Garrett TPE331-3UW
Service difficulty reports · 35
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 = 'TPE3313UW' 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 = 'TPE3313UW' 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 AU510001635Wire Harness · deterioratedFUEL BOOST PUMP WIRING HARNESSES PN 27-82015-810 AND PN 27-82015-811 DETERIORATED. FOUND DURING INSPECTION IAW AD/SWA226/51 AND SB226-28-011.SDR CA021227004Line · leaking(CAN) DURING INSPECTION A LARGE AMOUNT OF HYRAULIC FLUID WAS FOUND IN THE LT WHEEL WELL, FURTHER INVESTRICATION REVEALED A SMALL PIN HOLE IN THE LINE. THE LINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR AUS20010733Valve · stuck(AUS) OIL VENT VALVE STUCK OPEN.SDR CA001206009Brake Assy · seized(CAN) ON LDG, LT BRAKE FAILED TO RELEASE FULLY. A/C LANDED SAFELY BUT UNABLE TO TAXI, BLOCKING RWY. BRAKE RELIEVED OF PRESSURE & A/C TOWED FROM RWY. SUBSEQUENT INSPECTION REVEALED THAT NR 2 BRAKE ASSY UPPER PISTON INSULATOR PIN EXTENDED & STUCK AT APPROXIMASDR AU001148Pipe · leaking(AUS) HYDRAULIC POWER PACK PIPE LOCATED IN LT ENGINE NACELLE LEAKING.SDR CA001109010Indicator · failed(CAN) ON APPROACH TO YXM WHEN GEAR SELECTED DOWN NOSEGEAR FAILED TO EXTEND, LT & RT MAIN INDICATED DOWN & LOCKED. DUE TO POOR WEATHER & BETTER FACILITIES CREW ELECTED TO PROCEED TO THEIR ALT OF YTH. WHEN LDG GEA R AGAIN SELECTED DOWN ATYTH, TOWER CONFIRMED THASDR CA000621017Sensor · failed(CAN) DURING CRUISE FLIGHT THE LT WING OVERHEAT LIGHT ILLUMINATED FOR APPROXIMATELY 1 MINUTE AND REMAINED OFF FOR THE DURATION OF THE FLIGHT.A SUBSEQUENT INSPECTION COULD NOT REVEAL ANY FAULT, ALL ASSOCIATED WIRING WAS THOROUGHLY INSPECTED ALL LT BLED AIR LINESDR CA991209020Lighting Panel · melted(CAN) A DAMAGED LIGHT BULB IN THE PILOT'S LOWER SWITCH PANEL BACKLIGHTING CAUSED A SHORT WHICH MELTED PART OF THE PANEL RESULTING IN SOME SMOKE AND FUMES IN THE COCKPIT.SDR AU990434Mount · cracked(AUS) LOWER ENGINE MOUNT CRACKED.SDR CA990129007Line · chafed(CAN) .75 INCH STAINLESS HYDRAULIC LINE FOUND CHAFED IN THE RIGHT HAND NACELLE INBOARD. ACCESSIBLE THROUGH THE WHEELWELL PANELS. LINE HAD BEEN RUBBING ON A STRINGER.SDR AU990024Switch · leaking(AUS) NOSE LANDING GEAR PRESSURE SWITCH LEAKING OIL FROM WELDED SEAM.SDR AU981680Plenum · cracked(AUS) COMBUSTION CHAMBER (PLENUM) CASE CRACKED 11.1 MM (0.44 INCH) IN LENGTH BETWEEN THE 3RD AND 4TH FUEL NOZZLE, ADJACENT TO THE TURBINE SUPPORT DUCT MOUNTING FLANGE.SDR AU981234Web · cracked(AUS) WING CENTER SPAR WEB CRACKED. PART TC: 26,549.SDR AU981085Keelson · cracked(AUS) LEFT NACELLE STRUCTURE INBOARD KEELSON CRACKED. PART TC: 29,623.SDR AU980846Yoke · cracked(AUS) LEFT AND RIGHT MAIN LANDING GEAR YOKES CRACKED. FOUND DURING ULTRASONIC INSPECTION IAW AD/SWSA226/74-A3.SDR CA980629003Actuator · failed(CAN) BOTH PILOT AND COPILOT ELECTRIC TRIM FAILED AT THE SAME TIME. SUBMITTER SUGGESTED HAVING TWO INDEPENDENT SYSTEMS. AWAITING TEAR DOWN REPORT.SDR AU980713Keelson · cracked(AUS) LEFT NACELLE LEFT OUTBOARD KEELSON CRACKED FROM THE EDGE OF THE SKIN THROUGH THE LAST RIVET OF THE STIFFENER AND CONTINUES OUT AT AN ANGLE OF APPROXIMATELY 45 DEGREES. CRACK LENGTH 76.2 MM (3 INCHES). PART TOTAL CYCLES: 29,529.SDR AU980714Drag Brace · broken(AUS) MAIN LANDING GEAR DRAG BRACE ASSEMBLY CENTER TORQUE SHAFT SUPPORT LUGS BROKEN. TORQUE SHAFT BENT AND BROKEN.SDR CA980706003Bolt · wrong part(CAN) RIGHT ENGINE FIRE WARNING CAME ON AFTER TAKEOFF. PRIMARY FUEL NOZZLE GASKET HAD BLOWN OUT CAUSING FIRE DETECTOR TO ILLUMINATE FIRE WARNING LIGHT. IT WAS FOUND THAT THE BOLT SECURING THE FUEL NOZZLE WAS TOO LONG AND HAD BOTTOMED OUT AT LAST INSTALLATIONSDR