# Service difficulty reports: Garrett TPE331-10U

A list on [Garrett TPE331-10U](https://openairdocs.org/engine/garrett-tpe331-10u.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 183 reports

- [SDR 2025FA0000684](https://openairdocs.org/sdr/2025FA0000684.md): Housing · cracked · Oct 7, 2025 · Turbine Engine Oil System
  > OIL PRESSURE PUMP ASSEMBLY [PN: 3103217-3, SN: 98-14057-197] HOUSING ASSEMBLY [PN: 3102047-3] CRACKED.
- [SDR KY7A2020072215002](https://openairdocs.org/sdr/KY7A2020072215002.md): Manifold · leaking · Jul 15, 2020 · N788KL · Swrngn SA227AC · Turbine Engine Oil System
  > PILOT REPORTED NR 1 ENGINE LOST OIL. MX TROUBLESHOT AND LOCATED A LEAK AT 7/16 OIL MANIFOLD TO PROP GOVERNOR LINE. MX REMOVED AND REPLACED LINE AND REPOSITIONED MANIFOLD AS REQUIRED FOR FIT. POST ACTION OPS AND LEAK CHECKED GOOD AND SERVICED OIL.
- [SDR 2020F00246](https://openairdocs.org/sdr/2020F00246.md): Engine · faulty · Feb 25, 2020 · N360LG · Swrngn SA226TB · Engine (Turbine/Turboprop)
  > AFTER TAKE-OFF FROM DRT AND AT CRUISE ALTITUDE EN ROUTE TO SAT, #1 ENGINE EGT WENT TO MAX TEMPERATURE. TORQUE INDICATOR WENT DOWN TO 20% AND THEN TO 10% TORQUE. FUEL FLOW WENT BELOW 250 LBS. AND PLANE BEGAN TO YAW. THE CREW SHUT-DOWN THE #1 ENGINE AND FEATH
- [SDR KY7A20131217001](https://openairdocs.org/sdr/KY7A20131217001.md): Turbine · damaged · Dec 17, 2013 · N2728G · Frchld SA227CC · Turbine Section
  > PILOT REPORTED THAT ON CLIMB OUT THE ENG LOST OIL PRESS. PILOT SECURED THE ENG & RETURNED TO THE DEPARTURE AIRPORT & LANDED. MX FOUND SIGNIFICANT DAMAGE TO THE 3RD STAGE TURBINE & DISASSEMBLED ENG. AFT TURBINE BEARING WAS FOUND DESTROYED, FAILED. 1ST & 2ND
- [SDR OZCA20110831001](https://openairdocs.org/sdr/OZCA20110831001.md): Line · chafed · Aug 31, 2011 · N841BC · Swrngn SA226TC · Hydraulic System, Main
  > DURING CRUISE CLIMB THE PILOT NOTED BOTH HYD PRESSURE LIGHTS INLUMINATED. LANDING GEAR DOWN WAS SELECTED AND RETURN TO AIRPORT FOR AN UNEVENTFUL LANDING.
- [SDR CA110829014](https://openairdocs.org/sdr/CA110829014.md): Valve · inoperative · Aug 22, 2011 · Swrngn SA227AC · Trailing Edge Flap Control System
  > (CAN) ACFT WAS DIFFICULT TO MAINTAIN LEVEL FLT, WHEN THE CREW NOTICED THAT THE FLAPS WERE INDICATING 1/4 EVEN THOUGH THE SELECTOR WAS SET FOR FLAP UP. ALSO NOTICED THAT THE FLAPS BEGAN TO RUN TO THE FULL DOWN POSITION AND THAN COME BACK UP TO FULL UP. THIS
- [SDR 2011F00173](https://openairdocs.org/sdr/2011F00173.md): Heater · shorted · Aug 6, 2011 · N904EH · Bag JETSTM3101 · Windshield/Door Rain/Ice Removal
  > PILOTS WINDSHIELD HAD AN INTERNAL ELECTRICAL SHORT CAUSING INTERNAL DAMAGE TO WINDSHIELD.
