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.