The ELA 10 Eclipse has a single main rotor, a two-seats-in
tandem enclosed cockpit with a
bubble canopy,
tricycle landing gear with
wheel pants, plus a tail
caster and a four-cylinder, liquid and air-cooled,
four stroke Rotax 912 ULS or
turbocharged Rotax 914 engine in
pusher configuration. The aircraft
fuselage is made from composites. Its two-bladed rotor has a diameter of and a chord of . The aircraft has a typical empty weight of and a gross weight of with the Rotax 914 engine ( with the Rotax 912 ULS engine), giving a useful load of . With full fuel of the payload for the pilot, passengers and baggage is . ==Specifications (ELA 10 Eclipse)==