CANT 36

CANT 36

Role	Military trainer aircraft
Manufacturer	CANT
Designer	Raffaele Conflenti
First flight	1932
Number built	1

The CANT 36 was a trainer developed in Italy in the 1930s. It was a conventional design with fixed tailskid undercarriage and accommodation for the pilot and instructor in tandem, open cockpits. Intended for advanced training, it was equipped with a powerful 187 kW (250 hp) engine. The single prototype was evaluated by the Regia Aeronautica, but when no purchase order was forthcoming, no further examples were built.

Specifications

General characteristics

Crew: 2, pilot and instructor
Length: 8.50 m (27 ft 11 in)
Wingspan: 10.50 m (34 ft 5 in)
Empty weight: 950 kg (2,094 lb)
Powerplant: 1 × Isotta-Fraschini Asso 200, 187 kW (250 hp)

Performance

Maximum speed: 210 km/h (130 mph)
Service ceiling: 5,600 m (18,400 ft)

Armament

2 × 7.7 mm (.303 in) machine guns

References

Wikimedia Commons has media related to CANT 36.

Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 269.
aerei-italiani.net

CANT and CRDA aircraft

CANT	2 6 7 10 11 12 13 18 21 22 23 25 26 35 36 37 38

CRDA	Z.501 Z.504 Z.505 Z.506 Z.508 Z.509 Z.511 Z.514 Z.515 Z.516 Z.1007 Z.1010 Z.1011 Z.1012 Z.1015 Z.1018

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CANT 36

Specifications

See also

References