Garrett TPE331-12UHR

Service difficulty reports · 287

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 = 'TPE33112UHR'
  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.

SDR AU000128021Nut · not safetied(AU) THE LEFT ENGINE DID NOT RESPOND WHEN THE SPEED LEVER WAS ADVANCED FOR TAKEOFF. THE SPEED LEVER CONTROL CABLE WAS FOUND DISCONNECTED FROM THE BALL JOINT. THE RIGHT ENGINE SPEED LEVER CABLE WAS FOUND TO BE MISSING THE JAM NUT AND THE REMAINING NUT WAS NOT Nov 18, 1999 · Frchld SA227DC · Engine (Turbine/Turboprop)SDR AU991088Engine · seized(AUS) LEFT ENGINE HARD TO TURN. METAL CONTAMINATION OF ENGINE OIL SYSTEM. FURTHER INVESTIGATION FOUND PROPELLER AND OIL COOLER ALSO METAL CONTAMINATED.Oct 29, 1999 · Bag JETSTM3201 · Engine (Turbine/Turboprop)SDR AU990988Engine · overtemp(AUS) NR 2 ENGINE OVERTEMPED TO 700 DEGREES CELSIUS. INSPECTION IAW GARRETT MM. FOUND NO DEFECTS. EGT CONNECTOR (2KR31) FOUND TO HAVE A DISLODGED PIN.Sep 25, 1999 · Bag JETSTM3201 · Engine (Turbine/Turboprop)SDR AU990924Pipe · loose(AUS) LEFT FUEL FILTER BYPASS LINE 'B' NUT LOOSE AT FUEL FILTER END.Sep 15, 1999 · Frchld SA227DC · Engine Fuel Indicating SystemSDR AU990928O Ring · damaged(AUS) LEFT MAIN LANDING GEAR INBOARD BRAKE UNIT O-RING SEAL LEAKING. SUBMITTER SUSPECTED CAUSED BY BRAKE OVERHEATING DURING TAXI.Sep 10, 1999 · Frchld SA227DC · BrakeSDR AU990908Wire · worn(AUS) ENGINE FUEL BYPASS VALVE WIRE WORN AND SHORT CIRCUITING.Sep 8, 1999 · Frchld SA227DC · Engine Fuel Indicating SystemSDR AU990880Spar · cracked(AUS) WING SPAR WEB CRACKED IN THE AREA BETWEEN STRINGER NR 14 CUT-OUT AND THE ADJACENT TRIM CABLE CUT-OUT. CRACK LENGTH 1.016 MM (0.040 INCH).Sep 2, 1999 · Frchld SA227DC · Wing SparSDR AU990926Brake · overheated(AUS) NR 2 BRAKE PACKING BINDING AND OVERHEATING. WATER ALSO FOUND IN BRAKE MASTER CYLINDERS.Aug 25, 1999 · Frchld SA227DC · BrakeSDR AU990108Connector · contaminated(AUS) LT ENGINE EGT SYSTEM CONNECTION CONTAMINATED WITH MOISTURE.Feb 8, 1999 · Bag JETSTM3201 · Engine EGT/TIT Indicating SystemSDR AU990107Engine · malfunctioned(AUS) LT ENGINE LOST POWER AND DID NOT RESPOND TO THE LT POWER LEVER. EXTENSIVE INSPECTION AND GROUND RUN FOLLOWED BY A TEST FLIGHT COULD FIND NO FAULTS. ENGINE HAS OPERATED SATISFACTORILY SINCE. DEFECT NOT CONFIRMED.Feb 1, 1999 · Frchld SA227DC · Engine (Turbine/Turboprop)SDR AU990026Tailpipe · cracked(AUS) ROGHT ENGINE TAIL PIPE ASSEMBLY AFT END HAD EXCESSIVE ORBITAL MOVEMENT. THE PIPE WAS REMOVED AND IT WAS DISCOVERED THAT THE PIPE HAD CRACKED THE AFT END WAS SEPARATING FROM THE FORWARD FLANGED END FOR 99.5 PERCENT OF ITS CIRCUMFERENCE. THE CAUSE WAS FOUJan 20, 1999 · Bag JETSTM3201 · Engine Collector/Tailpipe/NozzleSDR SABA980050Engine · failedRDU - FLT 5215 - RIGHT ENGINE LOST RPM AND