Aero Ae 50

The Aero Ae 50 was a prototype propeller-driven military reconnaissance aircraft built in Czechoslovakia. == Design and development == In November 1947, the Czechoslovak Ministry of Defence issued requirements for two light aircraft for service in support of the Czechoslovak Army, a smaller two seat aircraft, to be powered by the 105 hp (78 kW) Walter Minor 4-III engine and a larger aircraft to be powered by the 160 horsepower (120 kW) Walter Minor 6-III engine.

Source: Wikipedia — Aero Ae 50 (CC BY-SA 4.0)

Aero Ae 50

The Aero Ae 50 was a prototype propeller-driven military reconnaissance aircraft built in Czechoslovakia. == Design and development == In November 1947, the Czechoslovak Ministry of Defence issued requirements for two light aircraft for service in support of the Czechoslovak Army, a smaller two seat aircraft, to be powered by the 105 hp (78 kW) Walter Minor 4-III engine and a larger aircraft to be powered by the 160 horsepower (120 kW) Walter Minor 6-III engine.

Source: Wikipedia "Aero Ae 50" · CC BY-SA 4.0

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