Type Two seat sportplane
Engine 1 Hirth HM 504 with 2-bladed prop. dia. 2,0 m. fuel consumption 13,8 l/ 100 km, oil consumption 0,12 l/ 100 km
Dimensions Length 7,4 m , height 2,24 m ,  span 9,95 m , chord at wingroot 1,3 m, wing area 12,4  m2  , fuselage width 1.02 m, wheel span 1,62 m Wheel size 420 x 150 mm, aileron 1,0 m2, stabilizer 1,68 m2, elevator 0,7 m2, fin 0,94 m2, rudder 0,65 m2, V-form 2 ° 10 min.,  angle 3 ° 50 min.
Weights Empty , loaded  , max. take off weight  
Performance Max.. speed 190 km/h , cruising speed  , range , endurance  , service ceiling   , climb
Werk.Nr Registration History
D-EQPA First flight on May 21, 1939. Destroyed in the fire on 21.5 1939
The Bücker Bü 134 was a side-by-side twoseat light cabin monoplane in a similar category to the Taylor Cub and intended for club and school use, the sole prototype of which (D-EQPA) was flown in 1936. Powered by a 105 hp Hirth HM 504 inverted four-cylinder inline aircooled engine, the Bü 134 was of mixed construction with a chrome-molybdenum steel tube fuselage and wooden wings and tail surfaces.
The Bücker Bü 134 was a strut-braced high-wing aircraft designed for use in civil aviation and as a sports and tourist aircraft. In The cockpit had two seats placed side by side for the pilot and passenger. Airplane was powered by a four-cylinder 100/105 hp air engine Hirth HM 504.
The frame of the fuselage of the aircraft was welded from chromium-molybdenum steel pipes. External The sheathing was linen. Removable motor frame to which the engine was attached, it was also made of chromium-molybdenum steel pipes.
The main landing gear was made separate and equipped with steel coil springs and oil shock absorbers. Wheels of the main landing gear were equipped with a braking system and had dimensions of 420×150 mm. Tail strut The landing gear was also sprung with an oil-fired steel coil spring Cushion. If necessary, the tail strut wheel could be connected to rudder and it can, like rudders, be deflected relative to the axis (or turn the wheel 360°).
The vertical and horizontal tails were cantilever bearing. Rudder was made in the form of a single solid section. The elevators were made in the form of two separate sections with adjustable trimmers.
The aircraft was made according to the high-wing scheme. The wing was made with a two-spar with wooden struts. The center section of the wing was glazed. The wing consoles were folding.
The power plant consisted of a four-cylinder 100/105 hp engine air-cooled Hirth HM 504, which rotated a two-bladed propeller of a fixed step with a diameter of about 2 meters.