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Advanced Aviation Cobra

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Cobra
Type	Homebuilt ultralight aircraft
Manufacturer	Advanced Aviation
Maiden flight	1980s
Primary user	Individual civilians

The Advanced Aviation Cobra was a U.S. ultralight aircraft of extremely minimalist design marketed for homebuilding. The pilot is seated in an open framework suspended beneath a fabric-covered wing on which the engine (adapted from a snowmobile) and pusher propeller are also mounted. Early Cobras (Model A) had spoliers for roll control, while the Model B had traditional full three-axis control using ailerons. A two-seat training version, known as the King Cobra was also available.

1 Specifications (Model B)
- 1.1 General characteristics
- 1.2 Performance
2 Related content
- 2.1 Related lists

[edit] Specifications (Model B)

This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.

[edit] General characteristics

Crew: 1
Length: ft in (m)
Wingspan: 35 ft 0 in (10.7 m)
Height: ft in (m)
Wing area: 162 ft² (15 m²)
Empty weight: 218 lb (99 kg)
Max takeoff weight: 468 lb (212 kg)
Powerplant: 1× 430 Cuyuna, 52 hp (39 kW)

[edit] Performance

Maximum speed: 75 mph (65 knots, 120 km/h)
Range: mi (nm, km)
Service ceiling: ft (m)
Rate of climb: ft/min (m/s)

[edit] Related content

[edit] Related lists

List of ultralight aircraft

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