# Service difficulty reports: Garrett TPE331-10

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

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 185 reports

- [SDR 2023FA0000572](https://openairdocs.org/sdr/2023FA0000572.md): Bearing Race · broken · May 25, 2023 · Engine (Turbine/Turboprop)
  > TORQUE SENSOR BEARING INNER RACE FAILED [PN: 3103585-1 TSN: 1,319.2, CSN: 898].
- [SDR X2ZR041220221](https://openairdocs.org/sdr/X2ZR041220221.md): None · worn · Apr 13, 2022 · Mtsbsi · Engine (Turbine/Turboprop)
  > THE LARGE SPUR GEAR, WHICH MATES WITH THE TACHOMETER DRIVE GEAR (PN: 896806-1), SHOWS PREMATURE, EXCESSIVE WEAR ON THE FACE (MATING SURFACE) OF ALL OF THE GEAR TEETH. THIS GEAR WAS INSTALLED IN A SERIES 3, PN: 3101726-3 TORQUE SENSOR, WHICH WAS MODIFIED IAW HO
- [SDR CA190711009](https://openairdocs.org/sdr/CA190711009.md): Actuator · failed · Feb 23, 2019 · Mtsbsi MU2B60 · Landing Gear Actuator
  > (CAN) WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH, THE LANDING GEAR DID NOT EXTEND AND THE LANDING GEAR DOORS DID NOT OPEN. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED WITH OUT INCIDENT. MAINTENANCE DISCOVERED THAT THE LANDING GEA
- [SDR CA180423014](https://openairdocs.org/sdr/CA180423014.md): Gear · damaged · Apr 19, 2018 · Mtsbsi MU2B60 · Propeller Indication System
  > (CAN) AFTER LANDING THE PILOT WENT TO SPIN THE PROPELLER, PER ROUTINE PROCEDURES, AND FOUND THAT THE ENGINE WOULD NOT TURN. AFTER SEVERAL ATTEMPTS THE ENGINE DID ROTATE, BUT A REASON FOR THE PROBLEM COULD NOT BE DETERMINED. THE ENGINE WAS REPLACED AND IS NOW
- [SDR 39LA20151004145](https://openairdocs.org/sdr/39LA20151004145.md): Blade · cracked · Oct 4, 2015 · N602AR · Casa C212200 · Propeller Blade Section
  > DURING POST FLIGHT WALK AROUND, THE FLIGHT CREW DISCOVERED ON THE LT PROPELLER ONE OF THE BLADES WAS CRACKED.
- [SDR 8EKA20150630001](https://openairdocs.org/sdr/8EKA20150630001.md): Governor · sticks · Jun 11, 2015 · N502FS · Casa C212200 · Propeller Governor
  > PROP GOVERNOR STUCK IN FLIGHT. ACFT RETURNED TO BASE. GOVERNOR FOUND TO BE STICKY.
- [SDR 39LA20150430134](https://openairdocs.org/sdr/39LA20150430134.md): Control Quadrant · corroded · Apr 30, 2015 · N602AR · Casa C212CC · Aileron Control System
  > LEFT AILERON CABLE QUADRANT HAS AN AREA OF EXFOLIATION CORROSION APPROX 1.00 INCH BY.750 INCH BY.125 DEEP. REPLACED LT AILERON CABLE QUADRANT IAW AMM 27-11-02 P BLOCK 401.
- [SDR 39LA20150326110](https://openairdocs.org/sdr/39LA20150326110.md): Cap · corroded · Mar 26, 2015 · N602AR · Casa C212200 · Ailerons
  > RIGHT AILERON END CAP FOUND CORRODED THROUGH, AT COUNTERWEIGHT. REPAIRED IAW COMPANY ENGINEERING ORDER 14022-300.
- [SDR 39LA20150326112](https://openairdocs.org/sdr/39LA20150326112.md): Floorbeam · corroded · Mar 26, 2015 · N602AR · Casa C212CC · Fuselage Main, Floor Beam
  > FLOORBEAM UPPER CAP LT SIDE AT FS 8326, BL 20 FOUND CORRODED. REPAIRED IAW EO 14022-300, ITEM 8 16.
- [SDR 39LA20150326126](https://openairdocs.org/sdr/39LA20150326126.md): Structure · corroded · Mar 26, 2015 · N602AR · Casa C212CC · Trailing Edge Flaps
  > LEFT WING TE FLAP WELL WS 6300 EXFOLIATION CORROSION FOUND DURING HEAVY CHECK INSPECTION. REPAIRED IAW EO 14022-300.
