# Service difficulty reports: Garrett TPE331-12UA

A list on [Garrett TPE331-12UA](https://openairdocs.org/engine/garrett-tpe331-12ua.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 344 reports

- [SDR VPOA2015F00041](https://openairdocs.org/sdr/VPOA2015F00041.md): Fire Detector · false indication · Feb 19, 2015 · N770TR · Swrngn SA227BC · Fire Detection
  > LEFT ENGINE FIRE LIGHT CAME ON AFTER TAKEOFF. CREW PERFORMED A FULL SHUTDOWN, RETURNED TO THE FIELD AND LANDED WITHOUT ANY FURTHER INCIDENT. NO APPARENT FIRE. POST FLIGHT INSPECTION BY THE CREW DID NOT SHOW ANY TRACE OF FIRE. MAINTENANCE STILL INVESTIGATIN
- [SDR CA150501009](https://openairdocs.org/sdr/CA150501009.md): Ring · misinstalled · Jan 27, 2015 · Frchld SA227DC · Propeller Assembly
  > (CAN) PROPELLER WAS RECEIVED DUE TO PROPELLER LATCHES MALFUNCTIONING. AFTER BENCH TESTING AND DISASSEMBLY THE FOLLOWING OBSERVATIONS AND CONCERNS ARE THE PISTON BACKUP RING HAD BEEN PREVIOUSLY INSTALLED ON THE WRONG SIDE OF THE O-RING. PREVIOUS TECH HAD INS
- [SDR CA140326017](https://openairdocs.org/sdr/CA140326017.md): Annunciator · failed · Mar 25, 2014 · Frchld SA227DC · Central Warning
  > (CAN) STRONG ELECTRICAL ODOR COMING FROM COCKPIT AFTER SHUTDOWN. IT WAS CONFIRMED THAT THE BURNED ELECTRICAL ODOR CAME FROM THE COCKPIT ANNUNCIATOR PANEL. ANNUNCIATOR PANEL WAS REPLACED AND ACFT RETURNED TO SERVICE. NO OTHER FAULTS WERE FOUND.
- [SDR CA121210010](https://openairdocs.org/sdr/CA121210010.md): Boss · cracked · Dec 9, 2012 · Swrngn SA227* · Main Landing Gear
  > (CAN) DURING DAILY INSPECTION ON ACFT THE LT MAIN GEAR WAS INSPECTED AND NOTED THAT THE LOWER TORQUE KNEE GEAR BOSS WAS CRACKED ON THE GEAR. THE LOWER GEAR HOUSING AND TORQUE KNEE WERE REPLACED WITH SERVICIBLE UNITS. THE TORQUE KNEE PIN WAS INSPECTED AS SERVI
- [SDR CA120720001](https://openairdocs.org/sdr/CA120720001.md): Hose · failed · Jul 20, 2012 · Bag JETSTM3212 · Engine Bleed Air System
  > (CAN) WHEN GROUND TESTING ENGINES FOR UNSCHEDULED PROPELLERS DYNAMIC BALANCE, RT ENGINE FLEXIBLE HOSE ASSY OF P3 BLEED AIR HAS CRACKED AT FLANGE AND SEPARATED FROM ENGINE CASE CAUSING ABNORMAL EGT VALUES, ENGINE LOSS OF POWER, PRESSURIZATION SYSTEM FAILURE, ON
- [SDR CA111121001](https://openairdocs.org/sdr/CA111121001.md): Spinner · iced · Nov 18, 2011 · Frchld SA227DC · Propeller Spinner Section
  > (CAN) VIBRATION ON RT ENGINE, ACFT RETURNED TO BASE. TROUBLESHOT AND FOUND THE SPINNER TO HAVE ICE ACCUMULATED ON THE INTERIOR. ICE WAS REMOVED, SPINNER WAS CLEANED AND ENGINE/PROPELLER OPERATIONAL. GROUND CHECKS WERE CARRIED OUT WITH NO FURTHER VIBRATIONS N
- [SDR P4YA2010112800001](https://openairdocs.org/sdr/P4YA2010112800001.md): Spar · cracked · Nov 28, 2010 · N955BW · Frchld SA227DC · Wing Spar
  > DURING NDT INSP ST-UN-M003-9-6, A CRACK WAS VISUALLY IDENTIFIED AT THE STRINGER 14 AREA ON THE WING SPAR SHEAR WEB. CURRENTLY IN CONTACT WITH ENGINEERING FOR REPAIR DISPOSITION.
