Garrett TPE331-10UA
Service difficulty reports · 375
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 = 'TPE33110UA' 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 = 'TPE33110UA' 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 CA070720005Actuator · malfunctioned(CAN) AFTER FLAP RETRACTION, FLIGHT CREW DISCOVERED THAT THEY HAD NO CONTROL OF PITCH TRIM USING PRIMARY OR SECONDARY CIRCUITS. AFTER DISCUSSION WITH MAINTENANCE, FLIGHT CONTINUED TO MAINTENANCE BASE WHERE MAINTENANCE REPLACED TRIM ACTUATOR. (TC NR 20070720005SDR CA070727008Master Cylinder · faulted(CAN) AIRCRAFT ABORTED TAKEOFF DUE TO A DRAGGING BRAKE. UPON MAINTENANCE INSPECTION THE RT BRAKE MASTER CYLINDERS WERE FOUND AT FAULT. BRAKE PRESSURE COULD NOT BE RELEASED BY THE AFFECTED MASTER CYLINDERS. BOTH NR 2 AND NR 4 BRAKE MASTER CYLINDERS WERE REPLASDR CA070704001Exhaust Duct · cracked(CAN) UPON ROUTINE INSPECTION, THE MAINTENENCE CREW FOUND THE EXHAUST DUCT CRACKED. THE ENGINE WAS REMOVED AND THE EXHAUST DUCT WAS REPLACED WITH A OVERHAULED ONE. NO OTHER PROBLEMS WERE DETECTED AT THIS INSPECTION. (TC NR 20070704001)SDR CA070614003Line · cracked(CAN) CREW NOTICED A LARGE PUDDLE OF HYDRAULIC FLUID COMING FROM THE NOSE WHEEL WELL AREA. DETERMINED TO BE A CRACKED LINE ON A BEND RADIUS, WHICH WAS THE SUPPLY LINE TO THE NWS SYSTEM. THE SYSTEM WAS DISABLED AND PLACED ON AN MEL DEFERRAL, CLEANED AND LEAK SDR CA070503010Control Cable · failed(CAN) CONTROL CABLE FAILED WHERE IT MAKES A BEND COMING OUT OF THE CENTER PEDESTAL. COMMON FAILURE POINT. REPLACED WITH NEW PART, REPLACED OTHER SIDE AS A PRECAUTION AS WELL. (TC NR 20070503010)SDR CA070424011Idler Gear · loose(CAN) FOUND ON TAKEOFF ROLL, THE RT CHIP LIGHT CAME ON THROUGH 70 KTS. THE TAKEOFF WAS ABORTED AND THE AC TAXIED BACK TO THE RAMP WITHOUT ANY FURTHER INCIDENT. AT THIS TIME MAINT HAD DONE A SOAP SAMPLE AND FOUND METAL IN THE OIL FILTER. WHEN THE ENGINE WAS TSDR CA070417001Valve · stuck(CAN) THE AC RT MLG TIRES WERE BLOWN UPON LANDING. DURING INSPECTION IT WAS FOUND THAT THE RT BRAKE ASSY WERE DRAGGING AND OVERHEATED CAUSING THE WHEELS NOT TO TURN FREELY UPON TOUCHDOWN. TIRES, BRAKES AND AFFECTED BRAKE MASTER CYLINDERS WERE REPLACED. AN INISDR CA070403002Windshield · cracked(CAN) THE FLIGHT CREW OBSERVED THE LT HEATED WINDSHEILD DELAMINATE AND CRACK DURING FLIGHT. THEY CARRIED OUT THEIR EMERGENCY PROCEDURES AND LANDED AT THEIR POINT OF DESTINATION. MAINTENANCE REPLACED THE