- [SDR 39LA20150326127](https://openairdocs.org/sdr/39LA20150326127.md): Spar · corroded · Mar 26, 2015 · N602AR · Casa C212CC · Wing Spar
  > RIGHT WING LE SPAR WING STATION 7700 FOUND TO HAVE LEVEL 2 EXFOLIATION CORROSION. REPAIRED IAW EO 14022-300.
- [SDR CA141223004](https://openairdocs.org/sdr/CA141223004.md): Adapter · broken · Dec 21, 2014 · Mtsbsi MU2B60 · Turbine Engine Oil System
  > (CAN) LEFT ENGINE OIL PRESSURE WAS FLICKERING IN THE YELLOW DURING GROUND RUNS. FOUND THE OIL FILTER ADAPTER HOUSING HAD TWO BROKEN MOUNTING TABS. ADAPTER WAS REPLACED & AIRCRAFT RETURNED TO SERVICE.
- [SDR FEHR2015FA0000030](https://openairdocs.org/sdr/FEHR2015FA0000030.md): Bypass Valve · leaking · Dec 1, 2014 · N441G · Cessna 441 · Fuel Control/Turbine Engines
  > WHILE TROUBLESHOOTING THE LT BETA LIGHT SYSTEM, FOUND FUEL LEAKING FROM THE LT ENGINE FUEL CONTROL BYPASS VALVE, DUMPING FUEL ONTO THE HOT SECTION OF THE ENGINE. THE FUEL CONTROL WAS REMOVED AND SENT TO MFG FOR OVERHAUL.
- [SDR CA141015002](https://openairdocs.org/sdr/CA141015002.md): Housing · cracked · Oct 8, 2014 · Mtsbsi MU2B60 · Turbine Engine Oil System
  > (CAN) PILOT RETURNED TO BASE DUE TO FLUCTUATING OIL PRESSURE. MAINTENANCE OBSERVED OIL LEAK AND DETERMINED IT WAS COMING FROM THE END OF THE OIL FILTER HOUSING.UPON FURTHER EXAMINATION A CRACK WAS FOUND IN THE CHAMFERED END OF THE HOUSING. (TC# 20141015002)
- [SDR 3SVA2014072100001](https://openairdocs.org/sdr/3SVA2014072100001.md): Filter · clogged · Jul 21, 2014 · N441BD · Cessna 441 · Fuel Control/Turbine Engines
  > DURING TAXI FOR TAKEOFF, LT ENGINE FUEL COMPUTER TRIPPED OFFLINE. THE ENGINE RPMS THEN BEGAN TO DECAY AND THE LT GENERATOR DROPPED OFF LINE. PILOT SHUTDOWN THE ENGINE, PERFORMED A RESTART AND RETURNED TO BASE.
- [SDR 39LA2013112725](https://openairdocs.org/sdr/39LA2013112725.md): Unknown · odor · Nov 27, 2013 · N602AR · Casa C212CC · Air Distribution System
  > DURING FLIGHT WITH ENG BLEED AIR ON, OIL SMELL IN CABIN WITH SMOKE DETECTORS BEING SET OFF. ENG BLEED AIR TURNED OFF, SMOKE SMELL DISSIPATED & SMOKE DETECTORS SILENCED.
- [SDR CA131030006](https://openairdocs.org/sdr/CA131030006.md): Strut · cracked · Oct 30, 2013 · Mtsbsi MU2B60 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) DURING SCHEDULED MAGNETIC PARTICLE INSPECTION THE RT NLG STRUT WAS FOUND CRACKED. PART WAS REPLACED AND ACFT RETURNED TO SERVICE.
- [SDR CA131022007](https://openairdocs.org/sdr/CA131022007.md): Wire · damaged · Oct 22, 2013 · Mtsbsi MU2B60 · Ice/Rain Protection System Wiring
  > (CAN) WHILE TAXING AFTER LANDING, THE CREW SHUTOFF WINDSHIELD HEAT ON THE OVERHEAD SWITCH CONSOLE. A FLASH WAS NOTICED AND SPARKS FELL DOWN. MAINTENANCE DISCOVER AN ANTI-ICE POWER FEEDER WIRE HAD ARCED A STRINGER. THE WIRE WAS FOUND STRIPPED OF INSULATION 1
- [SDR CA130327003](https://openairdocs.org/sdr/CA130327003.md): Adapter · cracked · Mar 26, 2013 · Mtsbsi MU2B60 · Engine Bleed Air System
  > (CAN) DURING ROUTINE INSPECTION ON THE RH ENGINE THE BLEED AIR ADAPTER WAS FOUND CRACKED WHERE THE SMALL LINE SEPARATES FROM THE MAIN LINE. THIS ADAPTER CAN BE STRESSED DURING ENGINE REMOVAL AND INSTALLATION.
