The Delta Pegass is a Czech two-seat ultralight cabin monoplane designed and built by Delta System-Air.
Design.
The Pegass is a strut-braced high-wing monoplane powered by either an Rotax 912UL or a Rotax 582UL engine driving a three-bladed tractor propeller. It has a fixed tricycle landing gear and a cabin with two seats side-by-side, a door on each side of the fuselage for access.
Specifications (Rotax 912UL).
"Data from" General characteristics* Crew: 1* Capacity: 1* Length: ()* Wingspan: ()* Height: ()* Wing area: ()* Empty weight: ()* Gross weight: ()* Powerplant: 1 × Rotax 912UL
Performance* Maximum speed: (, ) * Stall speed: (, ) * Endurance: 4 hours 0 minutes
References.
Notes.
 ;templatestyles src="Reflist/styles.css" / ;
Bibliography.
 ;templatestyles src="Refbegin/styles.css" / ;