Avia B-158

Length
12 m
Flat Wing Span
16 m
Height
5.2 m
Flat Wing Area
43 m²
Cruise Speed
365 km/h
Max Speed
435 km/h
Max Ceiling
8500 m
Number of Engines
2
First Flight
1938-01-01
Number Built
1
Maximum Take-Off Weight
7.26 t (paragliders: kg)
Maximum Range
1100 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Avia B-158 7.26 1100

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All data (19 fields)
Name
Avia B-158
Manufacturer
Avia Motors
Description
The Avia B.158 was a prototype Czechoslovak twin-engined light bomber aircraft of the 1930s.
First Flight
1938-01-01
Designer
Avia Motors
Length (m)
12
Height (m)
5.2
Max Speed (km/h)
435
Cruise Speed (km/h)
365
Max Ceiling (m)
8500
Rate of Climb (m/s)
7
Armament
3×7.92 mm vz.30 (Česká zbrojovka Strakonice) machine guns in nose, dorsal and ventral positions; 1,000 kg (2,200 lb)
National Origin
Czechoslovakia
Number Built
1
Powerplant Description
2 × Avia (Hispano-Suiza) 12Ydrs liquid-cooled V12 engine, 634 kW (850 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Avia_B-158
Flat Wing Span (m)
16
Flat Wing Area (m²)
43
Number of Engines
2