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Aerospatiale SA316C

1972 · Single-engine light turbine helicopter

Replaced the SA316B in production from 1972, with a higher rated turboshaft engine and an increased all up weight to 2250kg.

Specifications

Engine1 x Safran Artouste IIID 550 shp
Capacity1 + 5
Length (m)12.84
Height (m)3
Blades3
Rotor diam. (m)11.02
Disc area (m2)95.38
Weight (kgs)Empty: 1134 Max: 2250
Speed (km/h)Cruise: 195 Max: 220
Range (km)540
Ceiling (m)4000
Rate/Climb (m/min)270
blueprints SA316C

Airframes (1)

C/NModelBuiltReg
1995sa316c1978N17414 HB-XHP ZA-XHP