CANT 36
(Redirected from CRDA 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
[edit]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, 110 kn)
- Service ceiling: 5,600 m (18,400 ft)
Armament
- 2 × 7.7 mm (.303 in) machine guns
References
[edit]
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
