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https://it.wikipedia.org/wiki/CANSA_C.6_Falchetto#:~:text=Il CANSA C.,anni quaranta del XX secolo.
On November 24, 1940, the Directorate General for Aeronautical Construction (DGCA) issued a requirement relating to a biplane, single-seat, fixed-gear training aircraft, equipped with full aerobatic characteristics, even in inverted flight, and which could also have a version two-seater. The single-seat aircraft had to have the following characteristics: maximum speed of 250 km/h, stall speed of 80 km/h, climb to 3 000 m in 10', range of 500 km, and landing on an 8 m obstacle in 300- 350 m. Furthermore, the two-seater version had to have a range of 200-300 km to allow navigation training. On January 23, 1941, the DGCA communicated to the Projects Committee that five proposals for acrobatic aircraft had arrived from as many companies, all equipped with an Isotta-Fraschini Beta engine. These were the Caproni-Predappio Ca.605 (single-seater) and Ca.606 (two-seater), Breda Ba.205, Saiman 207B and CANSA C.6 Falchetto.
Designed by the engineer Giacomo Mosso, the mockup of the C.6 Falchetto was presented to the DGCA on 11 December 1940. It was an aircraft derived from the previous C.5, equipped with modern construction techniques such as the transfer of the horizontal tail planes, and the interchangeability between wings and upper and lower ailerons, built entirely with national timber . On 23 January 1941 the DGCA gave a favorable opinion on the C.6, attributing a safety coefficient of 12, and observing that the wings of equal span gave safety during inverted flight. An increase of 2 m2 in the wing surface was requested, which reduced the wing load to 50 kg/m2 for the single-seater version and 55 kg/m2 for the two-seater version, an increase in the surfaces of the ailerons, a lowering of the height of the fuselage to in order to improve the visibility of the pilot, with a consequent increase in the length of the fuselage. Furthermore, a single fuel tank placed in a barycentral position was adopted, and a small supplementary tank placed in the central plane of the upper wing, increased the distance of the tail planes from the airframe to improve its aerodynamic efficiency, some tweaks to the design, and for reasons of economy a tail skid was adopted instead of the wheel. The flight characteristics developed by the Superior Direction for Studies and Experiences were better than those expected by the company, and in this situation CANSA was invited to design the two-seater version.
During the 58th meeting of the Projects Committee it was agreed to equip the Regia Aeronautica with an advanced aerobatic training aircraft.On March 24, 1941, General Francesco Pricolo authorized the construction of two prototypes each of the Breda 205, CANSA C.6, and SAIMAN 207.
Technical description:
Biplane, single-engine, two-seat trainer aircraft.[1] The wings were of equal span, both fitted with ailerons, and both wings and ailerons were interchangeable. The fuselage was entirely made of wood and covered with canvas.[4] The tail was of the classic single stem type, with unbraced horizontal planes.[4] The landing gear was of the classic tricycle type, with the main wheels covered by a hood, and integrated at the rear by a tail skid.[4]
Two-seater, equipped with two open cockpits in tandem, the front one for the pilot and the rear one for the student, equipped with a windscreen.[4]
Propulsion was entrusted to an in-line Isotta-Fraschini Beta RC.10 6-cylinder air-cooled engine, delivering a power of 280 HP and driving a two-blade wooden propeller.[1] The weight of the engine was equal to 285 kg. [2]
Operational use
The prototype of the C.6B (Biposto), serial number MM.464, flew for the first time in Cameri, in the province of Novara, on 30 June 1941, in the hands of test pilot Fausto Moroni.Problems immediately emerged with the Isotta Fraschini Beta R.C.10 engine, which proved difficult to set up.In August, the test driver Moroni attempted to transfer the first prototype to the Experimental Center of Guidonia. During the flight there was an engine failure above the Cisa pass, in an area where bad weather was raging. Unable to make an emergency landing, the pilot jumped with a parachute, abandoning the plane. However, Moroni had flown many hours on the C.6, reporting a good impression of it, and considering it successful for the task to which it had been assigned.The second prototype (MM.475) was transferred to Guidonia on 6 May 1942, but was lost during a subsequent test flight carried out by marshal pilot Bertolini, seconded to t he Technical Surveillance Office of Cameri, with a lieutenant engineer of the G.A.r.i. Due to an engine failure, the aircraft, which was making an approach to the runway, ended up against trees on the edge of the airport, suffering irreparable damage. None of those on board were injured.