Learjet 35A

Service difficulty reports · 726

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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 aircraft_model_key = '35A'
  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 O9IAAML0779Starter Gen · crackedDURING ROUTINE ENGINE INSPECTION FOUND STARTER GENERATOR FLANGE CRACKED. REPLACED GENERATOR WITH OVERHAULED UNIT. NO OTHER DISCREPANCIES NOTED.Oct 30, 2009 · N144LG · Lear 35A · Starter-GeneratorSDR CA091006001Nut · cracked(CAN) CREW NOTICED HYD FLUID ON THE SIDE OF FUSELAGE WILL REMOVING CARGO FROM AFT CARGO POD. INVESTIGATION OF THE ACFT FOUND A CRACKED BACK UP NUT ON THE LT MAIN GEAR ACTUATOR RETRACTION FITTING. BACK UP NUT REPLACED, SYS FLUID REPLENISHED AND GEAR SWINGS COMOct 2, 2009 · Lear 35A · Landing Gear ActuatorSDR RMV2009F00001Door · unsecureAFTER TAKEOFF, THE FLIGHT CREW NOTICED AIRFRAME VIBRATION. ACFT LANDED AT THE CLOSEST AIRPORT WITHOUT INCIDENT. A VISUAL INSPECTION OF THE RT COWLING SHOWED THAT THE FWD OTBD 2 LATCHES WERE UNLATCHED AND THE AFT OTBD LATCH WAS SECURED. THE UPPER AND LOWER CSep 30, 2009 · N70AX · Lear 35A · Nacelle/Pylon, Main FrameSDR 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 CA090918002Selector Valve · faulted(CAN) DURING APPROACH ALL 3 GEAR WOULD NOT EXTEND. PILOTS PERFORMED ABNORMAL CHECKLIST, THEN PERFORMED THE EMERGENCY GEAR EXTENSION, WHICH WORKED PROPERLY AND INDICATED ALL 3 GEAR WERE DOWN. THE CONTROL TOWER WAS INFORMED AND EMERGENCY VEHICLES DISPATCHED AS ASep 9, 2009 · Lear 35A · Landing Gear Retraction/Extension SystemSDR BSYA2009048Valve · bypassingON APPROACH INTO ORL COULD NOT GET NOSE GEAR DOWN AND LOCK LIGHT. DID A GO-AROUND, RECYCLED GEAR THEN GOT ALL THREE DOWN AND LOCK LIGHTS. ON LANDING ALL BRAKES WERE WEAK. MAINTENANCE FOUND NR 4 POWER BRAKE VALVE BY-PASSING. REMOVED AND REPLACED VALVE OPS, Sep 9, 2009 · N122JW · Lear 35A · Landing Gear Brake SystemSDR BSYA2009046Seal · wornAFTER TAKEOFF OUT OF LCK THE LEFT BLEED AIR CAME ON AND A FEW MINUTES LATER THE RIGHT BLEED AIR LIGHT CAME ON, PILOT THEN ELECTED TO RETURN TO LCK. MAINTENANCE REPLACED BOTH PYLON AIR DUCT SEALS AND THE LEFT BLEED AIR TEMP. SWITCH NOW OPS CHECKS GOOD.Sep 2, 2009 · N684HA · Lear 35A · Pneumatic Distribution SystemSDR BSYA2009045Volt Regulator · faultyEN ROUTE FROM TEB TO CPS LEFT GENERATOR KEPT FALLING OFF LINE, PILOT THEN DIVERTED INTO LCK. REMOVED AND REPLACED LEFT VOLTAGE REGULATOR, OPS CHECKS GOOD.Aug 26, 2009 · N27TT · Lear 35A · DC RegulatorSDR 2009F00078Blower Motor · burned outWHEN ARRIVING AT 27000 FT, NOTICED