OIL PRESSURE. SHUT THE ENGINE DOWN. CREW DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY NO INCIDENTS. REMOVED AND REPLACED RIGHT ENGINE IAW JE32 MM ATA 71-00-01. (M)Oct 8, 1998 · N941AE · Bag JETSTM3201 · Engine (Turbine/Turboprop)SDR SABA980016P3 Line · looseCLT - FLT 5167 - ON FLIGHT FROM LEX TO CLT, PILOT REPORTED TO DISPATCH THAT THE RIGHT ENGINE STARTED LOOSING POWER. THE ENGINE FINALLY SHUT ITSELF DOWN. AIRCREW DECLARED AN INFLIGHT EMERGENCY AND LANDED SAFELY AT CLT. MAINTENANCE FOUND THE P3 LINE ON THE RTMar 9, 1998 · N959AE · Bag JETSTM3201 · Fuel Controlling SystemSDR SABA980013Engine · failedFAY - FLT 5078 - ON FLIGHT FROM OAJ TO CLT, PILOT STATED THERE WAS A SLIGHT ENGINE SURGE AND RAPIDLY FOLLOWED BY A RT ENGINE SHUTDOWN. ALL ENGINE INDICATIONS NORMAL PRIOR TO SHUTDOWN OF RT ENGINE. AIRCREW DECLARED AN IN-FLIGHT EMERGENCY. AIRCREW ALSO TRIED Feb 10, 1998 · N941AE · Bag JETSTM3201 · Engine (Turbine/Turboprop)SDR 98ZZZX122Bleed Line · looseHOT/SAT - FLT 9907 - ACFT FERRIED HOT/SAT FOR HORIZ STAB EXCESSIVE PLAY. AT 80 KTS DURING TAKEOFF ROLL, EGT AND TORQUE SPLIT NOTED. AT V1, EGT SPLIT WAS 70 DEG AND TORQUE 10 PERCENT LOWER ON LT ENG. SIMULTANEOUS WITH ROTATION, LT ENG FIRE WARNING. AT 400 Oct 22, 1997 · N854LS · Frchld SA227DC · Pneumatic Distribution SystemSDR 97ZZZX771Seal · crackedSEAL CRACKED AT FLANGE. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO PROVIDE INCREASED SEAL PLATE TENSION AGAINST THE 1ST STAGE ROTOR ASSY. INCREASED TENSION CAUSES CRACKING AT FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIMIT 20,000 CYCLES. Dec 24, 1996 · Turbine SectionSDR 97ZZZX772Seal · crackedSEAL FOUND CRACKED AT SEALING FLANGE. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO PROVIDE INCREASED SEAL TENSION AGAINST FIRST ROTOR ASSY. INCREASED TENSION RESULTS IN CRACKING AT FLANGE. PART IS A CRITICAL LIFE LIMITED ROTATING GROUP COMPONENT. LIMNov 15, 1996 · Turbine SectionSDR 97ZZZX6191Bearing · failedENGINE RECEIVED FROM AIR CARRIER FOR THIS REPAIR. REPAIR STA NOT SURE IF THERE WAS AN IN-FLIGHT SHUT DOWN OCCURRENCE. REPAIR OF ENGINE WAS TO REPLACE ACCESSORY GEAR ASSEMBLY WITH OVERHAULED UNIT OF SAME PART NUMBER, CONTAINING NEW 3103035-1 BEARINGS. THESE BNov 13, 1996 · Turbine Engine Accessory DriveSDR 97ZZZX770Bearing · failedREAR TURBINE BEARING FAILED RESULTING IN MOVEMENT OF MAIN ROTATING GROUP. SECONDARY DAMAGE INCLUDED SEVERE RUBBING OF ALL ROTATING COMPONENTS DUE TO FREE MOVEMENT OF MAINSHAFT CAUSED BY BEARING FAILURE. IMPACT DAMAGE ALSO AFFECTED EXHAUST GAS TEMPERATURE HARNov 5, 1996 · Turbine SectionSDR 96ZZZM1172Idler Gear · failedAFTER TAKEOFF FROM WDG, THE CREW GOT A CHIP LIGHT ON THE RIGHT ENGINE. THE CAPTAIN DECIDED TO RETURN TO WDG AND MAKE A PRECAUTIONARY SHUTDOWN OF THE RIGHT