TW2-117A / AG TURBINE engine

Description & utilization:

TW2-117A / AG – turboshaft engine with maximum power of  1 103,3 kW which powers Mi-8 helicopter.

0
MRO's performed

Scope of services:

  • overhaul,
  • unscheduled overhaul and repairs,
  • engine: control, oil, fuel and electric accessories overhaul and repairs,
  • warranty and post-warranty service,
  • on-wing repairs.

The Mi-8 (NATO reporting name: Hip) – is a medium twin-turbine helicopter, originally designed in the Soviet Union by Michaił Mil design bureau, and now produced in Russia. Serves as a transport helicopter, the Mi-8 is also used as an airborne command post, armed gunship, and reconnaissance platform.