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 AUS20031016Wire · worn(AUS) CHAFED WIRES WITHIN LOOM LOCATED IN RT ENGINE NACELLE.SDR 505091703B-Nut · looseENROUTE TO DESTINATION, AIRPORT CREW NOTICED THE ILLUMINATION OF THE LOW HYDRALIC PRESSURE ANNUNCIATORS FOLLOWED BY A DECREASE IN HYDRAULIC SYSTEM PRESSURE ON THE PRESSURE GAUGE. CREW RETURNED TO THE DEPARTURE AIRPORT AND PERFORMED MANUAL GEAR EXTENSION AND LSDR AUS20030939Plunger · cracked(AUS) RUDDER GUST LOCK ASSEMBLY PLUNGER CORRODED, BENT AND CRACKED.SDR AUS20030880Actuator · faulty(AUS) PITCH TRIM ACTUATOR ROD ENDS HAD EXCESSIVE FREE PLAY. FOUND DURING INSPECTION IAW AD/SWSA226/68A5.SDR AUS20030883Fitting · cracked(AUS) HORIZONTAL STABILIZER PITCH TRIM ACTUATOR UPPER ATTACHMENT BRACKETS CRACKED ALONG LUG. FURTHER INVESTIGATION REVEALED THAT THERE WAS CONSIDERABLE CLEARANCE BETWEEN THE BUSHINGS AND ACTUATOR ROD ENDS WHICH RESULTED IN THE LUGS BEING STRESSED WHEN THE ATTASDR 510082703Blade · brokenDURING ROUTINE MAINTENANCE IT WAS DISCOVERED THAT APPROXIMATELY .7500 OF ONE THIRD STAGE TURBINE BLADE HAD BROKEN OFF AND EXITED OUT THE TAIL PIPE CAUSING DAMAGE TO THE TAIL PIPE AND SCAVENGE PUMP COVER. THE THIRD STAGE T-WHEEL ASSEMBLY HAS A SERVICE LIFE OF SDR AUS20030884Line · leaking(AUS) HYDRAULIC PRESSURE LINE LOCATED IN AREA BELOW PILOTS RUDDER PEDALS CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID.SDR AUS20030853Elbow · cracked(AUS) RT PROPELLER GOVERNOR OUTLET PRESSURE ELBOW CRACKED IN AREA ABOVE LOCKNUT.SDR AUS20030715Line · corroded(AUS) LANDING GEAR RETRACTION SYSTEM HYDRAULIC LINE CORRODED AND LEAKING.SDR AUS20030644Bushing · missing(AUS) PITCH TRIM SERVO ACTUATOR LOWER ATTACHMENT POINT PIVOT BUSHING MISSING AND ATTACHMENT BOLTS WORN.SDR CA030702004Governor · failed(CAN) ON TAKEOFF ROLL LT ENGINE DID NOT PRODUCE TORQUE FOR TAKEOFF (PROP PARTIALLY CAME OFF LOCKS). ABORTED TAKEOFF. RETURNED TO MAINTENANCE FACILITY.SDR PNSA030601Limiter · faultyDURING TAKEOFF ROLL RT ENGINE AUTOMATIC TEMP LIMITER SYSTEM CAME ON BYPASSING FUEL WITH AN ASSOCIATED DROP IN TORQUE. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PROBLEM, DEFERRED TEMP LIMITER SYSDR AUS20030665Housing · damaged(AUS) SECOND STAGE COMPRESSOR HOUSING PLASMA METAL COATING SEPARATED CAUSING BLOCKAGE OF NOZZLE VANE SEGMENT COOLING AIR SLOTS INFIRST STAGE TURBINE NOZZLE AND METAL SPRAY DEPOSITS ON DIFFUSER VANES.SDR AUS20030573Actuator · faulty(AUS) RUDDER TRIM TAB ACTUATOR FAULTY.SDR 20035Lock · wornAFTER TAKEOFF AT APPROXIMATELY 600 FEET AGL, PILOT REPORTED THAT BOTH LEFT AND RIGHT FUEL BY-PASS ANNUNCIATORS ILLUMINATED, ACOMPANIED WITH