Garrett TFE731-2

Service difficulty reports · 201

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 = 'TFE7312'
  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 2025FA0000623Brake Assy · misoverhauledINTERNAL CONTAMINATION BLOCKING THE BLEED PORTS AND STATOR MISALIGNMENT WERE DISCOVERED DURING INSTALLATION/ROUTINE MAINTENANCE OF ELEVEN (11) BRAKE ASSEMBLIES OVERHAULED BY VSE AVIATION (FORMERLY AERO WHEEL AND BRAKE SERVICE CORP) ON OR AFTER 07/16/2025. P/NSep 3, 2025 · Lear 35A · Landing Gear Brake SystemSDR 2025FA0000358Boot · burnedUPON POST FLIGHT WALK AROUND INSPECTION BY FLIGHT CREW, IT WAS DISCOVERED THAT THE LEFT HORIZONTAL STABILIZER ANTI-ICE BOOT HAD SHORTED OUT AND BURNT A HOLE IN THE BOOT AND LEADING EDGE OF THE STABILIZER, NEAR THE CUFF.May 15, 2025 · N240B · Lear 31A · Airfoil Anti/De-ice SystemSDR G1IA202402130057Connector · dirtyPERFORMED VISUAL INSPECTION OF #1 ENGINE FIRE DETECTION LOOP ROUTING AND CONDITION PER LEAR 45 AMM. PERFORMED OPERATIONAL CHECK OF THE ENGINE FIRE DETECTION SYSTEM PER LEAR 45 AMM. CLEANED CONNECTOR AT A37. COULD NOT DUPLICATE DISCREPANCY AT THIS TIME.Feb 10, 2024 · N435DC · Lear 45LEAR · Fire Protection System WiringSDR 2022F00351Hydraulic Line · leakingAFTER TAKEOFF FROM KFXE, I RAN THE AFTER TAKE OFF CHECKLIST. I CHECKED THE HYDRAULIC PRESSURE, AND IT WAS NORMAL. UPON REACHING 10,000FT, THE CREW NOTICED THE "LOW HYD" LIGHT CAME ON AND THERE WAS NO HYDRAULIC PRESSURE. AFTER RUNNING THREE "AMBER" NORMAL CHECKAug 19, 2022 · N441PC · Lear 35A · Hydraulic Fluid ServicingSDR O9IA202107185571Fcu · faultedIN CRUISE FLIGHT, THE FLIGHT CREW NOTICED THAT THE LH THROTTLE WAS STUCK IN THE MCR POSITION. ALL ATTEMPTS TO REDUCE THE THROTTLE WERE UNSUCCESSFUL. UPON CONSULTATION WITH THE MAINTENANCE DEPARTMENT, VIA SATELLITE PHONE, IT WAS DETERMINED THAT A LANDING AT TJul 17, 2021 · N557LM · Beech 45 · Fuel Control/Turbine EnginesSDR KC8A20170907006Oil System · leakingDURING CLIMB THROUGH FL310, THE LEFT ENGINE OIL PRESSURE DROPPING STEADILY, FOLLOWED BY A LOW OIL PRESSURE LIGHT AND MASTER WARNING. THE ENGINE WAS SHUT DOWN AND AN UNEVENTFULL LANDING WAS MADE. UPON INSPECTION, OIL APPEARED TO BE LEAKING FROM THE ENGINE DIPSTAug 31, 2017 · N295CK · Lear 35A · Turbine Engine Oil SystemSDR T6FA20160322001Seal · lack of lubeAIRCRAFT WAS CLIMBING THROUGH FL380, THE CREW GOT AN AMBER AP AIL MISTRIM CAS MSG. AUTOPILOT WAS DISENGAGED TO FIND THAT THEY HAD NO AILERON CONTROL. CONTROL