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Purpose:
Auxiliary power unit
Description:
Designed to supply compressed air to air starting systems of Yak-40, М-15 aircraft, D-2, Мi-14, Mi-24, Ка-27,
Ка-31, Ка-32, Ка-50, Ка-52, Ка-60 helicopters.
The engine has Type Certificate.
Technical details:
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Performance (SLS, ISA)
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Bled airflow, kg/s, not less than
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0.38
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Bled air pressure, total, MPa, not less than
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0.24
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Bled air temperature,
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130
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Fuel consumption, kg/h, not more than
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75
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Dimensions, mm
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740х515х490
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Engine weight as delivered, kg
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45.9
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Assigned service life, starts
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18000
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