WINDSHEILD. NO REASON FOR THE FAILURE (IE IMPACT) COULD BSDR CA070208005Windshield · cracked(CAN) DURING TAXI WITH THE WINDSHEILD HEAT SELECTED ON THE RT COCKPIT HEATED WINDSHEILD CRACKED. THE FLIGHTCREW RETURNED TO THE TERMINAL AND THE AIRCRAFT WINDOW HAS BEEN REPALCED BY MAINTENANCE. NO CAUSE OF THE CRACKED GLASS COULD BE DETERMINED. THIS IS THE THSDR CA070117003Windshield · delaminated(CAN) DURING FLIGHT THE FLIGHT CREW HEARD A LOUD CRACK FROM THE RT HEATED WINDSHIELD. THEY IMMEDIATELY NOTICED THE WINDOW PANES BEGIN TO DELAMINATE. NO OBJECT WAS WITNESSED HITTING THE AIRCRAFT OR WINDSHIELD. THE AIRCRAFT LANDED SAFELY AND THEN RETURNED TO BASSDR CA070112003Windshield · cracked(CAN) UPON LANDING THE FLIGHT CREW WITNESSED THE LT HEATED WINDSHIELD CRACK FROM THE LOWER RT CORNER TO THE UPPER CENTER PORTION OF THE WINDOW. THE LANDING WAS REPORTED AS NORMAL AND NO ABNORMAL INDICATIONS WERE NOTICED PRIOR TO FAILURE OF THE WINDOW. UPON INSDR CA061219027Windshield · failed(CAN) DURING FLIGHT THE RT COCKPIT HEATED WINDSHEILD SHATTERED BUT REMAINED INTACT. THE FLIGHT CREW DECALRED AN EMERGENCY AND RETURNED TO THE AIRPORT UNEVENTFULLY. THE WINDOW WAS REPLACED BY MAINTENANCE. THE CREW EXPLAINED THAT PRIOR TO THE WINDOW SHATTERING ASDR CA061212008Turbine Wheel · damaged(CAN) FOUND UPON INSPECTION AT THE HSI INSPECTION THAT THE RIVETS WERE LOOSE AND DEFORMED TO THE POINT THAT THE RIVETS WERE GOING TO COME OUT AND POSSIBLY WOULD CAUSE MORE DAMAGE INSIDE THE ENGINE. (TC NR 20061212008)SDR CA061124005Channel · cracked(CAN) DURING OVERHAUL OF THE RT FLAP ASSY, THE CENTER HINGE CHANNEL WAS REMOVED FOR REPLACEMENT AND WAS FOUND CRACKED BETWEEN (2) RIVET HOLES. THE CHANNEL HAS BEEN REPLACED. (TC NR 20061124005)SDR CA061219025Windshield · failed(CAN) DURING FLIGHT THE LT COCKPIT HEATED WINDSHEILD SHATTERED BUT REMAINED INTACT. THE AIRCRAFT IMMEDIATLY RETURNED TO THE AIRPORT AND THE WINDOW WAS REPLACED BY MAINTENANCE. NO CAUSE COULD BE DETERMINED AS TO WHY THIS WINDOW SHATTERED. (TC NR 20061219025)SDR CA061006002Actuator · malfunctioned(CAN) MAINTENANCE WAS COMPLETING AN ENGINE CHANGE. AN AME TAXI`D THE AIRCRAFT FROM THE HANGER TO THE DESIGNATED RUNUP AREA. ON THE TAXI WAY, THE AIRCRAFT ABRUPTLY VEERED TO THE RT, AND THE RT PROPELLER STRUCK A TAXIWAY MARKER. THE ENGINE WAS SHUTDOWN AND DASDR CA060901006Switch · odor(CAN) CREW NOTED BEFORE TAKEOFF A BURNING SMELL IN THE COCKPIT PRIOR TO TAKEOFF. NO SYSTEM FAULTS WERE NOTED