APU TA-6V engine

Aircraft auxiliary gas turbine engine APU TA-6V

In a repair fund condition, with a form. In a shipping box.

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

The engine is intended for installation on a line of various aircraft. It is used for long-term autonomous power supply on the ground or emergency power supply in the air with electric power of aircraft systems and supply of hot compressed air to the air conditioning system, as well as for starting the main engines of the aircraft. TA-6 APUs were used on Tu-154, Il-62M, Il-76 and Tu-22M, An-22A aircraft. TA-6V - developed in 1974 for Yak-42 aircraft.

• State: Used
• Payment: Any form of payment
• Documents: Sold with documents

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