1997 Bombardier LearJet 31A
 
1997 Lear 31A-136




Aircraft Specification Sheet

Performance Specifications:

GENERAL:
Crew Capacity: 2
Passengers: 8



RANGE:
Maximum:   1,447 NM,   1,665 SM,   2,680 Km
(IFR Reserves, ISA, with 4 Passengers/2 Crew)

SPEED:
High Speed Cruise:    533 mph
Typical Cruise:           525 mph
Long Range Cruise:   483 mph

CEILING:
Maximum Operating Altitude:  51,000 ft

PAYLOAD:
Max 601 lbs. Per Person (including baggage)

Aircraft Specifications:

1997 Learjet 31A
Registration No. N47TR
LR-31A S/N: 31A-136

Airframe:


Engines:



Exterior:


Interior:


Avionics:











Additional:
4,842 Total Hours on Airframe
4,199 Total Landings

Left Engine 4,708 TT
Right Engine 4,672 TT
(Engines are enrolled on the Honeywell MSP Gold Program)

Interior is a double club configuration with an aft 2-place divan and a belted foward lavatory seat.

King EFIS-50 5 tube
Dual Collins VHF22C COMs
Honeywell DF-431B ADF
Chelton DMH21-1 DME
Honeywell TR5014 Radar Altimeter
King RDR-2000 Weather Radar
Dual King KCP 420 Auto Pilot
Dual King MST-76A Mode "S" Transponders
Honeywell KDC0481T TCAS II Processor(7)
Additional Avionics Information Available in the Aircraft Specification Sheet

For additional information or to schedule a showing please contact Raynor Combs jrcombs@spitfireaviation.com