Garrett TPE331-10

Service difficulty reports · 185

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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 = 'TPE33110'
  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 2023FA0000572Bearing Race · brokenTORQUE SENSOR BEARING INNER RACE FAILED [PN: 3103585-1 TSN: 1,319.2, CSN: 898].May 25, 2023 · Engine (Turbine/Turboprop)SDR X2ZR041220221None · wornTHE 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 HOApr 13, 2022 · Mtsbsi · Engine (Turbine/Turboprop)SDR CA190711009Actuator · failed(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 GEAFeb 23, 2019 · Mtsbsi MU2B60 · Landing Gear ActuatorSDR CA180423014Gear · damaged(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 NOWApr 19, 2018 · Mtsbsi MU2B60 · Propeller Indication SystemSDR 39LA20151004145Blade · crackedDURING POST FLIGHT WALK AROUND, THE FLIGHT CREW DISCOVERED ON THE LT PROPELLER ONE OF THE BLADES WAS CRACKED.Oct 4, 2015 · N602AR · Casa C212200 · Propeller Blade SectionSDR 8EKA20150630001Governor · sticksPROP GOVERNOR STUCK IN FLIGHT. ACFT RETURNED TO BASE. GOVERNOR FOUND TO BE STICKY.Jun 11, 2015 · N502FS · Casa C212200 · Propeller GovernorSDR 39LA20150430134Control Quadrant · corrodedLEFT 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.Apr 30, 2015 · N602AR · Casa C212CC · Aileron Control SystemSDR 39LA20150326110Cap · corrodedRIGHT AILERON END CAP FOUND CORRODED THROUGH, AT COUNTERWEIGHT. REPAIRED IAW COMPANY ENGINEERING ORDER 14022-300.Mar 26, 2015 · N602AR · Casa C212200 · AileronsSDR 39LA20150326112Floorbeam · corrodedFLOORBEAM UPPER CAP LT SIDE AT FS 8326, BL 20 FOUND CORRODED. REPAIRED IAW EO 14022-300, ITEM 8 16.Mar 26, 2015 · N602AR · Casa C212CC · Fuselage Main, Floor BeamSDR 39LA20150326126Structure · corrodedLEFT WING TE FLAP WELL WS 6300 EXFOLIATION CORROSION FOUND DURING HEAVY CHECK INSPECTION. REPAIRED IAW EO 14022-300.Mar 26, 2015 · N602AR · Casa C212CC · Trailing Edge FlapsSDR 39LA20150326127Spar · corrodedRIGHT WING LE SPAR WING STATION 7700 FOUND TO HAVE LEVEL 2 EXFOLIATION CORROSION. REPAIRED IAW EO 14022-300.Mar 26, 2015 · N602AR · Casa C212CC · Wing SparSDR CA141223004Adapter · broken(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.Dec 21, 2014 · Mtsbsi MU2B60 · Turbine Engine Oil SystemSDR FEHR2015FA0000030Bypass Valve · leakingWHILE 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.Dec 1, 2014 · N441G · Cessna 441 · Fuel Control/Turbine EnginesSDR CA141015002Housing · cracked(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)Oct 8, 2014 · Mtsbsi MU2B60 · Turbine Engine Oil SystemSDR 3SVA2014072100001Filter · cloggedDURING 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.Jul 21, 2014 · N441BD · Cessna 441 · Fuel Control/Turbine EnginesSDR 39LA2013112725Unknown · odorDURING 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.Nov 27, 2013 · N602AR · Casa C212CC · Air Distribution SystemSDR CA131030006Strut · cracked(CAN) DURING SCHEDULED MAGNETIC PARTICLE INSPECTION THE RT NLG STRUT WAS FOUND CRACKED. PART WAS REPLACED AND ACFT RETURNED TO SERVICE.Oct 30, 2013 · Mtsbsi MU2B60 · Nose/Tail Landing Gear Strut/AxleSDR CA131022007Wire · damaged(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 1Oct 22, 2013 · Mtsbsi MU2B60 · Ice/Rain Protection System WiringSDR CA130327003Adapter · cracked(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.Mar 26, 2013 · Mtsbsi MU2B60 · Engine Bleed Air SystemSDR 39LA2013020600014Engine · power lossDURING 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.Feb 5, 2013 · N607AR · Casa C212CD · Engine (Turbine/Turboprop)SDR CA130109005Angle · cracked(CAN) FOUND ANGLE CRACKED DURING SCHEDULED INSPECTION.Jan 8, 2013 · Mtsbsi MU2B60 · Fuselage Miscellaneous StructureSDR 3SVAN441BD91912Engine · flamed outRIGHT ENGINE FLAMED OUT ON CLIMBOUT OF ANC. PLIOT SECURED THE ENGINE AND RETURNED TO BASE.Sep 18, 2012 · N441BD · Cessna 441 · Engine (Turbine/Turboprop)SDR EHAA20120824007Gearbox · inoperativeDURING 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 DAug 24, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)SDR P4YA2012091200001Cable · separatedDURING HEAVY CHECK, FOUND NR 1 ENGINE TELEFLEX CABLE DAMAGED/PULLED APART AT THE SWAGE HOUSING.Aug 