AI-222-25 Turbofan Engine

The engine has been optimized to be operated on up-to-date trainer, combat trainer, and light combat aircraft and complies with strict requirements for the engines of this class.
Using the AI-222-25 engine will allow creating a number of highly competitive aircraft. At customer’s request, AI-222-25 engine can be equipped with vectored thrust nozzles or theirversions with afterburners can be developed.

MAIN ADVANTAGES OF THE ENGINE:
- high reliability; 
- optimum performance; 
- low noise, emission, and infrared signature; 
- long service life; 
- low operating costs

SPECIFICATIONS
Maximum power condition (SLS, ISA, σin=1.0): 
Thrust, kgf (kN)2500 (24.52)
SFC,kg/kgf•h (kg/kN•h)  0.64 (65.2)
Maximum power condition (H=5000 m;Mfl=0.6; ISÀ, σin=0.97): 
Thrust, kgf (kN)1450 (14.22)
Cruise power condition (H=10000 m; Mfl=0.6; ISÀ, σin=0.97): 
Thrust, kgf (kN)   300 (2.94)
SFC,kg/kgf•h (kg/kN•h)0.875 (89.2)
Dry weight, kg  440
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