- [SDR CA090925002](https://openairdocs.org/sdr/CA090925002.md): Fcu · leaking · Sep 22, 2009 · Bag JETSTM3212 · Fuel Control/Turbine Engines
  > (CAN) REPORT OF HIGH THAN NORMAL TORQUE AT FLIGHT IDLE AND ON FLARE. UNABLE TO DUPLICATE ON GROUND. SUSPECT INTERNAL P3 LEAK IN FCU. FCU REPLACED AND TEST FLIGHT COMPLETED WITH SATISFACTORY RESULTS.
- [SDR CA070108009](https://openairdocs.org/sdr/CA070108009.md): Engine · damaged · Jan 5, 2007 · Frchld SA227CC · Engine (Turbine/Turboprop)
  > (CAN) UPON SHORT FINAL A "POP" WAS HEARD SIMILAR TO THE SOUND OF A DOOR SEAL. THE AIRCRAFT YAWED A BIT YET NOT ENOEGH TO ALERT THE FLIGHT CREW THAT IT WAS ANYTHING MORE THAN TURBULENCE. OIL PRESSURE WAS NOTED TO BE DROPPING. AN ENGINE FAILURE OCCURED ON THE
- [SDR O3X06119211](https://openairdocs.org/sdr/O3X06119211.md): Turbine · cracked · Nov 30, 2006 · N921AE · Bag JETSTM3201 · Turbine Section
  > CANNED ENGINE FROM AIRCRAFT (IN HEAVY CHECK), DOING VISUAL INSPECTION ON PROP PITCH CONTROL INSTALLATION AND NOTICED A CRACK IN HOT SECTION CASE WHERE REAR BEARING SCAVENGE TUBE IS LOCATED (APPROX 3 O’CLOCK POSITION) THIS HAIRLINE CRACK IS APPROX 1.25 INCHES I
- [SDR O3X04229241](https://openairdocs.org/sdr/O3X04229241.md): Engine · flamed out · Apr 22, 2006 · N924AE · Bag JETSTM3201 · Engine (Turbine/Turboprop)
  > AIRCRAFT WAS IN CRUISE FLIGHT, WHEN THE RT ENGINE SHUTDOWN. EMERGENCY PROCEDURES WERE FOLLOWED. THE CREW ATTEMPTED AN ENGINE RESTART. ENGINE WOULD NOT ACCELERATE BEYOND 30 PERCENT. THE ENGINE WAS SECURED. AIRCRAFT LANDED SAFELY. MAINTENANCE NOTICED A LOU
- [SDR O3X06039221](https://openairdocs.org/sdr/O3X06039221.md): Switch · malfunctioned · Mar 22, 2006 · N922CX · Bag JETSTM3201 · Landing Gear Position and Warning
  > THE AIRCRAFT WAS ON APPROACH, WHEN THE LANDING GEAR WAS SELECTED DOWN. NEITHER THE TRANSIT NOR THE DOWN AND LOCKED GREEN LIGHT CAME ON. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER ISSUES. MAINTENANCE FOUND THAT TH
- [SDR AU510001677](https://openairdocs.org/sdr/AU510001677.md): Engine · fluctuates · Dec 12, 2005 · Swrngn SA227* · Engine (Turbine/Turboprop)
  > (AUS) LT ENGINE EGT, TORQUE AND FUEL FLOW FLUCTUATING. LT FUEL BYPASS VALVE AND LT EGT SHORT LEAD CHANGED. GROUND RUNS AND TEST FLIGHT CARRIED OUT WITH NIL DEFECTS EVIDENT.
- [SDR AU510001678](https://openairdocs.org/sdr/AU510001678.md): Fcu · faulty · Dec 12, 2005 · Swrngn SA227* · Fuel Control/Turbine Engines
  > LT ENGINE EGT, TORQUE AND FUEL FLOW FLUCTUATING. FUEL CONTROL UNIT CHANGED. GROUND RUN AND TEST FLIGHT CARRIED OUT SERVICEABLE.
