Garrett TPE331-11U
Service difficulty reports · 625
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 = 'TPE33111U' 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 = 'TPE33111U' 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 CA000321002Blade · cracked(CAN) 30 1ST STAGE TURBINE BLADES FOUND CRACKED ON LEADING EDGE ADJACENT TO THE LEADING EDGE TIP CORNER. CRACKS SEEM TO HAVE ORIGINATED FROM THE COOLING HOLES LOCATED AT THE BLADE TIPS. FAA, HONEYWELL AND OPERATOR INFORMED OF E-MAIL GENERATED FROM THIS OFFICESDR 20000427SH007Computer · malfunctionedHLN - FLT 2585 - LEFT ENGINE BYPASS LIGHT CAME ON. TORQUE REDUCED TO 35 PERCENT, THEN BYPASS LIGHT CYCLED ON AND OFF. CREW DECLARED EMERGENCY AND RETURNED TO HELENA. LEFT ENGINE SRL COMPUTER FAILURE. SRL COMPUTER WAS DEFERRED PER MEL, FLIGHT RESUMED AND COMSDR CA000224033Windshield · cracked(CAN) RIGHT WINSHIELD CRACKED DURING CLIMB.SDR PNSA000104Wire · chafedDURING CLIMB AND IN IMC WITH SNOW LT IGNITION CB POPPED AND WOULD NOT RESET. RETURNED TO BASE, FOUND WIRE CHAFED AT CENTER WING FAIRING FEED THROUGH BL 0.0. REPAIRED WIRE, OPS CHECKED OK.SDR CA000118042Starter Gen · failed(CAN) ENGINE FAILED TO ROTATE AT START UP.SDR CA991209070Switch · shorted(CAN) DURING TAXI, THE CREW DETECTED A BURNING PLASTIC SMELL. THE CREW NOTICED THE ANNUNCIATOR PANEL GO ON AND OFF AS WELL AS LOSING SOME INDICATORS. THE AIRCRAFT RETURNED TO BASE FOR MAINTENANCE. THE MAINTENANCE CREW DETERMINED THAT THE GPS/NAV SWITCH HAD SHOSDR CA991103009Brush · cracked(CAN) 5 MINUTES AFTER TAKEOFF, THE RIGHT GENERATOR WENT OFF-LINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE DETERMINED THAT THE STARTER/GENERATOR BRUSHES HAD CRACKED AND THE LEADS HAD SEPARATED FROM THE REMAINING BRUSH MATERIAL.SDR CA991028010Line · cracked(CAN) ALUMINUM HYDRAULIC LINE CRACKED AT CLAMP POINT IN FORWARD CONTAINMENT BAG. SUBMITTER SUGGESTED CLAMP WAS IMPROPERLY INSTALLED AT THE FACTORY.SDR CA991007073Motor · overheated(CAN) AFTER TAKEOFF, THE CREW SMELLED SMOKE/BURNING SMELL. AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE INVESTIGATED AND FOUND THE WIPER MOTOR TOO HOT TO TOUCH. CREW REPORTED THAT ON THE PREVIOUS FLIGHT, THE WIPER SYSTEM CAME ON, THEN WENT OFF.SDR AU990955Wire · failed(AUS) LEFT ENGINE OVERHEAT DETECTOR WIRING HARNESS CHAFED AND SHORT CIRCUITED BENEATH HEAT SHRINK. FALSE FIRE WARNING RESULTED IN DISCHARGE OF FIRE EXTINGUISHER.SDR PNSA990701Seal · wornWHILE TAXIING TO RUNWAY WITH LT ENGINE RPM AT LOW, OIL TEMPURATURE CLIMBED TO RED LINE. AIRCRAFT RETURNED TO GATE. REPLACED