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Aerospatiale / Sud-Aviation SA 321 Super Frelon

Aerospatiale SA-321JA Super Frelon © Gary Shephard
Photo ©: Gary Shephard (Photos at airliners.net)

SA 321 Super Frelon

Heavy Transport & Anti Submarine Helicopter

Crew2
Passengers27
 
Propulsion3 Turboshaft Engines
Engine ModelTurbomeca Turmo IIIC6
Engine Power (each)1140 kW1529 shp
 
Speed274 km/h148 kts
  170 mph
Service Ceiling3.100 m10.171 ft
Range1.020 km551 NM
634 mi.
 
Empty Weight6.863 kg15.130 lbs
max. Takeoff Weight13.000 kg28.660 lbs
 
Rotor Blades (main/tail)6/56/5
Main Rotor Diameter18,90 m62,0 ft
Tail Rotor Diameter5,04 m16,5 ft
Rotor Disc Area280,6 m²3020 ft²
Length (Fuselage)20,08 m65,9 ft
Length23,03 m75,6 ft
Height6,76 m22,2 ft
 
First Flight10.06.1959
Production Statusout of production
Total Production99
 
ICAO CodeFREL
FAA TCDSH1EU
Data for (Version)Aerospatiale SA321G Super Frelon

Remarks
Total Production of 99 includes chinese license production.


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