Garrett TPE331-8
Service difficulty reports · 89
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 = 'TPE3318' 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 = 'TPE3318' 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 DSCR20151005001Relief Valve · fracturedDURING CRUISE PHASE OF FLIGHT, THE RT ENG EXPERIENCED LOSS OF FUEL PRESS. PILOT SHUT THE RT ENG DOWN, CONTACTED ATC & WAS DIVERTED. TECHNICIANS INSPECTED THE ENG & FOUND THE CAP HAD SEPARATED FROM THE HIGH PRESS RELIEF VLV, WHICH RESULTED IN THE LOSS OF FUELSDR 5XWR201307110363Structure · misoverhauledPERFORMED A PHASE 2, 3, & D, TASK A361004, BLEED AIR LINE EXHIBITED CORROSION WHERE ITS FLANGE FASTENS TO THE FUSELAGE SKIN BS 187.87 RBL 27, AND WL 62.79. ON DISASSEMBLY, FLANGE TO FUSELAGE JOINT FOUND WITH HEAVY DISSIMILAR METAL CORROSION. INVESTIGATION SDR CA080304011Actuator · failed(CAN) AIRCRAFT INDICATED (3 GREEN) ON APPROACH, UPON LANDING, NOSE GEAR RETRACTED RESULTING IN AC DAMAGE. UPON ARRIVAL, MAINT NOTED GEAR INDICATION REMAINED (3 GREEN) AND AC WAS SITTING ON ITS NOSE. THE AC WAS RAISED AND THE NOSE GEAR WAS PULLED INTO THE DOWN SDR AU510001538Tensioner · shearedHF ANTENNA SUPPORT AND TENSION UNIT SNAPPED AT ANTENNA CONNECTION TO VERTICAL STABILIZER.SDR AU510001559Actuator · faultyRT MAIN LANDING GEAR NIL DOWN INDICATION.SDR AU510001724Rivet · crackedELEVATOR LT OUTBOARD HINGE BRACKET ATTACHMENT RIVET HEAD CRACKED. FOUND DURING INSPECTION IAW AD/C400/102 AMDT3.SDR AU510001767Cap · cracked(AUS) RT WING CANTED RIB CAP CRACKED. CRACK LENGTH APPROXIMATELY 40MM (1.574IN). CRACK WAS LOCATED IN THE RADIUS OF THE UPPER CAP AND TRAVELLED REARWARDS FROM THE AUXILIARY SPAR. FOUND DURING NDI IAW SB CQB03-01 PART B REV 1. (AD/SB DESC: SB CQB03-01 PART B RESDR AU510001768Bracket · cracked(AUS) LT ELEVATOR OB HINGE ASSY IB ATTACHMENT BRACKET CRACKED IN LOWER FORWARD RADIUS. FOUND DURING INSPECTION IAW AD/C400/102 AMDT 3 PART 3. BOTH LT AND RT ELEVATOR OB BRGS STIFF IN OPERATION. (AD/SB DESC: AD/C400/102 AMDT 3 PART 3 ) (CASA NR 510001768)SDR AU510001769Bulb · burned out(AUS) RT MAIN LANDING GEAR POSITION INDICATOR LIGHT BULB BLOWN. (CASA NR 510001769)SDR AU510001776Rib · crackedLT WING ROOT CANTED RIB UPPER CAP LOCATED AT CWS 26.85 CRACKED.SDR AU510001885Rib · crackedRT CANTED RIB CAP CRACKED BENEATH REPAIR.SDR AU510001886Rib · crackedRT CANTED RIB CAP FORWARD PN 5720001-4S AND AFT PN 5720001-6S ANGLES CRACKED, FOUND DURING EDDY CURRENT INSPECTION.SDR AU510001944Governor · faulty(AUS) RT ENGINE PROPELLER GOVERNOR FAULTY. INVESTIGATION CONTINUING. (CASA NR 510001944)SDR AU510001993Altimeter · failedENCODING ALTIMETER FAILED.SDR AU510002026Engine · seizedRT ENGINE SEIZED. INVESTIGATION CONTINUING.SDR AU510002156Door · separatedLT FORWARD NOSE LOCKER SEPARATED FROM AIRCRAFT SEVERING BOTH HINGES. ONE BAG LOST OVERBOARD. DOOR STRUCK PROPELLER CAUSING A TORQUE SHIFT IN THE ENGINE. LT ENGINE, PROPELLER AND LT WING INBOARD LEADING EDGE DAMAGED. INVESTIGATION CONTINUING.SDR AU510002181Acm · failedAIR CYCLE MACHINE (ACM) FAILED AND EMERGENCY PRESSURISATION VALVE AUTOMATICALLY OPENED.SDR AU510002089Skin · crackedUPPER AFT RT NACELLE SKIN CRACKED AND CORRODED.SDR AU510001809Rib · crackedLT WING UPPER FORWARD PN 572001-3S AND AFT PN 572001-5S DRAG ANGLES CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW CQB03-1 REV 1. EDDY CURRENT INSPECTION REVEALED A TOTAL OF NINE CRACKS ALL AROUND 5MM (0.196IN) IN LENGTH.SDR AUS20040448Selector Valve · faulty(AUS) LANDING GEAR SELECTOR VALVE SOLENOID FAILED.SDR AUS20040447O-Ring · damaged(AUS) NOSE LANDING GEAR UPLOCK ACTUATOR O-RING DAMAGED. HYDRAULIC FLUID LEAKING FROM ACTUATOR BODY.SDR AUS20040368Boot · failed(AUS) RT WING OUTER DE-ICE BOOT BURST AT THE UPPER SEAM AND SPLIT FOR THE ENTIRE LENGTH FROM THE OB RT NACELLE TO THE WINGTIP.SDR AUS20040324Wire · worn(AUS) RT FUEL TANK QUANTITY WIRE CHAFED ON STRINGERS LOCATED AT STATION PWS 61.80.SDR AUS20040327Pump · cracked(AUS) ENGINE OIL PUMP HOUSING CRACKED.SDR AUS20040333Valve · leaking(AUS) START FUEL VALVE LEAKING BETWEEN VALVE BODY AND SOLENOID.SDR AUS20040183Pipe · cracked(AUS) HYDRAULIC PIPE CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. PIPE IS LOCATED IN RT WING LEADING EDGE. INVESTIGATION FOUND TOOLING MARKS ON THE PIPE IN THE AREA OF THE PIPE BEND.SDR AUS20040128Switch · out of adjust(AUS) LT MAIN LANDING GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. MICROSWITCH WAS SWITCHING OFF LOADING VALVE BUT NOT THE IN TRANSIT LIGHT. INVESTIGATION FOUND SOME WEAR IN THE SWITCH WHICH AFFECTED ADJUSTMENT.SDR CA040220007Valve · failed(CAN) DURING THE CLIMB THE AIRCRAFT EMERGENCY PRESSURIZATION VALVE OPENED WITH OUT BEING SELECTED. THE CREW DEPRESSURIZED THE AIRCRAFT AND RETURNED TO BASE. THE EMERGENCY PRESSURIZATION VALVE WAS REPLACED AND THE AIRCRAFT SYSTEMS FUNCTION CHECKED SERVICABLESDR AUS20040076Spar · debonded(AUS) LT WING SPAR WEB DISBONDED IN AREA LOCATED AT CWS 57.SDR AUS20040037Bracket · cracked(AUS) LT WING OB AILERON ATTACHMENT BRACKET CRACKED. INVESTIGATION FOUND INDICATIONS OF SURFACE INTERGRANNULAR CORROSION AND CONFIRMATION OF A CRACK LOCATED APPROXIMATELY 3.175MM (0.125IN) BEHIND THE BEARING HOUSING. CRACK LENGTH APPROXIMATELY 12.7MM (0.5IN).SDR AUS20031313Seal · leaking(AUS) RT ENGINE COMPRESSOR SEAL SUSPECT FAULTY. LEAKING OIL CAUSED SMOKE