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General Info

Sikorsky S-76 Spirit
Utility helicopter

General information
Type Utility helicopter
National origin United States
Manufacturer Sikorsky Aircraft

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First flight 13 March 1977
Status In service
Primary users Bristow Helicopters / Coulson Firefighters
Produced 1977–present
Number built 875
Variants Sikorsky S-75

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History Sikorsky 
Sikorsky S-76 is a medium-size
commercial utility helicopter
First flight 13 March 1977, Status In service, Produced 1977–present

The Sikorsky S-76 is a medium-size commercial utility helicopter designed and produced by the American helicopter manufacturer Sikorsky Aircraft. It is the company's first helicopter specifically developed for the civilian market.

Design

S-76A++ used for Search and Rescue at Royal Australian Air Force bases operated by CHC Helicopter

The S-76 is of a conventional configuration, with a four-bladed fully articulated main rotor and a four-bladed anti-torque rotor on the port side of the tailboom. It is powered by a pair of turboshaft engines, which are located above the passenger cabin. On the prototypes and initial production aircraft, these engines were Allison 250-C30s, a variant of the popular Allison 250 engine that was developed specially for the S-76l it had a single-stage centrifugal compressor instead of the multi-stage axial/centrifugal compressor of earlier models of the engine, rated at 650 shp (480 kW) for takeoff. These engines are connected to the main rotor by the main gearbox, a three-stage unit with a bull gear as its final stage, rather than the planetary gear that had been used by previous generations of Sikorsky helicopters. This arrangement has 30% fewer parts and lower costs than a more conventional design

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Howard Sikorsky helicopters MD

Sikorsky, a Lockheed Martin Company
Sikorsky S-76 Spirit
commercial utility helicopter

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General Info

  • Crew: two
  • Capacity: 13 passengers
  • Length: 52 ft 6 in (16 m) from tip of main rotor to tip of tail rotor
  • Width: 10 ft 0 in (3.05 m) at horizontal stabilizer
  • Height: 14 ft 6 in (4.42 m) to tip of tail rotor)
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Powerplant

  • Empty weight: 7,005 lb (3,177 kg) in utility configuration
  • Gross weight: 11,700 lb (5,306 kg)
  • Fuel capacity: 281 US gallons (1,064 liters), with 50 or 102 US gallons (189 or 386 liters) available in extra auxiliary tanks
  • Powerplant: 2 × Turbomeca Arriel 2S2 turboshaft, 922 shp (688 kW) each
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Specifications

  • Maximum speed: 155 kn (178 mph, 287 km/h) at maximum takeoff weight at sea level in standard atmospheric conditions
  • Cruise speed: 155 kn (178 mph, 287 km/h) maximum cruise speed is the same as maximum speed
  • Range: 411 nmi (473 mi, 761 km) no reserves, at long-range cruise speed at 4,000 ft altitude
  • Service ceiling: 13,800 ft (4,200 m)
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Armament

Special Links Sikorsky CH-54/S-64 Tarhe-Skycrane

Links to Youtube & Others

The rate of manufacturing noticeably declined during the 2010s; only a dozen S-76s were delivered between 2016 and 2020. During September 2013, it was announced that the Chinese manufacturer Changhe Aircraft Industries Corporation had been contracted to produce the S-76D airframe. By 2022 April, in excess of 875 S-76s had reportedly been built.

Sikorsky S-76 utility helicopter

Development of the follow-on S-76D was subject to four years of delays due to technical problems

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Youtube Link

Early on in its commercial career, the S-76 became popular for offshore operations, such as to oil rigs. Numerous operators have either purchased or leased the type specifically to operate in this sector

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