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Purpose:
Auxiliary power unit
Description:
Designed as auxiliary power unit of An-140 aircraft and other aircraft and helicopters. Used for starting aircraft propulsive engines and conditioning cockpits and cabins, and also for powering airborne electric equipment.
The engine has Type Certificate.
Technical details:
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Performance (SLS, ISA +30
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aircraft electric system AC power, kV-A
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16
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bled airflow, kg/s
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0.4
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bled air pressure, total, MPa, not less than
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0.32
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bled air temperature, °С, not more than
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260
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fuel consumption, kg/h
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92
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Dimensions, mm
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1149.5х580.5х 663.5
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Engine weight as delivered, kg
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128
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Assigned service life, h
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8000
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