- [SDR 39LA2013020600014](https://openairdocs.org/sdr/39LA2013020600014.md): Engine · power loss · Feb 5, 2013 · N607AR · Casa C212CD · Engine (Turbine/Turboprop)
  > DURING THE TAKEOFF ROLL, IT WAS DETERMINED THAT THE RT ENGINE WAS NOT MAKING THE PREDICTED POWER. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT AND ACFT WAS TAXIED BACK TO THE RAMP FOR MX.
- [SDR CA130109005](https://openairdocs.org/sdr/CA130109005.md): Angle · cracked · Jan 8, 2013 · Mtsbsi MU2B60 · Fuselage Miscellaneous Structure
  > (CAN) FOUND ANGLE CRACKED DURING SCHEDULED INSPECTION.
- [SDR 3SVAN441BD91912](https://openairdocs.org/sdr/3SVAN441BD91912.md): Engine · flamed out · Sep 18, 2012 · N441BD · Cessna 441 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE FLAMED OUT ON CLIMBOUT OF ANC. PLIOT SECURED THE ENGINE AND RETURNED TO BASE.
- [SDR EHAA20120824007](https://openairdocs.org/sdr/EHAA20120824007.md): Gearbox · inoperative · Aug 24, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)
  > DURING CRUISE AT FL 85, THE NR 2 ENGINE RAPIDLY STARTED TO LOSE POWER AND DISPLAYED INDICATIONS OF FAILURE. THE COPILOT AND I NOTICED A CHANGE IN ACFT AND ENGINE PERFORMANCE, VERIFIED BY ENGINE TORQUE, RPM, FUEL FLOW, EGT AND SUBSEQUENT LOSS OF OIL PRESSURE D
- [SDR P4YA2012091200001](https://openairdocs.org/sdr/P4YA2012091200001.md): Cable · separated · Aug 24, 2012 · N962BW · Casa C212200 · Engine Controls
  > DURING HEAVY CHECK, FOUND NR 1 ENGINE TELEFLEX CABLE DAMAGED/PULLED APART AT THE SWAGE HOUSING.
- [SDR EHAA20120731006](https://openairdocs.org/sdr/EHAA20120731006.md): Engine · power loss · Jul 31, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)
  > DURING CLIMB, NR 2 ENGINE EGT DROPPED TO ZERO AND ENGINE LOST POWER.
- [SDR CA120703006](https://openairdocs.org/sdr/CA120703006.md): Engine · flamed out · Jun 28, 2012 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > (CAN) DURING INITIAL DESENT THE RT ENGINE FAILED, THE ENGINE WAS SECURED AND ACFT LANDED ON 1 ENGINE WITHOUT INCIDENT. OIL FILTER WAS PULLED AND FOUND METAL IN THE OIL. ENGINE REPLACED. WE ARE AWAITING THE TEARDOWN REPORT FROM THE ENGINE O/H FACILITY.
- [SDR CA120605007](https://openairdocs.org/sdr/CA120605007.md): Rod End · broken · May 23, 2012 · Mtsbsi MU2B60 · Landing Gear Door Retract Section
  > (CAN) DURING GEAR RETRACTION AND EXTENSION PILOT HEARD A LOUD BANG. ACFT LANDED WITHOUT INCIDENT AND MAINTENANCE FOUND THE RT FWD GEAR DOOR ROD END BROKEN. ROD END ASSEMBLY REPLACED AND CHECKED SERVICEABLE.
