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Initial Operational Capability (IOC): 1977
Maiden Flight: 1974
Total Production: ?
Also Known As: D-36-1A, D-36-2A and D-36-3A
Origin: Russia
Corporations: Ivchenko-Progress and Motor Sich
Parent System: D-36
Initial Operational Capability (IOC): 1977
Maiden Flight: 1974
Total Production: ?
Family Members: D-36-4A
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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-36-1 (D-36 Series 1) is the initial version intended to power the Yak-42 jetliner. More than 800 D-36-1 engines were produced by Motor Sich between 1977 through early 1990s. The D-36-1A/2A/3A (Series 1A, 2A and 3A) engines were designed to power the An-72/74 twin-engine aircraft family.

D-36-1 Applications

Airliners An-74TK Yak-42D Propulsion Systems D-136 D-436T1 Support Aircraft An-74

D-36-1 Specifications

Service Life Flight Hours: 18,000
Height: 2,270 millimeter (89 inch)
Length: 3,930 millimeter (155 inch)
Width: 2,030 millimeter (80 inch)
Dry Weight: 1,124 kilogram (2,478 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


Grand Total ?5
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