- [SDR CA110124008](https://openairdocs.org/sdr/CA110124008.md): Engine · malfunctioned · Jan 18, 2011 · Bag JETSTM3112 · Engine (Turbine/Turboprop)
  > (CAN) THE FLIGHT CREW REPORTED, WHILE CLIMBING THROUGH 16,000 FT THE TORQUE ON THE NR 2 ENGINE SURGED TO 120% AND THE AIRCRAFT YAWED TO THE LEFT. THE PILOT IN COMMAND SHUTDOWN THE NR 2 ENGINE, AND RETURNED TO FOR LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT
- [SDR CA100528006](https://openairdocs.org/sdr/CA100528006.md): Line · cracked · May 21, 2010 · Swrngn SA227AC · Propeller Governor
  > UPON LANDING THE LT OIL PRESSURE LIGHT FLICKERED AND THEN ILLUMINATED. LT ENGINE WAS SHUTDOWN AND MX WAS CONTACTED. THEY FOUND THE LT PROP GOVERNOR LINE WAS LEAKING. LINE WAS REPLACED. OIL WAS REPLENISHED AND GROUND RUNS CARRIED OUT IAW ENGINE MFR AND ACFT
- [SDR CA081124004](https://openairdocs.org/sdr/CA081124004.md): Switch · failed · Nov 17, 2008 · Swrngn SA226TC · Landing Gear Position and Warning
  > (CAN) DURING AN ATTEMPTED ENGINE START THE CREW WAS UNABLE TO GET ENGINE ROTATION OR LIGHT OFF. MX INVESTIGATED AND DETERMINED THE MLG SAFETY MICROSWITCH WHICH CONTROLS THE AIR/GROUND PORTION OF THE ENGINE START CONTROL SYS TO BE INOPERATIVE. MX REPLACED THE S
- [SDR CA081020009](https://openairdocs.org/sdr/CA081020009.md): Tire · separated · Oct 7, 2008 · Swrngn SA227AC · Tire
  > (CAN) DURING GROUND HANDLING PROCEDURES THE NR2 MAIN WHEEL WAS FOUND TO BE SHREDDED AND THE TREAD PORTION OF THE TIRE MISSING. THIS TIRE WAS A RECAPPED TIRE RECEIVED FROM A CERTIFIED FAA REPAIR STATION. THE TIRE WHEN IT SHREDDED CAUSED DAMAGE TO THE ACFT FLAP
- [SDR CA080403005](https://openairdocs.org/sdr/CA080403005.md): Windshield · cracked · Mar 31, 2008 · Swrngn SA226T · Flight Compartment Windows
  > IN LEVEL CRUISE AT FLIGHT LEVEL 220 APPROXIMATELY 25 MINUTES AFTER DEPARTURE, THE LEFT HEATED WINDSHIELD SUDDENLY SHATTERED. ATC WAS ADVISED AND DESCENT REQUESTED FOLLOWED BY REQUEST FOR RETURN TO CYWG. AFTER ESTABLISHING THE RETURN COURSE AND LEVELING AT 90
- [SDR CA080214002](https://openairdocs.org/sdr/CA080214002.md): Drive Shaft · failed · Feb 13, 2008 · Swrngn SA226TC · Engine RPM Indicating System
  > (CAN) TROUBLESHOT NO RPM INDICATION. REMOVED TACH GENERATOR FROM RT ENGINE, DRIVE SHAFT WAS STILL STUCK IN THE ENGINE. IT APPEARS THAT THE SHAFT SEPARATED FROM THE ARMATURE INSIDE. REMOVED THE SHAFT, NO DAMAGE TO THE ENGINE DRIVE. INSTALLED SERVICEABLE PART AN
