Capella Javelin | |
---|---|
Role | Ultralight aircraft |
National origin | United States |
Manufacturer | Capella Aircraft Corporation |
Introduction | 1999 |
Status | Production completed |
The Capella Javelin is a family of American open cockpit, high wing, tractor configuration, conventional landing gear-equipped ultralight aircraft that were produced in kit form by Capella Aircraft of Austin, Texas and intended for amateur construction.[1][2][3]
The single seat Javelin I was designed to comply with the American FAR 103 ultralight regulations, including that category's maximum 254 lb (115 kg) empty weight.[1][2][3]
Capella Aircraft went out of business in late 2007, and the type is no longer in production.