Aviation auxiliary gas turbine engine APU TA-6V

• Equivalent air capacity - 235 kW.
• The selected power of alternating current is 40 kVA.
• Starting height - 3000 m.
• Fuel consumption - 225 kg/h.
• The mass is 245 kg.
• The overall dimensions are 1585 × 620 × 735 mm.

Engine t-6V For auxiliary power plant (Armed Forces) is a single gas turbine engine.

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

- launch of marching engines of the aircraft using air launchers at airfields located at altitudes up to 3000 m above sea level;

- conditioning of cabs and compartments (salons) of the aircraft at airfields located at altitudes up to 3000 m, 'as well as on take -off and landing;

- power supply of the aircraft by electricity of alternating current at airfields located at altitudes up to 3000 m above sea level;

- power current of the aircraft on the aircraft and compressed air of the air drive units when using the engine in an emergency in flight at altitudes up to 3000 m.

• State: Used
• Documents: Sold with documents

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