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]
SW-4 · Length
Single sourceConfiguration
| Specification | Bell 412 | PZL SW-4 Puszczyk |
|---|---|---|
| Type | Multipurpose utility helicopter[source] | Multipurpose utility helicopter[source] |
| National origin | United States / Canada[source] | Poland[source] |
| Manufacturer | Bell Helicopter[source] | PZL-Świdnik[source] |
| Primary users | Japan Ground Self Defence Force See Operators for others[source] | — |
10.57 m (34 ft 8 in)[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]
SW-4 · 1 × Rolls-Royce 250-C20R/2 turboshaft engine
Single source1 × Rolls-Royce 250-C20R/2 turboshaft engine, 336 kW (451 hp)[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] |
40[source] |
| Manufactured | 1979–present[source] | 1996–present[source] |
|---|
| Introduction date | 1981 ( 1981 )[source] | 2002[source] |
|---|
| First flight | August 1979 ( 1979-08 )[source] | 29 October 1996[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] | 4 passengers[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] | 64 m 2 (690 sq ft)[source] |
|---|
| Power/mass | 0.2663 hp/lb (0.4378 kW/kg)[source] | 0.21 kW/kg (0.13 hp/lb)[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary user | — | Polish Armed Forces[source] |
|---|
| Disk loading | — | 25 kg/m 2 (5.1 lb/sq ft)[source] |
|---|
Maximum take-off; SW-4 · Max takeoff weight
Single source