[1] The Bagalini was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).
The aircraft features a strut-braced parasol wing, a single-seat open cockpit without a windshield, fixed tricycle landing gear and a single engine in pusher configuration.
[1] The Bagalini's fuselage is made from wood and metal, while the wings are a wooden frame covered in doped aircraft fabric.
[1] The manufacturer estimates the construction time from the supplied plans as 700 hours.
[1] Data from AeroCrafter and The Incomplete Guide to Airfoil Usage[1][2]General characteristics Performance