Alliedsign TFE731-60

Service difficulty reports · 43

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 = 'TFE73160'
  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.

SDR G13A202307254001Fuel Line · failedMETAL FUEL LINE ON #2 ENGINE FAILED LINE P/N 3061249-2 CAUSING LOSS OF FUEL QUANTITY. ENROUTE TO EUROPE. CREW DIVERTED TO CYQXJul 24, 2023 · N420PD · Amd FALCON900EX · Engine Fuel DistributionSDR 2020FA0000311Blade · brokenAFTER TAKEOFF, ENGINE 3 INDICATED AN ITT OF 1022. POWER WAS REDUCED ON #3 TO NORMAL OP TEMPS. IN THE CLIMB, IF AUTOTHROTTLES WERE USED, #3 ITT WOULD APPROACH TEMP LIMITS WHEN THE AUTO THROTTLES ACHIEVED MCT. AUTO THROTTLES WERE NOT USED AFTER THAT EXCEPT IN CRMay 31, 2020 · Amd FALCON900EX · Turbine Engine Compressor SectionSDR JGVR20181121001Shutoff Valve · mismanufacturedCREW EXPERIENCED #2 ENGINE POWER LEVER STUCK AT 95% IN-FLIGHT. ATTEMPT TO SHUT-DOWN THE #2 ENGINE FAILED AND THE ENGINE CONTINUED TO RUN AT 95% POWER. DURING DESCENT THE CREW WAS ABLE TO RETARD THE #2 POWER LEVER AND LAND NORMALLY. TROUBLESHOOTING OF THE FIREWNov 21, 2018 · N58CG · Amd FALCON900EX · Fuel Controlling SystemSDR DBCA2018101800006Fcu · failed1) DURING CLIMB PILOT NOTED NR 1 DEEC CAS MESSAGE. 2) PILOT RETURNED TO HOMEBASE. 3) MAINTENANCE INSPECTED AND REPLACED NR 1 FUEL CONTROL 4) AIRCRAFT RETURNED TO SERVICE.Oct 14, 2018 · N793CG · Amd FALCON900EX · Fuel Control/Turbine EnginesSDR 9PVA2015041700001Cable · meltedNUMBER 3 THROTTLE WAS STUCK IN THE IDLE POSITION. FURTHER INVESTIGATION FOUND FOUR MOUNTING SCREWS FOR BLEED AIR ANTI-ICE SWIVEL WERE LOOSE. THERE WAS THERMAL DAMAGE TO UPPER COWL DOOR, BURNT & DELAMINATION. TELEFLEX CABLE MELTED INTERNALLY, ENGINE AFTER BOApr 13, 2015 · N111SW · Amd FALCON900EX · Power LeverSDR ZN3R2015FA0000086Bearing · separatedREPAIR AND O/H FOR A METAL CONTAMINATION INSPECTION. DISASSEMBLY FINDINGS REVEALED THE SOURCE OF THE METAL CONTAMINATION WAS THE NR 4 ROLLER BEARING. THE BEARING EXHIBITED HEAVY SPALLING WITH DISCOLORATION IN THE FORM OF HEAT DAMAGE WITH ROLLER BEARING CAGE Feb 25, 2015 · Turbine Engine Compressor SectionSDR O2GA2014FA0000424Water Heater · leakingAT 40,000 FT CRUISE ALTITUDE, DURING FLIGHT NR 2 THROTTLE WENT TO FULL THROTTLE AND THROTTLE LEVER WOULD NOT MOVE. DESCENDED THRU 23,000 FT AND THROTTLE LOOSENED UP. DECISION WAS TO CONTINUE FLIGHT AND WAS UNEVENTFUL LANDING. INVESTIGATION FOUND THE LAV SINK Jul 6, 2014 · N111SW · Amd FALCON900EX · Potable Water SystemSDR 9JLA2014043004738Warning System · false activationTHE CREW REPORTED THAT DURING TAXI OUT FOR FLIGHT THAT A NR 3 EIED FAULT WAS NOTED. THE NR 3 ENG OIL FILTER WAS REMOVED & INSPECTED, NO DEFECTS WERE NOTED. PERFORMED AN ENG OIL SAMPLE IAW TFE731 LMM. PERFORMED GND & LEAK CHECKS, LEAK