PRONOUNCED ENGINE SURGING. AIRCRAFT RETURNED TO AIRPORT FOR UNEVENTFUL LANDING. MAINTENANCE LATER DETERMINED THAT THE SDR CA030410006Tube · fractured(CAN) LH AND RH ENGINE WOULD NOT DEVELOP TARGET TORQUE OF THE DAY.LH ENGINE HAD A BROKEN P3 TUBE ALLOWING EXCESSIVE COMPRESSOR LEAK.RH ENGINE HAD POWER PERFORMANCE PROBLEM DUE TO TEMPERATURE OF THE DAY.RH ENGINE WAS REPLACED AND P3 TUBE WAS REPLACED ON LH ENGISDR AUS20030385Control Cable · worn(AUS) RT RUDDER CONTROL CABLE WORN BEYOND LIMITS.SDR AUS20030180Yoke · cracked(AUS) LT MAIN LANDING GEAR YOKE CRACKED ON INNER SURFACE EXTENDING FROM THE FILLER VALVE UPWARDS FOR A LENGTH OF 10MM (0.393IN). FOUNDDURING ULTRASONIC INSPECTION.SDR AUS20030584Nozzle · blocked(AUS) ENGINE FUEL NOZZLES PARTIALLY BLOCKED.SDR CA030106009Line · chafed(CAN) AIRCRAFT EXPERIENCED A LOSS OF HYDRAULIC FLUID AND PRESSURE IN FLIGHT. EMERGENCY EXTENSION CARRIED OUT WITH A SAFE LANDING. CHAFED HYDRAULIC LINES FOUND RUBBED THROUGH BY PLASTIC DRAIN LINE IN LT NACELLE. HYDRAULIC LINES FOUND CHAFED WERE PN 2781006475 SDR 12190279Turbine Blades · failedAFTER TAKEOFF, TOWER REPORTED THAT AIRCRAFT WAS TRAILING SMOKE. THE NR 1 ENGINE LOSS OF OIL PRESSURE FOLLOWED BY OIL WARNING LIGHT. ELECTED TO SHUT ENGINE DOWN AND RETURN TO AIRPORT. SUBSEQUENT INSPECTION REVILED THAT A PROBABLE FAILURE OF ONE OR MORE 1ST STSDR AUS20021482Hub · cracked(AUS) FOLLOWING PILOT REPORTS OF PROPELLER VIBRATION, AN ULTRASONIC EXAMINATION WAS CARRIED OUT ON THE PROPELLER HUB. ONE CRACK LIKEDEFECT WAS DETECTED ADJACENT TO A THREADED INSERT HOLE. THE CRACK WAS LOCATED AT A DEPTH OF 13MM (0.512IN) AND HAD A LENGTH OFAPSDR AUS20021329Hub · cracked(AUS) PROPELLER HUB SUSPECT CRACKED IN TWO ADJACENT MOUNTING BOLT HOLES. FOUND DURING INSPECTION IAW DOWTY ROTOL SB/61/1125.SDR CA021105004Warning Light · false activation(CAN) AFTER TAKE-OFF AND AS THE AIRCRAFT BEGAN TO PRESSURIZE THE CARGO DOOR WARNING LIGHT ILLUMINATED. THECREW REQUESTED A RETURN TO BASE AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTION OF THE AIRCRAFT DET ERMINED THAT A FALSE WARNING INDICATION OF THE CARGO DSDR CA021105003Indicator · failed(CAN) UPON SELECTION OF THE LANDING GEAR ON APPROACH , THE NOSE DID NOT INDICATE DOWN AND LOCK. THE UNSAFE ANNUNCIATOR WAS NOT ILLUMINATED SUGGESTING THAT THE NOSE WAS EXTENDED. LAMP TEST OF THE NOSE LIGHT DID NOT WORK EITHER. THE NOSE GEAR COULD BE SEEN AS EXSDR CA021104004Line · chafed(CAN) IN CRUISE RT ENGINE BEGAN TO LOOSE TORQUE WITHIN 5-10 SECONDS. ENGINE TEMP DROPPED TO 400 DEGREES IN 30 SECONDS. PROP FEATHERED AND ENGINE SHUTDOWNN PROCEDURES CARRIED OUT. AIRCRAFT LANDED AND