ENGINE. DURING THE PRE-SHUTDOWN CHECKS, THE ENGINE FLAMED OUT. THE CREW THEN MADE A LANDING AT WDG WITJun 11, 1996 · N850LS · Frchld SA227DC · Turbine Engine Accessory DriveSDR 96ZZZM1021Bearing · failedAFTER LANDING AT ROW, THE CHIP DETECTOR LIGHT CAME ON. THE PILOT COMPLETED A NORMAL SHUTDOWN WITH NO FURTHER INDICATIONS. AFTER INSPECTING THE CHIP DETECTOR, IT WAS DETERMINED A FAILURE HAD TAKEN PLACE IN THE GEARBOX. AFTER INSPECTING THE GEARBOX, IT WAS FOMay 28, 1996 · N847LS · Frchld SA227DC · Turbine Engine Accessory DriveSDR 96ZZZM1022Idler Drive Assy · strippedAFTER STARTING ENGINES AND TAXIING FOR TAKEOFF, THE RIGHT ENGINE SHUTDOWN WITHOUT WARNING. THE AIRCRAFT TAXIED BACK TO THE GATE. UPON INSPECTION OF THE GEARBOX, THE ACCESSORY GEAR ASSEMBLY WAS FOUND TO BE STRIPPED IN THE CENTER OF THE GEAR. THIS GEAR, P/N 3May 26, 1996 · N853LS · Frchld SA227DC · Turbine Engine Accessory DriveSDR 96ZZZM1023Gear Assy · strippedAFTER STARTING ENGINES AND TAXIING FOR TAKEOFF, THE RIGHT ENGINE SHUTDOWN WITHOUT WARNING. THE AIRCRAFT TAXIED BACK TO THE GATE. UPON INSPECTION OF THE GEARBOX, THE ACCESSORY GEAR ASSEMBLY WAS FOUND TO BE STRIPPED IN THE CENTER OF THE GEAR. THIS GEAR, P/N 3May 26, 1996 · N853LS · Frchld SA227DC · Turbine Engine Accessory DriveSDR 96ZZZX1729Seal · flange crackedDURING SCHEDULED CAM INSPECTION, FOUND AIR SEAL CRACKED AT FLANGE. CRACKING RESULTED IN DEFLECTION OF SEALING SURFACE OF .040 INCH CAUSING LOSS OF COOLING AIR FOR TURBINE SECTION. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIFE-LIMIT IS 20,000 CYCLES. SUBMMar 14, 1996 · Turbine SectionSDR 96ZZZX1730Seal · flange crackedDURING SCHEDULED CAM INSPECTION, FOUND ROTATING AIR SEAL CRACKED AT FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIFE-LIMIT IS 20,000 CYCLES. SUBMITTER STATES THIS IS THE 29TH MALFUNCTION/DEFECT REPORT SUBMITTED BY THIS FACILITY ON THIS DISCREPANCY. Mar 14, 1996 · Turbine SectionSDR 96ZZZX1727Seal · flange crackedDURING SCHEDULED CAM INSPECTION, FOUND AIR SEAL CRACKED AT FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIFE-LIMIT IS 20,000 CYCLES. SUBMITTER SUGGESTS THIS IS THE 26TH MALFUNCTION/DEFECT REPORT ON THIS PART BY THIS FACILITY. PART TOTAL CYCLES, 7,435Feb 12, 1996 · Turbine SectionSDR 96ZZZX1728Seal · flange crackedDURING INSPECTION FOR BIRD INGESTION, FOUND AIR SEAL CRACKED AT FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIMIT - 20,000 CYCLES. SUBMITTER STATES THIS IS THE 27TH MALFUNCTION/DEFECT REPORT ON THIS PART BY THIS FACILITY. PART TOTAL CYCLES, 9,859.Jan 4, 1996 · Turbine SectionSDR 96ZZZX1726Seal · flange crackedDURING INSPECTION FOR METAL CONTAMINATION, FOUND AIR SEAL CRACKED AT SEALING FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIFE-LIMIT IS 20,000 CYCLES. SUBMITTER