CHECKED OK & OIL SAMPLEApr 12, 2014 · N928WK · Amd FALCON50MYST · Engine Oil Indicating SystemSDR 2012FA0000692Control Cable · wornNR 2 ENGINE POWER LEVER FROZE DURING CRUISE AT 43,000 FT. ISA -10. CONTROL CABLE WORN.Oct 8, 2012 · N111SW · Amd FALCON900EX · Power LeverSDR 9JLA201210162242Exciter · defectiveCREW REPORTED THE NR 3 ENGINE HAD ROTATION DURING START BUT WOULD NOT IGNITE. TROUBLESHOOTING IDENTIFIED THE IGNITER EXCITER AS DEFECTIVE. INSTALLED AN O/H EXCITER, FUNCTIONAL CHECKS SATISFACTORY.Aug 3, 2012 · N928WK · Amd FALCON50MYST · ExciterSDR 9JLA201207172237Pitot Head · obstructedTHE CREW REPORTED THAT ON TAKEOFF ROLL, THE COPILOTS AIRSPEED NEVER CAME ALIVE (INDICATED). GAINED ACCESS TO THE NR 2 PITOT AND FOUND DIRT AND DEBRIS CONSISTANT WITH THE MUD DOBBER WASP NEST. TUBE WAS CLEANED AND SYS CHECKS WERE SATISFACTORY. THE CREW WAS ADMay 21, 2012 · N928WK · Amd FALCON50MYST · Pitot/Static SystemSDR CA111227004Tube · worn(CAN) ENGINE HAD OIL SEEPAGE FROM THE LT SIDE OF THE ACCESSORY GEAR BOX WHERE THE OIL COOLER TUBE INSERTS INTO THE ACCESSORY GEAR BOX CAVITY. ITEM WAS ACCESSED AND INVESTIGATED DURING THE MAJOR PERIODIC INSPECTION. THE REMOVAL OF THE OIL COOLER TUBE REVELAEDec 21, 2011 · Amd FALCON900EX · Turbine Engine Oil SystemSDR 2011FA0000572Throttle Cable · bindingAT TOP OF DESCENT, NR 2 THROTTLE STUCK AT FULL FWD POSITION , AUTOTHROTTLES DISCONNECTED, MANAGED TO GET THROTTLE BACK TO IDLE HOWEVER IT WAS STUCK THERE AND WOULD NOT ADVANCE. APPEARED TO FREE UP AT AROUND 14000 FT . FLEW 2 ENG APPROCH. NR 2 TELEFLEX CABLEAug 28, 2011 · N146EX · Amd FALCON900EX · Power LeverSDR CA110719009Seal · damagedDURING COMPANY ROUTINE SERVICING/GREASING OF NOSE WHEEL ASSEMBLIES, THE INBD AND OTBD GREASE SEALS WERE FOUND DAMAGED. THE GREASE SEAL HAD FLAT SPOTTED AND WAS NICKED IN A COUPLE OF PLACES. THE BEARINGS THAT ARE LOCATED IN THIS AREA WERE FOUND DAMAGED. THE Jul 15, 2011 · Amd FALCON900EX · Wheel/Ski/FloatSDR CA110704011Pitot Head · obstructedON TAKE-OFF/ROLL, NO INCREASING IAS ON LT MFD. ALL FOLLOWING CAS MESSAGES DISPLAYED " AP1&2 FAIL, MACH TRIM FAIL, PITCH FEEL FAIL, AT1 AUTO SLATS FAIL". TAKEOFF ABORTED AT 80 KNOTS. LT PITOT PROBE FOUND PLUGGED WITH BUG/SPIDERS OR NEST MATERIAL ON VISUAL INSJun 28, 2011 · Amd FALCON900EX · Pitot/Static SystemSDR CWQA03032011Engine · failedNR 1 ENGINE FAILURE ON CLIMBOUT, CREW FELT THE ENGINE POP AND VIBRATE CLIMBING THROUGH 10,000FT WITH OIL PRESSURE LIGHT MASTER CAUTION AND ENGINE ITT SPIKE THROUGH LIMITS AS THE ENGINE SHUTDOWN, CHECK LIST FOLLOWED AND UNSCHEDULED LANDING PERFORMED WITHOUT FURMar 4, 2011 · N602CV · Amd FALCON900EX · Engine (Turbine/Turboprop)SDR DJFA2011002Throttle Cable · twistedCREW REPORTED MUST JIGGLE OR PUSH HARD ON NR1 HP COCK TO GET