Initial Operational Capability (IOC): November 2018
Total Production: ?
Origin: China
Parent System: WZ-10
Initial Operational Capability (IOC): November 2018
Total Production: ?
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Description: The WZ-10 is a 1,600-KW turboshaft engine developed by China to power the People's Liberation Army (PLA) Harbin Z-20 medium-lift helicopter. The more powerful engine is intended for operations at altitudes above 4,000 meters. The new engine is expected to be fielded along with the Z-20 helicopter beginning in November 2018.

WZ-10 Applications

Support Aircraft Z-20

WZ-10 Specifications

Max Power at TakeOff: 1,600 kW (2,145 hp)
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)

WZ-10 News

There are 2 news between
31 Aug 2018 and 10 Oct 2019
Thursday, October 10, 2019Chinese Z-20 Helicopter Engine Optimized for Operations at High Altitude Areas
Friday, August 31, 2018Chinese Z-20 Medium-Lift Helicopter to Enter Service in November

Operators & Related Equipment


Grand Total ?1
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