Avtek 400A

· Avtek
Length
11.99 m
Flat Wing Span
10.67 m
Height
3.47 m
Flat Wing Area
13.4 m²
Max Seating
9
Cruise Speed
550.0435 km/h
Max Speed
472.2596 km/h
Max Ceiling
12950 m
Number of Engines
1
First Flight
1984-09-17
Number Built
1
Maximum Take-Off Weight
2.948 t (paragliders: kg)
Maximum Range
1922 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Avtek 400A 2.948 1922

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All data (23 fields)
Name
Avtek 400A
Manufacturer
Avtek
Description
The Avtek 400A is an American prototype turboprop-powered business aircraft, which was developed in the early 1980s.
First Flight
1984-09-17
Designer
Al Mooney
Type
Business aircraft
Length (m)
11.99
Height (m)
3.47
Cockpit Crew
1
Max Seating
9
Max Speed (km/h)
472.2596
Cruise Speed (km/h)
550.0435
Min Speed (km/h)
153.7159
Max Ceiling (m)
12950
Rate of Climb (m/s)
23.52
Capacity Description
5-9 passengers
National Origin
Canada
Number Built
1
Powerplant Description
1 × Pratt & Whitney Canada PT6A-3L turboprop, 507 kW (680 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Avtek_400A
Flat Wing Span (m)
10.67
Flat Wing Area (m²)
13.4
Number of Engines
1