NR1 ENGINE TO SHUT OFF. DURING TROUBLESHOOTING, MX FOUND THE NR1 THROTTLE CABLE TWISTED ON PULLEY IN REAR BAY. THE THROTTLE CABLE WAS REPLACED.Jan 12, 2011 · N842FL · Raythn HAWKER800XP · Power LeverSDR CA100609006Transducer · inoperativeCREW NOTICED ABNORMALLY HIGH OIL PRESSURE JUST PRIOR TO LANDING. OIL PRESSURE WENT UP TO 101 PSI AND RANGED BETWEEN 85 AND 101 PSI. ENGINE WAS SHUTDOWN AS A PRECAUTION. OIL PRESSURE TRANSDUCER WAS REPLACED AND 2 LEGS HAVE BEEN COMPLETED WITH NO FURTHER OCCOJun 7, 2010 · Amd FALCON900EX · Engine Oil Indicating SystemSDR CA100518002Bolt · crackedTHE MAIN CABIN DOOR PRESSURIZATION LOAD IS CARRIED BY 10 SQUALLS (BOLT STOPS). FOUND THE 1 NUT AND STUD PORTION MISSING ON POST FLIGHT. THE CONTACT HEAD WAS STILL IN PLACE SO PRESSURIZATION LOAD WAS DISTRIBUTED NORMAL. BOLT WAS REPLACED, WITH FAILED UNIT SENMay 13, 2010 · Amd FALCON900EX · Passenger/Crew DoorsSDR 2010FA0000299Muffler · crackedCOCKPIT ECS MUFFLER ASSY DEVELOPED CRACKS ON EACH END OF THE MUFFLER IN THE WELDED SEAMS AND ALONG THE SIDE OF THE MUFFLER IN THE BEND RADIUS. THE MUFFLER IS FABRICATED FROM ALUMINUM WITH DUCTS WELDED TO EACH END AND IS WRAPPED WITH INSULATION AND FIBERGLASS TApr 8, 2010 · N882CA · Lear 45LEAR · Air Distribution SystemSDR 2010FA0000246Controller · failedON TAKEOFF ROLL THE CREW NOTED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT. THE TAKEOFF WAS ABORTED. THE ACFT WAS SHUTDOWN, ELECTRICAL POWER WAS TURNED OFF AND THE BATTERIES WERE DISCONNECTED. THE ACFT WAS THEN TOWED BACK TO THE HANGAR. THE SOURCE OF TFeb 23, 2010 · N127SF · Amd FALCON900EX · Cabin Temperature Control SystemSDR CA090504001Pump · unserviceable(CAN) POST FLIGHT ON RAMP CREW NOTICED LARGE AMOUNT OF OIL ON INSIDE FACE OF NR 1 ENGINE LOWER COWL. TROUBLESHOOTING DETERMINED ENGINE OIL LEAK FROM OIL LUBE PUMP, SERVICEABLE PUMP INSTALLED, ACFT RETURNED IN SERVICE.Apr 29, 2009 · Amd FALCON900EX · Turbine Engine Oil SystemSDR 2009FA0000274Switch · rupturedFAILURE OF HYDRAULIC PRESSURE SWITCH (R2DW) RESULTED IN THE LOSS OF ALL HYDRAULIC FLUID IN NR 1 HYDRAULIC SYSTEM.Mar 27, 2009 · N404F · Amd FALCON900EX · Hydraulic System, MainSDR 2008FA0000621Compressor Wheel · separatedTHE CREW REPORTED VIBRATION AND ITT RISE. POWER WAS PULLED BACK TO IDLE AND THE AC LANDED WITHOUT INCIDENCE. DISASSEMBLY FINDINGS REVEALED THE LPC2 ROTOR ASSY (PN 307241613). DISC PN 30603731, SN 990316003093, EXHIBITED MATERIAL LOSS IN THE FORM OF A DISC POSAug 26, 2008 · N58CG · Amd FALCON900EX · Turbine Engine Compressor SectionSDR 2007FA0000569Transmitter · reads lowTHE AIRCRAFT WAS CLIMBING AND THE NR 3 ENGINE OIL PRESSURE INDICATION STARTED TO DROP. AT 46 PSI IT WENT RED AND THE PILOT SHUTDOWN THE ENGINE AND LANDED THE AIRCRAFT. THE OIL LEVEL WAS IN LIMITS