATSDR 96ZZZX567Engine · seizedBNA - FLT 4539 - PILOT REPORTS: ON TAKEOFF, THE LEFT ENGINE FIRE WARNING LIGHT ILLUMINATED FOLLOWED BY A LOUD NOISE FROM THE LEFT ENGINE. DISCHARGED ENGINE FIRE BOTTLES AS A PRECAUTIONARY MEASURE. CREW ABORTED TAKEOFF. AS THEY WERE RETURNING TO THE GATE, TSDR 96ZZZX568Engine · failedBNA - FLT 4539 - PILOT REPORTS: ON TAKEOFF, THE LEFT ENGINE FAILED, CAPTAIN LOOKED OUT THE WINDOW AND VERIFIED FLAMES. CREW ABORTED TAKEOFF AND FIRED BOTTLES. UPON TAXIING BACK IN, CFR STOPPED THE A/C AND TOLD THEM THERE WERE STILL RESIDUAL FLAMES. PASSENGSDR 95ZZZX4606Seal Plate · crackedDURING INSPECTION/REPAIR FOR LOW POWER, FOUND SEAL PLATE CRACKED. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO INCREASE SEAL PLATE TENISON AGAINST FIRST STAGE ROTOR ASSEMBLY. INCREASED TENSION OF THE SEAL FLANGE RESULTS IN CRACKING AT THE EDGE PROPOGATSDR 95ZZZX4605Seal Plate · crackedDURING SCHEDULED INSPECTION, FOUND SEAL PLATE CRACKED 5 PLACES. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO PROVIDE INCREASED SEAL PLATE TENSION AGAINST FIRST STAGE ROTOR ASSEMBLY. INCREASED TENSION ON THE SEAL FLANGE RESULTS IN CRACKING AT THE SEAL PSDR 95ZZZX2446Seal · crackedDURING INSPECTION FOR COMPRESSOR DAMAGE, FOUND PART CRACKED 11 PLACES. SB 72-0840 AUTHORIZES INSTALLATION OF PN 3107085-2 TO PROVIDE INCREASED SEAL PLATE TENSION AGAINST FIRST ROTOR ASSY. THIS PART WAS MODIFIED TO PN 3107085-2 BY INCORPORATING A SHIM BETWEENSDR WWMA9500038Compressor Seal · defectiveFLIGHT 3280 - BFL/LAX - PILOT REPORTED THAT THE LEFT ENGINE FLOW SMELLS OF OIL. MAINTENANCE REMOVED THE COMPRESSOR SEAL AND ROTOR AND REPLACED WITH NEW SERVICABLE UNIT. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR 95ZZZX1992Seal · crackedDURING CAM INSPECTION, FOUND SEAL CRACKED 3 PLACES. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO PROVIDE INCREASED PRESSURE AGAINST 1ST STAGE ROTOR. THIS INCREASED PRESSURE RESULTS IN CRACKING OF THE SEAL EDGE DIAMETER. SUGGEST ALLIED SIGNAL ENGINEERISDR 95ZZZX2445Seal · crackedDURING INSPECTION FOR LOW POWER, FOUND PART CRACKED 12 PLACES UP TO APPROXIMATELY .5 INCH. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO PROVIDE INCREASED SEAL PLATE TENSION AGAINST FIRST STAGE ROTOR. THIS INCREASED TENSION RESULTS IN CRACKING AT THE SESDR VTZA95114Tt2 Sensor · dirtyFLT 6186 - LYH-IAD - ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE AND EGT FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENTS. MAINTENANCE OPENED DMI NR 08518 IAW MEL 76-2. MAINTENANCE LATER CLEARED DMI NR 08518 BY CLEANING THE TT2 SENSOR CANNON PSDR 95ZZZX1483Seal · crackedDURING HOT SECTION INSPECTION, FOUND PART CRACKED. SB 72-0840 AUTHORIZES INSTALLATION OF EITHER PN 3103315-05 OR PN 31070825-2 TO PROVIDE INCREASED SEAL PLATE TENSION AGAINST FIRST ROTOR ASSY. THIS PARTICULAR PART WAS MODIFIED TO PN 3107085-2 BY INCORPORATINSDR 95ZZZX1484Seal · crackedDURING HOT SECTION INSPECTION, FOUND PART CRACKED. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO PROVIDE INCREASED SEAL PLATE TENSION AGAINST FIRST ROTOR ASSY. SUBMITTER BELIEVES THIS INCREASED TENSION IS CAUSING THIS PART TO CRACK. SUGGEST ALLIED SIGNSDR 95ZZZZ52P2-T2 Sensor · failedFLT 4580 - BNA - ON CLIMB-OUT THE LEFT ENGINE TQ AND FUEL FLOW SURGED. THE LEFT ENGINE WAS SHUT DOWN, THE CREW DECLARED AND EMERGENCY AND LANDED BACK AT BNA WITHOUT INCIDENT. REPLACED LEFT ENGINE P2-T2 SENSOR. (Z)
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