CA980317095Wire · broken(CAN) WING OVERHEAT DETECTION SYSTEM FAILED TO TEST. INSPECTION FOUND THAT A WIRE HAD BROKEN OFF THE WING OVERHEAT SENSOR IN THE LEFT WING LEADING EDGE.SDR CA980317093Fire Detector · intermittent(CAN) RIGHT WING OVERHEAT LIGHT FLICKERED ON JUST PRIOR TO TAKEOFF. THE FIRE DETECT CIRCUIT WAS GROUNDING CAUSING AN INTERMITTENT LIGHT. REWIRED WING O/H DETECT SYSTEM, REPLACED THE 250 DEGREE SENSOR AND REPLACED THE WHEEL WELL 550 DEGREE O/H DETECTOR. ALSO SDR CA971003003Line · melted(CAN) DURING ROUTINE INSPECTION OF OXYGEN SYSTEM IN AFT CABIN SIDE WALL SUBMITTER FOUND THAT A SECTION OF PLASTIC OXYGEN LINE NEAR THE BACK OF THE CABIN WAS FOUND MELTED. IN ADDITION, A SMALL SPOT WAS ALSO FOUND AT MID CABIN ON LEFT SIDE. SUBMITTER SUSPECTS THSDR AU970616Bearing · disintegrated(AUS) LH OUTBOARD WHEEL BEARING CONE DISINTEGRATED - WHEEL SEPARATED FROM AXLE DURING TAKEOFF - WHEEL RETAINING NUT STILL IN PLACESDR CA970520002Stop Screws · backed out(CAN) ON SHUTDOWN AFTER A TRAINING FLIGHT THE PROPELLER DID NOT FEATHER. SUBSEQUENT INVESTIGATION FOUND THE STOP SCREWS HAD BACKED OUT OF THE ROD GUIDE ENDS. THIS HAD THE EFFECT OF CAUSING THE STOP LOCKS TO MISS CATCHING THE SCREWS PRIOR TO SHUTDOWN AND PREVENSDR 97ZZZX2706Seal · leakLEFT ENGINE OIL PRESSURE FLUCTUATED DURING FLIGHT BACK FROM GCN. FLIGHT CREW MADE A PRECAUTIONARY LANDING AT IFP. MAINTENANCE FOUND OIL LEVEL LOW, SERVICED OIL TO FULL. RAN ENGINE, OIL PRESSURE WAS STABLE. CHECKED OIL LEVEL. IT REMAINED THE SAME, AIRCRAFTSDR 97ZZZX2703Engine · low oilLEFT ENGINE OIL PRESSURE DROPPED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE INSPECTED ENGINE, SERVICED ENGINE WITH 3 QUARTS OF OIL. TEST FLEW AIRCRAFT FOR 30 MINUTES. PRESSURE CHECK AND QUANTITY CHECKED OK AFTER TEST FLIGHT. THIS ENGINE WILLSDR CA961024016Cable · broken(CAN) AFTER START UP THE RIGHT HAND ENGINE DID NOT RESPOND TO SPEED LEVER INPUT. AIRCRAFT RETURNED TO TERMINAL. INSPECTION FOUND THAT THE INNER RIBBON OF THE 'COCKPIT TO WING ROOT ASSEMBLY' HAD FAILED AT THE QUADRANT. ACCORDING TO SUBMITTER THIS CABLE HAD BEENSDR CA961022006Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES SDR CA961022011Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES SDR CA961022012Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES SDR CA961003004Balance Weight · broken(CAN) LEFT AILERON INBOARD BALANCE WEIGHT FOUND BROKEN AT CENTRE ATTACH BOLT. WEIGHT HAD BEEN CRACKED FOR SOME TIME. REST OF FLEET OF 12 AIRCRAFT CHECKED AND 6 OTHERS FOUND WITH BROKEN BALANCE WEIGHTS AT SAME PLACE. ALL CRACKED BALANCE WEIGHTS FOLLOWED A SIMILSDR CA961003010Balance Weight · cracked(CAN) LEFT AILERON OUTBOARD BALANCE WEIGHT FOUND CRACKED AT CENTRE HOLE. 6 OF 12 OTHER AIRCRAFT FOUND WITH SIMILAR PROBLEM.SDR CA961001006Turbine · damaged(CAN) ON APPROACH, ENGINE SHUT DOWN AND THE PROPELLER FEATHERED. THE LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. THE FLIGHT CREW CHECKED THE L/H ENGINE AND FOUND THAT THE PROPELLER COULD NOT BE TURNED BY HAND. MAINTENANCE DISPATCHED AND ENGINE REPLACED. FIELD RSDR AU960384Support · cracked(AUS) RH MAIN LANDING GEAR OUTBOARD UPPER DRAG BRACE SUPPORT STRUCTURE CRACKED - PART NUMBERS OF CRACKED COMPONENTS:- 1. HAT SECTION PNO S27-35011-055M - CRACKED 2. T DOUBLER PNO S27-35011-23M - CRACKED3. DOUBLER PNO S27-35011-017M - CRACKED 4. DOUBLER PNO SDR CA960116006Fcu · erratic(CAN)THIS FUEL CONTROL UNIT WAS REMOVED DUE TO MALFUNCTION CAUSED BY THE MAXIMUM POWER ADJUSTMENT SETTING BEING BOTTOMED OUT. ONE MONTH LATER THIS SAME FCU WAS SENT BACK FOR OVERHAUL DUE TO TORQUE JUMPING ERRATICALLY.
Back to Garrett TPE331-3UW