The T250A features a single main rotor and tail rotor, a two-seats-in
side-by-side configuration enclosed cockpit with a windshield,
skid landing gear and a
PBS TS 100 turboshaft engine made by PBS Velká Bíteš. The aircraft
fuselage is made from composites. Its two-bladed rotor has a diameter of . The aircraft has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for the crew, passenger and baggage is . The aircraft was built to
ISO 9001 and
EN 9100 standards. ==Specifications (T250A) ==