WHEEL WOULD NOT MOVE FROM THE CTR POSITION. PERFORMED ROLL DISCONNECT, WAS ABLE TO CONTROL ACFT & LMar 20, 2016 · N90XR · Lear 45LEAR · Aileron Control SystemSDR CA160104006Bolt · failed(CAN) AFTER LANDING THE CREW DEPLOYED THE TR AND TR DEPLOYED NORMALLY BUT COULD NOT APPLY TR POWER TO LEFT HAND ENGINE. SELECTED TR STOWED BY PIGGY BACK LEVER BUT TR DID NOT STOW. THE THROTTLE WOULD NOT MOVE FORWARD OR BACK FROM IDLE POSITION. CREW TAXIED AIRCDec 17, 2015 · Lear 45LEAR · Power LeverSDR O9IA20150713001Fuel Control · faultyRIGHT ENG FUEL COMPUTER LIGHT ILLUMINATED IN FLIGHT FOLLOWED BY ROLL BACK OF RT ENG. ENG SUBSEQUENTLY SHUTDOWN. ACFT RETURNED TO BASE ON SINGLE ENG. DOWNLOAD OF FUEL COMPUTER IDENTIFIED FAULT IN THE PLA OF THE FUEL CONTROL. FUEL CONTROL CHANGED. PLA FUNCTJul 12, 2015 · N163AL · Lear 31A · Fuel Control/Turbine EnginesSDR 2015F00084Washer · misinstalledRIGHT ENG FIRE LIGHT ILLUMINATED IN CLIMB. LIGHT INTERMITTENTLY ILLUMINATED UNTIL IT REMAINED CONSTANT. PILOT FOLLOWED CHECKLIST & IT STARTED ILLUMINATING INTERMITTENTLY AGAIN. AFTER THE CHECKLIST WAS COMPLETED THE LIGHT STAYED ON, AT WHICH POINT THE PILOT Jun 2, 2015 · N825LJ · Lear 35A · Fire DetectionSDR CA150114004Rub Strip · departed(CAN) RH ENGINE FOD INJESTION, WING TO FUSELAGE FAIRING LEADING EDGE RUBBING STRIP CAME LOOSE AND WENT THROUGH ENGINE IN FLIGHT. PROBLEM KNOWN BY LEARJET (KNOW FOR COMING OFF BUT NOT GOING THROUGH THE ENGINE), SB45-57-10 ALREADY EXISTS TO REPLACE THE EXISTING Jan 13, 2015 · Lear 45LEAR · Aerodynamic FairingsSDR CA140729006Control Unit · failed(CAN) DURING SHORT FINAL CREW NOTED LH/RH OUTBD BRAKE FAIL CAS MESSAGE. ON TOUCHDOWN BRAKES APPLIED BUT SEEMED INEFFECTIVE. CREW ELECTED TO USE EMERG BRAKES. THE AIRCRAFT CAME TO A SAFE STOP ON THE RUNWAY BUT ALL FOUR MAIN TIRES FAILED AND AS A RESULT ALL FOURJul 25, 2014 · Lear 45LEAR · Landing Gear Brake SystemSDR 2014F00127Gasket · leakingLEFT ENGINE FIRE LIGHT ILLUMINATED DURING CLIMBOUT, PASSING THROUGH 5000 MSL. THROTTLE WAS REDUCED AND INDICATION WENT AWAY. ACFT RETURNED TO BASE, UNEVENTFUL LANDING. INSPECTION FOUND THAT THE HP BLEED DUCT AT 12:00 POSITION HAD AN OLDER STYLE PAPER GASKEJun 24, 2014 · N51FN · Lear 35A · Pneumatic Distribution SystemSDR CA140107010Control Unit · malfunctioned(CAN) ACFT DISPATCHED WITH A BRAKE SYSTEM FAULT, WHITE BRAKE FAULT CAS MESSAGE, REF MEL/DDG 32-3. ON RETURN DURING DEFECT TROUBLESHOOTING, DAMAGE WAS OBSERVED ON BOTH OTBD