- [SDR 2007FA0000640](https://openairdocs.org/sdr/2007FA0000640.md): Solenoid Valve · failed · Jul 2, 2007 · N749L · Swrngn SA226T · Landing Gear Steering System
  > THE NOSE WHEEL STEERING WAS TESTED PRIOR TO FLIGHT, AD TESTED SATISFACTORY. AT AROUND 60 TO 70 KNOTS DURING THE TAKEOFF ROLL, THE AC STEERING FAILED IN A MANOR THAT RESULTED IN THE AC PULLING HARD TO THE LEFT. USING HARD RT BRAKE AND RT REVERSE THRUST THE AC
- [SDR CA070525003](https://openairdocs.org/sdr/CA070525003.md): Bolt · sheared · May 24, 2007 · Bag JETSTM3101 · Landing Gear Retraction/Extension System
  > (CAN) NLG RETRACTION JACK MOUNT UPPER IB MOUNTING BOLT SHEARED. DISCOVERED DURING SCHEDULED NLG RETRACTION, JACK ATTACH BOLT INTEGRITY INSPECTION. ALL MOUNTING BOLTS REPLACED WITH NEW. (TC NR 20070525003)
- [SDR 2007FA0000313](https://openairdocs.org/sdr/2007FA0000313.md): Bearing · misinstalled · Mar 30, 2007 · Turbine Engine Reduction Gear
  > SUBASSEMBLY BEARINGS TO 2ND IDLER GEAR ASSEMBLED BACKWARDS, CAGE FAILED.
- [SDR CA061212007](https://openairdocs.org/sdr/CA061212007.md): Turbine Wheel · damaged · Oct 30, 2006 · Turbine Section
  > (CAN) FOUND UPON DOING A HSI INSPECTION THAT THE NR 2 ROTOR THE RIVETS WERE FOUND LOOSE TO THE POINT THAT THEY WERE GOING TO START COMING OUT. THIS WHEEL IN QUESTION ONLY HAD 1409 CYCLES TOTAL ON IT. (TC NR 20061212007)
- [SDR AU510001532](https://openairdocs.org/sdr/AU510001532.md): Plate · cracked · Dec 12, 2005 · Bag JETSTM3107 · Fuselage Miscellaneous Structure
  > PASSENGER CUTOUT INTERCOSTAL UPPER JOINT PLATE LOCATED AT FS 223 LT CRACKED. FOUND DURING INSPECTION IAW AD/JETSTREAM/98 AND SB51-JA030544 R1.
- [SDR CA050707007](https://openairdocs.org/sdr/CA050707007.md): Bearing · failed · Jun 30, 2005 · Bag JETSTM3212 · Turbine Engine Compressor Section
  > PILOT REPORTED, WHEN TURNING THE LT ENGINE PROPELLER AFTER SHUTDOWN, NOTICED A GRINDING NOISE COMING FROM THE ENGINE. AFTER INVESTIGATION, THE ENGINE GEARBOX WAS OPENED AND THE FWD COMPRESSOR BEARING WAS FOUND DAMAGED AND TO BE THE CAUSE OF THE NOISE AND FRIC
- [SDR CA050414005](https://openairdocs.org/sdr/CA050414005.md): Windshield · fractured · Mar 22, 2005 · Bag JETSTM4112 · Flight Compartment Windows
  > 40 MINUTES IN FLIGHT AT FL220, SUDDEN POP AND RT WINDSHIELD FRACTURED. PRESSURIZATON WAS RAPIDLY REDUCE, DESCENT TO 8000 FT WAS CARRIED OUT, AFTER VERIFING THE WINDOW WAS STILL INTACT FLIGHT CONTINUEDTO DESTINATION UNEVENTFUL.
