Beneš-Mráz Be-56 Beta-Major

· Beneš-Mráz · 1 × Walter Major

Airplanes

Length

7.55 m

Flat Wing Span

10.66 m

Height

2.02 m

Flat Wing Area

14 m²

Cruise Speed

205 km/h

Max Speed

240 km/h

Max Ceiling

6000 m

Number of Engines

Aircraft Engine

First Flight

1936-07-20

Number Built

Maximum Take-Off Weight

0.71 t (paragliders: kg)

Total Fuel Capacity

100

Maximum Range

600 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Beneš-Mráz Be-56 Beta-Major	0.71	100	600

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Auster Atom	Continental O-170	7.62	10.9728		Compare
Aquila A 211		7.4	10.3		Compare
Aero Boero AB-95	Continental O-200	6.9	10.42	2	Compare
Anderson Kingfisher	Lycoming O-235	7.0104	10.9728	1	Compare
Aquila A 210	Rotax 912	7.3	10.3		Compare
Aero Boero AB-115		7.273	10.72	2	Compare

All data (18 fields)

Name: Beneš-Mráz Be-56 Beta-Major
Manufacturer: Beneš-Mráz
Description: The Beneš-Mráz Be-56 Beta-Major was a single-seat aerobatic advanced trainer manufactured in Czechoslovakia shortly before World War II.
First Flight: 1936-07-20
Designer: Pavel Beneš
Length (m): 7.55
Height (m): 2.02
Cockpit Crew: 1
Max Speed (km/h): 240
Cruise Speed (km/h): 205
Max Ceiling (m): 6000
Number Built: 1
Powerplant Description: 1 × Walter Major 4-cyl. inverted air-cooled in-line piston engine, 97 kW (130 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Bene%C5%A1-Mr%C3%A1z_Be-56_Beta-Major
Flat Wing Span (m): 10.66
Flat Wing Area (m²): 14
Aircraft Engine: Walter Major
Number of Engines: 1