- [SDR SIMA200531501](https://openairdocs.org/sdr/SIMA200531501.md): Battery · discharged · Nov 8, 2005 · N844AE · Emb EMB135KL · Emergency Lighting
  > CREW FOUND EMERGENCY LIGHTS INTERMITTENT. REPLACED NR 1, NR 2, NR 3, AND NR 4 EMERGENCY LIGHTNING BATTERIES. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. NR 1) PN OFF 2013-1A, SN OFF 60708. NR 2) PN OFF 2013-1A, SN OFF 81147. NR 3) PN OFF 2013-1A, SN
- [SDR O3X06089371](https://openairdocs.org/sdr/O3X06089371.md): Piston Rod · cracked · Sep 23, 2005 · N937AE · Bag JETSTM3201 · Landing Gear Steering System
  > AIRCRAFT WAS TAXING FROM THE GATE FOR TAKEOFF. THE NOSE WHEEL STEERING BECAME UNRESPONSIVE. AIRCRAFT RETURNED TO THE GATE AREA INSPECTION REVEALED THAT THE NOSE WHEEL STEERING JACK SHAFT HAD SHEARED AT THE ROD END ATTACH AREA THE JACK WAS REPLACED AND THE AI
- [SDR AU510001957](https://openairdocs.org/sdr/AU510001957.md): Structure · damaged · May 10, 2005 · Swrngn SA227* · Ailerons
  > (AUS) DURING CONTROL CHECKS AILERONS FELT STRANGE WHEN MOVED IN LT DIRECTION. INVESTIGATION FOUND THE RT AILERON HAD SUFFERED INTERFERENCE DAMAGE WITH THE WING LOWER TRAILING EDGE CAUSING THE AILERON SKIN TO BIND WITH THE WING SKIN AND JAM. FURTHER INVESTIGATI
- [SDR O3X02098711](https://openairdocs.org/sdr/O3X02098711.md): Engine · shutdown · Feb 10, 2005 · N871JX · Bag JETSTM3201 · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED, ENROUTE, ON DESCENT, AT APPROX 1900 FT, THE RT ENGINE SHUT ITSELF DOWN. THE CREW PERFORMED EMERGENCY PROCEDURES, CLIMBED TO APPROX 6000 FT, AND SUCCESSFULLY RESTARTED THE ENGINE. CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. (K)
- [SDR O3X04129212](https://openairdocs.org/sdr/O3X04129212.md): Gasket · leaking · Dec 13, 2004 · N921AE · Bag JETSTM3201 · Turbine Engine Oil System
  > AIRCRAFT WAS ENROUTE, WHEN THE LT ENGINE LOW OIL PRESSURE WARNING ILLUMINATED, THE OIL PRESSURE STARTED TO DROP AND THE OIL TEMPERATURE INCREASED. THE ENGINE WAS SHUT DOWN AND THE AC RETURNED WITHOUT FURTHER PROBLEMS. OIL WAS LEAKING FROM THE REAR TURBINE BE
- [SDR 2005FA0000056](https://openairdocs.org/sdr/2005FA0000056.md): Line · failed · Oct 14, 2004 · N1119K · Frchld SA227DC · Hydraulic System, Main
  > MRR-M04-15, BOTH HYDRAULIC PRESSURE LOW LIGHTS CAME ON INFLIGHT. CREW CHECKED GAGE AND FOUND HYDRAULIC PRESSURE AT (0). HYDRAULIC FLUID LOSS DO TO SYSTEM LEAK. REPLACED LINE IN LEFT WHEEL WELL. LEAK CHECKED ALL SYSTEM LINES AFTER REPAIR, NO ADDITIONAL LEAK
- [SDR O3X09098801](https://openairdocs.org/sdr/O3X09098801.md): Line · cracked · Sep 9, 2004 · N880TE · Bag JETSTM3201 · Turbine Engine Oil System
  > AC DEPARTED, RT ENGINE LOST OIL PRESSURE DURING CLIMB. ENGINE OIL PRESSURE WARNING LIGHT CAME ON AND ENGINE RPM STARTED TO FLUCUTATE AND EGT WENT TO 750 DEGREES (C). RT ENGINE STOPPED AND FEATHER WAS PULLED AND ENGINE SHUT DOWN. AC RETURNED TO DEPARTURE WIT
- [SDR 2005FA0000054](https://openairdocs.org/sdr/2005FA0000054.md): Seal · pinched · Aug 11, 2004 · N853LS · Frchld SA227DC · Cargo/Baggage Doors
  > MRR-M04-12, CARGO DOOR WARNING LIGHT ON ANNUNCIATOR AND SECONDARY DOOR UNSAFE WARNING ON SIDE PANEL BOTH CAME ON DURING CLIMBOUT. CREW FOLLOWED PROCEDURES, RETURNED. CREW CHECKED CARGO DOOR HANDLE, FOUND FULLY STOWED UPON RETURN. RIGGING OR ADJUSTMENT OF DO
- [SDR AUS20040266](https://openairdocs.org/sdr/AUS20040266.md): Switch · faulty · Apr 10, 2004 · Swrngn SA227* · Cabin Cooling System
  > (AUS) LEADING EDGE DUCT THERMAL SWITCH FAULTY.
