Learjet 35A

Service difficulty reports · 726

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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 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 BKAA2014F00078Engine · flamed outLEFT ENGINE EXPERIENCED AND LOUD BANG FOLLOWED BY A VIBRATION AND FLAME OUT. PILOTS SHUTDOWN ENGINE IAW EMERGENCY PROCEDURES, DECLARED AN EMERGENCY AND LANDED AT WITHOUT FURTHER INCIDENT. WHEN ENGINE IS ROTATED BY HAND A GRINDING NOISE IS HEARD AND RESISTANCEMar 14, 2014 · N770JP · Lear 35A · Engine (Turbine/Turboprop)SDR O2JA2014F00092Computer · failedPILOTS REPORTED THAT THE YAW DAMPER, WHEN ENGAGED, THE BALL WAS WAY OUT TO THE LEFT, WHEN DISENGAGED HAD TO RETRIM ACFT, WHEN ENGAGED SECONDARY YAW DAMPER WITH SAME RESULTS, DISENGAGED AGAIN TRIMMED ACFT AND ENGAGED AUTO PILOT WITH THE AUTO PILOT AND NOTICEMar 5, 2014 · N991AL · Lear 35A · Autopilot SystemSDR G1IA20140210001Blower Motor · defectiveCREW NOTICED ELEC BURNING SMELL IN CABIN ON APPROACH INTO ANC. MX FOUND COCKPIT & CABIN BLOWER ASSEMBLY PN 6608267-2 MOTOR INOPERATIVE. ASSEMBLY WAS REPLACED & THE ACFT WAS RETURNED TO SERVICE.Feb 9, 2014 · N60WL · Lear 35A · Air Distribution FanSDR FJTA2014017011Cap · unsecureAIRCRAFT HAD JUST COMPLETED HEAVY MX CHECK IN KSGH. DURING THE REPOSITION FLIGHT TO KMQY AT THE TOP OF THE CLIMB, THE RT ENG OIL PRESS SLOWLY DECREASED. THE OIL PRESS ANNUNCIATOR ILLUMINATED AT WHICH POINT THE CREW SHUT DOWN THE RT ENG. CONTINUED FLIGHT DUEJan 16, 2014 · N701DA · Lear 35A · Engine Oil Distribution (Airframe Furnished)SDR MFGA20140116011Controller · slowN42HN TOOK OFF FROM KCLT THE CAPTAIN NOTICED THE CABIN DID NOT SEEM TO BE PRESSURIZING. HE CHECKED THE SETTINGS & ASKED CONTROL TO COME BACK TO KCLT. ON THE WAY BACK THEY REALIZED THAT IT WAS WORKING & THEY LANDED AT KCLT. PERFORMED THE GND TEST & CHECKS ONJan 15, 2014 · N42HN · Lear 35A · Cabin Pressure ControllerSDR E8BA2014013100001Relay · failedAFTER TAKEOFF, CREW NOTED A LOT OF RT RUDDER INPUT WAS REQUIRED TO TRIM AIRCRAFT TO FLY STRAIGHT. CREW NOTED RUDDER TRIM INDICATOR WAS READING FULL LEFT RUDDER TRIM AND COULD NOT ADJUST BACK TO NEUTRAL. DIVERTED, AND LANDED WITHOUT INCIDENT. AFTER TROUBLESHJan 9, 2014 · N220GS · Lear 35A · Wing Miscellaneous StructureSDR CA140114002Pump · failed(CAN) ENGINE FAILED TO LIGHT OFF DURING START SEQUENCE. TROUBLESHOOTING FOUND ENGINE DRIVE FUEL PUMP TO BE AT FAULT. REPLACEMENT OF FUEL PUMP CORRECTED THE ISSUE.Jan 3, 2014 · Lear 35A · Engine Fuel PumpSDR CA131210001Case · cracked(CAN) DURING VISUAL INSPECTION OF THE ENGINE GEARBOX IT WAS NOTED THAT THE OIL FILTER HOUSING