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Aerospatiale / Sud-Aviation SA 318C / SE 313B Alouette II

Aerospatiale / Sud-Aviation Alouette II © Karsten Palt
Photo ©: Karsten Palt

SA 318C / SE 313B Alouette II

Light Utility Helicopter

Crew1
Passengers4
 
Propulsion1 Turboshaft Engine
Engine ModelTurbomeca Artouste II C6
Engine Power265 kW355 hp
 
Speed185 km/h100 kts
  115 mph
Service Ceiling3.200 m10.500 ft
Range720 km389 NM
448 mi.
 
Empty Weight895 kg1.973 lbs
max. Takeoff Weight1.600 kg3.527 lbs
 
Rotor Blades (main/tail)3/23/2
Main Rotor Diameter10,20 m33,5 ft
Tail Rotor Diameter1,81 m5,9 ft
Rotor Disc Area81,7 m²879 ft²
Length (Fuselage)9,70 m31,8 ft
Length12,05 m39,5 ft
Height2,75 m9,0 ft
 
First Flight31.07.1952 (SE 3120), 12.03.1955 (SE 3130)
Production Statusout of production
Total Production> 1300
 
ICAO CodeALO2
FAA TCDS7H1
Data for (Version)Aerospatiale SE 313B

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