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D-36
Roll-Out: 1974
IOC: 1977
D-36-1
Also Known As
D-36-1A D-36-2A D-36-3A
Origin Russia
Contractor/s
Ivchenko-Progress Motor Sich
Applications
An-74 An-74TK D-136 D-436T1 Yak-42D
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.
Specifications
Dimensions: Height 2,270 mm 1,711.5mm D-36-1A/2A/3A engines, Length 3,930 mm 3,192mm D-36-1A/2A/3A engines, Width 2,030 mm 1,541mm D-36-1A/2A/3A engines
Weights: Dry Weight 1,124 kg (2,478 lb)
Engine/s Performance: Max Cruise Thrust 1,600 kg (3,527 lb), Max Takeoff Thrust 6,500 kg (14,330 lb)
Other: Service Life (Flight Hours) 18,000 D-36-1A and D-36-2A 24,000 flight hours
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)
Last Updated: Saturday, November 22, 2008
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