ASSY LOWER MOUNTING STUD EAR WAS CRACKED. REPLACED THE AFT GEARBOX HOUSING CASE.Dec 6, 2013 · Lear 35A · Accessory GearboxesSDR K6LR2014F00040Cabin Pressure · failedDURING A POSITIONING FLIGHT, THERE WAS AN UNCONTROLLED LOSS OF CABIN PRESSURIZATION. THE PILOT MADE AN EMERGENCY DECENT AND DIVERTED FOR MAINTENANCE.Dec 6, 2013 · N58MM · Lear 35A · Cabin Pressure Control SystemSDR BSYR20131127001Unknown · malfunctionedON APPROACH INTO FTY, CREW DID NOT HAVE LT MLG DOWN LOCK INDICATION AFTER GEAR SELECTED DOWN. CREW DIVERTED TO ATL, PROCEEDED TO BLOW THE LG DOWN & LANDED SAFELY AT ATL WITHOUT INCIDENT. MAINTENANCE IS INSPECTING.Nov 27, 2013 · N31WR · Lear 35A · Landing Gear Retraction/Extension SystemSDR CA131121012Control Valve · cracked(CAN) PN 48C48641, SN 1036, PLEASE SEE ATTACHED DOCS AND PICS REGARDING THIS O/H VALVE THAT WAS INSTALLED ON ACFT ON JULY 27, 2012. THE HOUSING ON THIS VALVE IS CRACKED RIGHT THROUGH NOW. THE LAST FLIGHT ON THIS AC WAS IN APRIL, 2013. DURING OUR PREBUY INSP INov 21, 2013 · Lear 35A · Landing Gear Retraction/Extension SystemSDR O9IA20131008544Insulation · misinstalledSMOKE SEEN COMING FROM IN FRONT OF DIVAN SEAT. INVESTIGATION REVEALED POOR INSULATION COVERING THE LT WING/STAB HEAT DUCT PIPE. THIS PIPE WAS REWRAPPED WITH INSULATION MATERIAL. RESULTANT CHECK FLIGHT WAS SATISFACTORY.Oct 8, 2013 · N544LM · Lear 35A · Standard Practices/StructuresSDR O9IA544LM100613Duct · leakingWHEN WING AND STAB HEAT TURNED ON, THERE IS A BURNING ODOR IN CABIN AND COCKPIT. GROUND RUNS/CHECKS WERE UNABLE TO IDENTIFY PROBLEM. CHECK FLIGHT PERFORMED. NO FINDINGS. SECOND IDENTIFIED VERY LIGHT SMOKE FROM LT WING/STAB HEAT PIPE. PIPE HAD BEEN REWRAOct 6, 2013 · N544LM · Lear 35A · Airfoil Anti/De-ice SystemSDR CA130917001Wire · corroded(CAN) ONE TIRE BLOWN ON LANDING, THEN TWO TIRES BLOWN ON SECOND LANDING. FIRST THOUGHT TO BE CAUSE BY SURFACE CONDITION AND CREW, FINAL CONCLUSION: ANTI-SKID SYS DID NOT FUNCTION CORRECTLY, FOUND ANTI-SKID COMPUTER GROUND CORRODED, COMPUTER WAS SERVICEABLE, Sep 17, 2013 · Lear 35A · Landing Gear System WiringSDR ESPA2013062700370Circuit Breaker · trippedAFTER TAKEOFF, CREW DISCOVERED ACFT WOULD NOT PRESSURIZE AND AIR CONDITIONING SYS WOULD ONLY PRODUCE HEAT. