The CAP Aviation CAP-232 is a high-performance carbon-fiber monoplane aircraft designed for competition aerobatics. The design has won the World Championships in 1998 and 2000, as well as a number of other national-level competitions. With a roll rate of 420° per second and a climb rate of nearly 3,300 feet per minute, the CAP-232 is well suited for the aerobatic circuit.
Specifications (CAP-232)
General Characteristics
- Crew: one pilot
- Capacity: pilot only
- Length: 6.76 m (22 ft 2 in)
- Wingspan: 7.39 (24 ft 3 in)
- Height: m (ft in)
- Wing area: 10.1 m² (109 ft²)
- Empty: 586 kg (1,290 lb)
- Loaded: lb ( kg)
- Maximum takeoff: 823 kg (1,810 lb)
- Powerplant: Lycoming AEIO-540 , 224 kW (300 hp)
Performance
- Maximum speed: 158 km/h (252 mph)
- Range: 1,170 km (731 miles)
- Service ceiling: ft ( m)
- Rate of climb: 1,000 m/min (3,290 ft/min)
- Wing loading:
- Power/Mass:
Related content
Related development:
Comparable aircraft:
Zivko Edge 540 -
Sukhoi Su-26 -
Extra 300
Designation sequence:
CAP-222 -
CAP-231 -
CAP-232
Last updated: 10-15-2005 21:53:24