Aérospatiale SA315

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

280 nm
Range
103 Kts
Cruise Speed
4
Passengers Carried
Total in India
1,135 Kgs
Payload
17,715
Service Ceiling
Price
Number Built


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