A SLIGHT ODOR COMING FROM THE CABIN. TURNED OFF THE CABIN BLOWER AND COCKPIT BLOWER TO TRY AND ISOLATE FROM WHERE THE SMELL WAS COMING FROM. AFTER ABOUT 5 MINUTES THE ODOR WAS GONE AND DECIDED TO TURN ON THE CABIN FAN. ABOAug 25, 2009 · N50FN · Lear 35A · Air Distribution FanSDR KC8AN72CKFuel Control · uncontrollableRIGHT ENGINE ITT INDICATION INCREASED DURING CRUISE, STRAIGHT AND LEVEL FLIGHT, WITH NO CHANGE IN THE N1, N2 OR FUEL FLOW. PILOT SELECTED MANUAL MODE POSITION ON THE FUEL COMPUTER AND THE ITT DECREASED TO NORMAL. THE PILOT ELECTED TO TURN THE FUEL COMPUTER BAug 20, 2009 · N72CK · Lear 35A · Fuel Control/Turbine EnginesSDR 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 A8JA0003Squat Switch · defectiveUPON DEPARTURE ENROUTE, CREW RETRACTED GEAR. GREEN MAIN LIGHTS REMAINED ILLUMINATED AND RED MAIN LIGHTS ILLUMINATED. GEAR DID NOT RETRACT. CREW SELECTED DOWN POSITION AND RETURNED TO DEPARTURE. CREW LANDED ACFT WITHOUT INCIDENT.Jul 12, 2009 · N990L · Lear 35A · Landing Gear Position and WarningSDR A8JA0002Jam-Nut · crackedON SHORT FINAL, CREW EXTENDED GEAR AND NOTICED GEAR UNSAFE LIGHT. THEY ALSO NOTICED LOW HYDRAULIC PRESSURE. ACFT WAS CONFIGURED FOR LANDING AND HAD 20 DEGREE FLAPS. CREW ACTIVATED AUX HYD PUMP AND GEAR WENT DOWN AND LOCKED. CREW WAS ABLE TO TAXI AND USE WHMay 27, 2009 · N990L · Lear 35A · Main Landing GearSDR G1IA2009382O-Ring · missing5/10/2009 AT APPROXIMATELY 1:00 AM, ACFT WAS CLIMBING OUT OF BFI. THE FLIGHT CREW EXPERIENCE A LT ENGINE LOW OIL LIGHT. THEY COMPLIED WITH A PRECAUTIONARY LT ENGINE SHUTDOWN AND RETURNED TO BFI WITHOUT FURTHER PROBLEMS. MX WAS CONTACTED TO CORRECT THE PROBLEM May 4, 2009 · N60WL · Lear 35A · Turbine Engine Oil SystemSDR BKER 20090420 1Generator · failedDEPARTED, RT GEN AMBER ANNUNCIATOR LIGHT ILLUMINATED IN-FLIGHT, 0 AMPS ON RT SIDE. COMPLIED WITH CHECKLIST AND RESET PROCEDURES FOR SINGLE GEN FAIL. NO RESET WAS POSSIBLE. RETURNED TO DEPARTURE FOR MX.Apr 20, 2009 · N535JM · Lear 35A · AC Generator-AlternatorSDR BSYA2009025Pressure System · malfunctionedAFTER TAKEOFF OUT OF DPA CREW HAD TROUBLE WITH MAINTAINING CABIN PRESSURE, DIVERTED TO LCK. MAINTENANCE CHECKED BOTH ENGINE MODULATING VALVES AND CABIN LEAK RATE ALL WHERE NORMAL, RETURNED AIRCRAFT TO SERVICE.Apr 14, 2009 · N959SA · Lear 35A · Cabin Pressure Control SystemSDR G1IA2009622Pump · inoperativeDEPARTING BFI EXPERIENCE A UNCONTROLLED SHUT DOWN ON THE RIGHT ENGINE. THIS HAPPENED ON CLIMBOUT AT APPROXIMATELY 2000 FEET. THE FLIGHT CREW WITH MEDICS (NO PATIENT) RETURNED TO BFI WITHOUT FURTHER