OR BREAKERS POPPED AND THE SMELL WENT AWAY, SO THE FLIGHT CONTINUED IT`S LAST LEG. NO FAULTS NOTED IN FLIGHT. IT WAS LATER DISCOVERED A SPEED SWITCHSDR CA060905007Wire · damaged(CAN) AIRCRAFT HAD EXPERIENCED PROBLEMS WITH BATTERY DISCONNECTING INTERMITTENTLY. FIRST TIME WAS CIRCUIT BREAKER POPPED. NEXT TIME FOUND CORROSION ON BATTERY RELAY, REPLACED RELAY. THIS IS A COMMON DEFECT WITH THESE TYPE OF RELAYS. THIRD INSTANCE WAS ON NESDR CA060824004Line · leaking(CAN) AIRCRAFT WAS IN CRUISE, CREW NOTED HYDRAULIC LEAKAGE ON THE COCKPIT FLOOR. CONDUCTED A NORMAL LANDING, NOSE GEAR UP LINE IN COKPIT WAS LEAKING. REPLACED LINE, ON NEXT LEG, A LINE FAILED IN THE LH GEAR WELL, CREW ACTIVATED EMERGENCY EXTENSION AND NORMAL SDR CA060824003Fuel Control · malfunctioned(CAN) UPON LANDING, CREW APPLIED REVERSE THRUST. BELOW 70 KIAS, THE RPM LEVER WAS SELECTED TO (LOW). ON THE TAXIWAY, THE CREW NOTED VERY LOW ENGINE RPM, LOW OIL PRESSURE LIGHT, AND LOW EGT. THEY DETERMINED THE ENGINE HAD FLAMED OUT AND PARTIALLY RESTARTED. SDR CA060627004Bearing · failed(CAN) THE FRONT SCAVENGE PUMP DRIVE GEAR SHAFT SHEARED IN THE SCAVENGE PUMP, DUE TO THE SCAVENGE PUMP BUSHING THAT SEIZED FROM OIL STARVATION AND METAL CONTAMINATION CAUSED BY THE TORQUE SENSOR BEARING. THE OIL PRESSURE PUMP SHAFT AND BUSHING ALSO HAVE WEAR ONSDR CA060530007Carrier Assy · making metal(CAN) OIL SAMPLE RECEIVED FROM WEAR CHECK INDICATING HIGH OIL FILTER WEIGHT W/MAJOR ALUMINUM, MINOR CARBON STEEL IN SAMPLE. ENG REMOVED FOR INSP. DURING TEARDOWN: PLANETARY CARRIER SPLINE LOCKS STRIPPED/DESTROYED. CARRIER WORN DUE TO EXCESS PIN LOADING. ALL SDR CA060428001Oil Filter · broken(CAN) DURING A ROUTINE DAILY INSPECTION THE OIL FILTER BYPASS PIN WAS FOUND POPPED INDICATING AN OBSTRUCTED OIL FILTER. UPON INSPECTION OF THE FILTER IT WAS FOUND TO BE BROKEN AT THE OIL INLET MOUNTING FLANGE. PREVIOUS SDR'S HAVE BEEN ISSUED FOR THIS PROBLEM, SDR CA060321004Cable · broken(CAN) FLIGHT CREW REPORTED THAT DURING START THE RPM WAS UNCONTROLLABLE AND INITIATED A MANUAL SHUT DOWN. MAINTENANCE DISCOVERED THE POWER LEVER BROKEN APPROX. 