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Sikorsky S-61

From PlaneSpottingWorld, for aviation fans everywhere
S-61L/S-61N
S61b.jpg
HeliJet's S-61N at Vancouver International Airport
Type Medium-lift transport/airliner helicopter
Manufacturer Sikorsky
Maiden flight March 11 1959
Status Active service
Primary users Canadian Coast Guard
Bristow Helicopters
HeliJet
New York Airways
Number built 119[1]
Developed from SH-3 Sea King
Variants Sikorsky S-61R
File:Wsa-lightning-complex S61type1-drop ron-blaylock.jpg
A Carson Helicopters Fire King drops on the 2007 WSA Lightning Complex fire.
File:Wsa-lightning-complex S61type1-drop scott-linn.jpg
A Carson Helicopters Fire King drops on the 2007 WSA Lightning Complex fire.
File:S61-snorkel.jpeg
An S-61 helitanker uses a snorkel to refill its internal water tanks

The Sikorsky S-61L and S-61N are civil variants of the successful SH-3 Sea King helicopter. They are two of the most widely used airliner and oil rig support helicopters built.[1]

Design and development

In September 1957, Sikorsky won a US Navy development contract for an amphibious anti-submarine warfare (ASW) helicopter capable of detecting and attacking submarines.[1] The XHSS-2 Sea King prototype flew on March 11 1959. Production deliveries of the HSS-2 (later designated SH-3A) began in September 1961, with the initial production aircraft being powered by by two 930kW (1250shp) General Electric T58-GE-8B turboshafts.

Sikorsky was quick to develop a commercial model of the Sea King.[1] The S-61L first flew on November 2 1961, and was 4ft 3in (1.27m) longer than the HSS-2 in order to carry a substantial payload of freight or passengers. Initial production S-61Ls were powered by two 1350shp (1005kW) GE CT58-140 turboshafts, the civil version of the T58. The S-61L features a modified landing gear without float stabilisers.

On August 7 1962, the S-61N made its first flight.[1] Otherwise identical to the S-61L, this version is optimized for overwater operations, particularly oil rig support, by retaining the SH-3's floats. Both the S-61L and S-61N were subsequently updated to Mk II standard with improvements including more powerful CT58-110 engines giving better hot and high performance, vibration damping and other detail refinements.

The Payloader, a stripped down version optimised for aerial crane work, was the third civil model of the S-61.[1] The Payloader features the fixed undercarriage of the S-61L, but with an empty weight almost 2000lb (900kg) less than the standard S-61N.

A unique version is the S-61 Shortsky conversion of S-61Ls and Ns by Helipro International.[1] The fuselage is shortened by 50in (1.6m) to increase single engine performance and external payload. The Shortsky conversion first flew in February 1996.

Variants

S-61L 
Non-amphibious civil transport version. It can seat up to 30 passengers (13 Built).
S-61L Mk II 
Improved version of the S-61L helicopter.
S-61N 
Amphibious civil transport version.
S-61N Mk II 
Improved version of the S-61N helicopter.
S-61 Payloader 
Stripped down machine optimised for aerial crane work; features the fixed undercarriage of the S-61L, but with an empty weight almost 900kg (2000lb) less than the standard S-61N.
S-61 Shortsky 
Shortened conversion of the S-61L and N, designed to increase single engine performance and external payload.

Operators

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Specifications (S-61N Mk II)

Data from International Directiory of Civil Aircraft[1]

General characteristics

  • Crew: 2 pilots
  • Capacity: up to 30 passengers
  • Length: 58 ft 11 in (17.96 m)
  • Rotor diameter: 62 ft (18.9 m)
  • Height: 17 ft 6 in (5.32 m)
  • Disc area: 3,019 ft² (280.6 m²)
  • Empty weight: 12,336 lb (5,595 kg)
  • Loaded weight: lb (kg)
  • Max takeoff weight: 19,000 lb (8,620 kg)
  • Powerplant:General Electric CT58-140 turboshafts, 1,500 shp (1,120 kW) each

Performance


References

  1. 1.0 1.1 1.2 1.3 1.4 1.5 1.6 1.7 Frawley, Gerard: The International Directiory of Civil Aircraft, 2003-2004, page 194. Aerospace Publications Pty Ltd, 2003. ISBN 1-875671-58-7

External links

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See also

Template:Sikorsky Aircraft