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LEARJET Learjet 40

From SKYbrary Wiki

LJ40
Aircraft
Name Learjet 40
Manufacturer LEARJET
Body Narrow
Wing Fixed Wing
Position Low wing (winglets)
Tail T-tail
WTC Medium
APC C
Type code L2J
Engine Jet
Engine count Multi
Position Both sides of rear fuselage
Landing gear Tricycle retractable
Mass group 3


Manufacturered as:

LEARJET 40


LEARJET Learjet 40

LEARJET Learjet 40 LEARJET Learjet 40 3D

Description

The Learjet 40 is derived from the Learjet 45, but with a shorter fuselage (60 cm), and is powered by two Honeywell TFE731-20AR engines.

The Learjet 40XR is an upgraded version introduced in October, 2004, offering higher takeoff weights, faster cruise speeds and faster time-to-climb rates as compared to the LJ40. The increases are due to the upgrading of the engines to the TFE731-20BR configuration. The LJ40 is a member of the Bombardier Learjet Family.

Technical Data

Wing span 14.56 m47.769 ft
Length 16.93 m55.545 ft
Height 4.31 m14.14 ft
Powerplant 2 x Honeywell TFE731-20AR or TFE731-20-20BR in the Learjet 40XR turbofan engines, 3500 lbs (15.56 kN) each.
Engine model Honeywell TFE731

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 457 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 1542 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH 0.81 ROD ft/min ROD ft/min MCS kts Distance 1306 m
MTOW 92309,230 kg
9.23 tonnes
kg
Ceiling FL510 ROD ft/min APC C
WTC M Range 18571,857 nm
3,439,164 m
3,439.164 km
11,283,346.465 ft
NM

Accidents & Serious Incidents involving LJ40

None on SKYbrary