Credit
Calfo ( talk ) · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
SA 315B Lama · Length
Single source10.24 m (33 ft 7.25 in)[source]
Bell 412EP · including rotors
Configuration
| Specification | Aérospatiale SA 315B Lama | Bell 412 |
|---|---|---|
| Type | Utility helicopter[source] | Multipurpose utility helicopter[source] |
| National origin | France[source] | United States / Canada[source] |
| Manufacturer | Aérospatiale[source] | Bell Helicopter[source] |
| Built by | Helibras Hindustan Aeronautics Limited (HAL)[source] | — |
56 ft 1 in (17.09 m) including rotors[source]
SA 315B Lama · 1 × Turbomeca Artouste IIIB turboshaft derated to
Single sourceSA 315B Lama · Powerplant
Single source1 × Turbomeca Artouste IIIB turboshaft , 649 kW (870 hp) derated to 410 kW (550 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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | — |
|---|
| Primary user | Afghan Air Force Indian Air Force[source] | — |
|---|
| Introduction date | July 1971[source] | 1981 ( 1981 )[source] |
|---|
| First flight | 17 March 1969[source] | August 1979 ( 1979-08 )[source] |
|---|
| Developed from | Aérospatiale Alouette II[source] | Bell 212[source] |
|---|
| Capacity | 4 passengers or 1,135 kg (2,500 lb) slung payload[source] | up to 13 passengers, maximum external load of almost 6,614 lb (3,000 kg)[source] |
|---|
| Main rotor area | 95.38 m 2 (1,026 sq ft)[source] | 1,662 sq ft (154.4 m 2 )[source] |
|---|
| Primary users | — | Japan Ground Self Defence Force See Operators for others[source] |
|---|
| Number built | — | 1,300+[source] |
|---|
| Manufactured | — | 1979–present[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] |
|---|
| Power/mass | — | 0.2663 hp/lb (0.4378 kW/kg)[source] |
|---|