ASPIRATOR SEAL. AIRCRAFT RETURNED TO SERVICE.SDR CA990728050Engine · failed(CAN) E.G.T. ERRATIC. FAULTY CONNECTION ON LEAD FROM TEMP TRANSMITTER.SDR AU990587Brake · faulty(AUS) LT MAIN LANDING GEAR BRAKE ASSEMBLY OVERHEATED AND CAUSED PAINT AND GREASE ON THE WHEEL TO CATCH FIRE. SUSPECT CAUSED BY A PINCHED PISTON SEAL WHICH OCCURRED DURING ASSEMBLY.SDR PNSA990502Gasket · rupturedDURING CLIMBOUT, RT ENGINE FIRE LIGHTS ILLUMINATED. ENGINE WAS SECURED AND AIRCRAFT RETURNED FOR AN UNEVENTFUL LANDING. P-3 GASKET AT THE 4 O'CLOCK (FACING FORWARD) PRIMARY NOZZLE BLANK OUT PLUG WAS FOUND BLOWN OUT. REPLACED GASKET, FLIGHT CHECK WAS SATISFSDR PNSA990505Engine · surgedRT ENGINE SURGED ON TAKEOFF. TAKEOFF WAS ABORTED. PILOT DETERMINED THE ENGINE HAD SURGED DUE TO TEMP LIMITER BYPASS. SECOND TAKEOFF WAS NORMAL NO FURTHER PROBLEMS NOTED.SDR PNSA990504Indicator · malfunctionedLT ENGINE POWER FLUCTUATING DURING CRUISE. AIRCRAFT WAS FERRIED BACK TO ANC FOR MAINTENANCE. REPLACED EGT INDICATOR, OPERATIONAL CHECK OK. AIRCRAFT EXPERIENCED NO FURTHER PROBLEMS.SDR CA990521049Roll Pin · sheared(CAN) ON APPROACH, THE RT ENGINE TACHOMETER BECAME ERRATIC THEN DROPPED TO ZERO RPM. MAINTENANCE FOUND THE TACH GENERATOR DRIVE SHAFT ROLL PIN SHEARED.SDR AU990430026Pump · worn(AU) NR 1 ENGINE HYDRAULIC WARNING LIGHT CAME ON PRIOR TO LANDING. ON NR 2 ENGINE SHUTDOWN, THE HYDRAULIC PRESSURE WENT TO ZERO. FLUID LEVEL CHECKED WITHIN LIMITS. NR 1 ENGINE HYDRAULIC PUMP DRIVE SPLINES WERE FOUND WORN BEYOND LIMITS DUE TO PUMP SEIZURE. SDR AU990321Throttle · broken(AUS) LEFT POWER LEVER BROKEN IN TWO DUE TO CHAFING ON THE PEDESTAL. EVIDENCE OF CORROSION ON THE POWER LEVER. THE LEVER HAD BEEN INCORRECTLY REPAIRED AND WAS HELD TOGETHER WITH LOCKWIRE.SDR CA990330050Blade · fractured(CAN) NR 1 ENGINE WAS SHUTDOWN ON TAKEOFF DUE TO A LOUD BANG FOLLOWED BY A DROP IN OIL PRESSURE. POST-TAKEOFF INSPECTION FOUND 1ST STAGE COMPRESSOR BLADE FAILED DUE TO AN INCLUSION CRACK. EVERYTHING DOWNSTREAM WAS DAMAGED BEYOND REPAIR. THE ENGINE WAS REPLACSDR PNSA990204Governor · out of adjustAT ROTATION LT ENGINE RPM DROPPED 5 PERCENT. FLIGHT CREW REPORTED THAT POWER LEVER WAS NOT RESPONDING NORMALLY AND SPEED COULD NOT BE RETURNED TO 100 PERCENT. FLIGHT CREW ELECTED TO BURN FUEL LOAD DOWN TO LANDING WEIGHT AND THEN MADE AN UNEVENTFUL LANDING. SDR CA990311021Switch · intermittent(CAN) RIGHT MLG DOWN LIGHT INTERMITTENT. RIGHT MLG SWITCH REPLACED.SDR CA990311018Line · cracked(CAN) GEAR DOWN LINE FOUND CRACKED COMING FROM POWER PACK.SDR CA990311015Line · chafed(CAN) HYDRAULIC