MAIN WHEELS AND INBD MLG DOORS IAW ATTACHED REPORT. IT IS EVIDENT THAT THE MAIN WHEELJan 6, 2014 · Lear 45LEAR · Landing Gear Brake SystemSDR 2014FA0000006Generator · failedMECHANIC REMOVED RT ENGINE COWL AND FOUND SIGNIFICANT INTERNAL AND EXTERNAL DAMAGE TO THE RT GENERATOR. AFT SECTION OF THE GENERATOR CASE WAS SEPARATED, GENERATOR SHAFT WAS SHEARED AND BEARINGS APPEAR TO HAVE FROZEN UP.Jan 5, 2014 · N363PJ · Lear 36A · DC Generating SystemSDR CA131215001Wheel · failed(CAN) DURING A POST FLIGHT INSPECTION, CREW NOTICED A FLAT TIRE AND THEN NOTICED A LARGE PORTION OF THE INBD WHEEL HALF MISSING. THERE WERE NO SIGNS OF OVERHEAT, SUDDEN STOPS, EXCESSIVE BREAKING OR SKID MARKS ON THE TIRE OR BRAKE ASSY. THIS WHEEL ASSY WAS BDec 13, 2013 · Lear 36A · Wheel/Ski/FloatSDR 2013FA0000475Fuel Control · malfunctionedCREW REPORTED LT ENGINE THROTTLE STUCK AND UNABLE TO RETARD. AFTER MOVING THE THROTTLE THEY WERE ABLE TO BRING TO IDLE FOR LANDING. REMOVED FUEL CONTROL AND FOUND TWO SCREW HEADS BROKEN OFF AND FLOATING AROUND MECHANICAL LINKAGE.Aug 20, 2013 · N30PC · Lear 45LEAR · Fuel Control/Reciprocating EnginesSDR G41A20130731004Solenoid · shortedDURING CLIMB, NR 1 ENGINE EXPERIENCED A SUDDEN SURGE FOLLOWED BY A ROLLBACK OF APPROXIMATELY 15 PERCENT N1. CAPTAIN NOTICED LT FUEL COMPUTER LIGHT ON & CO-PILOT EXECUTED CHECKLIST. FUEL COMPUTER DID NOT RESET. DECIDED TO RETURN. AFTER BURNING OFF FUEL, LANJul 27, 2013 · N61SJ · Lear 55LEAR · Fuel Controlling SystemSDR 2013F00048Terminal · brokenA FEW MINUTES AFTER TAKEOFF, MASTER CAUTION LIGHT CAME ON DUE TO THE LOSS OF THE RT GENERATOR. AT THE SAME TIME SEVERAL CIRCUIT BREAKERS TRIPPED RESULTING IN THE LOSS OF MOST OF THE RT SIDE OF THE COCKPIT. AFTER TROUBLESHOOTING, FOUND B TERMINAL WIRE TERMFeb 3, 2013 · N71PG · Lear 36LEAR · Turbine Engine System WiringSDR 2013F00018Swivel Fitting · blew outAFTER TAKEOFF PILOT REPORTED NO HYD PRESSURE. UPON LANDING SAFELY AND TROUBLESHOOTING THE ISSUE , FOUND THE MLG ACTUATOR RETRACT SWIVEL FITTING HAD FAILED. R & R THE SWIVEL FITTING WITH A NEW PART (PN 142870). PERFORMED ALL GEAR SWINGS AND ASSOCIATED HYDJan 15, 2013 · N568PA · Lear 35A · Hydraulic System, MainSDR CA120812001Wheel Half · damaged(CAN) AIRCREW REPORTED TIRE BLOW OUT ON ROLL OUT AFTER LANDING. TIRE WAS SERVICED DAY BEFORE FLIGHT NO-DEFECTS WERE REPORTED. THE NR 3 MAIN WHEEL WAS FOUND TO BE DAMAGED. THE ACFT WAS INSPECTED, WHEEL ASSY WAS REPLACED AND ACFT WAS RETURNED TO