*****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