- [SDR 2005FA0000045](https://openairdocs.org/sdr/2005FA0000045.md): Door · malfunctioned · Mar 20, 2004 · N854LS · Frchld SA227DC · Cargo/Baggage Doors
  > THE CARGO DOOR WARNING LIGHT CAME ON DURING CLIMBOUT, CREW RETURNED TO THE STATION. ONE OF THE FOLLOWING: DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, DOOR CLICK CLACK RIGGING/ LUBRICATION, OR SWITCH RIGGING. ALL SWITCHES AND CLICK CLACKS WERE INSPECTED AND
- [SDR 2005FA0000044](https://openairdocs.org/sdr/2005FA0000044.md): Block · leaking · Mar 7, 2004 · N850LS · Frchld SA227DC · Propeller Controlling System
  > AFTER TURNING BLEEDS ON DURING CLIMB, CREW IMMEDIATELY NOTICED AN ODOR AND THEN SAW SMOKE. BLEEDS WERE TURNED OFF, CHECKLIST ITEMS COMPLETED. CHECKED FOR ANNUNCIATOR LIGHTS, PRESSURE INDICATIONS, AND FIRE LIGHT INDICATIONS, ALL WERE NORMAL. CREW RETURNED TO
- [SDR AUS20040109](https://openairdocs.org/sdr/AUS20040109.md): Hose · failed · Feb 13, 2004 · Bag JETSTM3201 · Hydraulic System, Main
  > (AUS) RT MAIN LANDING GEAR UPLOCK FLEXIBLE HOSE FAILED. LOSS OF HYDRAULIC FLUID.
- [SDR AUS20031262](https://openairdocs.org/sdr/AUS20031262.md): Valve · faulty · Dec 1, 2003 · Bag JETSTM3201 · Trailing Edge Flap Control System
  > (AUS) FLAP EMERGENCY RELEASE VALVE OPERATED (POPPED).
- [SDR AUS20031036](https://openairdocs.org/sdr/AUS20031036.md): Rivet · loose · Sep 25, 2003 · Cessna 441 · Elevator Structure
  > (AUS) LT HORIZONTAL STABILIZER ELEVATOR HINGE ATTACHMENT RIVETS (3OFF) LOOSE. RIVETS WERE CHERRY-MAX TYPE. FOUND DURING INSPECTION IAW AD/CESSNA400/012 AMDT3.
- [SDR AUS20030949](https://openairdocs.org/sdr/AUS20030949.md): O-Ring · leaking · Sep 11, 2003 · Bag JETSTM3201 · Propeller Hub Section
  > (AUS) RT PROPELLER LEAKING OIL. THE PROPELLER HAD JUST BEEN REMOVED AND REFITTED FOLLOWING REPAIR TO THE DEICE BOOT. NEW O-RING SEALS PN A163372 HAD BEEN FITTED AT INSTALLATION. THOROUGH INVESTIGATION COULD FIND NO REASON FOR THE LEAK.
- [SDR AUS20030850](https://openairdocs.org/sdr/AUS20030850.md): Controller · fluctuates · Aug 13, 2003 · Swrngn SA227* · Cabin Pressure Controller
  > (AUS) CABIN PRESSURISATION FLUCTUATING. INVESTIGATION CONTINUING.