SERVICE. DETAug 4, 2012 · Lear 35A · Wheel/Ski/FloatSDR CA120130008Uplock · failed(CAN) THE PART IN QUESTION WAS INSTALLED TO REPLACE A UNIT THAT WAS LEAKING HYDRAULICS. IT WAS INSTALLED AND TESTED IAW WITH ALL MM REQUIREMENTS AND RELEASED TO SERVICE. ON TAKEOFF, ONCE THE GEAR WAS RETRACTED AND THE ACFT ACCELERATED THROUGH 200 KTS, THE CRJan 28, 2012 · Lear 45LEAR · Landing Gear Retraction/Extension SystemSDR CA110923012Pulley · out of tolerance(CAN) DURING A MX WALK AROUND, FOUND A .7500" FREEPLAY IN THE RT AILERON. DURING INVESTIGATION, FOUND THAT THE RT AILERON PULLEY AND SHAFT WERE MOVING INDEPENDENTLY. ON DISASSEMBLY OF THE PULLEY AND SHAFT FOUND THAT THE PULLEY AND SHAFT WERE NOT A CLOSE TOLESep 22, 2011 · Lear 36A · Aileron Control SystemSDR CA110801001Converter · failedDURING PRE-FLIGHT, CREW MEMBERS NOTICED AN ELECTRICAL BURN ODOR. AFTER MX INVESTIGATION, THE EFB DC STEP DOWN CONVERTER WAS IDENTIFIED AS THE SOURCE. CONVERTERS ARE INSTALLED IAW TC LSTC C-LSA05-306/D.Jul 30, 2011 · Lear 45LEAR · DC Rectifier/ConverterSDR CA110715001Fire Loop · out of positionENGINE FIRE INDICATION AFTER TAKEOFF. ACFT RETURNED TO AIRPORT. MX ENGINEERS SENT TO TROUBLESHOOT, DUPLICATED FAULT ON GROUND WITH HIGH POWER SETTINGS ONLY. INSPECTED BLEED AIR DUCTS IN NACELLE AND RE-TORQUED ALL CLAMPS, FIRE WIRE REPOSITIONED AS IT WAS FOUJul 12, 2011 · Lear 45LEAR · Fire DetectionSDR CA110701002Pump · failedMAY 14, 2011, CREW REPORTED LOW OIL PRESSURE ON TOUCHDOWN (64 PSI) FOR A FEW SECONDS AND THEN BACK TO NORMAL. OIL PUMP WAS REPLACED WITH AN O/H UNIT. CREW REPORTED A FLUCTUATION OF THE OIL PRESSURE DURING THE CLIMB OUT THRU 33, 000 TO 37,000 FT. AFTER DISCUSJun 29, 2011 · Lear 45LEAR · Engine Oil PressureSDR CA110311003Starter Gen · failed(CAN) DURING THE DESCENT TO AIRPORT, AT APPROX. 110 MILES OUT CREW NOTICED VIBRATION. THEY WERE UNABLE TO DETERMINE FROM WHICH SIDE OR IF IT WAS COMING FROM THE ENGINES. A FEW MINUTES LATER THE L/H GENERATOR WHEN OFF LINE. WEATHER BEEN OK, CREW DECIDED TO CARRMar 9, 2011 · Lear 45LEAR · Starter-GeneratorSDR 2011F00031Generator · failedLT AND RT GENERATOR LIGHTS ILLUMINATED. THE GENERATOR FAILURE (DUAL) CHECKLIST WAS PERFORMED. CREW ELECTED TO DIVERT. THE FLIGHT WAS COMPLETED WITH LANDING, WITHOUT FURTHER INCIDENT. IT HAS NOT BEEN DETERMINED AT THIS TIME AS TO WHAT EXACTLY THE CAUSE OF TFeb 9, 2011 · N710GS · Lear 35LEAR · AC Generator-AlternatorSDR DBCA2010110800029Actuator · malfunctionedON