Type 2-seat light bomber and reconnaissanc aircraft
Engine 1 Avia Vr 36
Dimensions Length  11,08 m, height 3,60 m ,  span 14,70 m , wing area  44,3 m2 ,
Weights Empty 2040 kg, loaded  , max. take off weight  3219 kg
Performance Max.. speed  270 km/h, cruising speed  , range 900 km, endurance  , service ceiling  6500 m , climb 4,2 m/sec.
Armament 2 forward-firing 7.92 mm vz. 30 (Česká zbrojovka Strakonice) machine guns 2 7.92 mm vz. 30 (Česká zbrojovka Strakonice) machine guns in a ring mount for the observer
Bombs: 600 kg
Type Werk.Nr Registration History
The Aero A.100 was a biplane light bomber and reconnaissance aircraft built in Czechoslovakia during the 1930s. It was the final step in a design lineage that extended back to the Aero A.11 a decade earlier. A.100s remained in service throughout World War II and for a few years postwar.
Development of the A.100 was in response to a Czechoslovak Air Force requirement of 1932 for a uniform replacement for the A.11s, Aero Ap.32s, and Letov Š.16s then in service. Work began with a revision of the Aero A.430 that quickly became quite a different aircraft. Of standard biplane configuration, the A.100 was a somewhat ungainly-looking aircraft and somewhat obsolescent by the time of its first flight in 1933, a member of the final generation of biplane military aircraft to be designed in Europe.

Nevertheless, since the only other competitor for the air force contract, the Praga E.36 had not flown by the close of tenders, the A.100 was ordered for production. A total of 44 were built, in two batches