CAP Aviation CAP-232
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The CAP Aviation CAP-232 is a high-performance carbon-fiberwinged, wooden fuselaged 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: 350 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: Piel Emeraude, Super Emeraude - Mudry Cap-10 - Mudry Cap-10B - Mudry Cap-20 - Mudry Cap-20L - Mudry Cap-21 - Mudry Cap-230 - CAP-231 - Mudry Cap-231EX - CAP-232 - Cap Aviation Cap-222(Giles G-202)
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