TAXI FOR DEPARTURE CREW NOTED LT THRUST REVERSER UNLOCK LIGHT WOULD NOT EXTINGUISH AFTER TEST. CREW RETURNED TO RAMP. MX PINNED THRUST REVERSERS IAW AMM 78-30 AND DEFERRED IAW MEL 78-1. MAINTENANCE BLED HYDRAULIC LINE TO OVERCENTER LATCH ACTUATOR. OPS CNov 8, 2010 · N945HC · Lear 45LEAR · Engine Thrust ReverserSDR O9I2010F00000Fire Loop · shortedRETURNING WITH A PATIENT ON BOARD, RECEIVED A FIRE LIGHT ON NR 1 ENGINE DESCENDING THROUGH FL370 FROM OUR CRUISE ALTITUDE OF FL390. THE F/O WAS FLYING AND PILOT ACCOMPLISHED THE REQUIRED ITEMS FOR AN ENGINE FIRE. FIRELIGHT DID NOT GO OUT UNTIL 3 TO 4 MINUTESAug 16, 2010 · N543LM · Lear 35A · Fire DetectionSDR CA100721007Alternator · failedPILOTS REPORTED THAT THEY HAD A DOUBLE GENERATOR FAILURE ENROUTE. THEY WERE ABLE TO RESET THE LT GENERATOR BUT COULD NOT RESET THE RT GENERATOR. UPON ARRIVAL, MX FOUND THAT THE CURRENT LIMITER ON THE RT GENERATOR WAS `OPEN`. THE GENERATOR WAS REMOVED IN ORDER Jul 20, 2010 · Lear 35A · AC Generator-AlternatorSDR CA100721008Skin · debondedA DISBOND BLISTER WAS FOUND ON THE UPPER SKIN AT THE CTR ATTACH FITTING OF THE RT DELTA FIN ROOT AREA. A TAP TEST REVEALED THAT THE DISBOND WAS APPROX 16 SQ". THE DISBONDED SKIN WAS CUT OUT AND THE 3" THICK HONEYCOMB CORE WAS FOUND TO BE FULL OF WATER. THE Jul 19, 2010 · Lear 45LEAR · Fuselage Main, Plate/SkinSDR CA100701006Control Rod · chafed(CAN) DURING A SCHEDULED INSP, THE RUDDER NON ADJUSTABLE ROD WAS FOUND CHAFING AGAINST A STAINLESS STEEL BRAIDED HYDR LINE AT ZONE 324. ROD REPLACED WITH SERVICEABLE UNIT AND LINES REPOSITIONED.Jul 1, 2010 · Amd FALCON10 · Rudder Control SystemSDR CA100706007Shutoff Valve · failed(CAN) WHEN RETRIEVING ITEM FROM THE TAIL LOCKER, OBSERVED THE LATCH TO BE VERY HOT TO THE TOUCH. UPON FURTHER INVESTIGATION, DISCOVERED AN ELEVATED TEMPERATURE IN THE TAIL CONE AREA. ALSO, OBSERVED THE FIRE BOTTLE PRESSURE TO BE VERY HIGH. AFTER DISCUSSING Jun 25, 2010 · Lear 35A · Windshield/Door Rain/Ice RemovalSDR CA100525008Pressure Switch · leakingPILOT REPORTED AN HYD LOW CAS MESSAGE IN FLIGHT. UPON INVESTIGATION ON GROUND BY MX, IT WAS DISCOVERED THAT THERE WAS HYD FLUID ON LOWER FUSELAGE. IT WAS LATER DISCOVERED THAT AUX HYD LOW PRESSURE SWITCH S9 (LT ENGINE) WAS LEAKING BETWEEN THE ELECTRICAL CONNMay 21, 2010 · Lear 45LEAR · Hydraulic System, AuxiliarySDR J7SA452041100520Downlock Switch · out of rigLT MAIN GEAR INDICATOR DID NOT MATCH GEAR HANDLE POSITION. CREW CYCLED