PUMP BYPASS LINE, RT NACELLE AFT OF FIREWALL, CHAFED THROUGH AGAINST PRESSURE HYDRAULIC LINE RESULTING IN TOTAL LOSS OF HYDRAULIC FLUID. BOTH LINES REPLACED.SDR CA990311016Switch · out of rig(CAN) GEAR FAILED TO FULLY RETRACT WHEN COLD. GEAR UP SWITCHES RIGGED IAW MM SYSTEM SERVICEABLE.SDR CA990311012Actuator · worn(CAN) VIBRATION FELT IN THE RUDDER PEDALS DURING CRUISE. TAB ACTUATOR AS FOUND OUT OF LIMITS AND REPLACED.SDR 99ZZZM36Bypass Valve · inoperativeDURING TAKEOFF FROM POS, THE RIGHT ENGINE EXPERIENCED A LOSS OF TORQUE AND THE TAKEOFF WAS ABORTED. A STATIC RUN UP WAS COMPLIED WITH FOR BOTH ENGINES AND WAS SATISFACTORY. THE CAPTAIN ATTEMPTED A SECOND TAKEOFF, THE LOSS OF TORQUE WAS EXPERIENCED AGAIN AND SDR CA990311026Brush Block · misinstalled(CAN) PILOT REPORTED A STRONG SMELL OF RUBBER AND THE PROPELLER CIRCUIT BREAKER TRIPPED. ON LANDING, SEVERAL PASSENGERS REPORTED SEEING SPARKS FROM THE FRONT OF THE ENGINE. INSPECTION FOUND THE BRUSH BLOCK WAS NOT SHIMMED EVENLY AND THERE WAS EVIDENCE OF BIRSDR CA981209011Wire · chafed(CAN) AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT AND LANDING GEAR CIRCUIT BREAKER WAS TRIPPED. MAINTENANCE FOUND THAT THE INSULATION ON THE WIRE COMING FROM DIODE 309 AT TS 305/TS 311 WAS WORN ALLOWING IT TO SHORT OUT.SDR PNSA981102Fuel Control · out of adjustLEFT ENGINE DID NOT REACH TARGET TORQUE, ABORTED TAKE-OFF. ADJUSTED MAX POWER FUEL FLOW SUBSEQUENT OPS CHECK OF TORQUE OK, AIRCRAFT RETURNED TO SERVICE.SDR CA981125075Line · loose(CAN) AIRCRAFT LOST ALL HYDRAULIC PRESSURE AND FLUID AND RETURNED TO BASE. AIRCRAFT HAD A LOOSE FITTING WHICH ALLOWED FLUID TO ESCAPE. LINE SECURED.SDR CA981125072Wire · chafed(CAN) WHEN GEAR SELECTED UP, THE GEAR REMAINED IN THE DOWN POSITION. AIRCRAFT RETURNED TO BASE. WIRING TO SQUAT SWITCH FOUND CHAFED AND WAS REPAIRED.. PART TC: 9,574.SDR AU981651Line · leaking(AUS) DURING CRUISE, THE LT 'RED' HYDRAULIC ANNUNCIATOR LIGHT ILLUMINATED AND HYDRAULIC PRESSURE DROPPED TO ZERO. GROUND INVESTIGATION FOUND A HYDRAULIC PIPE HAD CHAFED AGAINST THE OIL TANK CAUSING A PIN HOLE LEAK.SDR CA981125068Trim Actuator · seized(CAN) RUDDER TRIM SEIZED IN-FLIGHT. AIRCRAFT LANDED OK.SDR CA981125067Trim Actuator · seized(CAN) RUDDER TRIM SEIZED IN-FLIGHT. AIRCRAFT RETURNED OK. ACTUATOR REPLACED.SDR CA981125064Actuator · malfunctioned(CAN) LINEAR ACTUATOR FAILED THE SERVICE LETTER 227-SL-031 3.C (22)-(25) BY 0.011 INCH. PART TC: 2,884.SDR CA980825022Valve · failed(CAN) NR 1 ENGINE WOULD NOT SHUT OFF WITH THE STOP BUTTON. THE FUEL SHUTOFF