AI-9V-1
The unit is used as aground and in-flight power source effecting supply of compressed air to the starting system of engines and electric power to the aircraft mains when checking the helicopter electrical and radio equipment.
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Main advantages of the engine:
- high standart of reliability;
- desing simplicity;
- ease of maintenance and high repairability.
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Basic specifications:
| Air bleeds, kg/s |
0.4 |
| Bleed air total pressure, MPa, min |
0.31 |
| Bleed air temperature, K |
433 |
| Power across generator terminals, kw |
9 |
| Fuel consumption, kg/h, max |
100 |
| Dry weight, kg, max (without generator) |
58 |
Max aerodrome elevation for the APU starting
and operation on the ground, m |
5,000 |
| Max fight altitube for the APU operation, m |
7,000 |
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