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Sikorsky H-19 - Wikipedia, the free encyclopedia

Sikorsky H-19

From Wikipedia, the free encyclopedia

For other uses of "H19" see H19 (disambiguation).

H-19 Chickasaw
Type Utility helicopter
Manufacturer Sikorsky
Maiden flight November 10 1949
Introduced 1950
Variants Westland Whirlwind

The Sikorsky H-19, (also known as the S-55) was a multi-purpose helicopter used by the United States Army. It was also license-built by Westland Aircraft as the Westland Whirlwind in the United Kingdom. United States Navy and Coast Guard models were designated HO4S, while those of the U.S. Marine Corps were HRS.

Contents

[edit] Design and development

The H-19's first flight was on November 10, 1949 and it entered operations in 1950. Over 1,000 of the helicopters were manufactured by Sikorsky for the United States. An additional 550 were manufactured by licensees of the helicopter including Westland Aircraft, Sud-Est in France and Mitsubishi in Japan.

The helicopter was widely exported, used by many other nations, including Greece, Israel, Chile, South Africa, Denmark and Turkey.

[edit] Operational history

UH-19B at the Milestones of Flight Museum, Fox Field, Lancaster, California.  This helicopter had been operated by T&G Aviation of Chandler, Arizona, under contract to the USFS hauling firefighters and performing bucket water drops. In 1989 it was part of an exchange program where historic aircraft were provided to museums in exchange for surplus Air Force C-130s.
UH-19B at the Milestones of Flight Museum, Fox Field, Lancaster, California. This helicopter had been operated by T&G Aviation of Chandler, Arizona, under contract to the USFS hauling firefighters and performing bucket water drops. In 1989 it was part of an exchange program where historic aircraft were provided to museums in exchange for surplus Air Force C-130s.
A Sikorsky S-55B in service with Golden West Helicopters, St. Albert, Alberta, 1985
A Sikorsky S-55B in service with Golden West Helicopters, St. Albert, Alberta, 1985
Sikorsky UH-19 at the Canadian Museum of Flight 1988.The aircraft is painted as it would have looked while working on the construction of the Mid-Canada Line
Sikorsky UH-19 at the Canadian Museum of Flight 1988.The aircraft is painted as it would have looked while working on the construction of the Mid-Canada Line
UH-19B, USAF Museum
UH-19B, USAF Museum

The H-19 underwent live service tests during the Korean War beginning in 1951 as an unarmed transport helicopter. Undergoing tests such as medical evacuation, tactical control and front-line cargo support, the helicopter succeeded admirably in surpassing the capabilities of the H-5 Dragonfly which had been used throughout the Korean conflict by the Army.

In 1956, the French Air Force experimented with arming the H-19 Chickasaw aka Sikorsky S-55, then being superseded in service by the more capable Piasecki H-21 and Sikorsky H-34 helicopters. The H-19 was originally fitted with a 20-mm cannon, two rocket launchers, plus a 20-mm cannon, two 12.7-mm machine guns, and a 7.5-mm light machine gun firing from the cabin windows, but this load proved far too heavy, and even lightly-armed H-19 gunships fitted with flexible machine guns for self-defense proved underpowered.

The H-19 was also used in the early days of the Vietnam War before being supplanted by the Sikorsky H-34 Choctaw, which was based on the H-19.