- [SDR 3RAA2012212001](https://openairdocs.org/sdr/3RAA2012212001.md): Mount Bracket · broken · Mar 29, 2012 · N467CS · Casa C212200 · Rudder Control System
  > DURING CLIMB AFTER TAKEOFF, THE PILOTS RUDDER PEDALS MOVED ALL THE WAY FORWARD. THE COPILOT TOOK OVER AND SAFELY LANDED THE AIRCRAFT. MAINTENANCE INVESTIGATED AND DISCOVED THE PILOTS RUDDER PEDAL ADJUSTMENT MOUNT BRACKET HAD BROKEN OFF IT'S MOUNT ALLOWING TH
- [SDR CA111205007](https://openairdocs.org/sdr/CA111205007.md): Oil Filter · damaged · Nov 29, 2011 · Swrngn SA226TC · Turbine Engine Oil System
  > (CAN) FLIGHT CREW NOTED AN ENGINE OIL BYPASS PIN POPPED ON PREFLIGHT. REMOVED OIL FILTER FOR INSPECTION AND FOUND PEICES OF THE OIL FILTER ALUMINUM CASE TRAPPED IN THE FILTER. THE END OF THE FILTER THAT CONTAINS THE O-RING HAD BROKEN AND PIECES WERE DRAWN IN
- [SDR CA111108003](https://openairdocs.org/sdr/CA111108003.md): Engine · shutdown · Nov 7, 2011 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > (CAN) DURING CLIMBOUT, RT ENGINE SHUTDOWN, ENGINE WAS SECURED AND ACFT LANDED WITH 1 ENGINE, WITHOUT INCIDENT. AWAITING ENGINE TEARDOWN REPORT FOR FURTHER INFORMATION.
- [SDR CA110805002](https://openairdocs.org/sdr/CA110805002.md): Clamp · worn · Aug 4, 2011 · Mtsbsi MU2B60 · Flight Compartment Equipment
  > AFTER TAKEOFF ACFT HAD SOME SMOKE IN THE COCKPIT FROM THE OVERHEAD PANEL, THE PILOTS SHUTOFF ALL THE SWITCHES TO THE PANEL AND THE SMOKE STOPPED THEY THEN RETURNED TO BASE AND LANDED WITHOUT INCIDENT. THE OVERHEAD PANEL WAS REMOVED AND WIRING INSPECTED, WE F
- [SDR CA110622006](https://openairdocs.org/sdr/CA110622006.md): Starter Gen · failed · Jun 19, 2011 · Dhav DHC3 · Starter-Generator
  > STARTER GENERATOR FAILED - ENGINE START ABORTED. REPLACED STARTER GEN WITH SERVICEABLE START GEN - ENGINE START NORMAL - ACFT RETURNED TO SERVICE.
- [SDR CA110430001](https://openairdocs.org/sdr/CA110430001.md): Isolator · corroded · Apr 30, 2011 · Gulstm 695A · Engine Mount Section
  > (CAN) DURING SCHEDULED 3600 HOUR REPLACEMENT OF ENGINE ISOLATORS, ISOLATOR WAS FOUND CORRODED ONCE REMOVED FROM THE AIRCRAFT. THE MOUNTING DESIGN OF THE ISOLATOR DOES NOT ALLOW A VISUAL INSPECTION OF THIS AREA OF THE ISOLATOR. IT COULD ONLY BE OBSERVED ONCE RE
- [SDR CA110406006](https://openairdocs.org/sdr/CA110406006.md): Oil Cap · worn · Apr 1, 2011 · Mtsbsi MU2B60 · Turbine Engine Oil System
  > (CAN) DURING ROUTINE ENG INSPECTION THE OIL FILTER CAP WAS FOUND TO BE CONTACTING THE ENG MOUNT CAUSING WEAR ON THE CAP. THIS ENG HAD SERVICE BULLETIN 79-0012 OIL FILTER HOUSING ADAPTER INCORPORATED THAT ALLOWED THE CONTACT. THE FILTER CAP WAS REPLACED & THE
- [SDR BIGA01/28/11](https://openairdocs.org/sdr/BIGA01%2F28%2F11.md): Pin · missing · Jan 28, 2011 · N117BH · Casa C212200 · Propeller Hub Section
  > THE ACFT WAS PERFORMING A TEST FLIGHT FOR A NTS AND FLIGHT IDLE FF DECENT CHECK AFTER THE INSTALLATION OF A O/H LT ENG AND A REPAIRED LT PROPELLER. WHILE PERFORMING THE FLIGHT IDLE FUEL FLOW FOR SINK RATE THE ACFT BEGAN TO VIBRATE BADLY. IT WAS QUICKLY IDENT
- [SDR SROM2010016](https://openairdocs.org/sdr/SROM2010016.md): Servo · jammed · Nov 22, 2010 · N405CP · Casa C212 · Rudder Control System
  > RUDDER SERVO FAILED 4.4 HOURS AFTER INSTALL. RUDDER WENT HARD OVER TO THE LT AND JAMMED IN PLACE. ONCE POWER WAS REMOVED THE PILOTS COULD AT LEAST MOVE THE RUDDER EVEN THOUGHT THE CLUTCH WAS STILL ENGAGED. UPON TEARDOWN FOUND CLUTCH HUB SCREWS HAD BACKED OU
- [SDR CA101116011](https://openairdocs.org/sdr/CA101116011.md): Limit Switch · frozen · Nov 15, 2010 · Mtsbsi MU2B60 · Landing Gear Position and Warning
  > AFTER THE PILOT SELECTED GEAR UP THE NOSE GEAR "DOWN" LIGHT REMAINED ILLUMINATED. CREW CONTINUED TO A MAINTENANCE BASE AND COMPLETED A MANUAL EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR DOWN LIMIT SWITCH CONTAMINATED WITH I
- [SDR CA101012010](https://openairdocs.org/sdr/CA101012010.md): Gyro · inaccurate · Oct 8, 2010 · Bag JETSTM3112 · Attitude Gyro and Indicating System
  > LT AI TOPPLED DURING STEEP TURN, AND DID NOT FLAG. ACFT RETURNED TO BASE AND INSTRUMENT WAS R & R WITH SERVICABLE UNIT. UPON INSP OF RECORDS IT WAS DISCOVERED UNIT HAS BEEN REPAIRED 4 TIMES IN 3 YEARS DUE TO VARIOUS FAULTS.