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. UPON ARRIVAL, DISCOVERED CIRCUIT BREAKER FOR RT MODULATION VALVE WAS TRIPPED. RESET TRIPPED BREAKER Jun 26, 2013 · N549PA · Lear 35A · Cabin Pressure Control SystemSDR BSYR20130626050Unknown · odorTWENTY MINUTES AFTER DEPARTURE, CREW NOTICED BURNING ODOR IN COCKPIT. FLIGHT RETURNED AND LANDED SAFELY WITHOUT INCIDENT. MX INSPECTED, COULD NOT DUPLICATE DICREPENCY.Jun 25, 2013 · N959SA · Lear 35A · Air Distribution SystemSDR O9IA2013052000001Heat Shield · loosePASSENGERS COMPLAINED OF BURNING PLASTIC ODOR WHICH MADE THEM NAUSEAS. FOUND WING ANTI-ICE DUCT HEAT SHIELD OUT OF POSITION ALLOWING HEAT TO BE TRANSFERRED TO PLASTIC. ADJUSTED AND PERFORMED SYS CHECK WITH NO DISCREPANCIES FOUND. A SUBSEQUENT FLIGHT HAD A May 17, 2013 · N544LM · Lear 35A · Airfoil Anti/De-ice SystemSDR CA130515008Tire · damaged(CAN) DURING DAILY INSPECTION, A PIECE OF THREAD MISSING FROM NR 3 MAIN WHEEL TIRE WAS NOTICED.May 13, 2013 · Lear 35A · TireSDR BSYR2012047Unknown · malfunctionedAPPROXIMATELY 60 MILES OUT FROM SUS, PILOT NOTICED COMPLETE LOSS OF HYDRAULIC PRESSURE. PILOT NOTIFIED ATC OF SITUATION, PILOT COMPLETED EMERGENCY GEAR EXTENSION AND LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE HAS BEEN NOTIFIED AND INSPECTING AIRCRAFT.May 10, 2013 · N27BL · Lear 35A · Hydraulic System, MainSDR V6NA20130426001Tube · leakingENROUTE, HYD SYS INDICATED ZERO SYS PRESSURE. DIVERTED, PERFORMED A MANUAL GEAR EXTENSION IAW CHECKLIST. RAN CHECKLIST FOR, "FAILED HYD LANDING". LANDED WITHOUT INCIDENT. HYD PRESSURE WAS AVAILABLE FROM THE AUX PUMP FOR USE WITH BRAKING. DETERMINED TO BE Apr 26, 2013 · N352HS · Lear 35A · Hydraulic System, MainSDR V6NA20130429001Tube · leakingENROUTE, HYDRAULIC SYSTEM INDICATED ZERO SYSTEM PRESSURE. DIVERTED, PERFORMED A MANUAL GEAR EXTENSION IAW CHECKLIST. RAN CHECKLIST FOR, "FAILED HYD LANDING". LANDED WITHOUT INCIDENT. HYD PRESSURE WAS AVAILABLE FROM THE AUX PUMP FOR USE WITH BRAKING. DETERApr 26, 2013 · N352H · Lear 35A · Hydraulic System, MainSDR FJTA20130422321Engine · making metalDURING FLIGHT FROM K36U TO KBNA, THE FLIGHT CREW WAS IN LEVEL FLIGHT AT 41000, CLEAR AIR NO TURBULENCE. HEARD A LOUD BAG FROM THE LEFT ENGINE ACCOMPANIED BY THE FOLLOWING INDICATIONS. N1 WAS SPOOLING DOWN, N2 WAS ERRATIC NEEDLE MOVING UP AND DOWN, THERE WAS Apr 18, 2013 · N32PE · Lear 35A · Engine (Turbine/Turboprop)SDR KC8A201303250001Casting · crackedDURING ROUTINE INSPECTION, CRACKS WERE FOUND ON THE RIGHT TIP TANK UPPER AND LOWER FORWARD ATTACH CASTING. REPAIRED.Mar 20, 2013 · N72CK · Lear 35A · Wing Main, Frame StructureSDR 2013FA0000144Modulating Valve · malfunctionedPNEUMATIC SHUTOFF MODULATING VALVE FAILURE RESULTING IN DEPRESSURIZATION OF ACFT IN FLIGHT.Feb 25, 2013 · N131AJ · Lear 35A · Pneumatic Distribution SystemSDR ZP7A20130214001Master Switch · faultyFAILURE OF PRIMARY PITCH TRIM. AFTER ROTATION, PF NOTICED INCREASED CONTROL PRESSURES REQUIRED TO MAINTAIN FLIGHT ATTITUDE, DESPITE ACTUATING NOSE DOWN