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Bücker Bü 134

1st Flight 1936

The Bücker Bü 134, a prototype of a German single-engine, high-wing cabin monoplane, was developed in 1936 by the Bücker Flugzeugbau company as their inaugural monoplane design.

Designed for light general aviation with side-by-side seating, it featured foldable wings for easy storage.

However, flight tests were unsuccessful, leading to the decision not to proceed with series production.

The sole prototype, registered as D-EQPA, was lost in a hangar fire on May 21, 1939.

Specifications

Crew

2

Length

6.02 m (19 ft 9 in)

Wingspan

6.6 m (21 ft 8 in)

Height

2.2 m (7 ft 3 in)

Wing area

12 m2 (130 sq ft)

Powerplant

2 × Hirth HM 504 4-cyl

Air-cooled inverted inline piston engine,

78 kW (105 hp) each

Performance

Maximum speed

190 km/h (120 mph, 100 kn).

Sources

Profile Publications No. 222: Bucker Bu 131 Jungmann.

CASA 1.131 Jungmann / Bücker Bü 131 Aircraft Instruction Manual.

Flugzeug Profile 027-Bucker Bu-131.

Luftwaffe Fledglings, 1935-1945, Luftwaffe Training Units & Their Aircraft-Barry Ketley & Mark Rolfe.

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