SEVERAL TIMES AND LIGHT EVENTUALLY ILLUMINATED ON LT GEAR DOWN POSITION. CREW PERFORMED TOWER FLYBY TO CONFIRM GEAR POSITION. LANDING UNEVENTFUL, ALTHOUGH TOWER DID CALL FOR EMERGENCY SERVIMay 20, 2010 · N614FX · Lear 45LEAR · Landing Gear Position and WarningSDR CA100204007Downlock Switch · out of rig(CAN) GEAR SWING CARRIED OUT AFTER REPLACEMENT OF STEERING MOTOR. FOUND SERVICEABLE. ACFT ACCEPTANCE TEST FLIGHT WAS CARRIED OUT AND CREW EXPERIENCED NO DOWN LOCK INDICATION ON LT MAIN. SECONDARY INDICATION FOR DOWN & LOCK ALSO NOT PRESENT. GEAR EMERGENCY EXTFeb 2, 2010 · Lear 35A · Landing Gear Position and WarningSDR CA100127001Throttle Cable · sheared(CAN) ACFT WAS LEAVING AT ABOUT 0330AM. AT THE THRESHOLD, PILOT STARTED TO PUSH THE THROTTLES FWD, WHEN HE NOTICED THAT AT 60 PERCENT N1 THE RT ENGINE WAS ABNORMAL, RETARDED THE THROTTLE AND THE ENGINE SHUTDOWN. PILOT TRIED MULTIPLE RESTARTS, WITH NO SUCCESJan 23, 2010 · Lear 35A · Power LeverSDR CA100122006Sleeve · cracked(CAN) DURING THE COMPLETION OF SB45-27-40 IT WAS DETERMINED THAT NR 3 (RT INBD) FLAP ACTUATOR BALLSCREW SLEEVE WAS CRACKED APPROX 0.250 INCHES LONG, CTR OF THE SLEEVE. REMAINING FLAP ACTUATORS (POSITIONS 1, 2, AND 4) WERE FOUND TO BE SERVICEABLE AT TIME OF INJan 21, 2010 · Lear 45LEAR · Trailing Edge Flap ActuatorSDR CA090717005Axle · corroded(CAN) DURING THE INSTALLATION OF A LANDING GEAR SB (SB45-32-29R1) IT WAS REQUESTED THAT INSP OF THE INTERNAL SURFACES OF THE LANDING GEAR AXLE BEAM ASSY FOR POSSIBLE CORROSION. BOROSCOPE INSPECTIONS COMPLETED, CORROSION IDENTIFIED AND MFG CONTACT WITH THE RESJul 14, 2009 · Lear 45LEAR · Nose/Tail Landing Gear Strut/AxleSDR CA090714004Wire · burned(CAN) DURING POST-FLIGHT CHECK, NOTICED LT LANDING LIGHT WAS INOPERATIVE. FURTHER TROUBLESHOOTING FOUND BURNED WIRE, RAA0238-14, APPROX 12 INCHES AFT OF LT AFT DISTRIBUTION PANEL, A FEW INCHES FWD OF SPLICE SP302 WHERE ONE WIRE GOES FROM GAUGE 14 TO TWO 20 GAUJul 13, 2009 · Lear 45LEAR · Exterior LightingSDR CA090414002Flex Duct · cracked(CAN) AFTER PILOT REPORTED A "WING/STAB LEAK" MASTER CAUTION MESSAGE, INVESTIGATION OF THE PROBLEM ENDED WHEN A TECH FOUND THE LT HORIZ STABILIZER`S ANTI-ICE FLEXIBLE DUCT (LOCATED AT THE VERTICAL STAB TO HORIZONTAL STAB JUNCTION) CRACKED. THE CRACK WAS PROBABApr 13, 2009 · Lear 45LEAR · Airfoil Anti/De-ice SystemSDR CA090414004Flex Duct · cracked(CAN) AFTER PILOT REPORTED A "WING/STAB LEAK" MASTER CAUTION MESSAGE, INVESTIGATION