INCIDENT. GALVIN FLYING SERVICE WAS CONTACTED TO TROUBLESHOMar 3, 2009 · N81MR · Lear 35A · Engine Fuel PumpSDR 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 BSYA2009005Switch · out of adjustAFTER TAKEOFF OUT OF LCK PILOT SELECTED GEAR UP, AFTER GEAR CAME UP ALL THREE GEAR UNSAFE LIGHTS STAYED ON. PILOT RETURNED TO LCK. MAINTENANCE FOUND THE LEFT THROTTLE SWITCH OUT OF ADJUSTMENT, ADJUSTED SWITCH OPS CHECKS GOOD.Jan 21, 2009 · N684HA · Lear 35A · Landing Gear Position and WarningSDR 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 ESPADJ2008-2Wire · brokenON LIFT OFF, CREW NOTED FUMES AND SMOKE IN ACFT, AND THE ACFT PRESSURIZATION SYS WAS IN EMERGENCY. POWER WAS REDUCED AND ENGINE BLEED AIR SWITCHES WERE CYCLED, BUT LT ENGINE REMAINED IN EMERGENCY. CAPTAIN DECLARED AN EMERGENCY TO GET PRIORITY LANDING AND RETURNov 17, 2008 · N568PA · Lear 35A · Engine Bleed Air System WiringSDR 2008FA0000669Attach Bracket · crackedDURING 600 HOUR INSPECTION FOUND TWO SHEARED ALUMINUM RIVETS, ALONG WITH A 0NE INCH CRACK IN LT FLAP ACTUATOR ATTACHMENT BRACKET, P/N 2325079-11. INSTALLED NEW BRACKET ASSEMBLY, P/N 2325079-17. THIS BRACKET HAS TWO STEEL RIVETS IN PLACE OF THE ORIGINAL ALUM Oct 2, 2008 · N308BW · Lear 35A · Trailing Edge Flap ActuatorSDR CA080930007Spacer · cracked(CAN) UPON REMOVAL OF LT GEAR ACTUATOR DUE TO HYDR BYPASS, CONICAL SPACER, P/N 2441007-1, ITEM NR 32 IN IPC 32-32-20, WAS FOUND CRACKED. RT ACTUATOR REMOVED, SPACER VISUALLY INSPECTED. NO CRACK INDICATIONS. BOTH ACTUATOR PILLARS REMOVED, CLEANED AND MAGNETIC PSep 30, 2008 · Lear 35A · Main Landing GearSDR BSY2008F00009O-Ring · cutAIRCRAFT ENROUTE, WHEN PILOT NOTICED A DROP IN OIL PRESSURE LT ENGINE. SHUTDOWN ENGINE LANDED, NO PROBLEMS. MAINT FOUND OIL DIP STICK, O-RING CUT, REMOVED AND REPLACED O-RING. (K)Sep 25, 2008 · N25AN · Lear 35A · Reciprocating Engine Oil 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 ESP2008F00000Circuit Breaker · loose(30) MINUTES AFTER THE ACTIVATION OF WINDSHIELD HEAT, THE RT ESSENTIAL BUS CIRCUIT BREAKER POPPED. CREW COMPLETED EMERGENCY CHECKLIST FOR AN ELECTRICAL FAILURE. THE CIRCUIT BREAKER WOULD NOT RESET. ATC GAVE VECTORS AND DESCENT. CREW DID A VISUAL APPROACH. Jul 5, 2008 · N568PA · Lear 35A · Electrical Power System WiringSDR EHA2008F00000Pressure Valve · stuckEMERGENCY PRESSURIZATION ACTIVATED. T/S FOUND LT EMERGENCY PRESSURE VALVE STUCK IN EMERGENCY. SUSPECT BURNED SOLENOID. (K)Jun 24, 2008 · N405PC · Lear 35A · Pressure Regulator/Outflow ValveSDR 2008F00017Valve · malfunctionedAT FL400 ENROUTE, RAT