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Also Known As | Zhi-20
| | First Flight | 23 December 2013
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| Initial Operational Capability (IOC) | November 2018
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| Total Production | +++
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| Origin | China
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| Corporations | AVICOPTER and Harbin Aviation Industry
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| Roles |
Ground Attack
Close-Air Support (CAS)
Anti-Submarine Warfare (ASW)
Anti-Ship
Transport
VIP Transport
Medical Evacuation (MEDEVAC)
Search and Rescue (SAR)
Reconnaissance (RECCE)
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| diameter of the rotor | 16.2-16.5 m
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| Overall helicopter length | 19.5 m
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| Fuselage Length | 49.2 ft (15 m)
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| Width/Span | 52.5 ft (16 m)
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| Fuselage Height | 11.5 ft (3.5 m)
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| Overall height of the helicopter | 5.0 m
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| Empty Weight | 10,700-11,000 lb (4850-5,000 kg)
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| Max Takeoff Weight MTOW | 9,800-10,000 kilogram (20,000-22,000 pounds)
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| Payload | 1,500 kilogram (3,300 pound)
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| Weight External Payload | 5,000 kilogram
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| Number of Engines | 2 x turboshaft engines
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| Powerplant | 2 × WZ-10 Zhuzhou Aeroengine Factory
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| Power | 2 × 1,600 kW / 2145 hp
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| Max Power at TakeOff | 3,200 kW (4,290 hp)
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| Main Rotor Blades | 5
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| Tail Rotor Blades | 4
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| Maximum flight speed | 320 km/h
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| Cruising speed | 170 mph (275 kph; 150 kts)
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| Service Ceiling | 17,000-18,000 feet ( 5,400-5,500 m; 3.4 miles)
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| Maximum Range | 350-400 miles (560-600 km; 300 nm)
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| Maximum flight distance | 1200 km
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| Ferry range | 2200 km
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| Rate-of-Climb | 1,400 ft/min (425 m/min)
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| Crew | 2 person
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| Capacity | 10 people
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