- [SDR AU510002203](https://openairdocs.org/sdr/AU510002203.md): Clamp · broken · Feb 12, 2005 · Bag JETSTM3107 · Hydraulic System, Main
  > (AUS) HYDRAULIC PIPES PN 1379007D441 AND PN 1379007D443 LOCATED IN LT WING LEADING EDGE RUBBING TOGETHER DUE TO A BROKEN CLAMP. ONE PIPE WAS WORN THROUGH. LOSS OF HYDRAULIC FLUID. (OTHER CAUSE: BROKEN CLAMP) (CASA NR 510002203)
- [SDR CA041109002](https://openairdocs.org/sdr/CA041109002.md): Duct · contaminated · Oct 24, 2004 · Bag JETSTM3101 · Heating System
  > AFTER T/O CREW ADJUSTED TEMP CONTROL TO WARM UP CABIN. SHORTLY AFTER CABIN START’S TO FILL WITH SMOKE. TEMP WAS REDUCED, ATC NOTIFIED OF PROBLEM, QRH DRILL FOLLOWED. SMOKE CLEARED, A/C LANDED BACK IN 4 MM WITHOUT INCIDENT. MX INSPECTION REVEALED, INSULATIO
- [SDR LDI2004F00001](https://openairdocs.org/sdr/LDI2004F00001.md): Gear Shaft · sheared · Oct 20, 2003 · N903EH · Bag JETSTM3101 · Turbine Engine Oil System
  > OIL PUMP SHAFT SHEARED THUS UNCOUPLING THE FUEL PUMP FROM THE ENGINES GEARBOX. THE CRACK THAT CAUSED THE EVENTUAL SHEARING OF THE GEARSHAFT APPARENTLY ORIGINATED AT A SLOT FOR THE LOCKING KEY THAT WAS MACHINED DURING A PAST REWORK (MODIFICATION) THAT HAD BEE
- [SDR AUS20031024](https://openairdocs.org/sdr/AUS20031024.md): Selector Valve · malfunctioned · Oct 4, 2003 · Bag JETSTM3107 · Steering Unit
  > (AUS) STEERING SELECTOR VALVE INTERNAL FAULT.
- [SDR DU22003F00000](https://openairdocs.org/sdr/DU22003F00000.md): Torque Sensor · failed · Sep 16, 2003 · N903EH · Bag JETSTM3101 · Engine BMEP/Torque Indicating
  > THE ENGINE SHUT DOWN ON FINAL APPROACH. IT WILL NOT BE KNOWN UNTIL THE ENGINE IS APART ON WHAT EXACTLY FAILED. IT IS SUSPECTED THAT THE TORQUE SENSOR FAILED. THE FAILURE OF THIS UNIT CAUSED THE ACCESSORY DRIVE FOR THE ENGINE DRIVEN FUEL PUMP TO STOP ROTATIO
- [SDR BMAC030003](https://openairdocs.org/sdr/BMAC030003.md): Engine · malfunctioned · Feb 4, 2003 · N536PA · Bag JETSTM3101 · Engine (Turbine/Turboprop)
  > PILOT REPORTED TAKEOFF ABORTED DUE TO RT ENGINE NOT GENERATING POWER. MAINTENANCE CHECKED ALL CONNECTOR PLUGS AND C/W TWO HIGH SPEED TAXI RUNS. SYSTEM OPS CHECKED NORMAL ON GROUND IAW MM.
