Agusta CP-110
From Wikipedia, the free encyclopedia
| CP-110 | |
|---|---|
| Type | Light cabin monoplane |
| Manufacturer | Agusta |
| Maiden flight | 1951 |
| Number built | 1 |
The Agusta CP-110 was a prototype Italian four-seat light aircraft first flown in 1951. It failed to attract interest from either civil or military operators, although it was evaluated by the Italian Air Force.
[edit] Specifications
General characteristics
- Crew: one pilot
- Capacity: 3 passengers
- Length: 7.3 m (23 ft 11 in)
- Wingspan: 10.6 m (34 ft 9 in)
- Gross weight: 1,100 kg (2,400 lb)
- Powerplant: 1 × Alfa Romeo 110-ter piston engine, 108 kW (145 hp)
Performance
- Maximum speed: 275 km/h (170 mph)
- Range: 1,000 km (620 miles)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 41.
- luftfahrt-archiv.de
[edit] See also
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