Garrett TFE731 series

Service difficulty reports · 742

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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 = 'TFE731'
  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 J7SA452051090710Connector · damagedCREW ADVISED CAS ILLUMINATED. FLAPS & GEAR BOTH RETRACTED. FOLLOWED CHECKLIST & USED EMERGENCY BRAKING, BLOWING BOTH LT MAIN TIRES. CAS NOT ASSOCIATED WITH GEAR EXTENSION, & EMERGENCY BRAKING PROCEDURES HAD TO BE USED IAW CHECKLIST. MX REPORTED ON ENGINE RSep 7, 2010 · N615FX · Lear 45LEAR · Landing Gear System WiringSDR UVVR2010081300014Skin · corroded(UVVR) EXTERIOR SURFACE OF SKINS ON LOWER ENGINE COWLINGS SHOW EVIDENCE OF CORROSION AROUND RIVET HEADS. PAINT IS BLISTERING.Aug 13, 2010 · N710R · Lear 45LEAR · Nacelle/Pylon, Plate/SkinSDR EZKA2010F00193Unknown · multiple failON VISUAL APPROACH, EXPERIENCED ELECTRICAL FAILURE IN ACFT. SELECTED FLAPS 8, AND COMPLIED WITH SPEED RESTRICTION OF 170 KNOTS, STARTED A DECENT FROM 2000 FT. FELT CABIN LOSE PRESSURIZATION AND GREEN NOSE WHEEL STEERING ANNUNCIATOR ILLUMINATED WITHOUT NOSE Aug 13, 2010 · N35GC · Lear 35A · Electrical Power SystemSDR 2010FA0000815Switch · intermittentCREW PERFORMED ALL PREFLIGHT FUNCTIONAL CHECKS OF ALL ACFT SYS. AT THAT TIME THE SPEED BRAKE/SPOILERON SYS WAS REPORTED BY CREW TO TEST NORMALLY. PAX LOADED AND CREW PREPARED FOR DEPARTURE. ON TAKEOFF ROLL "AIRSPEED WAS ALIVE". AT APPROX 80 KTS INDICATED AIRSAug 5, 2010 · N645G · Lear 35LEAR · Drag Control SystemSDR BKEA201008011Valve · openDURING REPOSITION FLIGHT WITH NO PASSENGERS ON ACFT, AFTER TAKEOFF. DURING CLIMB OUT, ACFT EXPERIENCED IN FLIGHT SMOKE IN CABIN. ACFT RETUREND TO DEPARTURE, HAVING DECLARED AN EMERGENCY, COCKPIT AUX HEAT VALVE WAS FOUND PARTIALLY OPEN AFTER MX, THIS WAS THE FAug 1, 2010 · N752CS · Raythn HAWKER800 · Cabin Cooling SystemSDR BSYA2010032Pump · defectiveON APPROACH INTO CPS RIGHT ENGINE LOW OIL PRESSURE LIGHT CAME ON AND OIL PRESSURE GAUGE WAS AT THE TOP OF RED LINE. PILOT ELECTED TO SHUT THE ENGINE DOWN, AND LANDED NO PROBLEMS. REMOVED AND REPLACED OIL PUMP.Jun 30, 2010 · N400JE · Lear 35A · Turbine Engine Oil SystemSDR 2010FA0001233Skin · misinstalled(CNQ8) FOUND SHY EDGE DISTANCE ON 2 RIVETS ON THE PILOTS AND COPILOTS SIDE WINDOW FRAMES REQUIRING REPLACEMENT OF THE SKINS.Jun 23, 2010 · N211CQ · Cessna 650 · Fuselage Main, Plate/SkinSDR N382010F00000Fire Loop · out of positionDURING CLIMB, LT ENGINE FIRE T-HANDLE ILLUMINATED. ALL ENGINE GAUGES INDICATED NORMAL. REDUCED POWER ON LT ENGINE. LIGHT EXTINGUISHED IN ABOUT 3 SECONDS AND FIRE LOOP TESTED NORMALLY. RAN THE APPROPRIATE CHECK LIST AND CONTINUED WITHOUT FURTHER ISSUE. WROTJun 17, 2010 · N825LJ · Lear 35A · Fire DetectionSDR 2010FA0000417Muffler · crackedWELDED