Avia B-534

Length
8.1 m
Flat Wing Span
9.4 m
Height
3.15 m
Flat Wing Area
23.56 m²
Cruise Speed
345 km/h
Max Speed
405 km/h
Max Ceiling
10600 m
Number of Engines
1
First Flight
1933-05-25
Entry Into service
1935-01-01
Number Built
568
Maximum Take-Off Weight
1.98 t (paragliders: kg)
Maximum Range
600 km

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Maximum Range (km)
Avia B-534 1.98 600

Similar airplanes

All data (23 fields)
Name
Avia B-534
Manufacturer
Avia Motors
Description
The Avia B-534 is a Czechoslovak biplane fighter developed and manufactured by aviation company Avia.
First Flight
1933-05-25
Entry Into service
1935-01-01
Designer
František Novotný
Type
Fighter aircraft
Length (m)
8.1
Height (m)
3.15
Max Speed (km/h)
405
Cruise Speed (km/h)
345
Max Ceiling (m)
10600
Rate of Climb (m/s)
15.15
Armament
4× 7.92 mm (0.312 in) Letecky kulomet vz. 30 (Česká zbrojovka Strakonice) machine guns with 250–300 rpg; 6× 10 kg (22 lb) or 4x 20 kg (44 lb) bombs
National Origin
Czechoslovakia
Number Built
568
Powerplant Description
1 × Hispano-Suiza 12Ydrs liquid-cooled V12 engine, 633 kW (849 hp) each
Primary Users
Czechoslovak Air Force
Status
Retired
Wikipedia Article (URL)
en.wikipedia.org/wiki/Avia_B-534
Flat Wing Span (m)
9.4
Flat Wing Area (m²)
23.56
Number of Engines
1