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D-36-4A  
Initial Operational Capability (IOC):
Total Production: ?
Origin: Russia
Corporations: Ivchenko-Progress* and Motor Sich   (*) lead contractor
Parent System: D-36
Initial Operational Capability (IOC): 1977
Maiden Flight: 1974
Total Production: ?
Family Members: D-36-1
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Description: The Ivchenko-Progress D-36 is a high bypass ratio engine family providing 14,000 pounds of thrust developed to power the Yak-42 passenger aircraft and the An-72 and An-74 transport aircraft. The program aim was to provide power to the tri-jet Yak-42 airliner. Engine flight trials started in 1974 and the first version entered series production in 1977. The basic D-36 consists of three-shaft composed of 10 modules. The D-36 engine is the basis for a family of derivative engines comprising: the D-136, D-236 and D-436 aircraft engines.

The D-36-4A (Series 4A) is a variant of the D-36-3A engine modified for underwing mounting and introducing a reverser. It has been designed to power all the versions of the An-74TK-300 aircraft. The engine is manufactured by Motor Sich as the other D-36 engine versions.

D-36-4A Applications


Airliners An-74TK

D-36-4A Specifications

Service Life Flight Hours: 40,000
Dimensions
Height: 1,919 millimeter (76 inch)
Length: 3,733 millimeter (147 inch)
Width: 1,802 millimeter (71 inch)
Weight
Dry Weight: 1,130 kilogram (2,491 pound)
Max Cruise Thrust: 1,600 kilogram
Max Takeoff Thrust: 6,500 kilogram (14,330 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)

Operators & Related Equipment


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