Basic specifications:
2.5-min power
60-min continuous power I (1CP) with OEI
(H=0, M=0, ISA): |
Power,h.p. (kW) |
2800(2059) |
flat-rated up to toat, °C |
+38 |
60-min continuous power II (2CP) with OEI
30-min continuous take-off power
Take-off power (H=0, M=0, ISA):
|
Power, h.p. (kW) |
2000*(1470) ... 2500*(1838) |
flat-rated up to toat, °C |
+58 ...+37 |
Specific fuel consumption,kg/h.p.·h (kg/kW·h) |
0.220(0.299) ... 0.209(0.284) |
Cruise power (H=0, M=0, ISA): |
Power, h.p. (kW) |
1500(1104) ...1750(1278) |
flat-rated up to toat, °C |
+45 ...+35 |
Engine dry weight, kg |
295 |
* Engine automatic control system allows adjusting take-off power rating value – 2500, 2400, 2200 и 2000 h.p. (depending on aircraft type, powered by the engine).
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