4 INCHES FROM THE END JUST SHORT OF THE QUICK DISCONNECT FITTING. DUE TO THE FACT THAT THE TELE-FLESDR 2006F00019Truss · brokenLEFT ENGINE MOUNT LOWER TRUSS OUTBARD TUBE WAS FOUND SEPERATED FORWARD OF THE CENTER INTERCONNECT TUBE OUTER BRACE PLATE. TUBE WAS COMPLETLY BROKEN AROUND THE CIRCUMFERENCE OF THE TUBE. NO FURTHER DEFECTS WERE NOTED DURING FURTHER INSPECTION OF THE ENGINE MOUNSDR CA060221009Control Cable · failedCREW ATTEMPTED TO START THE ENGINE ON 4TH LEG OF THE DAY. ENGINE ACCELERATED TO 30 PERCENT AND TEMPERATURE INCREASED. ENGINE WAS SHUT DOWN. MAINTENANCE DISCOVERED THE POWER LEVER CABLE HAD SEVERED IN THE PEDASTAL AND THE ENGINE WAS STUCK IN FULL REVERSE. (SDR CA060221006Panel · crackedWHILE UN-COWLING, RT ENGINE MAINTEANCE FOUND A PIECE OF STAINLESS STEEL IN THE LOWER SECTION OF COWL. INVESTIGATION REVEALED A HOLE IN THE LT SIDE OF ASPIRATOR ASSEMBLY ABOVE THE OIL COOLER. THE ASPIRATOR WAS REPLACED AND AIRCRAFT SINCE RETURNED TO SERVICE. SDR CA060126007Blade · damaged(CAN) DISCOVERED WARPED TRAILING EDGE OF PROPELLER BY MAINTENANCE. UNIT HAD BEEN OVERHAULED FEB 2003 THEN RETURNED FOR THIN TRAILING EDGE APRIL 2003. REPAIRED BY SAME FACILITY. TRAILING EDGE WAS SIGNIFICANTLY THINNER THAN SIMILAR IN FLEET. REMOVED PROPELLESDR CA060112005Door · jammedDURING APPROACH, CREW ATTEMPTED TO EXTEND L/G AND NOTICED RT MAIN WAS NOT DOWN AND LOCKED. IT WAS DETERMINED LANDING GEAR WAS NOT COMING OUT OF RT W/W. IT TOOK SEVEN ATTEMPTS TO GET LANDING GEAR TO COME DOWN AND LOCK INTO POSITION. INSPECTION REVEALED RT I/SDR CA051027009Web · cracked(CAN) DURING INSPECTION, MAINTENANCE FOUND SEVERAL FATIGUE CRACKS IN THE CENTER AISLE FLOORBOARD WEBS AND FLOOR FRAMES BETWEEN STATIONS 174 AND 427. THESE CRACKS WERE FOUND ON BOTH THE LT AND RT SIDES OF THE AISLE. BOTH WEBS WERE REPLACED.SDR CA050804010Release Cable · sheared(CAN) WHEN COMPLYING WITH AN UNRELATED INSPECTION UNDER THE COCKPIT FLOOR, MAINTENANCE DISCOVERED THE NOSE LANDING GEAR EMERGENCY RELEASE CABLE WAS SHEARED AT THE CLEVIS WHERE IT ATTACHES TO THE HANDLE BELLCRANK. THIS AIRCAFT HAD RECENTLY (WITHIN 50 HOURS) UNSDR CA050725007Fcu · leaking(CAN) UPON LANDING AND SHUTDOWN OF THE LT ENGINE IT WAS NOTICED THAT THE OVERBOARD ENGINE DRAIN FOR THE FUEL CONTROL UNIT WAS LEAKING FUEL. THE FUEL CONTROL WAS REPLACED. THE LAST TIME THIS FCU WAS REPAIRED IT WAS FOR THE SAME FUEL LEAK PROBLEM IN MARCH OF 200SDR CA050725003Carrier Assy · cracked(CAN) DURING ENGINE TREND RECORDING BY THE FLIGHT CREW IT WAS NOTICED THAT THE LH ENGINE OIL PRESSURE INDICTION HAD DECREASED 15 PSI WITHIN A WEEK OF OPERATION. UPON ARRIVAL MAINTENACE WAS ADVISED AND ELECTED TO REMOVE THE ENGINE FOR INSPECTION. UPON INSPECTIOSDR CA050623004Torque Tube · chafedDURING AN INSPECTION, IT WAS DISCOVERED THAT THE RIGHT ELEVATOR