ABOUT -38 C AND NOT IN ICING CONDITIONS. DURING DESCENT, NOTED ABNORMALLY HIGH N1 AND ITT INDICATIONS FOR DESCENDING FLT AT IDLE. FOUND COULD ADD POWER, BUT NOT REDUCE IT. ACTIVATED NAC HEAT ON BOTH ENGINES IN AN ATTEMPT TO RESTORE NORMALJun 12, 2008 · N35AX · Lear 35A · Pneumatic Distribution SystemSDR BSYA2008011Light · shortedAFTER TAKEOFF OUT OF PHX CREW NOTICED CABIN DOOR LIGHT ON, CREW TRIED TAPPING WARNING LIGHT CAPSULE, NOTICED SOME SMOKE COMING FROM THE DOOR LIGHT CAPSULE. RETURNED TO PHX WITH NO PROBLEMS. MAINTENANCE FOUND DOOR WARNING LIGHT CAPSULE SHORTED. DISCONNECTED May 27, 2008 · N15WH · Lear 35A · Door Warning SystemSDR VQ82008F00000Tube · corrodedDURING TAXI FOR DEPARTURE, PILOT NOTICED REDUCED BRAKING ABILITY OF THE AC. UPON RETURNING TO THE TERMINAL IT WAS NOTICED THAT A LARGE AMOUNT OF HYDR FLUID WAS COMING FROM LT WHEEL WELL FURTHER INVESTIGATION BY MFG REVEALED A RUPTURE IN A SPOILER RETRACT LINEMay 22, 2008 · N135WE · Lear 35A · Drag Control SystemSDR 20082Servo · unknownAT APPROXIMATELY 18,000 FT, VMC, PIC NOTED AUTOPILOT HAD DIFFICULTY BANKING AND TURNING LEFT. AUTO PILOT WAS DISENGAGED AND YAW DAMPERS SWITCHED WITH NEG RESULTS FOR LEFT TURN. PIC ESTIMATES 35 LBS OF FORCE WAS USED TO OVERCOME RESISTANCE WHILE TURNING LEFT.Apr 28, 2008 · N39HJ · Lear 35A · Autopilot Main ServoSDR CDN2008F00000Hinge · crackedCREW NOTICED A LANDING GEAR DOOR UNSAFE INDICATION IN FLIGHT. THE GEAR WAS LOWERED WITH GEAR DOWN AND LOCKED INDICATIONS NORMAL. INSPECTION REVEALED THAT THE OB RT GEAR DOOR HINGE WAS CRACKED WHICH CAUSED THE DOOR TO NOT FULLY CLOSE. THE CONDITION WAS AGRIVMar 4, 2008 · N78MC · Lear 35A · Landing Gear DoorsSDR BSYA2008006Landing Gear · lack of lubeAFTER TAKEOFF OUT OF LCK THE RIGHT MAIN INBOARD GEAR DOOR STAYED UNSAFE (LIGHT ON) ,PILOT RETURNED TO LCK. BROUGHT AIRCRAFT INTO WARM HANGAR, THAWED ICE OUT OF WHEEL WELLS, CLEANED AND LUBED GEAR AND OPS CHECKS GOOD.Mar 4, 2008 · N25AN · Lear 35A · Landing Gear Retraction/Extension SystemSDR G1I2008F00000Defog System · burnedAFTER DEPARTING, THE FLIGHT CREW EXPERIENCED SMOKE IN THE CABIN. THE FLIGHT CREW TURNED BACK TO DEPARTURE. MAINTENANCE WAS CONTRACTED TO FIND THE PROBLEM AND DISCOVERED THE COPILOT AUX WINDSHIELD DEFOGGER OVERHEATED. MX INSPECTED THE WIRING, SWITCH, AND REMOVEFeb 7, 2008 · N60WL · Lear 35A · Windshield/Door Rain/Ice RemovalSDR 2008FA0000214Defog System · burnedRIGHT AFTER TAKEOFF, AUX DE-FOG UNIT ON CO-PILOT SIDE BURNED AND SMOKE FROM BLOWER FAILURE. NO WIRE PROBLEMS OR CIRCUIT BREAKER ISSUES FOUND. UNIT FAILURE CAUSED SMOKE