MUFFLER SEAM CRACKED AT THE TOP INBOARD EDGE OF THE BOX. CRACKED TOOK PLACE OVER NORMAL OPERATING CONDITIONS.Apr 27, 2010 · N863CA · Lear 45LEAR · Air Distribution SystemSDR 2010FA0000396Line · chafedTHE SOURCE OF A FUEL LEAK WAS TRACED TO THE RT MAIN FUEL LINE TO THE FILTER AND SHUTOFF VALVE IN THE AFT EQUIPMENT BAY JUST FWD OF THE RT MAIN SHIP BATTERY. THE FUEL LINE WAS CHAFED BY THE UNION FITTING OF A HYD LINE RUNNING PARALLEL TO THE FUEL LINE. UPON REMApr 21, 2010 · N10AH · Lear 35A · Aircraft Fuel Distribution SystemSDR 2010FA0000289Link Pin · corrodedDURING THE REPLACEMENT OF THE NLG STEERING PIN (PN 25UN605) IAW MANDATORY SB 32-3962, REV 2, THE STEERING LINK PIN, PN 25UN619, WAS FOUND CORRODED.Mar 22, 2010 · N86MN · Raythn HAWKER800XP · Landing Gear Steering SystemSDR 2010FA0000250Life Raft · bulgedTHIS LIFE RAFT WAS REMOVED FROM THE ACFT DURING A SCHEDULED 4A+, INSP FOR A NORMAL RECERTIFICATION OF THE LIFE RAFT. THE CONTAINER WAS NOTED AS BEING " BULGED" COMPARED TO THE OTHER LIFE RAFT ON BOARD THE ACFT. BOTH RAFTS WERE SENT FOR INSPECTION AND RECERTIMar 10, 2010 · N78LF · Amd FALCON50MYST · Life RaftSDR 2010FA0000183Inlet · damagedON POST FLIGHT INSP, DISCOVERED 2 RIVET HEADS MISSING FROM THE LT ENGINE INLET COWL. THE ENGINE WAS VISUALLY INSPECTED AND DAMAGE TO THE FAN BLADES WAS NOTED. A BOROSCOPE INSP WAS ACCOMPLISHED ON THE 1ST STAGE COMPRESSOR BLADES AND DAMAGE WAS NOTED. THE ENGINEFeb 24, 2010 · N900PE · Raythn HAWKER900XP · Engine Air Intake SystemSDR UVVR2010022600006Floorbeam · corrodedANGLE CORRODED (EXFOLIATED) ON LOWER FS 166.3 FUSELAGE FLOOR SUPPORT WEB RT BP 8-10, ATTACHED TO LOWER FUSELAGE SKIN AND WEB.Feb 23, 2010 · N47SE · Rkwell NA26565 · Fuselage Main, Floor BeamSDR 2010F00045Downlock Switch · intermittentWHEN SELECTING "GEAR DOWN" ON APPROACH TO DESTINATION AIRPORT THERE WAS NO RT DOWNLOCK "GREEN" ANNUNCIATOR. LANDING GEAR WAS CYCLED 5 TIMES. THE 5TH TIME SHOWED "3 GREEN" AND ACFT WAS LANDED WITHOUT INCIDENT. ACFT WAS JACKED AND GEAR WAS SWUNG. FOUND INTERMITTFeb 16, 2010 · N70AX · Lear 35A · Landing Gear Position and WarningSDR 2010F00029Warning Light · illuminatedAS THE FLIGHT CREW TAXIED TOWARDS THE RUNWAY, THEY NOTICED RT ENGINE "FUEL COMPUTER MANUAL" LIGHT ILLUMINATED. CREW RETURNED TO THE HANGER AND NOTIFIED MX. MX PERSONNEL DOWNLOADED AND CLEARED DEECS' AND FOUND CODES 2,237, AND 242. CHECKED N1 RESISTANCE AND INFeb 8, 2010 · N40FC · Cessna 650 · Engine Fuel and ControlSDR 2010FA0000089Trim System · malfunctionedCLIMBING ON DEPARTURE FROM PSP WITH AUTOPILOT ENGAGED, AUTOPILOT WAS DISCONNECTED MANUALLY BECAUSE IT WAS GOING TO GO THROUGH THE LEVEL OFF ALTITUDE, THE TRIM WHEEL CONTINUED TO TRIM NOSE UP UNTIL IT WAS HELD AND FORCED TO STOP. RED TRIM LIGHT AND MACH TRIM FFeb 4, 2010 · N897QS · Raythn HAWKER900XP · Autopilot Trim ServoSDR CA100208009Fuel Control · malfunctioned(CAN) DISCREPANCY NR 1 ENGINE SURGING AFTER VR ON TAKEOFF WITH AN APR EVENT. WITH ENGINE POWER REDUCED TO IDLE THE N1 STABILIZED AND REMAINED AT IDLE FOR THE REMAINDER OF THE FLIGHT. KEPT THE ENGINE RUNNING AT IDLE TILL AFTER LANDING. RECTIFICATION LT FUELFeb 1, 2010 · Raythn HAWKER900XP · Fuel Control/Turbine EnginesSDR 2010F00031Drag Chute · missingABOUT 75 MILES FROM DESTINATION, WHILE IN A STABILIZED DECENT OF 2000 FPM FROM FLIGHT LEVEL 400 TO FLIGHT LEVEL 220 (AROUND FLIGHT LEVEL 220) FLIGHT CREW HEARD A LOUD BANG. THERE WAS NO CHANGE IN FLIGHT COORDINATION OF THE ACFT, NO CHANGE IN ANY INDICATION, ORJan 31, 2010 · N905RL · Lear 55LEAR · Emergency EquipmentSDR 2009FA0001048Bearing · failedS.O.A.P. SAMPLE REVEALED A TRACE OF CARBON STEAL, ALUMINUM AND GRIT (CARBON/GRIT) WITH MAJOR AMOUNTS OF M50 WITH SHINY PLATELETS. THE FILTER WEIGHT WAS 7,806 MGS. THE ENGINE WAS DISASSEMBLED IAW THE CURRENT MM AS REQUIRED TO ACCESS ALL BEARINGS. DISASSEMBLYNov 30, 2009 · N700WY · Raythn HAWKER900XP · Engine (Turbine/Turboprop)SDR IEY2009F00000Control Valve · stickingAFTER TAKEOFF, PASSENGERS REPORTED SUDDEN AND EXCESSIVE RISE IN CABIN TEMPERATURE. PILOT`S REPORTED TO TOWER THEY WERE RETURNING TO DEPARTURE AIRPORT. TROUBLESHOOTING RESULTED IN THE REPLACEMENT OF THE CABIN TEMPERATURE CONTROL VALVE. ALTHOUGH SMOKE IN CABIOct 18, 2009 · N390GG · Lear 45LEAR · Air Distribution SystemSDR BSYA2009051Computer · failedEN ROUTE FROM TEB TO CPS WHEN THE LEFT ENGINE COMPUTER FAILED. DIVERTED TO LCK. MAINTENANCE FOUND THE FUEL COMPUTER WAS DEFECTIVE. REMOVED AND REPLACED FUEL COMPUTER, OPS CHECKS GOOD.Sep 30, 2009 · N72JF · Lear 35A · Fuel Controlling SystemSDR DXTA2009091603787Engine · power lossWHILE PERFORMING TC13, DURING STEP 3, NR1 ENG ROLLED BACK FROM 94 PERCENT TO 64 PERCENT; NR 2 ENG ROLLED BACK FROM 94 PERCENT TO 84 PERCENT. PERFORMED FUEL CONTROL MANUAL MODE ADJUSTMENT PROCEDURES ON ENG NR 1 AND 2 MANUAL MODE GOVERNORS WERE FOUND TO BE FUNCSep 15, 2009 · N878QS · Raythn HAWKER900XP · Engine (Turbine/Turboprop)SDR 2009FA0000766Line · corrodedLINE HAD CORROSION ON 90 DEGREE BENDS ADJACENT TO FERRULES FOR B-NUTS. THE PORTION OF THE LINE AT BOTH ENDS HAD CORROSION THA WAS PRESENT WHERE THE PROTECTIVE COATING WAS REMOVED, APPARENTLY DURING MFG OF THE PART. THE CORROSION HAD EATEN THROUGH ONE END OF Aug 19, 2009 · N325NW · Lear 35A · Hydraulic System, MainSDR CA090717003Line · leaking(CAN) DURING A ROUTINE ACFT WALK AROUND A SMALL QUANTITY OF FUEL WAS NOTED ON THE GROUND, CTR FUSELAGE, MID WING. INVESTIGATION OF THIS AREA FOUND BOTH FUSELAGE TO WING TANK FUEL LINES WEEPING FUEL. MFG WAS CONTACTED AND INFORMED OF THE ISSUE. THEY IDENTIFIEJul 10, 2009 · Lear 45LEAR · Aircraft Fuel Distribution SystemSDR 2009FA0000596Actuator · failedON APPROACH TO LANDING GOT A PRIMARY PITCH TRIM FAILURE LIGHT, SWITCHED TO SECONDARY PITCH TRIM NO STAB MOVEMENT. RUN CHECKLIST STILL NO STAB MOVEMENT IN PRIMARY OR SECONDARY MODE. REENGAGED AUTO PILOT PRIMARY PITCH TRIM WORKED FOR A MOMENT THEN FAILED AGAINJul 1, 2009 · N97AL · Cessna 650 · Stabilizer Control SystemSDR CA090618001Dipstick · broken(CAN) DURING OIL LEVEL CHECK, FOUND PART OF THE RT ENGINE OIL LEVEL DIPSTICK WAS MISSING. OIL RESERVOIR WAS DRAINED AND THE MISSING PART OF THE DIPSTICK WAS FOUND LAYING IN THE TANK BOTTOM. MAGNETIC CHIP DETECTOR WAS INSPECTED AND NO EVIDENCE OF DEBRIS WERE Jun 15, 2009 · Lear 45LEAR · Turbine Engine Oil SystemSDR DXTA2009060803683Fan · vibrationLT ENGINE VIBRATION AT FL 400. VIBRATION STARTED WHEN THROTTLE WAS RETARDED FROM 98.3 TO 97 PERCENT N1. THROTTLE MOVEMENTS HAD NOT EFFECT ON VIBRATION. SOUND DECREASED AS ACFT DESCENDED. REMOVED FAN BLADES FAN HUB AND RE INDEXED FAN HUB 180 DEGREES FROM ORIGIJun 5, 2009 · N894QS · Raythn HAWKER900XP · Turbine Engine Compressor SectionSDR CA090514003Line · leaking(CAN) DURING A BASE INSP, MX FOUND THE BOTOM FUSELAGE STROBE BEACON LIGHT LENS HAD 1 INCH OF FLUID IN THE BOTTOM FURTHER INVESTIGATION REVEALED THE FLUID TO BE JET FUEL SEEPING THROUGH FUSELAGE THE SOURCE OF THE FUEL LEAK CAME FROM THE FEEDER LINE CONNECTING May 12, 2009 · Lear 45LEAR · Aircraft Fuel Distribution SystemSDR 2009FA0000382Switch · corrodedDURING POSTFLIGHT INSPECTION FOUND THAT THE CABIN ALT WARNING HORN WOULD NOT SILENCE. LEG DOWNLOCK MICROSWITCH (JM)P/N 9006EN42 FOUND TO BE LEAKING 4 VOLTS FROM PIN 4 TO PIN 5 DUE TO CORROSION . 4 VOLTS WAS NOT ENOUGH TO PULL IN THE COIL ON RELAY (AD) BUT IT WMay 7, 2009 · N733A · Raythn HAWKER800XP · Landing Gear Position and WarningSDR 2009FA0000694Holder · failedWHILE TROUBLESHOOTING A PULSE LIGHT SYS PROBLEM ON OUR ACFT, FOUND AN ISSUE INVOLVING 2 IN-LINE FUSE HOLDERS WHICH WERE INSTALLED IN COMPLIANCE WITH MANDATORY SB 33-3682 (RE-ACTIVATION OF PULSE LIGHT SYS). THESE 2 FUSE HOLDERS (PN 155020A) ARE IN-LINE WITH THApr 15, 2009 · N875LP · Raythn HAWKER800XP · Lighting SystemSDR DXTA2009040603584Engine · failedAT FL380, .76M, A THUMP WAS FELT IN THE AIRFRAME WITH A CONSTANT VIBRATION. LT NR 1 OIL PRESS TURNED RED AND COMPLETED THE LOW OIL PRESS MEM ITEMS AND SHUT THE ENGINE DOWN. NR1 CHIP DETECT IS TRIPPED. INSPECTED CHIP DETECTORS AND OIL FILTER. FOUND METAL SHAApr 5, 2009 · N897QS · Raythn HAWKER900XP · Engine (Turbine/Turboprop)SDR 2009FA0000765Bearing · damagedTHE SUBJECT ENGINE WAS REMOVED FOLLOWING A COMMANDED INFLIGHT SHUTDOWN ON APRIL 5TH, 2009. SHUTDOWN DETAILS: AT APPROX 39K, CREW NOTED NR 1 ENGINE THUMP AND VIBRATION, WITH OIL PRESSURE INDICATION IN