TORQUE TUBE HORN WAS CHAFFED. THE CAUSE OF THE CHAFF WAS A SCREW, WHICH ATTACHES A CLOSING PANEL ON THE VERTICAL STAB. THE TORQUE TUBE WAS REPLACED AND A SHORTER SCREW INSTALLED.SDR TCA004Engine · overservicedTHE PILOT REPORTED THAT INBOUND FLIGHT TO LRD THERE WAS A SMELL OF OIL IN THE COCKPIT. SHUT DOWN THE BLEED AIR AND THE SMELL DISAPPEARED. DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. AFTER LANDING, WAS INSTRUCTED BY BASE MX IN TOL TO CHECK ALL SDR CA050518017Carrier Assy · crackedFLIGHT CREW OBSERVED THE ENGINE OIL PRESSURE TREND TO BE STEADILY DECREASING OVER A SHORT PERIOD OF TIME. AS AN EXPERIENCED OPERATOR OF THIS ENGINE, THIS TREND INDICATED A CRACKING PROBLEM WITH THE PLANETARY GEAR CARRIER IN THE ENGINE GEARBOX. THE ENGINE WASSDR CA060407009Receptacle · crackedWHEN COMPLYING WITH SERVICE LETTER 226-SL-027, WHICH DEALS WITH INSPECTION OF THE DOOR CLICK CLACK RECEPTACLES, TWO WERE FOUND CRACKED ON THE PASSENGER DOOR. THIS IS THE FIRST TWO PASSENGER DOOR RECEPTACLES THIS OPERATOR HAS FOUND CRACKED. ONE WAS BROKEN IN SDR CA050426007Fuel Control · unresponsive(CAN) DURING DESCENT, FLIGHT CREW ATTEMPTED TO REDUCE POWER WITH LITTLE TO NO RESPONSE. POWER LEVER HAD TO BE BROUGHT BACK ALMOST TO FLIGHT IDLE BEFORE ENGINE RESPONSE WAS OBTAINED, RESPONSE WAS SUDDEN AND ABRUPT. AC LANDED WITHOUT INCIDENT. UPON INSPECTION ASDR CA050405012Pump · leaking(CAN) LOSS OF HYDRAULICS, FLT WAS CONTINUED, UNEVENTFUL FLAPLESS LANDING COMPLETED. INSP OF AC, NOTED, ALL OF FLUID LEAKED OVERBOARD FROM LT ENG HYD PUMP. INSP OF PUMP REVEALED EXTRUDED O-RING SEAL FROM PUMP HSG SPLIT LINE. BOLTS HOLDING 2 PUMP HSG HALVES TOGSDR CA050317004Fcu · failed(CAN) CREW WAS UNABLE TO REDUCE PWR ON RT ENG ON DESCENT. SPEED LEVERS HIGH, POWER LEVERS AT FLIGHT IDLE, ENG REMAINED AT 54 PERCENT TORQUE, CREW COULD NOT CONTROL ENG PWR, ELECTED TO SHUTDOWN ENG AS A PRECAUTION. FCU WAS REPLACED, NORMAL ENG OPS WERE RESTORESDR CA050308010Shaft · loose(CAN) UPON CLIMB OUT, RT ENGINE BEGAN TO SURGE WITH NO RESPONSE FROM PWR LEVER INPUTS. FLIGHT CREW ELECTED TO SHUTDOWN ENG AS A PRECAUTION AND CARRIED OUT AN UNEVENTFUL LANDING. UPON INSP OF ENG, IT WAS FOUND THAT ENG CNTRL CENTER SHAFT OR CHRISTMAS TREE DISCSDR CA050307013Planetary Gear · cracked(CAN) DURING ROUTINE MAINTENANCE, THE OIL PRESSURE TREND WAS NOTICED TO HAVE DROPPED ABOUT 12 PSI IN RECENT DAYS. THIS TOGETHER WITH A BAD OIL SAMPLE INDICATED A PLANETARY CARRIER PROBLEM AS