IN COCKPIT, CREW DECLARED EMERGENCY AND RETURNED TO AIRPORT WITHOUT FURTHER INCIDENT.Feb 7, 2008 · N60WL · Lear 35A · Windshield/Door Rain/Ice RemovalSDR 2008FA0000053Pressure Sensor · malfunctionedLOSS OF CABIN PRESSURE AT 25K FT. PRESSURE SENSOR MALFUNCTIONEDJan 17, 2008 · N55FN · Lear 35A · Cabin Pressure SensorSDR JBG2008F00000Fitting · looseHYDRAULIC PRESSURE LOSS DUE TO LEAKS NOTED AT LT MLG DOOR IB UNLATCH ACTUATOR SHUTTLE VALVE FITTINGS, AND THE RT IB MAIN GEAR DOOR ACTUATOR FITTINGS DUE TO INSUFFICIENT TORQUE AND BAD SEALS. A LOOSE FITTING WAS ALSO NOTED ON THE RT MLG ACTUATOR RETRACT LINE. Dec 29, 2007 · N357LJ · Lear 35A · Landing Gear Door Retract SectionSDR 12262007Circuit Breaker · defectiveLOSS OF ESSENTIAL BUSS POWER. CAPTAINS ESSENTIAL BUSS CIRCUIT BREAKER POPPED. CO-PILOTS ESSENTIAL BUSS CIRCUIT BREAKER POPPED WHILE SUPPLYING THE CAPTAINS ESSENTIAL BUSS THROUGH THE BUSS TIE. THE AIRCRAFT LOST COMM, AND NAV. FOUND THE CAPTAINS ESSENTIAL BUSS Dec 26, 2007 · N73CK · Lear 35A · Electrical Power System WiringSDR 073371Controller · malfunctionedAT FL 295 WHILE CLIMBING TO FL 390, CREW OBSERVED 2500 FT/MIN CABIN CLIMB. INITIATED EMERGENCY DESCENT PER AFM. FINAL MAINTENANCE FINDING, REPLACED DIFFERENTIAL PRESSURE CONTROLLER. FLIGHT TEST OK.Dec 3, 2007 · N123DA · Lear 35A · Cabin Pressure ControllerSDR VUC2007F00001Fire Warning · false activationUPON TAKEOFF, AC CLEARED TO FL410 AND THEN REQUESTED, AND WAS APPROVED FOR FL430. DURING CLIMB TO FL430, RT ENGINE FIRE WARNING LIGHT ILLUMINATED. FLIGHT CREW SLIGHTLY RETARDED THE POWER BACK ON THE RT ENGINE (WHICH WAS AT MAX CONTINUOUS ITT INDICATION) REQUNov 26, 2007 · N35TJ · Lear 35A · Fire DetectionSDR VUC2007F00000Fire Warning · false activationDURING CLIMB, RT ENGINE FIRE WARNING LIGHT ILLUMINATED. FLT CREW RETARDED POWER PACK ON RT ENGINE (WHICH WAS AT MAX CONTINUOUS ITT INDICATION), REQUESTED CLEARANCE TO FL 390 AND DECLARED AN EMERGENCY. UPON PULLING POWER BACK THE FIRE WARNING LIGHT EXTINGUISHNov 26, 2007 · N35TJ · Lear 35A · Fire DetectionSDR VQ82007F00000Fire Warning · false indicationAT 200 FT ON NOV 13, 2007, AC DEPARTED, DURING FLIGHT, A FIRE WARNING INDICATION LIGHT FROM THE NR 2 ENGINE CAME ON. THE AC RETURNED TO DEPARTURE AND IS CURRENTLY IN MAINTENANCE. MAINTENANCE PERSONNEL INFORMS THAT THERE IS NO INDICATION THAT A FIRE OCCURRED Nov 13, 2007 · N136WE · Lear 35A · Fire DetectionSDR ZED2007F00001Fire Warning · intermittentFALSE ENGINE FIRE LIGHT. THIS IS AN INTERMITTENT DISCREPANCY; WE HAVE ALREADY SENT A SDR EARLIER THIS MONTH. COULD NOT