PD-14A  
Initial Operational Capability (IOC): 2017
Maiden Flight: 2014
Total Production: 70
Development Cost: RUB70 billion   (USD$959 million)
Also Known As: PD-14, PS-12 and PS-14
Origin: Russia
Corporations: Aviadvigatel Perm Engine Company*, MMPP Salut, NPO Saturn and UMPO   (*) lead contractor
Parent System: PD-14
Initial Operational Capability (IOC): 2017
Total Production: 70
Family Members: PD-10, PD-14M and PD-18R
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Description: The PD-14, formerly known as the PS-12 and/or PS-14, is a fifth generation civil turbofan engine being developed by Aviadvigatel Perm Motors, a part of United Engine Corporation (UEC), to be one of the alternative power plants to power the MS-21 twin-jet passenger aircraft family. The PD-14 designation was announced in early 2010 with its development cost estimated at 35 billion Russian Rubles ($1.1 billion at that time). By mid-2012 the developmental cost estimation has increased to 70 billion Rubles. The PD-14 program is expected to deliver an engine family ranging from 9 to 18 tons of thrust. The MS-21 airliner equipped with PD-14 engines may enter revenue service by 2017 with the engine to receive certification in 2015-2017.
The PD-14 engine is based on classic double-flow scheme without mixing of internal and external flows and that results in 12 to 16 percent fuel economy, hazardous emission (by 30 to 45 percent lower than CAEP 6) and noise level reduction. Noise requirements will be satisfied with installation of a new second generation noise reduction system and a new fan. The first PD-14 engine demonstrator was assembled by a variety of enterprises part of the UEC on May 30, 2012, and is expected to begin testing in the second half of 2012.
The PD-14A turbofan engine is intended to power the basic MS-21 airliner and will develop 14 tons of thrust per engine at takeoff. In June 2012, Russian Technologies became the launch customer for the PD-14A engine powering 35 MS-21 airliners. The PD-14A engine may enter service in 2017.

PD-14A Applications


Airliners MS-21-200 MS-21-300 MS-21-400

PD-14A Specifications

Weight
Max Takeoff Thrust: 14,000 kilogram (30,864 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)

PD-14A News

There are 4 news between
23 Mar 2010 and 2 Sep 2015
Wednesday, September 2, 2015Russia and China to Develop New Heavy-Lift Helicopter Powered by PD-14 Turbofan Engine
Wednesday, June 27, 2012Russian Technologies Places Order for 18 MS-21-200 and 17 MS-21-300 Airliners
Tuesday, June 5, 2012MS-21 Airliner PD-14 Turbofan Engine Enters Testing Phase
Tuesday, March 23, 2010Aviadvigatel PD-14 Turbofan Engine to Power MS-21 Jetliner

Operators & Related Equipment


OperatorsItems
Russia70
Engines powering Russian Technologies fleet of 35 MS-21 airliners (70 engines)

Grand Total 701
 

PD-14A Links & Resources

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