EXPERIENCED IN THE PAST BY THIS OPERATOR. THE ENGINE GEARBOX WAS DISASDR CA050117007Adapter · cracked(CAN) DURING ROUTINE ENGINE MAINTENANCE AN AME NOTICED THE LT ENGINE OIL FILTER ADAPTER WAS CRACKED AT THE MOUNTING FLANGE. THE OIL FILTER ADAPTER WAS REPLACED. THIS OIL FILTER ADAPTER CRACKED IN THE SAME AREA AS THE ADAPTER DISCUSSED IN SDR20050105015 AND SDRSDR CA050117005Adapter · cracked(CAN) A SPECIAL INSPECTION WAS CARRIED OUT TO FLEET AIRCRAFT OF SUSPECTED CRACKING OIL FILTER ADAPTERS. EDDY CURRENT METHOD WAS USED TO DISCOVER THIS CRACKED ADAPTER . ALTHOUGH VISIBLE WITH THE NAKED EYE, INITIAL DETECTION MAY BE DIFFICULT DUE TO THE ADAPTERSDR CA050105015Adapter · crackedDURING CRUISE, RT ENG OIL PRESS WARNING LIGHT ILLUM ON ANNUNCIATOR. UPON LOOKING AT RT OIL PRESS IND FLT CREW NOTICED OIL PRESS DECREASING THROUGH 40 PSI. CREW ELECTED TO SHUTDOWN RT ENG AS A PRECAUTION. A/C CONTINUED IT'S FLIGHT TO YWG WHERE IS LANDED W/O SDR CA041202001Rivet · separatedUPON A REGULARLY SCHEDULED HOT SECTION INSPECTION THE NR 2 TURBINE WHEEL WAS FOUND TO HAVE A RIVET MISSING AT THE BASE OF ONE OF THE TURBINE BLADES. THIS RIVET INSTALLATION IS FOR EXPANSION PURPOSES. THE 3RD STAGE TURBINE AND STATOR ASSY WAS FOUND DAMAGED FRSDR CA041123009Windshield · broken(CAN) UPON REACHING CRUISING ALTITUDE OF 14, 000 FEET CO-PILOTS HEATED WINDSHIELD SHATTERED. WINDOW REMAINED INTACT AND FLIGHT CREW DEPRESSURIZED AIRPLANE AND FLEW TO A SAFE ALTITUDE. FLIGHT CREW NOTICED A SPARK OR FLASH INSIDE WINDSHEILD PRIOR TO IT SHATTERSDR CA051108009Fitting · cracked(CAN) DURING A ROUTINE PHASE INSPECTION OF THE WING AND CENTER SECTION OF THE AIRCRAFT, SMALL CRACKS WERE FOUND IN THE RT WING AFT SPAR WING TO FUSELAGE ATTACH FITTINGS (PN 27-22136-006 AND 27-22135-006). THE CRACKS WERE FOUND VISUALLY AND CONFIRMED USING EDSDR CA041110018Clamp · crackedPROPELLER RECEIVED FOR INSPECTION UNDER AD 88-24-15. DURING ROUTINE VISUAL INSPECTION OF THE BLADE CLAMP ASSEMBLES, A CRACKED WAS DETECTED IN ONE OF THE OUTBOARD CLAMP BOLT HOLES ON S/N EE1910. CLAMP HAS BEEN REMOVED FROM SERVICE AND REPLACED WITH AN OVERHAUSDR CA041103004Bellcrank · wornDURING EXTENSION OF MLG, NOTICED RT MLG WOULD NOT EXTEND. NO INTRANSIT OR DOWN & LOCKED IND. CREW ATTEMPTED A VISUAL TO CONFIRM MLG EXTEND BUT COULD NOT SEE IT FROM INSIDE A/C. CREW MANUALLY EXTENDED MLG. MLG PROCEEDED TO COME DOWN & REMAINED LOCKED. MX CONTAC
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