Breda Ba.65 - Design and Development

Design and Development

An evolution of Ba.64, the Ba.65 was designed by Antonio Parano and Giuseppe Panzeri. The Ba.65 was a single-seat, all-metal, low-wing cantilever monoplane with aft-retracting main undercarriage. Like its predecessor, it was intended to undertake aeroplano di combattimento multiple roles as a fighter, attack and reconnaissance aircraft. The Ba.65 carried wing-mounted armament of two 12.7 mm (0.5 in) and two 7.7 mm (0.303 in) Breda-SAFAT machine guns, with internal stowage for a 200 kg (440 lb) bombload in addition to external ordnance that could total 1,000 kg (2,200 lb). The prototype, which was first flown in September 1935, like the initial production aircraft, used the 522 kW (700 hp) Gnôme-Rhône K-14 radial engine produced under license by Isotta-Fraschini. Starting from the 82nd aircraft, the more powerful Fiat A.80 RC.41 18-cylinder, twin-row radial with a takeoff rating of 746 kW (1,000 hp) engine was adopted. Production ceased in July 1939 after 218 aircraft were built by Breda and Caproni.

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