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.
Parent type: Mil Mi-8/Mi-14/Mi-17
Aircraft status: No longer flying
VTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Tail rotor
Crew required: 3 in Side-by-side arrangement
Landing gear: Wheels (non-retractable)