The Ba 75 was an experimental prototype produced in 1939 for both the reconnaissance and ground attack roles. Bearing a family resemblance to the Ba 65, the Ba 75 was a shoulder-wing monoplane with a stalky, fixed and liberally strutted undercarriage, powered by the 900-hp (670kW) Isotta-Fraschini K.14 radial.
The bottom and lower sides of the fuselage were glazed to allow observation of the ground.
One prototype was built, intended to use structural components of the Ba.65. The only Ba.75 was built and test flown in 1939.
Engine: 900-h.p. Isotta-Fraschini K.14
Wing span: 15.60m
Length: 11.20 m
Height: 3.00 m
Wing area: 36.15 m²
Empty Weight: 2600 kg
Takeoff Weight: 4600 kg
Maximum speed: 375 km/h
Cruising speed: 300 km/h
Range: 1700 km
Ceiling: 7000 m
Crew: 2-3
All Aero 