24, 2012 · N962BW · Casa C212200 · Engine ControlsSDR EHAA20120731006Engine · power lossDURING CLIMB, NR 2 ENGINE EGT DROPPED TO ZERO AND ENGINE LOST POWER.Jul 31, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)SDR CA120703006Engine · flamed out(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.Jun 28, 2012 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)SDR CA120605007Rod End · broken(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.May 23, 2012 · Mtsbsi MU2B60 · Landing Gear Door Retract SectionSDR 3RAA2012212001Mount Bracket · brokenDURING 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 THMar 29, 2012 · N467CS · Casa C212200 · Rudder Control SystemSDR CA111205007Oil Filter · damaged(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 INNov 29, 2011 · Swrngn SA226TC · Turbine Engine Oil SystemSDR CA111108003Engine · shutdown(CAN) DURING CLIMBOUT, RT ENGINE SHUTDOWN, ENGINE WAS SECURED AND ACFT LANDED WITH 1 ENGINE, WITHOUT INCIDENT. AWAITING ENGINE TEARDOWN REPORT FOR FURTHER INFORMATION.Nov 7, 2011 · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)SDR CA110805002Clamp · wornAFTER 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 FAug 4, 2011 · Mtsbsi MU2B60 · Flight Compartment EquipmentSDR CA110622006Starter Gen · failedSTARTER GENERATOR FAILED - ENGINE START ABORTED. REPLACED STARTER GEN WITH SERVICEABLE START GEN - ENGINE START NORMAL - ACFT RETURNED TO SERVICE.Jun 19, 2011 · Dhav DHC3 · Starter-GeneratorSDR CA110430001Isolator · corroded(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 REApr 30, 2011 · Gulstm 695A · Engine Mount SectionSDR CA110406006Oil Cap · worn(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 & THEApr 1, 2011 · Mtsbsi MU2B60 · Turbine Engine Oil SystemSDR BIGA01/28/11Pin · missingTHE 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 IDENTJan 28, 2011 · N117BH · Casa C212200 · Propeller Hub SectionSDR SROM2010016Servo · jammedRUDDER 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 OUNov 22, 2010 · N405CP · Casa C212 · Rudder Control SystemSDR CA101116011Limit Switch · frozenAFTER 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 INov 15, 2010 · Mtsbsi MU2B60 · Landing Gear Position and WarningSDR CA101012010Gyro · inaccurateLT 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.Oct 8, 2010 · Bag JETSTM3112 · Attitude Gyro and Indicating SystemSDR P4YA2010031600001Skin · crackedDURING 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 Apr 14, 2010 · N967BW · Casa C212CD · Wing, Center BoxSDR CA100112001Wheel · cracked(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 NRJan 6, 2010 · Mtsbsi MU2B60 · Wheel/Ski/FloatSDR CA091006002Motor · intermittent(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 DOOct 2, 2009 · Mtsbsi MU2B60 · Landing Gear ActuatorSDR CA090424003Hinge · cracked(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.Apr 17, 2009 · Mtsbsi MU2B60 · Landing Gear DoorsSDR CA081027001Shaft · binding(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 LUBROct 23, 2008 · Mtsbsi MU2B36 · Propeller Controlling SystemSDR CA081007006O-Ring · failed(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 LOCKOct 7, 2008 · Bag JETSTM3112 · Hydraulic System, MainSDR BKA2008F00000Engine · shutdownDEPARTING , 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 TOAug 27, 2008 · N8083A · Mtsbsi MU2B60 · Engine (Turbine/Turboprop)SDR CA080902002Battery · thermal runaway(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 BATTERAug 27, 2008 · Mtsbsi MU2B60 · Battery/Charger SystemSDR CA080821006Attach Fitting · cracked(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.Aug 18, 2008 · Mtsbsi MU2B60 · Nose/Tail Landing Gear Attach SectionSDR WIW2008F00000Torque Sensor · failedON 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 ALLOAug 13, 2008 · N30591 · Ayres S2RHGT65 · Engine BMEP/Torque IndicatingSDR CA080623002Motor · inoperative(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/MOJun 19, 2008 · Mtsbsi MU2B60 · Landing Gear Retraction/Extension SystemSDR CA080613010Lock Plate · worn(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.Jun 11, 2008 · Mtsbsi MU2B60 · Propeller Controlling System
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