Acro Sport I
From Wikipedia, the free encyclopedia
The Acro Sport I is a single-seat aerobatic sportsplane designed by Paul Poberezny in the early 1970s for home-building and manufactured by Acro Sport Inc.
It is a short-span biplane of conventional taildragger configuration, typically built with an open cockpit and spatted main undercarriage. Its structure is fabric-covered steel tube.
[edit] Specifications (Typical Acro Sport I)
[edit] General characteristics
- Crew: one pilot
- Capacity: pilot only
- Length: 17 ft 6 in (5.34 m)
- Wingspan: 19 ft 7 in (5.97 m)
- Height: ft in ( m)
- Wing area: ft² ( m²)
- Empty: lb ( kg)
- Loaded: lb ( kg)
- Maximum takeoff: lb ( kg)
- Powerplant: various, typically in the 100-200 hp range (75-150 kW)
[edit] Performance
- Maximum speed: 130 mph (208 km/h)
- Range: miles ( km)
- Service ceiling: ft ( m)
- Rate of climb: ft/min ( m/min)
- Wing loading:
- Power/Mass:
[edit] Related content
Related development: Acro Sport II
Comparable aircraft:
Designation sequence: Acro Sport I - Acro Sport II
Lists relating to