GENERAL
| Description | |
| Wake Turbulence Category | L |
| Aerodrome Reference Category | |
| Approach Category | |
| Variants | SA 315B Lama, HB 315B Gaviao, HAL Cheetah, HAL Lancer, HAL Cheetal |
| Manufacturer | Aérospatiale |
| First Flight | 17th March 1969 |
| Launch Organisation | July 1971 |
| Largest Operator | |
| First Registered In India | |
| Users In India | Indian Air Force |
Takeoff
Landing
RUNWAY REQUIRED AT MTOW/MLW
SPECIFICATIONS
| Crew | 2 |
| Passenger Capacity | 15 |
| Length | 13.53 m |
| Wingspan | |
| Height | 4.95 m |
| Wing Area | |
| Max Ramp Weight | 6,400 Kgs |
| Fuel Capacity | 1,255 L |
| Engine | Pratt & Whitney Canada PT6C-67C |
| Thrust | 1676 SHP |
Fleet Detail
| MSN | TAIL | MAKER | MODEL | ENGINE | CONF | FIRST FLT | LESSOR | REMARKS |
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