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Initial Operational Capability (IOC): 2000
Maiden Flight: 1999
Total Production: ?
Also Known As: D-436T2 and D-436T3
Origin: Russia
Corporations: Ivchenko-Progress, MMPP Salut, Motor Sich and UMPO
Parent System: D-436
Initial Operational Capability (IOC):
Total Production: ?
Family Members: D-436-148B and D-436TP
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Description: The Ivchenko-Progress D-436 engine family, based on the D-36 engine, has been designed to power twin-engine short-range turbojet passenger aircraft. Its basic design comprises 14 modules. The D-436 engines feature low fuel consumption, high environmental safety standards, low operating costs and longer service life than previous engines powering twin-engine short range aircraft. The Tu-334, Be-200, Yak-42D-100 and An-148 aircraft are powered by the D-436 engine family.

The D-436T1/T2/T3 engines have been designed to power the Tupolev Tu-334 aircraft family. The D-436T1 engine powers the Tu-334 basic model, the D-436T2 engine is intended to power the Tu-334-200, and the D-436T3 is intended for the Tu-230 aircraft. The D-436T1 was certified in 2000. Motor Sich, Salut and Ufa Engine Manufacturing plant produce the engine in cooperation.

The AI-436T12, formerly known as the D-436TX, is a derivative of D-436T1 engine developing up to 12,000 kg of thrust at takeoff.

D-436T1 Applications

Airliners Tu-334-100 Yak-42D

D-436T1 Specifications

Service Life Flight Hours: 40,000
Height: 1,949 millimeter (77 inch)
Length: 3,829 millimeter (151 inch)
Width: 1,802 millimeter (71 inch)
Dry Weight: 1,450 kilogram (3,197 pound)
Max Cruise Thrust: 1,600 kilogram
Max Takeoff Thrust: 7,500 kilogram (16,534 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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