VALVE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 98ZZZM689Engine · failedMIA-ZQA - DURING TAKEOFF, THE RIGHT ENGINE WOULD NOT MAKE CHARTED TORQUE AND THE TAKEOFF WAS ABORTED. MAINTENANCE INSPECTED THE ARICRAFT AND FOUND IT SAFE FOR A FERRY FLIGHT. AIRCRAFT WAS FERRIED TO OPF FOR MAINTENANCE AND THE RIGHT ENGINE WAS REMOVED AND RESDR CA980818024Pump · worn(CAN) HYDRAULIC PUMP FAILURE ON LEFT SIDE FOLLOWING GEAR RETRACTION. PUMP SPLINES HAD WORN OFF UNTIL THEY STARTED TO SLIP. PUMP HARD TO TURN INDICATING A SPLINE PROBLEM.SDR CA980724041Water Injector · failed(CAN) ON TAKEOFF WHEN WATER METHANOL WAS SELECTED, BOTH ENGINES LOST POWER. WATER METHANOL WAS TURNED OFF AND ENGINE POWER WAS REGAINED. INSPECTION FOUND THE METHANOL MIXTURE HIGH IN WATER CONTENT. WATER METHANOL SERVICE HAS BEEN DISCONTINUED UNTIL CAUSE CASDR CA980724043Torque Knee · cracked(CAN) UPPER TORQUE KNEE FOUND CRACKED IN THE MACHINED RADIUS PER SERVICE BULLETIN 32-041. THIS IS 4TH UPPER TORQUE KNEE FOUND CRACKED BY THIS OPERATOR.SDR CA980707056Engine · malfunctioned(CAN) NEWLY OVERHAULED ENGINE STARTED HOTTER THAN NORMAL. AFTER EXTENSIVE TROUBLESHOOTING THE ENGINE WAS REMOVED FOR FURTHER INVESTIGATION. AWAITING INFORMATION.SDR CA980707057Rivets · loose(CAN) NOISE EMITTING FROM ENGINE FOUND TO BE LOOSE RIVETS. ENGINE REMOVED FOR REPAIR. PART TC: 3,008.SDR AU980633Fcu · faulty(AUS) ENGINE FUEL CONTROL UNIT FAULTY.SDR CA980707054Bearing · failed(CAN) COULD NOT GET GENERATOR ON LINE AND AIRCRAFT RETURNED TO BASE. STARTER/GENERATOR BEARING HAD LET GO. PART TC: 677.SDR PNSA980502Lever · out of positionRPM ROLLED BACK ON BOTH MOTORS DURING TAKEOFF ROLL. TAKEOFF ABORTED. PILOT NOTED SPEED LEVERS WERE NO LONGER IN THE TAKEOFF POSITION. SPEED LEVERS RESET AND FRICTION LOCKS SET, NEXT TAKEOFF UNEVENTFUL. NO FAULTS FOUND.SDR AU980553Pipe · cracked(AUS) DP/P TRANSDUCER RIGID SUPPLY PIPE CRACKED AROUND BEND RADIUS.SDR CA980602067Temp Limiter · malfucntioned(CAN) AIRCRAFT LIMITING FUEL ON RIGHT HAND ENGINE AT 620 DEGREES CELSIUS. TEMPERATURE LIMITER SYSTEM WAS DEFERRED, AND SYSTEM DISABLED BY PULLING TEMPERATURE LIMITER CIRCUIT BREAKER. UNKNOWINGLY, THIS ALSO DISABLED THE WATER METHONAL ON THE SAME SIDE. NO INSDR CA980529016Control Cable · damaged(CAN) DURING INSPECTION, A BROKEN STRAND OF WIRE WAS FOUND ON THE ELEVATOR DOWNSPRING CABLE. WHEN CABLE WAS REMOVED, OTHER AREAS WERE FOUND BROKEN.SDR AU980516Pump · failed(AUS) ENGINE TURBINE OIL SCAVENGE PUMP DRIVE GEAR TEETH MISSING. TURBINE SEAL AND TURBINE ALSO DAMAGED.
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