DUPLICATE. CHECKED FIRE LOOPS, WIRING, CHECKED FOR BLEED AIR LEAKS, GROUND RAN, AND SWAPPED ENGINE FIRE DETECT CONTROL. (SUSPECT ENGINE EOct 29, 2007 · N394PA · Lear 35A · Fire DetectionSDR CA071030005Connector · transposed(CAN) DURING A 300HR INSPECTION THE STALL WARNING ACCELEROMETER CHECK WAS DUE ( IAW AD 82-01-05). WHEN CHECK WAS CARRIED OUT, THE STALL WARNING SYSTEM FAILED. WHEN SYSTEM WAS TROUBLESHOT, IT WAS DISCOVERED THAT CONNECTORS BNC 3 AND BNC 4 (FORM PIN D AND PIN F Oct 16, 2007 · Lear 35A · Stall Warning SystemSDR ZED2007F00000Fire Warning · false activationSTILL TROUBLESHOOTING, DISCREPANCY WRITTEN UP BY PILOT, RT ENGINE FIRE LIGHT ILLUMINATED DURING FLIGHT. TEMPS/PRESSURES NORMAL. LIGHT EXTINGUISHED AFTER REDUCING POWER 10 PERCENT. CHECKED ENGINE PARAMETERS, ALL NORMAL, DIMMED COCKPIT LIGHTING AND LOOKED AT Oct 11, 2007 · N394PA · Lear 35A · Fire DetectionSDR DELA200720008Indication Sys · false indicationLOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICATED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKE OF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 1Oct 5, 2007 · N773DL · Lear 35A · Fuel Indicating SystemSDR DELA200700008Warning Light · false indicationLOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICATED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKE OF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 1Oct 5, 2007 · N773DL · Lear 35A · Fuel Indicating SystemSDR DELA200720009Indication Sys · intermittentLOW FUEL LIGHT ILLUMINATED WITH 4000 LBS TOTAL FUEL ON AIRPLANE AND 1200 LBS FUEL IN THE WINGS. FUEL READER GAUGE INDICATED 400 LBS OF FUEL ON RT WING. LATER ON WENT BACK TO INDICATE 1200 LBS ON THE WINGS. TAKEOFF (SIC) WITH 4000 LBS TOTAL LANDING WEIGHT WAS 1Oct 5, 2007 · N773DL · Lear 35A · Fuel Indicating SystemSDR 2007FA0000916Structure · damagedDURING THE PILOT PREFLIGHT, THE PILOT HAD NOTICED THAT THERE WAS A TEAR IN THE SHEET METAL OF THE LT ENGINE THRUST REVERSER INNER SKIN. WE COULD NOT IDENTIFY WHAT HAS CAUSED THIS TEAR. THE UNIT WILL BE REPAIRED BY THE MFG AND WILL INFORM YOU WITH ANY INFO THSep 28, 2007 · N10UF · Lear 35A · Engine Thrust ReverserSDR DELA200720007Connector · dirtyNOSE GEAR UNSAFE LIGHT ILLUMINATED ON APPROACH. FLY BY TOWER INDICATED GEAR WAS DOWN. LANDED UNEVENTFULLY. TROUBLESHOT WIRING TO NLG DOWNLOCK SWITCH, FOUND CONTACTS AT CONNECTOR PLUG NEEDED CLEANING. CLEANED AND REATTACHED. CONDUCTED GEAR SWING, OPS CHECKSep 27, 2007 · N431AS · Lear 35A · Landing Gear System Wiring
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