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D-436
D-436-148B
Roll-Out: Tuesday, March 30, 2004
IOC: 2006
Also Known As
D-436-148D
Origin Russia
Contractor/s
Ivchenko-Progress Motor Sich
Applications
An-148-100 An-148-200
Family Members
D-436T1 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-436-148, including D-436-148B and D-436-148D versions, is a version of D-436T1 engine designed to power the Antonov An-148 passenger aircraft with the powerplants mounted underwing. The D-436-148 engine features improved accessory gearbox and thrust reverser as well as composites introduced on the core fairing and main jet with noise-suppressing coatings and FADEC control. The engine entered flight tests in March 2004 and performed its maiden flight powering the An-148 on December 17, 2004.
Specifications
Dimensions: Height 1,930 mm, Length 3,830 mm, Width 1,784 mm
Weights: Dry Weight 1,400 kg (3,086 lb)
Engine/s Performance: Max Cruise Thrust 1,500 kg (3,307 lb), Max Takeoff Thrust 6,400 kg (14,109 lb) 6,800 kg D-436-148D
Other: Service Life (Flight Hours) 40,000
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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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