Shenzhen Nuobashi Trading Co.,Ltd

Specific fuel consumption by 15...20% lower than
that of current engines in this thrust class
Maximum takeoff(S/Lstatic;ISA)
Thrust, kgf .................................…..................10,300
Ambient air temperature to which this thrust is
maintained invariable, C .............................…............…..............+30
Takeoff(S/Lstatic;ISA)
Thrust, kgf
...................….....…......….....9,400
Ambient air temperature to which this thrust is
maintained invariable, ℃.........................,.. ... ... .….…….…….....…..........+30
Maximum cruise (H=11,000 m;M=0.8,ISA)
Thrust, kgf ... . ......…..……-..---..…......…............1,860
Specific fuel consumption, kg/h/kgf .................................0.545
Ambient air temperature to which this thrust is
maintained invariable, ℃.....................…............................................. +10