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SA315 Lama

ICAO: LAMA

helicopter • turboshaft • Aérospatiale

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Specifications

ICAO Code: LAMA

IATA Code: -

Family: helicopter

Engine Family: turboshaft

Engine Count: 1

Manufacturer:Aérospatiale

MLW: 1950 kilogram

MTOW: 1950 kilogram

Maximum operating altitude: 23000 foot

Vne: 118 knot

Fuel capacity: 555 litre

Tail rotor diameter: 1.91 metre

Tail rotor count: 1

Tail rotor blades: 3

Main rotor diameter: 11.02 metre

Main rotor count: 1

Main rotor blades: 3

Length: 10.24 metre

Width: 2.38 metre

Height: 3.09 metre

Overview

SA315 Lama is a helicopter powered by turboshaft engine(s).

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