STATES THIS IS THE 24TH MALFUNCTION/DEFECT REPORT SUBMITTED ON THIS PART BY THIS REPAIR STJan 3, 1996 · Turbine SectionSDR 96ZZZX1724Seal · flange crackedDURING SCHEDULED HOT SECTION INSPECTION, FOUND AIR SEAL CRACKED AT SEALING FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIFE-LIMIT IS 20,000 CYCLES. SUBMITTER SUGGESTS ALLIED SIGNAL ENGINEERING DETERMINE/CORRECT CAUSE OF CRACKING. THIS IS THE 22ND MDec 7, 1995 · Turbine SectionSDR 96ZZZX1725Seal · flange crackedDURING SCHEDULED HOT SECTION INSPECTION, FOUND AIR SEAL CRACKED AT FLANGE. THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIFE-LIMIT - 20,000 CYCLES. SUBMITTER SUGGESTS ALLIED SIGNAL ENGINEERING DETERMINE AND CORRECT CAUSE OF CRACKING. THIS IS THE 23RD MALFUNCTDec 7, 1995 · Turbine SectionSDR 96ZZZX1723Seal · flange crackedDURING SCHEUDLED CAM INSPECTION, FOUND AIR SEAL CRACKED AT FLANGE. THIS IS A MAIN ROTATING GROUP. CRITICAL LIFE-LIMIT IS 20,000 CYCLES. SUBMITTER SUGGESTS ALLIED SIGNAL ENGINEERING DETERMINE AND CORRECT THE CAUSE OF THIS PROBLEM. THIS IS THE 21ST MALFUNCTINov 27, 1995 · Turbine SectionSDR 96ZZZX1721Seal · flange crackedDURING REPAIR, FOUND AIR SEAL CRACKED AT SEAL FLANGE. CRACK RESULTED IN .025 INCH DEFLECTION OF SEALING FLANGE AND CORRESPONDING LOSS OF TURBINE SECTION COOLING AIR AROUND ENTIRE DIAMETER OF SEAL CAUSING SECONDARY DAMAGE TO TURBINE SECTION COMPONENTS. THIS IOct 4, 1995 · Turbine SectionSDR 96ZZZX1720Seal · flange crackedDURING SCHEDULED HOT SECTION INSPECTION, FOUND AIR SEAL CRACKED AT FLANGE APPROXIMATELY 19 PLACES. SUGGEST ALLIED SIGNAL ENGINEERING REVIEW PROBLEM. SUBMITTER STATED THIS IS A CRITICAL LIFE-LIMITED COMPONENT. LIFE LIMIT - 20,000 CYCLES. THIS IS THE 16TH ROSep 28, 1995 · Turbine SectionSDR 96ZZZX1719Seal · flange 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. SUBMITTER STATED THIS IS A Sep 7, 1995 · Turbine SectionSDR 96ZZZX1722Seal · flange crackedFOUND SEAL FLANGE CRACKED. SB 72-0840 AUTHORIZES INSTALLATION OF THIS PART TO INCREASE TENSION AGAINST 1ST STAGE ROTOR. INCREASED TENSION RESULTS IN CRACKING AT THE SEAL FLANGE. SUBMITTER STATES THIS IS A CRITICAL SERVICE, LIFE-LIMITED COMPONENT. LIMIT - 2Aug 23, 1995 · Turbine SectionSDR 96ZZZX1717Seal · flange 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 ASSY. INCREASED TENSION ON THE SEAL FLANGE RESULTS IN CRACKING AT THE EDGE PROPAGATING Aug 21, 1995 · Turbine SectionSDR 96ZZZX1718Seal · flange crackedFOUND SEAL CRACKED AT FLANGE APPROXIMATELY 14 PLACES. THIS IS A CRICITAL LIFE-LIMITED COMPONENT. LIMIT - 20,000 CYCLES. SUBMITTER SUGGESTS ALLIED SIGNAL ENGINEERING DETERMINE/CORRECT CAUSE. THIS IS THE 12TH SEAL PLATE FOUND CRACKED AT THIS FACILITY. PART Jul 6, 1995 · Turbine Section
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