SA315 Lama

Aircraft type

Data given for the Aérospatiale SA315 B Lama in basic configuration.

Manufacturer Aérospatiale
Aircraft family Helicopter
Engine type Turboshaft
Engine count 1
ICAO code LAMA

Technical specifications

Design
Main rotor blades
3
Main rotor count
1
Tail rotor blades
3
Tail rotor count
1
Dimensions
Height
3.09 m
10.14 ft
Length
10.24 m
33.6 ft
Main rotor diameter
11.02 m
36.15 ft
Tail rotor diameter
1.91 m
6.27 ft
Width
2.38 m
7.81 ft
Fuel
Fuel capacity
555 l
147 us gal
Performance
Service ceiling
23,000 ft
7,010 m
Speed limits
Vne
118 kt
219 km/h / 136 mph
Weight limits
MLW
1,950 kg
4,299 lb
MTOW
1,950 kg
4,299 lb

Aircraft models

Engine models