The first prototype of the Mil Mi-8 (NATO Designation: 'Hip-A') with a single engine. The aircraft is capable of holding 18 passengers in addition to three crew.
VTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 3
Crew seating: Side-by-side
Landing gear: Wheels (non-retractable)
Overall Width: 21.00 m (68.9 ft)