Wednesday, December 03, 2008

D-36

Roll-Out: 1974
IOC: 1977

D-36-4A

Origin
Russia

Contractor/s
Ivchenko-Progress *
Motor Sich

Applications
An-74TK

Family Members
D-36-1

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.

Specifications
Dimensions: Height 1,919.40 mm, Length 3,732.50 mm, Width 1,802.30 mm

Weights: Dry Weight 1,130 kg (2,491 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) 40,000

Operators

Ukraine

Image Gallery

Internet Resources
ivchenko-progress.com

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

Leave Feedback >>