- [SDR P4YA2010031600001](https://openairdocs.org/sdr/P4YA2010031600001.md): Skin · cracked · Apr 14, 2010 · N967BW · Casa C212CD · Wing, Center Box
  > DURING CENTER WING NDI DRIVEN BY THE REPETITIVE INSPECTION REQUIREMENT OF AD 2008-06-03 THROUGH THE INSP REQUIREMENTS OF AOL 212-018 REV2, EDDY CURRENT REVEALED A 50 PERCENT INDICATION AT STA YN=1037 BETWEEN LONGERONS 3 & 4. VISUAL INSP CONFIRMED AND REVEALED
- [SDR CA100112001](https://openairdocs.org/sdr/CA100112001.md): Wheel · cracked · Jan 6, 2010 · Mtsbsi MU2B60 · Wheel/Ski/Float
  > (CAN) AIRCRAFT LANDED WITH LOW TIRE PRESSURE WHEEL ASSY REPLACED AFTER WHEEL ASSY REPAIRED IT WAS FOUND THAT THE TUBE HAD 3 SMALL CRACKS ON THE SIDE WALL. NOTE OUTSIDE AIR TEMP WAS -30 DEGREES. TUBE AND TIRE REPLACED AND WHEEL ASSY RETURNED TO SERVICE (TC NR
- [SDR CA091006002](https://openairdocs.org/sdr/CA091006002.md): Motor · intermittent · Oct 2, 2009 · Mtsbsi MU2B60 · Landing Gear Actuator
  > (CAN) AFTER TAKEOFF ON CLIMB OUT GEAR UNSAFE LIGHT WAS STILL ON. ACFT RETURNED TO AIRPORT AND LANDED UNEVENTFULLY. AFTER LANDING THE GEAR UNSAFE LIGHT WENT OUT. A FERRY FLIGHT WAS COMPLETED BACK TO BASE WITH GEAR DOWN. THE ACTUATOR/MOTOR FOR THE FWD GEAR DO
- [SDR CA090424003](https://openairdocs.org/sdr/CA090424003.md): Hinge · cracked · Apr 17, 2009 · Mtsbsi MU2B60 · Landing Gear Doors
  > (CAN) LT FWD LANDING GEAR DOOR FWD DOOR SIDE HINGE WAS FOUND CRACKED. HINGE WAS REPLACED AND LANDING GEAR SWINGS COMPLETED AND FOUND SERVICEABLE. NOTE THIS SAME CRACK WAS FOUND PREVIOUSLY ON OTHER GEAR DOORS.