- [SDR 20031](https://openairdocs.org/sdr/20031.md): Valve · out of adjust · Jan 24, 2003 · N95AC · Swrngn SA226TB · Passenger/Crew Doors
  > AT 20,000 FT ALTITUDE, CREW NOTICED THAT THE CABIN ALTITUDE HAD STARTED TO CLIMB AT 2000 FPM. AFTER CHECKING THE PRESSURIZATION CONTROLS, DUMP VALVE SWITCH POSITION, AND THE CABIN DOOR ANNUNCIATOR AND FINDING NO IRREGULARITIES, THE CREW INITIATED A 180 DEG TU
- [SDR CA021115015](https://openairdocs.org/sdr/CA021115015.md): Hinge · cracked · Nov 6, 2002 · Bag JETSTM3212 · Passenger/Crew Doors
  > (CAN) WHEN DOOR HINGE WAS REMOVED FOR MAINTENANCE CRACKS WERE FOUND RUNNING TO THE OUTSIDE OF HINGE FROM THE 2 HOLES CLOSEST TO THE BEARING END. 3 AIRCRAFT WERE CHECKED AND 2 WERE FOUND WITH CRACKS SB 52-JM5319 ADDRESSES THIS PROBLEM BUT IT IS NOT A MANDITORY
- [SDR CA020718005](https://openairdocs.org/sdr/CA020718005.md): Bolt · sheared · Jul 7, 2002 · Bag JETSTM3212 · Nose/Tail Landing Gear Attach Section
  > (CAN) CAA AD 024-05-87 REQUIRES COMPLIANCE WITH BAE SB 53-A-JA870510. PART C OF THIS BULLETIN REQUIRES A 1600 CYCLE TORQUE CHECK OF THE NLG RETRACT JACK ATTACH BOLTS. DURING THE CHECK AT THIS TIME ONE OF THE BOLTS SHEARED. ALL BOLTS WERE REPLACED WITH NEW.
- [SDR CA010129005](https://openairdocs.org/sdr/CA010129005.md): Drive Shaft · failed · Dec 27, 2000 · Bag JETSTM3101 · Engine Fuel Pump
  > (CAN) UPON DISASSEMBLY OF THE FCU AND FUEL PUMP, IT WAS FOUND THAT THE DRIVESHAFT FOR THESE UNITS ROTATED FREELY HAVING BECOME DISENGAGED IN THE GEARBOX. THE ENGINE IS BEING SHIPPED TO NATIONAL FLIGHT FOR ASSESSMENT AND REPAIR. A REPORT ON FAILED PARTS WILL F
- [SDR CA001206011](https://openairdocs.org/sdr/CA001206011.md): Blade · broken · Oct 30, 2000 · Turbine Engine Compressor Section
  > (CAN) DURING DISASSEMBLY OF ENGINE TO COMPLY WITH GEARBOX INSPECTION AND HOT SECTION INSPECTION METAL FRAGMENTS WHERE FOUND IN THE COMBUSTOR,. INSPECTION OF THE COMPRESSOR REVEALED 3 BROKEN BLADES ON NR 2 IMPELLER S/N 2-03501-353 CAUSING MAJOR DAMAGE DOWN STR
- [SDR CHQA20000032](https://openairdocs.org/sdr/CHQA20000032.md): Master Cylinder · lack of lube · Sep 13, 2000 · N845JS · Bag JETSTM3101 · Master Cylinder/Brake Valve
  > CAPTAIN REPORTED THE RIGHT BRAKE PEDAL HAD NO PRESSURE DURING TAXI. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE MASTER CYLINDER NEEDED SERVICING. THE MASTER CYLINDER WAS SERVICED, SYSTEM BLED, WITH ALL INDICATIONS NORMAL.
- [SDR CHQA20000030](https://openairdocs.org/sdr/CHQA20000030.md): Battery · discharged · Sep 5, 2000 · N842JS · Bag JETSTM3101 · Emergency Lighting
  > FLIGHT CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE FOUND THE BATTERIES HAD BEEN LEFT ON. THE BATTERIES WERE REPLACED, SYSTEM OPS CHECKED NORMAL.
- [SDR CHQA20000022](https://openairdocs.org/sdr/CHQA20000022.md): Governor · failed · Aug 1, 2000 · N853JS · Bag JETSTM3101 · Turbine Governor
  > CREW EXPERIENCED A 30 PERCENT TORQUE FLUX IN CRUISE FLIGHT. SHUT DOWN ENGINE AND RETURNED TO THE FIELD. THE PROP GOVERNOR WAS REPLACED, GROUND RAN WITH ALL INDICATIONS NORMAL.
