FORCETALLY
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Measured figures
Bell 412EP · including rotors
Single source56 ft 1 in (17.09 m) including rotors[source]
Configuration
| Specification | Aerokopter AK1-3 Sanka | Bell 412 |
|---|---|---|
| Crew | one[source] | one-two pilots[source] |
| Type | Helicopter[source] | Multipurpose utility helicopter[source] |
| National origin | Ukraine[source] | United States / Canada[source] |
| Manufacturer | Aerokopter[source] | Bell Helicopter |
Bell 412EP · Height
Single source15 ft 0 in (4.57 m)[source]
Bell 412EP · Range
Single source529 nmi (609 mi, 980 km)[source]
AK1-3 · 1 × Subaru EJ25 four cylinder, water-cooled, four stroke automotive engine
Single source1 × Subaru EJ25 four cylinder, water-cooled, four stroke automotive engine, 116 kW (156 hp)[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]
Bell 412EP · Service ceiling
Single source20,000 ft (6,100 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In production (2014)[source] | — |
|---|
| Number built | 102 (December 2020)[source] | 1,300+[source] |
|---|
| First flight | 1999[source] | August 1979 ( 1979-08 )[source] |
|---|
| Capacity | one passenger[source] | up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[source] |
|---|
| Fuel capacity | 75 litres (16 imp gal; 20 US gal)[source] | — |
|---|
| Primary users | — | Japan Ground Self Defence Force See Operators for others[source] |
|---|
| Manufactured | — | 1979–present[source] |
|---|
| Introduction date | — | 1981 ( 1981 )[source] |
|---|
| Developed from | — | Bell 212[source] |
|---|
| Variant | — | Bell CH-146 Griffon[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] |
|---|