MAINTENANCE CREW DISPATCHED FROM YVR. FUEL LINE CHAFED.SDR AUS20021241Wire Harness · damaged(AUS) AIRCRAFT WIRING LOOM LOCATED UNDER THE FLOOR PLATE TO THE REAR OF THE LT COCKPIT BULKHEAD DAMAGED. INVESTIGATION FOUND TWELVE WIRES IN THE LOOM WERE BURNT. SUSPECT CAUSED BY DRILL DAMAGE. PERSONNEL/MAINTENANCE ERROR.SDR CA021009030Circuit Breaker · failed(CAN) AFTER LANDING THE NOSE WHEEL STEERING FUNCTION FAILED WHILE ATTEMPTING TO TAXI. THE AIRCRAFT WAS INSPECTED AND THE PROBLEM WAS TRACED TO A FAULTY CIRCUIT BREAKER WHICH HAD FAILED TO SUPPLY POWER TO POWER STEERING UNIT. CIRCUIT BREAKER WAS REPLACED AND SYSDR AUS20021113Warning System · faulty(AUS) LANDING GEAR INDICATIONS INCORRECT. GROUND RETRACTION TESTS COULD NOT DUPLICATE THE DEFECT.SDR CA021009029Connector · dirty(CAN) AFTER DEPARTURE FROM AIRPORT THE PILOT OBSERVED ABNORMAL/FLUCTUATING TORQUE AND EGT INDICATIONS FOR LT ENGINE. THE AIRCRAFT RETURNED TO BASE. WIRING CONNECTOR PLUG FOR SRL COMPUTER WAS CLEANED AND SRL COMPUTER WAS RE-CALIBRATED PER DATA SHEET, RUN-UP ANDSDR AUS20021054Engine · fire(AUS) LT ENGINE FIRE ON START UP. A BURST OF FLAME EXITED FROM EXHAUST AND COMPRESSOR. A SMALL FIRE IN THE TAILPIPE SELF EXTINGUISHED. THE TURBINE GLOWED RED FOR APPROXIMATELY TWO TO THREE MINUTES.THE ENGINE LOCKED UP AND WOULD NOT ROTATE.SDR AUS20021085Solenoid Valve · failed(AUS) FLAP SOLENOID VALVE FAULTY. VALVE COIL HAD SHORT CIRCUITED. VALVE IS LOCATED IN HYDRAULIC POWER PACK.SDR AUS20020989Hub · cracked(AUS) PROPELLER HUB CRACKED IN AREA ADJACENT TO THE BOTTOM OF THE MOUNTING BOLT INSERT. CRACK DEPTH APPROXIMATELY 13MM (0.51IN) TO 15MM (0.59IN). FOUND USING ULTRASONIC INSPECTION.SDR AUS20020977Manifold · cracked(AUS) LH ENGINE SECONDARY FUEL MANIFOLD CRACKED IN AREA OF UPPERNOZZLE END SWAGED FITTING. LEAKING FUEL CAUGHT FIRE CAUSING DAMAGE TO FIRE TUBING ON MANIFOLDS, SUPPLY LINE, ENGINE MOUNTSAND COWLS.SDR AUS20020946Valve · faulty(AUS) POWER PACK MOUNTED HYDRAULIC GEAR VALVE ASSEMBLY FAULTY.SDR CA020820011Tube · cracked(CAN) SHORTLY AFTER DEPARTURE THE CREW NOTED ILLUMINATION OF THE RT HYDRAULIC LIGHT. A FEW SECONDS LATER THE LEFT HYDRAULIC LIGHT ILLUMINATED FOLLOWED BY A LOSS OF PRESSURE ON THE HYDRAULIC PRESSURE GAUGE. THE AIRCRAFT RETURNED TO BASE AND LANDED UNEVENTFULLYSDR CA020906002Impeller · cracked(CAN) FIRST STAGE IMPELLER DAMAGE. THE ENGINE WAS REMOVED DUE TO A CRACK IN THE FIRST STAGE IMPELLER WHICH WAS NOTICED THROUGH THE INLET COWL. THE IMPELLER WAS REMOVED AND A COMPLETE DOD INSPECTION ACCOMPLISHED.SDR AUS20020794Bearing · failed(AUS) FLAP WALKING BEAM CENTRE BEARING DISINTEGRATED.SDR PNSA020702Compressor · crackedEngine removed for low power. During disassembly found 2nd stage compressor missing one piece from trailing edge of vane appeared to be fatigue crack.SDR AUS20020674Web · cracked(AUS) WING SPAR INNER WEB CRACKED. FOUND DURING INSPECTION IAWAD/SWSA226/86.SDR CA020718007Probe · out of position(CAN) AIRCRAFT UNDERWENT A CHANGE OF THE LT ENGINE. GROUND RUNS WERE MADE, ALL APPEARED NORMAL. AIRCRAFT WENT FLYING ON A TRIP FROM YVR TO SER. SHORTLY AFTER TAKEOFF, THE LT ENGINE FIRE WARNING LIGHT ILLUMINATED. THE CREW PERFORMED A SHUTDOWN AND DISCHARGED THSDR CA020718004Seal · leaking(CAN) WHILE ENROUTE FROM SEA TO YVR IN CRUISE, LT OIL PRESSURE DROPPED AS INDICATED ON GAUGE AND LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. CREW DID A PLANNED SHUTDOWN AND MADE AN UNEVENTFUL LANDING AT YVR. ATC WAS NOTIFIED BUT EMERGENCY NOT DECLARED. MAINTENSDR AUS20020505Spar · cracked(AUS) WING SPAR INNER WEB CRACKED IN TWO PLACES. CRACK LENGTH 12.7MM (0.5IN) LOCATED AT THE UPPER CENTER OF THE PORT STRINGER 13 CUTOUT. CRACK LENGTH 12.7MM (0.5IN) LOCATED AT THE LOWER RH CORNER OF THE STARBOARD STRINGER 13 CUTOUT. FOUND DURING INSPECTION IAWSDR 2002F01088Carbon Seal · damagedAUA - FLT 7120 - PILOT REPORTED SMOKE IN COCKPIT AGAIN FROM RIGHT BLEED AIR. ENGINE IS USING OIL AND PILOT CAN SEE OIL VAPORS AND SMELL OIL VAPORS, IT IS NOT SMOKE. MAINTENANCE HAS DEFERRED THE RIGHT BLEED AIR DUE TO HIGH OIL CONSUMPTION CAUSING BAD SMELL ANSDR AUS20020411Insert · dislodged(AUS) LT ENGINE OIL BYPASS VALVE ATTACHMENT STUD INSERT PN 423-553-0121 (COMPLETE WITH BOLT) CAME LOOSE IN THE GEARBOX CASING ALLOWING THE OIL FILTER BYPASS VALVE BODY TO SEPARATE FROM THE CASING.SDR AUS20020270Actuator · failed(AUS) PITCH TRIM ACTUATOR MOTOR FAILED.SDR AUS20020158Spar · cracked(AUS) REAR SPAR WEB CRACKED ON RT SIDE AT WS 27.063. FOUND DURING INSPECTION IAW AD/SWSA226/86.SDR AUS20020264Line · worn(AUS) HYDRAULIC SUCTION LINE WORN THROUGH BY ELECTRICAL WIRINGASSOCIATED WITH THE LH OUTBOARD GEAR DOOR POSITION SWITCH. THELINE IS VISIBLE THROUGH PANEL 513 LOCATED IN THE LH WHEEL WELL.SDR CA020422008Impeller · broken(CAN) CUSTOMER REPORTED LOUD SQUEALING NOISE COMING FROM ENGINE. ENGINE WAS REMOVED. TEARDOWN REVEALED THAT REWORKED IMPELLER HAD A PIECE BROKEN OUT OF ONE VANE.SDR AUS20020006Wire Harness · burned(AUS) SMOKE IN COCKPIT. INVESTIGATION FOUND SUBSTANTIAL HEAT DAMAGE TO WIRING LOOMS IN RT PEDESTAL & UP TO RT INSTRUMENT PANEL. FAULTISOLATED TO RT AVIONICS BUSS LINK SHORT CCTING TO COPILOT'S AUDIO WIRING. RESULTANT HEAVY CURRENT CAUSED WIRES 103 TO JJ, 1C3 T
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