- [SDR CA001017011](https://openairdocs.org/sdr/CA001017011.md): Turbine Wheel · broken · Jul 24, 2000 · Turbine Section
  > (CAN) ENGINE REMOVED FOR HIGH TAXI AND GROUND IDLE SNAG. DISASSEMBLY REVEALED NR 1 COMPRESSOR IMPELLER HAD A PIECE BROKEN OUT OF THE TRAILING EDGE OF 1 BLADE.085 INCH UP FROM THE PLATE.480 INCH FROM THE OUTER RIM OF THE PLATE. THE RESULTING DAMAGE DOWN STRE
- [SDR 20000426SH029](https://openairdocs.org/sdr/20000426SH029.md): Tube · cracked · Mar 23, 2000 · N38TA · Swrngn SA226TB · Propeller Controlling System
  > DURING ROUTINE MAINTENANCE, THE BETA TUBE WAS REMOVED FROM THE RT ENGINE. THE TUBE APPEARED TO HAVE A CRACK IN THE RADIUS JUST BELOW THE LOWER FLANGE SURFACE OF THE TUBE. NDI VERIFIED THE TUBE WAS CRACKED ALL THE WAY AROUND THE OUTSIDE DIAMETER OF THE LOWER
- [SDR CA000301015](https://openairdocs.org/sdr/CA000301015.md): Downlock Switch · failed · Feb 16, 2000 · Bag JETSTM3101 · Landing Gear Position and Warning
  > (CAN) WHEN THE GEAR WAS SELECTED DOWN ON APPROACH, THE LEFT MAIN GEAR GREEN LIGHT DID NOT COME ON AND THE CREW CARRIED OUT A MISSED APPROACH. AFTER THE CREW CYCLED THE GEAR THE LIGHT DID COME ON AND THEY CARRIED OUT AN UNEVENTFUL LANDING. MAINTENANCE TRACED
- [SDR 99ZZZX3681](https://openairdocs.org/sdr/99ZZZX3681.md): Line · cracked · Sep 13, 1999 · N411MX · Bag JETSTM3101 · Engine Oil Distribution (Airframe Furnished)
  > LINE CRACKED DUE TO RESONANT VIBRATION SET UP BY STARTER/GENERATOR.
- [SDR 99ZZZX3973](https://openairdocs.org/sdr/99ZZZX3973.md): Bearing · worn · Sep 13, 1999 · N411MX · Bag JETSTM3101 · Starter-Generator
  > STARTER/GENERATOR BEARINGS WORN. CAUSED RESONANT VIBRATION THAT CRACKED OIL LINE.
- [SDR 99ZZZX2105](https://openairdocs.org/sdr/99ZZZX2105.md): Combustor · cracked · Apr 30, 1999 · N10UP · Bag JETSTM3101 · Turbine Engine Combustion Section
  > ONE ENGINE START, CREW NOTICED SLOW START ON NR 2 ENGINE AND 100 DEGREE CELCIUS EGT SPLIT DURING FLIGHT. UPON ARRIVAL AT DESTINATION, MAINTENANCE WAS NOTIFIED, INSPECTOR FOUND A 6 INCH CRACK ON COMBUSTOR CAN WHICH ALLOWED HOT BLEED AIR TO LEAK INTO ENGINE NAC
- [SDR AU981620](https://openairdocs.org/sdr/AU981620.md): Engine · malfunctioned · Dec 4, 1998 · Engine (Turbine/Turboprop)
  > (AUS) PILOT REPORTED POWER LOSS ON BOTH ENGINES WHEN BECOMING AIRBORNE. ON RETURN, ENGINES GROUND RUN IAW MAINTENANCE MANUAL. ENGINE PERFORMANCE WELL WITHIN BOOK FIGURES. ENGINE INSPECTION CARRIED OUT FOR BLEED AIR LEAKS, WIRING HARNESS INSPECTED, ALL IN GO
- [SDR 98ZZZX4013](https://openairdocs.org/sdr/98ZZZX4013.md): Nut · broke · Sep 17, 1998 · N193CS · Swrngn SA226TB · Turbine Section
  > TURBINE NUT FAILED ON ENGINE RUN-UP. ROTATING GROUP BECAME UNSTACKED RESULTING IN SHUTDOWN OF ENGINE. REPAIRED IAW TPE331 MM. C/W SB 72-0935, IMPROVED TURBINE NUT. FAILED NUT HAD BEEN INSTALLED PER SB 72-0592 AT ENGINE OVERHAUL.