TRIM. PF ASKED PNF TO ATTEMPT TO TRIM AC FROM THE RIGHT YOKE. NO EFFECT. MEMORY ITEMS WERE ACCOMPLISHED Feb 14, 2013 · N38PS · Lear 35A · Stabilizer Control SystemSDR BSYA20130211044Computer · malfunctionedAFTER TAKEOFF FROM FTY, CREW EXPERIENCED FLIGHT COMPUTER MALFUNCTION WHICH AFFECTED THE RVSM CAPABILITIES. CREW RETURNED AND LANDED SAFELY AT FTY WITHOUT INCIDENT. AVIONICS DEPARTMENT IS INSPECTING AIR DATA SYSTEM.Feb 10, 2013 · N88BG · Lear 35A · Air Data ComputerSDR CA130124026Pump · failed(CAN) REPORTED THAT AN ACFT OPERATING AS DA351 ON A IFR FLIGHT DECLARED AN EMERGENCY AT 2330Z DUE LT ENGINE FAILURE APPROXIMATELY 20NM SOUTH INBOUND TO DESTINATION. EMERGENCY CONTINGENCIES WERE PUT INTO EFFECT BY CARS O/C. ACFT LANDED SAFELY WITHOUT INCIDENT AJan 17, 2013 · Lear 35A · Engine Fuel PumpSDR 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 FJTA201212137011Brake · wornDURING LANDING, AFTER LANDING, FAILED TO STOP ON THE RUNWAY. THE ACFT ROLLED OF THE END OF THE RUNWAY, APPROX 30 FT, CREW REPORTED T/R DEPLOYED BUT COULD NOT ADD POWER. CREW ALSO REPORTED THEY HAD DIFFICULTY SLOWING THE ACFT DOWN. MX REPORTED 2 BRAKES WORN Dec 13, 2012 · N701DA · Lear 35A · BrakeSDR 2012FA0000767Wheel Half · damagedTHE WHEEL HALF STEEL KEYWAY RIVET FAILED CAUSING THE KEYWAY TO BEND OUTWARD FROM THE CENTRIFICAL FORCE, AND THEN MADE CONTACT WITH THE TIRE SIDEWALL AND THE UPPER GEAR TORQUE LINK. THERE WAS DAMAGE TO THE TIRE SIDEWALL AND THE TORQUE LINK HAD MINOR SCORING.Nov 19, 2012 · N721EC · Lear 35A · Wheel/Ski/FloatSDR SUZA20121104001Connector · corrodedTHE CREW DISCOVERED THAT THE LEFT BLEED OVERTEMP INDICATOR WAS INDICATING INTERMITTENTLY. THE CREW ISOLATED THE CAUSE AND FOLLOWED THE EMERGENCY CHECKLIST PROCEDURES BY DESCENDING TO FL280 AND TURNING OFF THE LEFT BLEED SYSTEM. THE CREW THEN DIVERTED THE FLINov 4, 2012 · N35NK · Lear 35A · Pneumatic Indicating SystemSDR BSYA2012041Steering Sys · erraticON TAKEOFF ROLL AT PHX, PILOT DISCOVERD NOSE STEERING ERRATIC. PILOT PROCEEDED BACK TO RAMP WITHOUT INCIDENT. PILOT DEFERRED NOSE STEERING SYSTEM AND PROCEEDED WITH SCHEDULED FLIGHT WITHOUT INCIDENT.Oct 26, 2012 · N959SA · Lear 35A · Landing Gear Steering SystemSDR 2012FA0000732Fuse · blown(YV499T) DEPARTED AIRPORT FOR A TEST FLIGHT. AFTER THE FLIGHT WAS ACCOMPLISHED, DURING DESCENT, PILOT'S ESS BUSS CIRCUIT BREAKER TRIPPED RESULTING IN A LOSS OF ALL DC ESSENTIAL POWERED COCKPIT SYSTEMS. ESS BUSS CIRCUT BREAKER WAS RESET AND ALL DC ESSENTIAL POOct 12, 2012 · Lear 35A · DC Power Distribution SystemSDR BSYA2012037Hydraulic Line · leakingEN ROUTE TO BWI FROM RIC, THE LOW HYDRAULIC LIGHT CAME ON. ON