*****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