Aviation auxiliary gas turbine engine APU TA-6A

• Equivalent air power - 235 kW.
• The selected AC power is 40 kVA.
• Launch altitude - 3000 m.
• Fuel consumption - 225 kg/h.
• Weight - 245 kg.
• Overall dimensions - 1585 × 620 × 735 mm.

Engine TA-6A for the auxiliary power unit (APU) is a single-shaft gas turbine engine.

The engine is installed in a special unsealed compartment on board the aircraft and is intended for:

- starting aircraft main engines using air launchers at airfields located at altitudes up to 3000 m above sea level;

- air conditioning of aircraft cabins and compartments at airfields located at altitudes up to 3000 m, as well as during takeoff and landing;

- powering the aircraft's on-board network with alternating current electricity at airfields located at altitudes up to 3000 m above sea level;

- supplying alternating current to the aircraft on-board network and compressed air to air-drive units when using the engine in an emergency situation in flight at altitudes up to 3000 m.

• State: Used
• Documents: Sold with documents

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