A development of the earlier
Ba.27 fighter (1932), the Ba.64 was designed in 1933 to requirements set out by the
Regia Aeronautica for an aircraft able to undertake multiple roles: fighter,
bomber and
reconnaissance. The aircraft featured an all-metal, low-wing
cantilever monoplane with a wire braced tail unit and fixed tail wheel. The open
cockpit was placed well forward on the
fuselage in line with the wing roots to provide an excellent field of vision down as well as forward. The headrest behind the cockpit was extended as a streamlined fairing all the way down the fuselage upper decking to the tail. Two
prototypes powered by a 522 kW (700 hp) Bristol Pegasus were developed, the first (MM 249) was a two-seater with fixed landing gear. The second (MM 250) was a single-seater fitted with a semi-retractable main landing gear that when in its rearward retracted position, provided less drag as well as protection in case of a wheels-up landing. The first prototype flew in 1934 but flight tests revealed a lacklustre performance. Nonetheless, a limited production order was placed as two-seater with the semi-retractable landing gear. The production variant was powered by a 485 kW (650 hp)
Alfa Romeo 125. Production of the 42 Ba.64s was complete by 1936. ==Operational history==