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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