| Manufacturer | Harbin Aircraft |
| Country | China |
| Commercial designation | WZ-19 |
| Technical designation | WZ-19 |
| Version, Variant | |
| Type | fenestron |
| Currently produced | 40/year |
| Typical missions | attack, scout |
| Flight conditions | |
| First flight | 2010 |
| Landing system | wheels |
| Blades number | 4 |
| Tail blades number | 11 |
| MTOW with external loads | 4500 kg | 9900 lbs |
| MTOW with only internal loading | 4500 kg | 9900 lbs |
| Empty weight | 2350 kg | 5180 lbs |
| External payload | 0 kg | 0 lbs |
| Internal payload | 0 kg | 0 lbs |
| Standard fuel tank | 0 kg | 0 lbs |
| external fuel tank | 0 kg | 0 lbs |
| Maximum cruise speed | 245 km/h | 133 kt |
| Vne | 0 km/h | 0 kt |
| Max negative g @ MTOW | 0 g |
| Max positive g @ MTOW | 0 g |
| Range w/ normal tanks | 700 km | 380 nm |
| Max range w/ external tanks | 0 km | 0 nm |
| Max endurance @ min consumption speed | 03:00:00 h:min |
| Rate of climb @ SL | 9-10 m/s | 1800 ft/min |
| Rate of climb @ SL @MTOW | 0 m/s | 0 ft/min |
| IGE max hovering altitude, MTOW | 0 m | 0 ft |
| IGE max hovering altitude, empty | 0 m | 0 ft |
| OGE max hovering altitude, MTOW | 2400 m | 7900 ft |
| OGE max hovering altitude, empty | 0 m | 0 ft |
| Service ceiling ISA, MTOW | 0 m | 0 ft |
| Max operating altitude, empty weight | 0 m | 0 ft |
| Engine manufacturer | |
| Model | WZ-8C Turbine Engine, |
| Engines quantity | 2 |
| Fuel consumption @ SL @ max continuous speed | 0 kg/kW/h | 0 lbs/hp/h |
| Engines nominal power | 0 kW | 0 hp |
| Crew | 2 |
| Max pax number | 0 |
| Armament |
57 mm or 90 mm multi-barrel rocket launcher
Up to 16 Red Arrows -8 / 9/10 Earth Shields
Up to 16 Tianyan-90 air-to-air missiles
23 mm cannon
|
