Credit
Sardaka · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
Bell 412EP · including rotors
Single source56 ft 1 in (17.09 m) including rotors[source]
Z-20 · Length
Single sourceConfiguration
| Specification | Bell 412 | Harbin Z-20 |
|---|---|---|
| Type | Multipurpose utility helicopter[source] | Medium lift helicopter[source] |
| National origin | United States / Canada[source] | China[source] |
| Manufacturer | Bell Helicopter[source] | Harbin Aircraft Industry Group[source] |
| Primary users | Japan Ground Self Defence Force See Operators for others[source] | People's Liberation Army Ground Force People's Liberation Army Naval Air Force People's Armed Police |
20 m (65 ft 7 in)[source]
Bell 412EP · Range
Single source529 nmi (609 mi, 980 km)[source]
Z-20 · Combat range
Single source560 km (350 mi, 300 nmi)[source]
Bell 412EP · 1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac coupled turboshaft engine - each, 1,250 shp (
Single source1 × Pratt & Whitney Canada PT6T-3D Twin-Pac or PT6T-3DF Twin-Pac coupled turboshaft engine - each, 1,250 shp (930 kW)[source]
Z-20 · 2 × WZ-10 turboshaft engines each
Single source2 × WZ-10 turboshaft engines, 1,600–2,000 kW (2,100–2,700 hp) each[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 1,300+[source] | 230+[source] |
|---|
| Manufactured | 1979–present[source] | — |
|---|
| Introduction date | 1981 ( 1981 )[source] | 1 October 2019[source] |
|---|
| First flight | August 1979 ( 1979-08 )[source] | 23 December 2013[source] |
|---|
| Developed from | Bell 212[source] | — |
|---|
| Variant | Bell CH-146 Griffon[source] | — |
|---|
| Capacity | up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[source] | 12-15 passengers, 1,500 kg (3,300 lb) of cargo internally, 4,000 kg (8,800 lb) of cargo externally[source] |
|---|
| Fuselage length | 43 ft (13 m)[source] | — |
|---|
| Blade sections | root: Boeing VR-7; tip: Wortmann FX 71-H-080[source] | — |
|---|
| Main rotor area | 1,662 sq ft (154.4 m 2 )[source] | — |
|---|
| Power/mass | 0.2663 hp/lb (0.4378 kW/kg)[source] | — |
|---|
| Status | — | In service, in production[source] |
|---|
| Developed into | — | Harbin Z-21[source] |
|---|
| Guns | — | Provision for machine guns and autocannons[source] |
|---|
| Hardpoints | — | 4 hardpoints on two stub wings , with provisions to carry combinations of: Rockets: Various rocket pods Missiles: AKD-9 laser-guided air-to-surface missile AKD-10 laser-guided air-to-surface missile CM-502KG or CM-502V NLOS air-to-surface missile CM-501G A NLOS air-to-surface missile CM-501XA loitering munition TY-90 air-to-air missile YJ-9 anti-ship missile[source] |
|---|
| Rockets | — | Various rocket pods[source] |
|---|
| Missiles | — | AKD-9 laser-guided air-to-surface missile AKD-10 laser-guided air-to-surface missile CM-502KG or CM-502V NLOS air-to-surface missile CM-501G A NLOS air-to-surface missile CM-501XA loitering munition TY-90 air-to-air missile YJ-9 anti-ship missile[source] |
|---|