N10AH

Cancelled 2019

Deregistered aircraft · 1990 Gates Learjet 35A · Garrett TFE731 series

Cancelled
October 17, 2019
Exported to
Australia
Status when cancelled
Valid registration
Serial number
657
Year built
1990
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 2, 1990
Certificate issued
August 26, 2019
Last registry action
August 26, 2019
Mode S code
A00263
Owner when cancelled
Gateway Air Center Inc
Location
Merced, CA
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 10

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR G1IA2019031100000Light · inoperativeFAR 135.415 REPORT. PILOT REPORTS "AFTER T/O COPILOT REACHED FOR GEAR HANDLE AND AFTER RETRACTION HE NOTICED THAT PRIOR TO GEAR RETRACTION, THE NOSE GEAR DOWN & LOCK LIGHT WASN'T ON.RETRACTION WAS NORMAL BUT BECAUSE THE LACK OF NOSE GEAR D&L INDIC., WE DECIDEDMar 7, 2019 · N10AH · Lear 35A · Landing Gear Position and WarningSDR G1IA2018012110AHRegister · obstructedCABIN CREW REPORTED LIGHT WHITE SMOKE IN THE CABIN, 10 MINUTES BEFORE LANDING. SMOKE APPEARED TO BE MOMENTANEOUS AND NOT APPARENT TO THE FLIGHT CREW. THE SMOKE CAME FROM BETWEEN MEDICAL BEDS AND SIDEWALL. REMOVED THE RT SIDEWALL AS REQUIRED AND INSPECTED FOJan 21, 2018 · N10AH · Lear 35A · Heating SystemSDR G1IA2017022210AH1Control Switch · stickingPILOT REPORTED AFTER DEPARTURE, PRIMARY PITCH TRIM CONTINUED TO RUN AFTER COPILOT RELEASED THE SWITCH. EXECUTED PITCH TRIM MALFUNCTION EMERGENCY CHECKLIST AND RETURNED TO DEPARTURE AND LANDED. MAINTENANCE WAS ABLE TO DUPLICATE THE PITCH TRIM PROBLEM. REPLACEFeb 22, 2017 · N10AH · Lear 35A · Stabilizer Control SystemSDR G1IA20160225001Warning System · false activationFLYING WITH A PATIENT, TWO PILOTS & TWO MEDICS. WE WERE AWARE OF ADVISORIES FOR SEVERE TURBULENCE AT HIGHER ALTITUDES SO WE WERE AT FL260, 280 - 290KNOTS, AT ABOUT 94% POWER & NO ABNORMALITIES IN THE GAUGES & NO TURBULENCE. HAD THE MAIN GEAR DOOR LIGHTS ONFeb 23, 2016 · N10AH · Lear 35A · Landing Gear Position and WarningSDR G1IA20151015001Unknown · odorFAR 135.415 REPORT, DURING ROUTINE CHECK FLIGHT, WHILE TESTING STAB HEAT, AN ENVIRONMENTAL BURNING SMELL WAS NOTICED AS SOON AS THE STAB HEAT WAS TURNED ON. SMELL INCREASED SO STAB WAS TURNED OFF & THE SMELL DISAPPEARED. FLIGHT RETURNED BACK TO BASE WITHOUT Oct 12, 2015 · N10AH · Lear 35LEAR · 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 2002FA0001181Computer · malfunctionedNOSE WHEEL STEERING WILL NOT ARM. FOUND NO OUTPUT VOLTAGE ON P224 PIN A. 1.0 VAC REQUIRED FROM THIS PIN.Oct 13, 2002 · N10AH · Lear 35A · Shimmy DamperSDR 2002FA0000264Solenoid · intermittentSPOILER OPERATION INTERMITTENT. MAINIFOLD ASSEMBLY HAS TWO SOLENOIDS, APPEARS THAT ONE MAY BE STICKING OR HAVE AN ELECTRICAL PROBLEM.Mar 13, 2001 · N10AH · Lear 35A · Drag Control SystemSDR 2000ZZZX373Rod End · wornDURING A 1,200 HOUR T/R INSPECTION, FOUND WORN ACTUATOR ROD END BUSHING BRACKET. THE BRACKETS ARE ACTUALLY PART OF THE THRUST REVERSER DOOR. THEY ARE CAST INTO THE DOOR.Jan 20, 2000 · N10AH · Lear 35A · Engine Thrust ReverserSDR 99ZZZX1727Bracket · crackedBRACKET CRACKED AT OPPOSITE END OF WHERE ACTUATOR MOUNTS. LEFT FLAP ACTUATOR BRACKET FOUND CRACKED AT INSPECTION. THE ENTIRE BRACKET IS COMPOSED OF 5 PIECES. THE TOP BRACKET IS CRACKED.Apr 9, 1999 · N10AH · Lear 35A · Trailing Edge Flap Actuator