Technical characteristics
Output AC electric power, kVА - 60
Air consumption, kg/s - 09÷1.27*
Air pressure, kg/cm2 - 4.52
Start and operation altitude, m - 11500
The TA18-100 is a base APU with power up to 250 kW. This New Generation APU is used on narrow-body aircraft with a seating capacity of up to 150 persons, and heavy helicopters.
It provides:
an air turbine start for the main engines
on-board AC electric power
air conditioning for cockpit and cabin
This APU has specific operating parameters at the best competitive level in the world. The engine is equipped with FADEC.
Type certificate No CT 211-ВД
APU modifications are used on An-178 and SSJ-100 aircraft. Planned to use this APU for a number of newly developed aircraft and helicopters as well as on the “in-service” models.