Aviatik Alliance Aleks-251

Length
10.54 m
Flat Wing Span
13.2 m
Height
3.66 m
Flat Wing Area
19.8 m²
Max Seating
6
Cruise Speed
200 km/h
Max Speed
240 km/h
Number of Engines
2
First Flight
2010-09-10
Maximum Take-Off Weight
2.5 t (paragliders: kg)
Total Fuel Capacity
700
Maximum Range
740 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Aviatik Alliance Aleks-251 2.5 700 740

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All data (22 fields)
Name
Aviatik Alliance Aleks-251
Manufacturer
Aviatik Alliance
Description
The Aviatik Alliance Aleks-251 is a twin engine, parasol wing amphibious aircraft designed and built in Russia in the early 2010s.
ICAO Code
A251
First Flight
2010-09-10
Designer
Aleksey Tantsyrev
Length (m)
10.54
Height (m)
3.66
Cockpit Crew
1
Max Seating
6
Max Speed (km/h)
240
Cruise Speed (km/h)
200
Min Speed (km/h)
95
Rate of Climb (m/s)
4
Capacity Description
up to 6 passengers
National Origin
Russia
Powerplant Description
2 × LOM M332S four cylinder piston, 127 kW (170 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Aviatik_Alliance_Aleks-251
Flat Wing Span (m)
13.2
Flat Wing Area (m²)
19.8
Wake Category
L
Number of Engines
2