IN COCKPIT.SDR AUS20031179Tire · deflated(AUS) RT MAIN LANDING GEAR TIRE, DEFLATED DURING LANDING ROLL.SDR AUS20030552Web · cracked(AUS) BEAM WEB CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).SDR AUS20030595Beam · cracked(AUS) BEAM WEB CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).SDR AUS20030485Bolt · missing(AUS) MAIN WHEEL BRAKE DISC RETAINING BOLTS (3OFF) MISSING AND FIVE BOLTS LOOSE.SDR CA030421010Bearing · failed(CAN) STARTER GEN WAS HAVING NEW BRUSHES SEATED AT MID-TBO USING GEN DRIVESTAND METHOD.APPRX 3 HRS INTO THE PROCESS, THE ANTI-DRIVE END BEARING FAILED COMPLETELY. 5 OF 8 BALLS DISINTEGRATED,AS DID THE CAGE.DAMAGE WAS SUSTAINED TO THE ARMATURE, STATOR, FAN ANDSDR AUS20021376Valve · failed(AUS) EMERGENCY PRESSURISATION VALVE FAILED.SDR AUS20021305Solenoid · leaking(AUS) LT ENGINE PRIMARY-ONLY SOLENOID LEAKING FROM VALVE BODY.SDR AUS20020943Boot · split(AUS) LEADING EDGE DE-ICE BOOT SPLIT LONGITUDINALLY.SDR AUS20020792Valve · failed(AUS) RT ENGINE PRIMARY FUEL SOLENOID VALVE FAULTY. INVESTIGATION FOUND THE OPERATING COIL SHORT CIRCUITED TO EARTH.SDR CA020611001Wire Harness · chafed(CAN) DURING INSPECTION AND COMPLYING WITH AD 2002-09-13 AND CESSNA SERVICE BULLITEN CQB02-1 REV. 1, FOUND THAT THE BLACK WIRE IN THE HARNESS WAS CHAFED THROUGH AND ARCING TO GROUND ON THE FUEL PUMP SHROUD. THE OTHER WIRES IN THE HARNESS WERE ALSO CHAFED, BUSDR AUS20020577Pump · failed(AUS) LT ENGINE TORQUE FLUCTUATIONS. METAL CONTAMINATION OF OIL FILTER AND CHIP DETECTOR. SUSPECT CAUSED BY FAILURE OF OIL SCAVENGE PUMP.SDR AUS20020530Wire Harness · chafed(AUS) FUEL BOOST PUMP WIRING HARNESSES CHAFED. FOUND DURING INSPECTION IAW AD/CESSNA400/111 (SB CQB02-1R1).SDR AUS20020464Harness · worn(AUS) LT FUEL BOOST PUMP WIRING HARNESS CHAFED. FOUND DURING INSPECTION IAW SB CQB02-1.SDR AUS20020453Fastener · misinstalled(AUS) CHERRY RIVETS IN FUSELAGE EMERGENCY EXIT DOOR CUTOUT FRAMEPREVENTING OPERATION OF EMERGENCY EXIT.SDR AUS20020408Harness · chafed(AUS) LT FUEL TANK HARNESS WIRE CHAFFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.SDR AUS20020409Harness · chafed(AUS) RT FUEL TANK HARNESS WIRE CHAFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.SDR AUS20020323Pump · cracked(AUS) LT ENGINE OIL PRESSURE PUMP CRACKED.SDR AUS20020263Pushrod · cracked(AUS) LT AILERON TRIM TAB PUSH ROD AFT ROD END CRACKED ACROSS BEARING RETAINER. RODEND BEARING CORRODED. CRACK FOUND WHEN PUSHROD WAS REMOVED FOR REPLACEMENT DUE TO WEAR.SDR AUS20020043Bearing · failed(AUS) LT OUTBOARD FLAP INBOARD BELLCRANK BEARING HAD EXCESSIVE PLAY. SUSPECT CAUSED BY WATER INGRESS.
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