- [SDR CA081027001](https://openairdocs.org/sdr/CA081027001.md): Shaft · binding · Oct 23, 2008 · Mtsbsi MU2B36 · Propeller Controlling System
  > (CAN) PROP OVERSEED DURING DESCENT. FOUND ENGINE INNER CONCENTRIC SHAFT TO BE BINDING ON OUTER CONCENTRIC SHAFT. AS POWER LEVER IS RETARDED, INNER CONCENTRIC SHAFT ROTATES SLIGHTLY CLOCKWISE INCREASING PROP GOVERNOR HIGH SETTING. THERE IS NO PROVISION FOR LUBR
- [SDR CA081007006](https://openairdocs.org/sdr/CA081007006.md): O-Ring · failed · Oct 7, 2008 · Bag JETSTM3112 · Hydraulic System, Main
  > (CAN) DURING GEAR DOWN LANDING CHECKS, ONLY NOSE GEAR LOCKED, BOTH MLG UNSAFE. REQUESTED LOW AND OVER-CYMM FSS CONFIRMED 3 GEAR DOWN. RE-POSITIONED TO A SAFE AREA AND PERFORMED ITEMS LISTED ON QRH. PUMPED GEAR DOWN MANUALLY, GEAR WAS CONFIRMED 3 DOWN AND LOCK
- [SDR BKA2008F00000](https://openairdocs.org/sdr/BKA2008F00000.md): Engine · shutdown · Aug 27, 2008 · N8083A · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)
  > DEPARTING, THE RT ENGINE BETA LIGHT CAME ON SHORTLY AFTER TAKEOFF. LOSS OF OIL PRESSURE WAS NOTED, THE OIL PRESSURE DID NOT DROP BELOW THE RED LINE BUT WAS IN THE YELLOW ARC. IAW EMERGENCY CHECK LIST RT ENGINE WAS SHUT DOWN, DECLARED EMERGENCY AND RETURNED TO
- [SDR CA080902002](https://openairdocs.org/sdr/CA080902002.md): Battery · thermal runaway · Aug 27, 2008 · Mtsbsi MU2B60 · Battery/Charger System
  > (CAN) DURING DAILY INSP OF ACFT, GPU USED. ACFT KEY TURNED (ON) TO CHARGE BATTERIES. APPROX. 2.5 HRS LATER, VENTING OF BATTERY NOTICED FROM ACFT. SMELL OF BURNING PLASTIC. GPU DISCONNECTED, KEY (OFF). ACFT MOVED OUTSIDE. AIRPORT FIRE DEPT. REMOVED NR 1 BATTER
- [SDR CA080821006](https://openairdocs.org/sdr/CA080821006.md): Attach Fitting · cracked · Aug 18, 2008 · Mtsbsi MU2B60 · Nose/Tail Landing Gear Attach Section
  > (CAN) DURING ROUTINE INSP, THE NOSE LANDING GEAR TRUNNION ATTACH FITTING WAS FOUND TO BE CRACKED. THE CRACK WAS MEASURED AT.3125 OF AN INCH. FITTING REPLACED.
- [SDR WIW2008F00000](https://openairdocs.org/sdr/WIW2008F00000.md): Torque Sensor · failed · Aug 13, 2008 · N30591 · Ayres S2RHGT65 · Engine BMEP/Torque Indicating
  > ON 8/13/2008 AT APPROX 07:40 AM, AIRPLANE WHILE PERFORMING AERIAL APPLICATION EXPERIENCED A LOSS OF ENGINE POWER AND MADE AN EMERGENCY LANDING IN A FIELD. SUBSEQUENT INVESTIAGATION REVEALED THE IDLER GEAR BRG (PN 3103035-1) IN THE TORQUE SENSOR HAD FAILED ALLO
- [SDR CA080623002](https://openairdocs.org/sdr/CA080623002.md): Motor · inoperative · Jun 19, 2008 · Mtsbsi MU2B60 · Landing Gear Retraction/Extension System
  > (CAN) PILOT SELECTED GEAR DOWN THE DOOR MOTOR CIRCUIT BREAKER POPPED. MANUAL GEAR EXTENSION COMPLETED AND ACFT LANDED WITHOUT INCIDENT. MECHANIC DISPATCHED AND FOUND THE GEAR DOOR ACTUATOR/MOTOR UNSERVICEABLE. ACFT FERRIED TO MAINTENANCE BASE, DOOR ACTUATOR/MO
- [SDR CA080613010](https://openairdocs.org/sdr/CA080613010.md): Lock Plate · worn · Jun 11, 2008 · Mtsbsi MU2B60 · Propeller Controlling System
  > (CAN) DURING A ROUTINE PROP INSP, IT WAS FOUND THAT THE PITCH LOCK PLATE ALLOWS THE LATCH PIN TO SLIP OFF THE EDGE AND COULD JAM THE PIN. THIS COULD PREVENT IN FIGHT ENGINE START.

Next page: https://openairdocs.org/engine/garrett-tpe331-10/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 = 'TPE33110'
ORDER BY difficulty_date DESC
```

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

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