FINAL APPROACH TO BWI CREW NOTICED LOSS OF ALL HYDRAULIC PRESSURE. THE CREW PROCEEDED TO LAND SAFELY WITH THE AID OF THE DRAG CHUTE AND AIR BRAKING SYSTEM. MAINTENANCE REPLACED DEFECTIVE RIGHT MASep 12, 2012 · N27BL · Lear 35A · Hydraulic System, MainSDR BSYA2012034Tire · flatAFTER LANDING AT ABQ, CREW DISCOVERED DURING POST FLIGHT INSPECTION THAT THE LEFT OUTBOARD MAIN TIRE WAS FLAT. MAINTENANCE REMOVED AND REPLACED TIRE AND COMPLIED WITH INSPECTION OF BRAKE SYSTEM, NO FURTHER DEFECTS NOTED.Sep 5, 2012 · N400JE · Lear 35A · TireSDR CIEA201209050003Insulation · meltedSMOKE IN CABIN COMING FROM LT BENCH DUCT REAR SEAT. DURING CRUISE FLIGHT AND EVENTUALLY SUBSIDED BEFORE RETURNING TO DEPARTURE AIRPORT. MX INVESTIGATED AND FOUND HOOK AND LOOP ATTACHING THE INSULATION THAT WRAPS AROUND THE WING ANTI-ICE LINE MELTED AGAINST THESep 1, 2012 · N312LG · Lear 35A · Airfoil Anti/De-ice SystemSDR 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 CA120710012Valve · failed(CAN) FLIGHT CREW REPORTED THE FOLLOWING: IN CRUISE AIRCRAFT WINDOW OVERHEAT TRIGGERS MASTER CAUTION. OAT -55, @ 40,000` WINDOW (HEAT WAS SELECTED) JUST CRACKED BUT STILL TRIPS. SYSTEM TROUBLE SHOT AND FOUND THE WINDSHIELD RAM AIR VALVE HAD INTERNALLY FAILED Jul 9, 2012 · Lear 35A · Windshield/Door Rain/Ice RemovalSDR RMV2012F00001Regulator · malfunctionedACFT DEPARTED, EN ROUTE THE FL180 CHECKS WERE COMPLETED, ALL NORMAL. AT FL340, THE CREW NOTICED THE CABIN WAS AT 8,000 FEET AND CLIMBING. TURNED THE CABIN PRESSURE CONTROL TO MANUAL AND TRIED TO DRIVE THE CABIN DOWN, WITH NO SUCCESS. THE CABIN CLIMBED TO 9,Jun 26, 2012 · N456CL · Lear 35A · Pressure Regulator/Outflow ValveSDR BHKR0621 12Warning Light · illuminatedDURING APPROACH, GEAR UP, FLAPS 8 DEGREES, NO TRANSIENT ELECTRICAL LOADS COMMANDED, THE LT GENERATOR AMBER CAUTION LIGHT WAS OBSERVED. ENROUTE TO THE DELTA PATTERN, CONDUCTED GENERATOR FAILURE (SINGLE) CHECKS, BUT THE GENERATOR WOULD NOT RESET. LANDING WASJun 21, 2012 · N51FN · Lear 35A · DC Generator-AlternatorSDR O9IA2012F00126Connector · inoperativeDURING APPROACH, FLIGHT CREW SELECTED GEAR DOWN. GEAR DID NOT EXTEND. SECOND ATTEMPT WAS TRIED WITH SAME RESULTS. LANDING GEAR WAS EXTENDED USING EMERGENCY EXTENSION PROCEDURES. LANDING . INVESTIGATION REVEALED FAULTY CONNECTOR ON LANDING GEAR SELECTOR VJun 13, 2012 · N544LM · Lear 35A · Landing Gear System WiringSDR BKEA2012052901Sensor · false indicationRT BLEED LIGHT CAME ON DURING CLIMBOUT. JETTISONED APPROX 1500 LBS FUEL. DIVERTED TO AND LANDED AT MX. FOUND RT BLEED AIR HIGH TEMP SENSOR, BAD.May 29, 2012 · N387HA · Lear 35A · Overheat DetectionSDR 