N241JA

Cancelled 2013

Deregistered aircraft · 1966 Learjet 24 · GE CJ610-SER series

Cancelled
August 15, 2013
Status when cancelled
Sale reported, canceled
Serial number
131
Year built
1966
Type
Fixed wing multi engine
Engine
Turbo-jet
Airworthiness
Standard, transport
Airworthiness date
September 29, 1967
Last registry action
July 10, 2007
Mode S code
A2347F
Owner when cancelled
Sale Reported
Location
Denver, CO
Owner type
Individual

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 · 6

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

SDR 20010411CW006Control Cable · bindingLT THROTTLE BINDING WHEN ADVANCED FOR TAKEOFF POWER. FOUND BINDING OF LEFT AFT ENGINE THROTTLE CONTROL DUE TO POSSIBLE EXCESSIVE ROUTING OF CONTROL TO CONFORM TO NACELLE SIZE. REROUTED CONTROL TO INCREASE RADIUS OF BEND INSIDE NACELLE AND CONTROL OPERATED NORMar 21, 2001 · N241JA · Lear 24 · Power LeverSDR 20010327CW014Check Valve · failedCABIN COULD NOT MAINTAIN PRESSURIZATION AT FL350, MAINTENANCE PERFORMED A GROUND PRESSURIZATION FUNCTIONAL CHECK NORMALLY. A PNEUMATIC CHECK VALVE DISCOVERED WITH BROKEN SPRING WAS REPLACED, HOWEVER, INITIAL FLIGHT TEST WAS NOT SUCCESSFUL. MAINTENANCE TROUBLFeb 1, 2001 · N241JA · Lear 24 · Cabin Pressure Control SystemSDR 20010213CW009Control Unit · malfunctionedAC COULD NOT MAINTAIN PRESSURIZATION AND INCREASE IN CABIN ALTITUDE RESULTED IN OXYGEN MASK DROP AND AURAL WARNINGS, AS APPROPRIATE. AC DESCENDED TO FL220 AND CREW WAS ABLE TO MANUALLY RESTORE CABIN ALTITUDE TO NORMAL. AC CONTINUED FLT TO HOME BASE, NORMALLYJan 10, 2001 · N241JA · Lear 24 · Cabin Pressure Control SystemSDR 20010213CW008Indicator · inoperativeLEFT ENGINE OIL PRESSURE GAGE NOTED TO HAVE DROPPED AND STUCK AT 12 PSI, OIL PRESSURE ON TAXI FOR TAKEOFF. AC WAS RETURNED TO MAINTENANCE AND A SERVICEABLE OIL PRESSURE INDICATOR WAS INSTALLED. OIL PRESSURE INDICATED NORMAL ON RUNUP/FUNCTIONAL CHECK.Jan 5, 2001 · N241JA · Lear 24 · Engine Oil PressureSDR 20001027SH002Tire · failedAIRCRAFT HAD 2 FLAT TIRES AFTER LANDING. ANTI-SKID SYSTEM WAS NON-OPERATIONAL (DEFERRED STATUS) AND POSSIBLE POOR RUNWAY BRAKING CAUSE OF TIRE FAILURE. TIRE AND WHEEL ASSYS (4 EACH) WERE REPLACED. AIRCRAFT RETURNED TO BASE MAINTENANCE AND MADE NORMAL LANDINMar 8, 2000 · N241JA · Lear 24 · TireSDR 99ZZZX5Stringer · crackedDISCOVERED SEVERAL SMALL CRACKS INSIDE HORIZONTAL STABILIZER LOCATED AT LEFT AND RIGHT BL 19.40. CRACKS WERE NOTED DURING SCHEDULED INSPECTION OF THE AREA. A REPAIR WAS PERFORMED BY AN FAA CERTIFIED REPAIR STATION, FOLLOWING N.D.T. CONFIRMATION OF THE CRACKSJun 22, 1998 · N241JA · Lear 24 · Horizontal Stabilizer Structure

Other aircraft with N241JA · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N241JA is registered now to the first aircraft listed.