RED (LOW). CREW PERFORMED ENGINE SHUTDOWN. ENG WAS RETURNApr 5, 2009 · N897QS · Raythn HAWKER900XP · Turbine Engine Compressor SectionSDR RMV2009F00000Brake · fireDURING A MX HIGH SPEED TAXI CHECK SMOKE NOTICED OUT OF PILOTS SIDE WINDOW. ACFT STOPPED ON RUNWAY AND CABIN DOOR OPENED AT WHICH TIME A FIRE WAS FOUND ON LT MLG WHEEL AREA. ACFT SHUTDOWN AND FIRE EXTINGUISHED. PRIOR TO THE TAXI TEST A FULL BRAKE AND ANTI-SKMar 30, 2009 · N40DK · Lear 55LEAR · Landing Gear Brake SystemSDR A9JA1Starter Gen · failedSTARTER GENERATOR PREMATURE FAILURE. REPLACED WITH OVERHAULED UNIT.Mar 22, 2009 · N3VJ · Lear 31A · Starter-GeneratorSDR BHKA10FNFEB252009Turbine Blades · failedWHILE CLIMBING AT 17,000 FT, APPROX 40 MINUTES INTO FLIGHT, HEARD LOUD BANGS COMING FROM THE RT ENG. THE ENGINE SHUTDOWN, AND THE A/C LANDED (UNSCHEDULED) WITHOUT INCIDENT. UPON VISUAL INSPECTION, IT WAS FOUND THERE WAS CONTAINED TURBINE FAILURE, AND BLADES WEFeb 25, 2009 · N10FN · Lear 36LEAR · Turbine SectionSDR BHKA52FN2202009Engine · failedTHE LT ENGINE ROLLED BACK TO SUB-IDLE DURING A SIMULATED ENGINE FAILURE DURING TAKEOFF. THE ENGINE PERFORMED NORMALLY DURING START, TAXI, AND THE INITIAL PORTION OF TAKEOFF. THE LT ENGINE ACCELERATED NORMALLY, AND THE THRUST LEVER POSITION AND ALL INDICATIONS Feb 20, 2009 · N52FN · Lear 35A · Engine (Reciprocating)SDR BKE2009F00000Windshield · crackedDEPARTED AIRPORT, ENROUTE, WHILE CLIMBING THROUGH APPROX FL230, THE LT WINDSHIELD SHATTERED. WE INITIATED AN EMERGENCY DESCENT AND RETURNED TO DEPARTURE. THERE WERE NO INJURIES AND THE LANDING WAS NORMAL. (K)Feb 18, 2009 · N450TJ · Lear 45LEAR · Flight Compartment WindowsSDR J1Q2009F00000Controller · defectiveINSTALLED REPAIRED PRESSURIZATION CONTROLLER PN 13300-020, SN 1574 INTO N720JC, SN 273 ON 01-07-2009. THIS CONTROLLER IS CAUSING THE OUTFLOW VALVE SOLENOID TO CHATTER WITH GROUND POWER APPLIED. THIS UNIT WAS REPAIRED , TRACKING NR 61977 DATED JUNE 15, 2007.Jan 7, 2009 · N720JC · Amd 20F5 · Cabin Pressure ControllerSDR 2008FA0000898Frame · corrodedWHILE INSPECTING THE LT AFT FUEL TANK STRUCTURE, DUE TO LIGHTENING DAMAGE EVENT, FOUND THE FOAM INSULATION WATER SOAKED, AND CAUSING SERIOUS CORROSION IN OUTER FLANGE OF AFT PRESSURE BULKHEAD AND SURROUNDING STRUCTURE. THE HOLE IN THE LT OUTER PRESSURE BULKDec 22, 2008 · N244LJ · Lear 35A · Fuselage Main, FrameSDR 2009FA0000095Axle · wornCONTINUOUS NOSE GEAR VIBRATIONS UPON LANDING. TEARDOWN AND INSP OF NOSE GEAR AXLE BARREL ASSY REVEALED THE NOSE AXLE TO BE WORN BEYOND LIMITATIONS. TWO .005 INCH GROOVES WORN INTO AXLE. ONE ON EACH SIDE WHERE THE AXLE BARREL COVER PLATE SEALS ARE LOCATED. Dec 12, 2008 · N483FG · Braero HS125700A · Nose/Tail Landing Gear Strut/AxleSDR DXTA200811223366Computer · malfunctionedNR 1 COMPUTER LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROX 60KTS. ABORTED TAKEOFF. DOWNLOAD DEEC AND FOUND ECTM DATA BUFFERS FULL. CLEANED ECTM DATA. PERFORMED IDLE RUN AND OPS CHECKS IAW MM.Nov 22, 2008 · N893QS · Raythn HAWKER800XP · Fuel Controlling SystemSDR J1QA20081019002Monopole · defectiveAIRCRAFT DEPARTED KEGE, DURING CLIMBOUT AT APPROXIMATELY 11,000FT MSL THE NR 2 ENGINE STARTED SURGING +/- 10% N1 ROTATION, FOLLOWED BY A NR 2 ENGINE COMPUTER LIGHT. THE CREW FOLLOWED THE AIRCRAFT CHECKLIST AND RESET THE ENGINE COMPUTER. THE ENGINE STABILIZEDNov 9, 2008 · N752JC · Amd FALCON50MYST · Engine Indicating SystemSDR JGV2008F00001Cartridge · failedDURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NNov 4, 2008 · N177JB · Lear 31A · Life JacketSDR CA081201003Connector · misinstalled(CAN) PASSENGER O2 MASK WOULD NOT DEPLOY WHEN TESTED. SYSTEM TROUBLESHOT AND FOUND CONNECTOR P108 WAS NOT INSTALLED CORRECTLY. CONNECTOR REMOVED, INSPECTED AND REINSTALLED .O2 MASK FUNCTION CHECKED SERVICEABLE IAW AMM 35.Oct 9, 2008 · Lear 45LEAR · Oxygen System WiringSDR ESPADJ2088-1Engine · lack of lubeDEPARTED CARTERSVILLE AIRPORT AND PASSING 2000FT MSL THE MASTER CAUTION AND OIL PRESSURE LIGHTS ILLUMINATED. THE CREW NOTED 0 OIL PRESSURE ON THE LEFT ENGINE AND RETURNED TO THE AIRPORT FOR AN UNEVENTFUL LANDING. GROUND CREW NOTED AN EXTENSIVE OIL LEAK AND COct 4, 2008 · N32PA · Lear 36A · Engine (Turbine/Turboprop)SDR J7E2008F00001Cdu · failedINITIALLY THE FMS WOULD NOT PASS THE SELF TEST. SCREEN WAS TELLING THE TECH THAT THE CDU/RAM FAILURE. REMOVED FMS INSTALLED OVERHAULED FMS. THIS WOULD INITIALIZE PROPERLY. FMS DOWNLOADED NAV DATABASE PROPERLY. WHEN PERFORMANCE DATABASE WAS INSTALLED, IT WSep 17, 2008 · N411AJ · Lear 45LEAR · Flight Management Computing Hardware SystemSDR FOM2008F00000Downlock Switch · intermittentON FINAL APPROACH, DURING PART 91 FLIGHT FOR AC OWNER, CREW NOTED THA THE LT MLG WOULD NOT INDICATE REQUIRED "GREEN" DOWN-LOCK INDICATION. ALL OTHER GEAR INDICATED PROPERLY AFTER NORMAL EXTENSION. CREW PROCEEDED WITH EMERGENCY CHECKLIST ITEMS IAW MFG, INCLUDAug 9, 2008 · N395MY · Lear 35A · Landing Gear Position and WarningSDR EYD2008F00000Check Valve · failedWHILE ENROUTE, THE FLIGHT CREW EXECUTED AN EMERGENCY DESCENT DUE TO A "CABIN ALTITUDE" WARNING LIGHT, MAINTENANCE HAS FOUND 2 DEFECTIVE CHECK VALVES, PN 130156-1 AND 2 PRESSURE REGULATORS, PN 1024665, THAT WERE SUSPECT. ARE ALSO REPLACING THE ENTRY DOOR SEAL Jul 27, 2008 · N411PA · Braero HS125700A · Data Recorders (Flight/Maintenance)SDR 2008FA0000502Amplifier · inoperativeAFTER (1) HOUR DISENGAGES AUTOPILOT. PRELIMINARY INSPECTION RESULTS, NO DEFECTS NOTED AFTER BENCH CHECK. (K)Jul 18, 2008 · N818JH · Israel 1124A · Auto Flight System
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