2012FA0000294Exhaust Duct · crackedLT ENGINE AFTER BODY, LOWER HALF DUCT, 4" CRACK EMMINATING FROM INNER IGNITION PLUG ACCESS PANEL. DOUBLER PATCH INSTALLED IAW SRM 51-00-00.May 10, 2012 · N890LJ · Lear 35A · Engine Collector/Tailpipe/NozzleSDR 2012FA0000325Wire · damagedLEFT ENGINE FIRE WARNING LIGHT ILLUMINATED ON FINAL APPROACH. ALL OTHER INDICATIONS WERE NORMAL. FOUND DAMAGED & FRAYED WIRE IN PYLON FOR AFT BODY FIRE LOOP. CUT BACK WIRE LEAD, CRIMPED NEW CONNECTOR PIN ON LEAD AND REASSEMBLED CONNECTOR. OPS CHECK OF SYS Apr 30, 2012 · N367DA · Lear 35A · Fire Protection System WiringSDR G1IAN20120427001Fuel Control · erraticSUPPLEMENTAL RECORD - THE LEFT FUEL CONTROL UNIT WAS REPLACED WITH A OVERHAULED UNIT. OPS CHECK NORMAL AND FLIGHT CHECK NORMAL.Apr 17, 2012 · N81MR · Lear 35A · Fuel Control/Turbine EnginesSDR BHKA201202270012Engine · overtempAFTER NORMAL START AND TAXI, THE ACFT BEGAN THE TAKEOFF ROLL. IMMEDIATELY AFTER THE "AIRSPEED'S ALIVE" CALL OUT (40 KNOTS) THE LT ITT READ 888 DEGREES C. THE TAKEOFF WAS IMMEDIATELY ABORTED WITH MINIMAL BRAKING (ACFT WEIGHT WAS 16,200). IN CHOCKS WITH BOTH Feb 27, 2012 · N52FN · Lear 35A · Engine (Turbine/Turboprop)SDR FJT12027011O-Ring · damagedDURING FLIGHT, DESCENDING THROUGH 18,000 FT, THE LT ENGINE LOST OIL PRESSURE. CREW SHUTDOWN ENGINE AND DIVERTED. THE ACFT LANDED SAFETLY WITHOUT FURTHER EVENT. ENGINE WAS INSPECTED. THE ENGINE LOST OIL FROM A BAD O-RING ON THE OIL FILLER CAP. THEY RESEALEFeb 15, 2012 · N701DA · Lear 35A · Turbine Engine Oil SystemSDR O2MA20120207001Pump · faultyDURING THE APPROACH THE LT ENGINE FLAMED OUT WHEN THE THROTTLE LEVER WAS RETARDED TOWARDS FLIGHT IDLE. THE PIC DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITH NO INCIDENT. THE LT ENGINE WAS NEVER ATTEMPTED TO BE RESTARTED DURING THE APPROACH. ATTEMPTS WEFeb 7, 2012 · N72AX · Lear 35A · Engine Fuel PumpSDR O2MA20120127001Monopole · shortedSHORTLY AFTER THROTTLING BACK TO FLIGHT IDLE TO DESCEND FROM 41,000 FT THE NR 2 ENGINE MOMENTARILY STAYED AT 80 PERCENT (APPROXIMATELY 15 SECONDS) AND THEN CONTINUED ROLLING DOWN AND FLAMED OUT. PILOT WINDMILL RESTARTED THE ENGINE AT APPROXIMATELY 26,000 FT AJan 27, 2012 · N72AX · Lear 35A · Power LeverSDR G1IAJAN12N35CYSwitch · out of adjustFAR 135.415(C) 1/13/12 ON CLIMBOUT OF FAI THE RIGHT THRUST REVERSER UNLOCK LIGHT CAME ON. THE FLIGHT CREW REDUCED THE AIRCRAFT SPEED AND THE LIGHT WENT OUT. RETURNED TO FAI AND LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND UPPER DOOR POSITION INDICATORJan 13, 2012 · N35CY · Lear 35A · Engine Thrust Reverser
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