*****AIRCRAFT “LET - L410”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

*****Aircraft Features*****

Aircraft Features

Wing position: High wing

Engine position: (Front) Wing leading mounted

Tail configuration: Regular tail, high set

Landing gear: Tricycle retractable

Wing Span: 20.0 m

Length: 14.4 m

Height: 5.8 m

Power plant: 410: 2 x 750 SHP Motorlet Walter M 601E turboprops with five blade propellers.

420: 2 x 775 SHP Motorlet Walter M 601F turboprops with five blade propellers.

Accommodation: Flightcrew of two and 19 passengers in commuter, 15 in executive configuration.

Notes: Twin turboprop commuter airliner. In service since 1998 (L-420 since 1998). Czech successful commuter aircraft development. Built in a few versions. L-420 improved version with more powerful engines and higher weight. Also used by military as light tactical and utility transport aircraft. AYRES is owner of LET since 1998. L-420: MTOW 6600 Kg.
Alternative names:
L-410/420 Turbolet, LET L-410/420 Turbolet, Turbolet.

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 6.400 kg

VMO - Maximum Operating Speed 200 KIAS

MMO - Maximum Operating Speed Mach   nd 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:               L

Distance:         900 mt

V2 (IAS):         85 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:                 115 kt

ROC:               1000 ft/min

-(to FL150)

IAS:                 160 kt

ROC:               500 ft/min

-(to FL240)

IAS:                 nd kt

ROC:               nd ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS:                200 kt

MACh:             no data

Ceiling:            FL210

Range:            600 NM

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 200 kt

ROD:               800 ft/min

 

*****Approach*****

IAS:                 200 kt

MCS:               nd kt

ROD:               800 ft/min

 

*****Landing*****

Vht (IAS):        85 kt

APC:                A

Distance:         800 mt