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