[edit] Variants

YH-19
Five early production S-55s for evaluation.
H-19A
USAF version of the YH-19 powered by a 600 hp R-1340-57 engine, redeisgnated UH-19A in 1962, 50 built.
SH-19A
H-19As modified for Air-Sea Rescue, redesignated HH-19A in 1962.
H-19B
H-19A with a more powerful 700hp R-1300-3 engine, redesignated UH-19B in 1962, 264 built.
SH-19B
H-19Bs modified for Air-Sea Rescue, redesignated HH-19B in 1962.
H-19C
US Army version of the H-19A, redesignated UH-19C in 1962, 72 built.
H-19D
US Army version of the H-19B, redesignated UH-19D in 1962, 301 built.
HO4S-1
US Navy version of the H-19A, 10 built.
H04S-2
Project for rescue version for the United States Coast Guard, not built.
H04S-3
Re-engined US Navy & Canadian version with 700 hp R-1300-3 engine, redesignated UH-19F (American variant) H04S-3 (Canadian variant) in 1962, 79 built.
HO4S-3G
United States Coast Guard version of the HO4S-3, redesignated HH-19G in 1962, 30 built.
HRS-1
United States Marine Corps version of the HO4S for eight troops, 60 built.
HRS-2
HRS-1 with equipment changes, 101 built.
HRS-3
HRS-2 with a 700 hp R-1300-3 engine, became CH-19E in 1962, 105 built and conversions from HRS-2.
HRS-4
Project for HRS-3 with a 1025 hp R-1820 radial engine, not built.
UH-19A
H-19A redesignated in 1962.
HH-19A
SH-19A redesignated in 1962.
UH-19B
H-19B redesignated in 1962.
HH-19B
SH-19B redesignated in 1962.
CH-19E
HRS-3 redesignated in 1962.
UH-19F
HO4S-3 redesignated in 1962.
HH-19G
HO4S-3G redesignated in 1962
S-55
Commercial version with 600hp R-1340 engine.
S-55A
Commercial version with 800hp R-1300-3 engine.
S-55C
S-55A with a 600 hp R-1340 engine.
S-55T
Modified aircraft with a 650 shp Garrett-AIRResearch TSE331-3U-303 turboshaft and updated equipment.
S-55QT
Commercial conversion. Ultra-quiet helicopter for sight-seeing flights over the Grand Canyon.
OHA-S-55 Heli-Camper
Commercial conversions carried out by Orlando Helicopters.
OHA-S-55 Nite-Writer
Commercial conversion. Aerial advertising helicopter, fitted with a 12.2-m x (40-ft x 8-ft) array of computer-controlled lights.
OHA-S-55 Bearcat
Commercial conversion. Agricultural helicopter.
OHA-S-55 Heavy Lift
Commercial conversion. Flying crane helicopter.
QS-55 Aggressors
Commercial conversion. S-55 helicopters converted into flying targets.
OHA-AT-55 Defender
Commercial conversion. Armed military helicopter.
Whirlwind HAR21
HRS-2 for Royal Navy, ten delivered.
Whirlwind HAS22
H04S-3 for Royal Navy, 15 delivered.

Later marks of Whirlwind were built under licence.

[edit] Operators

[edit] Specifications (H-19)

H-19 at National Museum of the United States Air Force, showing unusual mounting of engine
H-19 at National Museum of the United States Air Force, showing unusual mounting of engine
UH-19B rotor head
UH-19B rotor head

General characteristics

  • Crew: 2 (pilot, copilot)
  • Capacity: 12 troops or 8 litters
  • Length: 62 ft 7 in (19.1 m)
  • Rotor diameter: 53 ft (16.16 m)
  • Height: 13 ft 4 in (4.07 m)
  • Disc area: ft² (m²)
  • Empty weight: 4,795 lb (2,177 kg)
  • Loaded weight: 7,200 lb (3,266 kg)
  • Max takeoff weight: 7,900 lb (3,587 kg)
  • Powerplant: 1× Pratt & Whitney R-1340-57 radial engine, 600 hp (450 kW)

Performance


[edit] See also

Related development

Comparable aircraft

Related lists

[edit] References

  • Duke, R.A., Helicopter Operations in Algeria [Trans. French], Dept. of the Army (1959)
  • France, Operations Research Group, Report of the Operations Research Mission on H-21 Helicopter Dept. of the Army (1957)
  • Riley, David, French Helicopter Operations in Algeria, Marine Corps Gazette, February 1958, pp. 21-26.
  • Shrader, Charles R., The First Helicopter War: Logistics and Mobility in Algeria, 1954-1962, Westport, CT: Praeger Publishers (1999)
  • Spenser, Jay P., Whirlybirds: A History of the U.S. Helicopter Pioneers, Seattle, WA: University of Washington Press (1998)

[edit] External links

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