1961


Sikorsky S-61 H-3

S-61L







The S-61L first flew on 2 November 1961. It is was 4ft 3in (1.27m) longer than the standard S-61A/HSS-2/SH-3 in order to carry freight or passengers. Initial production S-61Ls were powered by two 1350shp (1005kW) GE CT58-140 turboshafts. The S-61L features a modified landing gear with straight strut legs on each side. Los Angeles Airways was the first civil operator of the S-61L, introducing them on 11 March 1962. Many S-61Ls were subsequently updated to Mk II standard with more powerful CT58-110 engines, vibration damping and other detail refinements.


Specifications S-61L


Engine 2 x GE CT58-140 1350 shp
Capacity 3 + 30
Length (m) 17.45
Height (m) 5.18
Blades 5
Rotor diam. (m) 18.9
Disc area (m2) 280.5
Weight (kgs) Empty: 5310     Max: 9300
Speed (km/h) Cruise: 222     Max: 245
Range (km) 428
Ceiling (m) 3810
Rate/Climb (m/min) 396
blueprints


  List of Operators of S-61L


Years Model Org
1962/71 usa Los Angeles Airways
1964/67 usa Chicago Helicopter Airways
1965/22 S-61 H-3 united kingdom British International Helicopters
1966/?? S-61 H-3 united kingdom UK Government
1966/89 S-61 H-3 united kingdom Westland
1973-    S-61 H-3 usa Carson Helicopters
1980/85 S-61 H-3 argentina Helicopteros Marinos
1980-    S-61 H-3 usa Croman Corp
1991-    S-61 H-3 canada VIH Helicopters Ltd
1993/00 S-61 H-3 united kingdom Brintel Helicopters

S-61 H-3 canada Okanagan Helicopters
S-61 H-3 canada Coulson Aircrane
S-61 H-3 canada Canadian Helicopters Ltd
S-61 H-3 south africa Court Helicopters
usa New York Airways



  Global Distribution of S-61L



14S-61L





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