- [SDR 2003F00585](https://openairdocs.org/sdr/2003F00585.md): Wire · broken · Jun 7, 2003 · N453LA · Frchld SA227DC · Electrical Power System Wiring
  > ON DESCENT TO THE STATION, HOT AIR AND SMOKE STARTED COMING OUT OF THE RIGHT BLEED, WITH THE RIGHT BLEED SHUTOFF AND DEFERRED. CREW FOLLOWED PROCEDURES AND LANDED AT THE NEXT STATION, WHICH WAS THE CLOSEST. THE FLOW CONTROL VALVE WAS RECEIVING AN UNCOMMANDED
- [SDR AUS20030426](https://openairdocs.org/sdr/AUS20030426.md): Line · cracked · Apr 13, 2003 · Swrngn SA227* · Hydraulic System, Main
  > (AUS) NUMEROUS HYDRAULIC PIPE UNIONS LOOSE. FLAP DOWN HYDRAULIC PIPE CRACKED AT WS 66.5. PIPE UNIONS LOOSE IN THE FOLLOWING AREAS:-1. HYDRAULIC BLEED AIR PIPE UNION AT WS 66.5 LT 2. BYPASS LINE UNION AT WS 81.1 LH3. FLAP UP AND DOWN PIPE UNIONS AT WS 66.5 AND
- [SDR AUS20030390](https://openairdocs.org/sdr/AUS20030390.md): Wire Harness · chafed · Mar 29, 2003 · Swrngn SA227* · Engine Starting System Wiring
  > (AUS) LT STARTER WIRING CHAFING ON STARTER RELAY BUS.
- [SDR 03X03038751](https://openairdocs.org/sdr/03X03038751.md): Arm · cracked · Mar 10, 2003 · N875AE · Bag JETSTM3201 · Rudder Control System
  > DURING A SCHEDULED INSPECTION THE RUDDER QUADRANT DRIVE ASSEMBLY WAS FOUND CRACKED AT THE RUDDER FEEL SPRING ATTACH ARM. THE FEEL SPRING ATTACH ARM IS ATTACHED IN TWO SECTIONS TO THE RUDDER QUADRANT, ONE SECTION WAS CRACKED ALL THE WAY THROUGH. IF THE ATTACH
- [SDR AUS20021366](https://openairdocs.org/sdr/AUS20021366.md): Line · cracked · Nov 27, 2002 · Swrngn SA227* · Hydraulic System, Main
  > (AUS) HYDRAULIC LINE CRACKED AT FLARE.
- [SDR AUS20021278](https://openairdocs.org/sdr/AUS20021278.md): Static Line · contaminated · Oct 30, 2002 · Swrngn SA227* · Pitot/Static System
  > (AUS) AIRCRAFT STATIC SYSTEM CONTAMINATED WITH WATER. FALSE GPWSWARNINGS DURING DESCENT.
- [SDR AUS20021236](https://openairdocs.org/sdr/AUS20021236.md): Shield · leaking · Oct 22, 2002 · Swrngn SA227* · Engine Anti-Icing System
  > (AUS) RT ENGINE FIRE WARNING LIGHTS ILLUMINATED IN FLIGHT. BOTTLES DISCHARGED. COULD FIND NO FIRE OR DAMAGE. ALL RT ENGINE FIRE DETECTORS AND FIRE BOTTLES REPLACED. DURING NEXT FLT, RT ENG FIRE WARNING AGAIN ILLUMINATED. FIRE BOTTLES AGAIN DISCHARGED. FURTHER
- [SDR AUS20021216](https://openairdocs.org/sdr/AUS20021216.md): Window · cracked · Oct 21, 2002 · Bag JETSTM3201 · Passenger Compartment Windows
  > (AUS) PASSENGER WINDOW OUTER PANE CRACKED. WINDOW IS THE THIRD WINDOW ON THE LH SIDE.
- [SDR AUS20021097](https://openairdocs.org/sdr/AUS20021097.md): Housing · unserviceable · Oct 2, 2002 · Swrngn SA227* · Hydraulic Pressure Sensor
  > (AUS) HYDRAULIC PRESSURE TRANSDUCER HOUSING SPLIT. TRANSDUCER ISLOCATED IN LT NACELLE
- [SDR AUS20021118](https://openairdocs.org/sdr/AUS20021118.md): Line · leaking · Aug 28, 2002 · Swrngn SA227* · Hydraulic System, Main
  > (AUS) LT MAIN LANDING GEAR DOWN' HYDRAULIC LINE LEAKING.
