Garrett TPE331-12UA
Service difficulty reports · 344
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 = 'TPE33112UA' 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 = 'TPE33112UA' 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 VPOA2015F00041Fire Detector · false indicationLEFT 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 INVESTIGATINSDR CA150501009Ring · misinstalled(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 INSSDR CA140326017Annunciator · failed(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 CA121210010Boss · cracked(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 SERVISDR CA120720001Hose · failed(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, ONSDR CA111121001Spinner · iced(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 NSDR P4YA2010112800001Spar · crackedDURING 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 CA090925002Fcu · leaking(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 CA070108009Engine · damaged(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 O3X06119211Turbine · crackedCANNED 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 ISDR O3X04229241Engine · flamed outAIRCRAFT 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 LOUSDR O3X06039221Switch · malfunctionedTHE 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 THSDR AU510001677Engine · fluctuates(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 AU510001678Fcu · faultyLT ENGINE EGT, TORQUE AND FUEL FLOW FLUCTUATING. FUEL CONTROL UNIT CHANGED. GROUND RUN AND TEST FLIGHT CARRIED OUT SERVICEABLE.SDR SIMA200531501Battery · dischargedCREW 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 O3X06089371Piston Rod · crackedAIRCRAFT 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 AISDR AU510001957Structure · damaged(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 INVESTIGATISDR O3X02098711Engine · shutdownAIRCRAFT 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 O3X04129212Gasket · leakingAIRCRAFT 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 BESDR 2005FA0000056Line · failedMRR-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 LEAKSDR O3X09098801Line · crackedAC 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 WITSDR 2005FA0000054Seal · pinchedMRR-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 DOSDR AUS20040266Switch · faulty(AUS) LEADING EDGE DUCT THERMAL SWITCH FAULTY.SDR 2005FA0000045Door · malfunctionedTHE 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 ANDSDR 2005FA0000044Block · leakingAFTER 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 TOSDR AUS20040109Hose · failed(AUS) RT MAIN LANDING GEAR UPLOCK FLEXIBLE HOSE FAILED. LOSS OF HYDRAULIC FLUID.SDR AUS20031262Valve · faulty(AUS) FLAP EMERGENCY RELEASE VALVE OPERATED (POPPED).SDR AUS20031036Rivet · loose(AUS) LT HORIZONTAL STABILIZER ELEVATOR HINGE ATTACHMENT RIVETS (3OFF) LOOSE. RIVETS WERE CHERRY-MAX TYPE. FOUND DURING INSPECTION IAW AD/CESSNA400/012 AMDT3.SDR AUS20030949O-Ring · leaking(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 AUS20030850Controller · fluctuates(AUS) CABIN PRESSURISATION FLUCTUATING. INVESTIGATION CONTINUING.SDR 2003F00585Wire · brokenON 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 AUS20030426Line · cracked(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 AUS20030390Wire Harness · chafed(AUS) LT STARTER WIRING CHAFING ON STARTER RELAY BUS.SDR 03X03038751Arm · crackedDURING 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 ATTACHSDR AUS20021366Line · cracked(AUS) HYDRAULIC LINE CRACKED AT FLARE.SDR AUS20021278Static Line · contaminated(AUS) AIRCRAFT STATIC SYSTEM CONTAMINATED WITH WATER. FALSE GPWSWARNINGS DURING DESCENT.SDR AUS20021236Shield · leaking(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. FURTHERSDR AUS20021216Window · cracked(AUS) PASSENGER WINDOW OUTER PANE CRACKED. WINDOW IS THE THIRD WINDOW ON THE LH SIDE.SDR AUS20021097Housing · unserviceable(AUS) HYDRAULIC PRESSURE TRANSDUCER HOUSING SPLIT. TRANSDUCER ISLOCATED IN LT NACELLESDR AUS20021118Line · leaking(AUS) LT MAIN LANDING GEAR DOWN' HYDRAULIC LINE LEAKING.SDR AUS20020893Valve · leaking(AUS) HYDRAULIC SYSTEM NON-RETURN VALVE LEAKING. SUSPECT LEAK EMANATING FROM ENGRAVED PART NUMBER IN CASE.SDR AUS20020504Tube · cracked(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 AUS20020342Line · leaking(AUS) STAINLESS STEEL HYDRAULIC PRESSURE LINE WORN THROUGH ON ADEL CLAMP BOLT. PIPE IS LOCATED BETWEEN HYDRAULIC PUMP AND FIREWALL.SDR 2002FA0000114Deflector · damagedP/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 REPSDR PNSA011009Scavenge Pump · seizedRT 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 AUS20010933Acm · seized(AUS) RT AIR CYCLE MACHINE (ACM) SEIZED.SDR AUS20010866Turbine Blades · damaged(AUS) LT ENGINE INTERNAL FAILURE. TURBINE BLADES AND EXHAUST NOZZLE DAMAGED.SDR AUS20010919Pump · unserviceable(AUS) ENGINE FUEL PUMP HOUSING CRACKED IN AREA OF CONCENTRIC SHAFTSUPPORT.SDR AUS20010692Pin · sheared(AUS) RH MAIN LANDING GEAR UPPER TORQUE LINK PIN SHEARED.SDR AUS20010427Hinge · broken(AUS) RUDDER CENTRE HINGE BRACKET CENTRE LUG FAILED DUE TO CORROSION.
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