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AI-22  
Initial Operational Capability (IOC):
Total Production: ?
Origin: Russia
Corporations: Ivchenko-Progress and Motor Sich
Parent System: AI-22
Initial Operational Capability (IOC):
Total Production: ?
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Description: The AI-22 is a turbofan engine derived from DV-2 engine core and designed to power the next-generation short-range airliners Tu-324 and Yak-48. The AI-22 modular design consists of 10 modules with highly developed monitoring and diagnosis systems to ensure on-condition operation. The AI-22 by-pass engine is provided with FADEC control system and rated at 8,421-lb at takeoff.

AI-22 Specifications

Service Life Flight Hours: 40,000
Dimensions
Height: 1,548 millimeter (61 inch)
Length: 3.01 meter (119 inch)
Width: 1,398 millimeter (55 inch)
Weight
Contingency Thrust: 4,340 kilogram
Dry Weight: 765 kilogram (1,687 pound)
Max Cruise Thrust: 775 kilogram
Max Takeoff Thrust: 3,820 kilogram (8,422 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

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