- [SDR AUS20020893](https://openairdocs.org/sdr/AUS20020893.md): Valve · leaking · Aug 9, 2002 · Bag JETSTM3201 · Hydraulic System, Main
  > (AUS) HYDRAULIC SYSTEM NON-RETURN VALVE LEAKING. SUSPECT LEAK EMANATING FROM ENGRAVED PART NUMBER IN CASE.
- [SDR AUS20020504](https://openairdocs.org/sdr/AUS20020504.md): Tube · cracked · May 30, 2002 · Swrngn SA227* · Gust Lock Damper System
  > (AUS) RUDDER GUST LOCK PLUNGER GUIDE TUBE FRACTURED APPROXIMATELY HALFWAY ALONG THE LENGTH. THE LOWER HALF OF THE FRACTURED TUBEHAD MOVED AND STARTED TO ENGAGE IN THE RUDDER GUST LOCK QUADRANTPREVENTING THE CORRECT OPERATION OF THE RUDDER.
- [SDR AUS20020342](https://openairdocs.org/sdr/AUS20020342.md): Line · leaking · Apr 10, 2002 · Swrngn SA227* · Hydraulic System, Main
  > (AUS) STAINLESS STEEL HYDRAULIC PRESSURE LINE WORN THROUGH ON ADEL CLAMP BOLT. PIPE IS LOCATED BETWEEN HYDRAULIC PUMP AND FIREWALL.
- [SDR 2002FA0000114](https://openairdocs.org/sdr/2002FA0000114.md): Deflector · damaged · Jan 7, 2002 · Turbine Section
  > P/N 3103302-1 DEFLECTOR COMPONENT OF P/N 3103783-9 SECOND STAGE TURBINE NOZZLE ASSEMBLY EXHIBITS WEAR AND MISSING MATERIAL. DAMAGE APPEARS THE RESULT OF INADEQUATE RETENTION AND SPINNING OF THE DEFLECTOR IN SERVICE. DAMAGE NOTED AT RECEIVING INSPECTION BY REP
- [SDR PNSA011009](https://openairdocs.org/sdr/PNSA011009.md): Scavenge Pump · seized · Oct 31, 2001 · N30135 · Frchld SA227DC · Turbine Engine Oil System
  > RT OIL PRESSURE LIGHT CAME ON. CREW SHUT DOWN ENGINE AND RETURNED TO CDB. MAINTENANCE FOUND EXCESSIVE OIL IN TAILPIPE AREA. ENGINE INSPECTED AND FOUND TURBINE SCAV PUMP SEIZED ALLOWING OIL TO DRAIN OVERBOARD.
- [SDR AUS20010933](https://openairdocs.org/sdr/AUS20010933.md): Acm · seized · Aug 20, 2001 · Swrngn SA227* · Cabin Cooling System
  > (AUS) RT AIR CYCLE MACHINE (ACM) SEIZED.
- [SDR AUS20010866](https://openairdocs.org/sdr/AUS20010866.md): Turbine Blades · damaged · Aug 12, 2001 · Swrngn SA227* · Turbine Section
  > (AUS) LT ENGINE INTERNAL FAILURE. TURBINE BLADES AND EXHAUST NOZZLE DAMAGED.
- [SDR AUS20010919](https://openairdocs.org/sdr/AUS20010919.md): Pump · unserviceable · Jul 31, 2001 · Bag JETSTM3201 · Engine Fuel Pump
  > (AUS) ENGINE FUEL PUMP HOUSING CRACKED IN AREA OF CONCENTRIC SHAFTSUPPORT.
- [SDR AUS20010692](https://openairdocs.org/sdr/AUS20010692.md): Pin · sheared · Jul 6, 2001 · Swrngn SA227* · Main Landing Gear
  > (AUS) RH MAIN LANDING GEAR UPPER TORQUE LINK PIN SHEARED.
- [SDR AUS20010427](https://openairdocs.org/sdr/AUS20010427.md): Hinge · broken · May 6, 2001 · Bag JETSTM3201 · Vertical Stabilizer, Attach Fittings
  > (AUS) RUDDER CENTRE HINGE BRACKET CENTRE LUG FAILED DUE TO CORROSION.

Next page: https://openairdocs.org/engine/garrett-tpe331-12ua/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 = 'TPE33112UA'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/garrett-tpe331-12ua/reports

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