AND NO EXTERNAL LEAKS WERE FOUND. A DIRECT READING PRESSURE May 17, 2007 · N127SF · Amd FALCON900EX · Engine Indicating SystemSDR 2007FA0000756Life Raft · partial inflateTHE LIFE RAFT VACUUM BAG INFLATED DUE TO CYLINDER LEAKAGE BETWEEN THE CYLINDER HEAD AND LIFE RAFT CYLINDER. THE AC WAS CRUISING AT 40,000 FT WHEN THE PILOT HEAR A LOUD POP. UPON INVESTIGATION, THE PILOT HAD DISCOVERED THE LIFE RAFT HAD AN UNCOMMANDED INFLATINov 12, 2006 · N191MC · Amd FALCON · Escape SlideSDR 2006FA0000731Igniter · brokenPART OF IGNITER PLUG THAT SURROUNDS ELECTRODE SEPARATES AND SHORTS AGAINST THE ELECTRODE CAUSING THE APU NOT TO START. PART COULD POSSIBLY ENTER THE COMBUSTION AREA OF THE APU. (NOTE: APU HAS ONE IGNITER, WE HAVE HAD 2 RECENT FAILURES). (K)Jul 2, 2006 · N882CA · Lear 45LEAR · APU Start/Ignition SystemSDR 2006FA0000656Engine · damagedAT FL350, AIRCRAFT EXPERIENCED A LOUD BANG AND FAILURE OF NR 1 ENGINE (ITT WENT TO RED AND N1 APPROXIMATELY 20 PERCENT). ENGINE WAS SHUTDOWN. DURING DESCENT EXPERIENCED VIBRATION IN AIR FRAME AND CONTROL COLUMN. POST FLIGHT INSPECTION REVEALED EXTENSIVE DAMJun 20, 2006 · N977LP · Amd FALCON900EX · Engine (Turbine/Turboprop)SDR JGV2004F00006Valve · crackedFUEL SUMP VERTICAL UPRIGHT FOR VALVE HOUSING. CRACKED THRU LOWER SOLDER WELD. FOUND AFTER SCREEN REMOVAL. CAUSE WELDING TEMP OR MATERIAL. DO NOT WELD ON SUMPS AND INCREASE MATERIAL THICKNESS.Jul 14, 2004 · N128M · Amd FALCON50MYST · Fuel Boost PumpSDR JGV2004F00004Valve · crackedFUEL DRAIN SUMP UPRIGHT BAR IS CRACKED THRU LOWER SPOT WELD. FOUND DEFECT AFTER REMOVING SUMP DEBRI SCREEN. HIGH TEMPERATURE AT WELDING TIME. RECOMMEND NO SCREENS.Jul 9, 2004 · N128M · Amd FALCON50MYST · Fuel Dump SystemSDR JGV2004F00005Valve · crackedFUEL DRAIN SUMP UPRIGHT BAR IS CRACKED THRU LOWER SPOT WELD. FOUND DEFECT AFTER REMOVING SUMP DEBRI SCREEN. HIGH TEMPERATURE AT WELDING TIME. RECOMMEND NO SCREENS.Jul 9, 2004 · N128M · Amd FALCON50MYST · Aircraft Fuel Distribution SystemSDR G1F2004F00001Tailpipe · corrodedIT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC. THE PAINT HAS BEEN BUBBLING AND THE STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON AC, ALL OF THE CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEETS THE TAILPIPE. THE Feb 9, 2004 · N312P · Amd FALCON900EX · Engine Collector/Tailpipe/NozzleSDR G1F2004F00002Tailpipe · corrodedIT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC, PAINT HAS BEEN BUBBLING AND STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON THIS SPECIFIC AC, ALL OF CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEETS THE TAILPIPE. AREFeb 9, 2004 · N312P · Amd FALCON900EX · Engine Collector/Tailpipe/NozzleSDR UO22003F00005Duct · crackedNR 1 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.Oct 13, 2003 · N377SC · Amd FALCON900EX · Turbine Engine Bypass SectionSDR UO22003F00006Duct · crackedNR 3 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.