- [SDR 98ZZZM789](https://openairdocs.org/sdr/98ZZZM789.md): Valve · failed · Aug 6, 1998 · N844JS · Bag JETSTM3101 · Fuel Controlling System
  > AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE FLUCTUATION. THE SYSTEM WAS INSPECTED AND THE BYPASS VALVE WAS FOUND TO BE AT FAULT. THE VALVE WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. (M)
- [SDR AU980975](https://openairdocs.org/sdr/AU980975.md): Engine · malfunctioned · Aug 6, 1998 · Engine (Turbine/Turboprop)
  > (AUS) RIGHT ENGINE WOULD NOT ACHEIVE TARGET TORQUE OF 104.5 PERCENT. MAXIMUM TORQUE ACHIEVED 99 PERCENT.
- [SDR AU981082](https://openairdocs.org/sdr/AU981082.md): Plenum · cracked · Aug 1, 1998 · Turbine Engine Compressor Section
  > (AUS) NR 2 ENGINE PLENUM CASE CRACKED IN THE 9 O'CLOCK POSITION. LEAKING P3 AIR CAUSED HEAT DAMAGE TO ELECTRICAL WIRING INSULATION AND PAINT. PART TC: 17,403.
- [SDR REXA98095](https://openairdocs.org/sdr/REXA98095.md): Turbine · fialed · May 6, 1998 · N318PX · Bag JETSTM3101 · Turbine Section
  > RIGHT ENGINE SHUT DOWN ON APPROACH TO MEM. CHANGED ENGINE DUE TO TURBINE FAILURE. (X)
- [SDR WTAA980077](https://openairdocs.org/sdr/WTAA980077.md): Engine · malfunctioned · May 5, 1998 · N402UE · Bag JETSTM3101 · Engine (Turbine/Turboprop)
  > FAT - LEFT ENGINE FAILED TO MAKE MINIMUM STATIC TAKEOFF TORQUE. TAKEOFF ABORTED. MAINTENANCE UNABLE TO DUPLICATE DISCREPANCY. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR AU980466](https://openairdocs.org/sdr/AU980466.md): Transmitter · failed · Apr 28, 1998 · Fuel Flow Sensor
  > (AUS) DURING CLIMB, THE LT ENGINE FUEL FLOW INDICATION FAILED. TRANSMITTER WAS REPLACED AND THE CONNECTOR PLUG CLEANED.
- [SDR WTAA980072](https://openairdocs.org/sdr/WTAA980072.md): Engine · failed · Apr 20, 1998 · N424UE · Bag JETSTM3101 · Engine (Turbine/Turboprop)
  > SMF - EN ROUTE SMF TO ACV RIGHT ENGINE REPORTED TO RUN ROUGH FOLLOWED BY ABNORMAL ENGINE NOISE, TORQUE LOSS AND DROP IN OIL PRESSURE. IN FLT SHUT DOWN OF RIGHT ENGINE ACCOMPLISHED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT EN
- [SDR WTAA980067](https://openairdocs.org/sdr/WTAA980067.md): Engine · bird strike · Apr 16, 1998 · N419UE · Bag JETSTM3101 · Engine (Turbine/Turboprop)
  > OXR - BIRD STRIKE TO RIGHT ENGINE ON APPROACH. MAINTENANCE INSPECTED ENGINE FOR DAMAGE. FOUND RIGHT ENGINE INGESTED BIRD. REPLACED RIGHT ENGINE. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M)

Next page: https://openairdocs.org/engine/garrett-tpe331-10u/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'TPE33110U'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/garrett-tpe331-10u/reports

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