OF THE PROBLEM REVEALED THAT THE LT HORIZ STAB ANTI ICE FLEXIBLE DUCT (LOCATED AT THE VERTICAL STAB TO HORIZ STAB JUNCTION) WAS CRACKED. THE CRACK WAS PROBABLY CAUSED BY THE DApr 13, 2009 · Lear 45LEAR · Airfoil Anti/De-ice SystemSDR CA090306005Drive Unit · leaking(CAN) UNIT WAS LEAKING FLUID, THIS IS THE 5TH UNIT WHICH HAS LEAKED AFTER INSTALATION, 0-LEAK RATE GIVEN BY AIRCRAFT MFR.Feb 28, 2009 · Lear 45LEAR · Trailing Edge Flap Control SystemSDR CA090223018Display · odor(CAN) THE CREW POWERED UP THE ACFT TO GET THEIR PREFLIGHT CHECK DONE. A FEW SECONDS AFTER POWER UP, THE DU NR 2 WENT BLANK AND A STRONG ELECTRICAL ODOR WENT THRU THE COCKPIT. PROBLEM, TROUBLESHOT TO THE DISPLAY UNIT ITSELF. A TECH WAS DISPATCHED TO REPOSITIONFeb 19, 2009 · Lear 45LEAR · Central DisplaySDR CA090223017Pump · failed(CAN) DURING TROUBLESHOOTING, WHITE CAS MESSAGE, L-CAB PRESS FAIL, MX NOTED UN-COMMANDED PRESSURIZATION DURING GROUND RUNS. TROUBLESHOOTING OF SYS, FOUND DEBRIS BLOCKING THE VACUUM EJECTOR PUMP, CAUSING OUTFLOW VALVES TO BE SLOW AND REMAINED CLOSED DURING GROUFeb 18, 2009 · Lear 45LEAR · Fuel Transfer ValveSDR J7SA452022081221Generator · failedR/H ENGINE VIBRATION NECESSITATED IN-FLIGHT SHUTDOWN. DURING VIBRATION THE 'EMER BATT' AND EMER SWITCH LIGHTS WOULD BLINK. AIRCRAFT DIVERTED TO KFLL. MAINTENANCE RAN ENGINE AND FOUND THE RT GENERATOR FAULTY. GENERATOR REPLACED AND GROUND RUNS PERFORMES SATISFDec 21, 2008 · N609FX · Lear 45LEAR · AC Generator-AlternatorSDR CA081222007Audio Panel · malfunctioned(CAN) DURING THE BASIC INSPECTION WITH AIRCRAFT POWER ON, FUMES AND LIGHT SMOKE WHERE NOTICED IN THE COCKPIT. AFTER INSPECTION THE AUDIO WARNING PANEL BOX WAS FOUND TO BE THE CAUSE. THE AUDIO WARNING PANEL BOX WAS REPLACED WITH A REPAIRED SERVICEABLE UNIT FRDec 19, 2008 · Amd FALCON10 · Audio Integrating SystemSDR CA081024006Ground Wire · open(CAN) ON LANDING, A WHITE CAS MESSAGE (SECONDARY TRIM FAULT) APPEARED. SYS TROUBLESHOT AND FOUND AN OPEN GROUND WIRE AT RBA0664N-22 AT SPLICESP322. SPLICE REPAIRED AND FUNCTION CHECKED SERVICEABLE.Oct 10, 2008 · Lear 45LEAR · Autopilot Trim ServoSDR CA080821012Windshield · broken(CAN) WHILE IN CRUISE AT FLT 400 ENROUTE, THE RT WINDSHIELD OUTTER PLY SHATTERED, CAUSING A LOUD BANG. NO DEPRESSURISATION OCCUR, RT WINDSHILED HEAT BECAME INOPERATIVE. RT WINDSHIELD REPLACED WITH NEW ONE. ACFT RETURN TO SERVICE.Aug 17, 2008 · Lear 45LEAR · Flight Compartment Windows
Back to Garrett TFE731-2