(K)Oct 13, 2003 · N377SC · Amd FALCON900EX · Turbine Engine Bypass SectionSDR UO22003F00007Duct · crackedNR 2 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.Oct 13, 2003 · N377SC · Amd FALCON900EX · Turbine Engine Bypass SectionSDR UO22003F00008Duct · crackedNR 3 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 O`CLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAN MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K)Oct 3, 2003 · N2425 · Amd FALCON900EX · Turbine Engine Bypass SectionSDR UO22003F00009Duct · crackedNR 2 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 OCLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAL MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K)Oct 3, 2003 · N2425 · Amd FALCON900EX · Turbine Engine Bypass SectionSDR UO22003F00010Duct · crackedNR 1 ENGINE AFT BY-PASS DUCT CRACK AROUND 9 O’CLOCK RIB DUCT, ALLOWED MOMENTARY DISENGAGEMENT OF OIL TRANSFER TUBE AND ORING FAILURE. OIL LEAK CAUSED LOSS OF OIL PRESSURE AT TAKEOFF. PILOT SHUT DOWN ENGINE AND LANDED AT NEAREST AIRPORT. AT REPLACEMENT OF Oct 3, 2003 · N2425 · Amd FALCON900EX · Turbine Engine Bypass SectionSDR 811AV032403Control Panel · smokeDURING CLIMB, CREW SMELLED A BURNING ODOR AND SMOKE IN THE VICINITY OF FLIGHT GUIDANCE CONTROL PANEL. CREW TURNED OFF BACK LIGHTING TO PANEL, SMOKE AND ODOR DISIPATED. FLIGHT CONTINUED TO DESTINATION UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED FLIGHT GUIDAMar 24, 2003 · N811AV · Amd FALCON900EX · Integrated Flight SystemSDR JGV2002F00014Rudder · out of rigUPON REINSTALLATION OF RUDDER AFTER INSTALLATION OF SB, FOUND THAT THE RUDDER TRAVEL WAS APPROXIMATELY 25 DEGREES IN LIEU OF 30+/-DEGREES IAW MM. WHEN TRAVEL WAS CORRECTED, DISCOVERED THAT THE BOTTOM SKIN OF RUDDER WAS CONTACTING THE SKIN PRIOR TO ACHIEVING FOct 28, 2002 · N882CA · Lear 45LEAR · Rudder Control SystemSDR ROCarbon Seal · brokenTHE NR 4 CARBON SEAL CERAMIC RING WAS FOUND TO BE BROKEN DURING THE ENGINE TEARDOWN. THE CARBON RING SEAL WAS ALSO FOUND BROKEN. THERE WAS MUCH COLLATERIAL DAMAGE. THE OPERATOR REPORTED OIL LOSS DURING FLIGHT WITH SUBSEQUENT OIL CONTAMINATION UPON POST FLIGHT Aug 20, 2001 · Amd FALCON900EX · Turbine Engine Compressor SectionSDR 20001218SH016Pump · leakingWHILE FLYING AND INITIATING CLIMB FROM 410 TO 430, OIL PRESSURE STARTED FLUCTUATING. OIL PRESSURE CONTINUED TO FALL. ENGINE SHUT DOWN AS PRECAUTIONARY MEASURE. OIL PUMP LEAKING OIL THROUGH POROUS CASTING. (X)Nov 15, 2000 · N331MC · Amd FALCON900EX · Turbine Engine Oil System
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