*****AIRCRAFT
“LearJet - 40”*****
REFERENCE INFORMATION (by Aircraft performance
database)
*****Aircraft
Features*****
Wing position: Low wing
(winglets)
Engine position: Both sides of rear fuselage
Tail configuration: T-tail
Landing gear: Tricycle retractable
Wing Span: 14.56 m
Length: 16.93 m
Height: 4.31 m
Power plant: 2 × Honeywell
TFE731-20AR, or -20BR in the Lear 40XR, turbofan engines, 3500 lbs (15.56 kN) each.
Accommodation: 2 pilots and 7 passengers.
Notes: The Learjet 40 is 60cm shorter than the Learjet 45. The
aircraft first flew on
31st August
2002. It entered service in January 2004.
*****Total
Flight Simulator aircraft weight with full fuel*****
000,000 lbs - 9.545 kg
VMO - Maximum Operating Speed 450 KIAS
MMO - Maximum Operating Speed Mach 0.79 Mach
Turbulent Air Penetration Speed 000 KIAS/.00 Mach
VLO - Maximum Gear Operating Speed 000 KIAS
VLE - Maximum Landing Gear Extension Speed 000 KIAS/.00 Mach
*****Maximum
Flap Placard Speeds*****
Flaps degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: M
Distance: 1306
mt
V2 (IAS): 110
kts
*****Climbing*****
-(to 5000 ft)
IAS: 160
kt
ROC: 2900
ft/min
-(to FL150)
IAS: 280
kt
ROC: 2400
ft/min
-(to FL240)
IAS: 280
kt
ROC: 1800
ft/min
-(mach)
mach: 0.78
ROC: 2000
ft/min
*****Cruise*****
TAS: 450
kt
MACh: 0.79 data
Ceiling: FL510
Range: 1692 NM
*****Descent
*****
mach: 0.79
ROD: 1500
ft/min
- (to FL240)
mach: 280
ROD: 2300
ft/min
- (to FL100)
IAS: 290
kt
ROD: 2300
ft/min
*****Approach*****
IAS: 250
kt
MCS: 180
kt
ROD: 1800
ft/min
*****Landing*****
Vht
(IAS): 115 kt
APC: B
Distance: 1354
mt