Z-18F  
Initial Operational Capability (IOC): 2015
Maiden Flight: 2014
Total Production: ?
Origin: China
Corporations: AVICOPTER and Changhe Aircraft
Parent System: SA 321 Super Frelon
Initial Operational Capability (IOC): 1966
Maiden Flight: 7 December 1962
Total Production: 182
Family Members: AC313, SA 321 Super Frelon, Z-18A and Z-18J
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Description: The People's Liberation Army (PLA) Z-18 is a medium-weight helicopter derived from the state-of-the-art AC-313 VIP transport helicopter and developed by Changhe Aircraft Industries Corporation (CAIC) and Avicopter. It is powered by three WZ-6 turboshaft engines and the airframe is made of composite materials and titanium. The Z-18 rotorcraft maximum takeoff weight is 13.8 tons and features integrated avionics as well as the non-retractable landing gear from the Super Frelon helicopter family. The Z-18F is an anti-submarine warfare (ASW) helicopter first revealed on the flight deck of the PLA Navy (PLAN) Liaoning aircraft carrier in 2013-2014. The Z-18F helicopter is equipped with surface search radar, dipping sonar, hardpoints intended for torpedoes and/or anti-ship missiles, and sonobuoys.

Z-18F Applications


Fighting Ships Type 001 Type 055

Z-18F Specifications

Main Rotor Blades: 6
Number of Engines: 3
Tail Rotor Blades: 5
Performance
Ceiling: 8,000 meter (26,247 foot)
Weight
Max Takeoff Weight: 13,800 kilogram (30,423 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)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
WZ-6x3
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