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General Info

S-58/H34 Choctaw Manufactured 1954–1970

General information
Type Helicopter
National origin United States
Manufacturer Sikorsky Aircraft
Status In service
Primary users United States ArmyUnited States Navy
United States Marine Corps
Number built 2,340 
History
Manufactured 1954–1970 (Foreign production of derivatives and sub-types continued under license after the Sikorsky production ended.)
Introduction date 1954
First flight 8 March 1954
Developed from Sikorsky H-19 Chickasaw
Developed into Westland Wessex
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History Sikorsky 
S-58/H34 Choctaw Manufactured 1954–1970 Introduction date 1954
First flight 8 March 1954

Radial engine of a H-34 under the fuselage

In the early 1950s Sikorsky developed the S-58, an improved version of the S-55, which had enter service as the H-19 with the United States. The United States Navy issued a contract in 1952 for the S-58, entering service as the HUS-1, the Army placing a contract in 1955 as the H-34, and the Marine Corp in 1957 (as the HUS-1). In 1962 these names were standardized to H-34, with additional prefixes and letters according to that U.S. designation system. Westland had already made a version of the predecessor of the S-58, the S-55 as the Westland Whirlwind, and they would go on to make a turbine powered version of the S-56 as the Westland Wessex.

Operational history

Entering service in the 1950s, the type served numerous roles in the late 20th century.

A U.S. Coast Guard HUS-1G in 1960.
Row of Westland Wessex HU.5, 1978

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Howard Sikorsky helicopters MD

Sikorsky, a Lockheed Martin Company
S-58/H34 Choctaw Manufactured 1954–1970
Introduction date 1954 First flight 8 March 1954

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General Info

  • Crew: 2
  • Capacity: 12 troops (H-34A) / 18 troops (H-34C) / 8 stretchers
  • Length: 47 ft 2 in (14.38 m) fuselage
  • 56 ft 8.5 in (17 m) rotors turning[]
    • Height: 14 ft 3.5 in (4.356 m)
2

Powerplant

  • Max takeoff weight: 13,300 lb (6,033 kg)
  • Fuel capacity: 198–307 US gal (165–256 imp gal; 750–1,160 L)
  • Powerplant: 1 × Wright R-1820-84 Cyclone , 1,525 hp (1,137 kW) for take-off
  • 1,275 hp (951 kW) METO for 5 minutes
    • Main rotor diameter: 56 ft 0 in (17.07 m)
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Specifications

  • Maximum speed: 122 mph (196 km/h, 106 kn)
  • Cruise speed: 97 mph (156 km/h, 84 kn)
  • Range: 190 mi (310 km, 170 nmi)
  • Service ceiling: 12,000 ft (3,700 m)
  • Hover ceiling IGE: 9,600 ft (2,926 m) (H-34A)
  • °F)
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Armament

Special Links Sikorsky CH-53K King Stallion

Links to Youtube & Others

The UH-60 entered service with the U.S. Army's 101st Combat Aviation Brigade of the 101st Airborne Division in June 1979.[92] The U.S. military first used the UH-60 in combat during the invasion of Grenada in 1983.

S-58/H34 Choctaw Manufactured 1954–1970

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Youtube Link

he Sikorsky CH-53K King Stallion (Sikorsky S-95) is a heavy-lift cargo helicopter

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