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Sikorsky H-34
Sikorsky H-34
from Wikipedia

A U.S. Coast Guard HUS-1G in 1960.

Key Information

Row of Westland Wessex HU.5, 1978

The Sikorsky H-34 (company designation S-58) is an American piston-engined military utility helicopter originally designed by Sikorsky as an anti-submarine warfare (ASW) aircraft for the United States Navy. A development of the smaller Sikorsky H-19 Chickasaw (S-55), the H-34 was originally powered by a radial engine, but was later adapted to turbine power by the British licensee as the Westland Wessex and by Sikorsky as the S-58T. The H-34 was also produced under license in France by Sud Aviation.

The H-34 was one of the first successful military utility helicopters, serving on every continent with the armed forces of 25 countries. It saw combat in the Dominican Republic, Nicaragua, the Six-Day War, the Vietnam War, and the Algerian War, where the French Air Force used it to pioneer modern air assault tactics. It was the last piston-engined helicopter to be operated by the United States Marine Corps (USMC), having been replaced by turbine-powered types such as the UH-1 Huey and CH-46 Sea Knight; in the USMC, the H-34 was often called the "HUS" after its original designation in that service. A total of 2,340 H-34s were manufactured between 1953 and 1970, including the license productions in the UK and France.[1]

Although most military forces retired the H-34 by the late 20th century, the type remains in limited civil use in transport and external cargo lift roles, and some have been restored and flown as warbirds.

Development

[edit]
A U.S. Navy HSS-1 with dipping sonar deployed, in 1960.
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 entered 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).[3] In 1962 these names were standardized to H-34, with additional prefixes and letters according to that U.S. designation system.[4] 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.[4]

The Sikorsky S-58 was developed as a lengthened and more powerful version of the Sikorsky Model S-55, or UH-19 Chickasaw, with a similar nose, but with a tail-dragger rear fuselage and landing gear, rather than the high-tail, 4-post pattern. It retained the nose-mounted radial reciprocating engine with the drive shaft passing through the cockpit placed high above the cargo compartment.

The aircraft first flew on 8 March 1954. The first production aircraft was ready in September and entered in service for the United States Navy initially designated HSS-1 Seabat (in its anti-submarine configuration) and HUS-1 Seahorse (in its utility transport configuration) under the U.S. Navy designation system for U.S. Navy, United States Marine Corps (USMC) and United States Coast Guard (USCG) aircraft. The U.S. Army and Marine Corps, respectively, ordered it in 1955 and 1957. Under the United States Army's aircraft designation system, also used by the United States Air Force, the helicopter was designated H-34. The U.S. Army also applied the name Choctaw to the helicopter. In 1962, under the new unified DoD aircraft designation system, the Seabat was redesignated SH-34, the Seahorse as the UH-34, and the Choctaw as the CH-34.

Roles included utility transport, anti-submarine warfare, search and rescue, and VIP transport. In its standard configuration, transport versions could carry 12 to 16 troops, or eight stretcher cases if utilized in the MedEvac role, while VIP transports carried significantly fewer people in much greater comfort.

A total of 135 H-34s were built in the US and assembled by Sud-Aviation in France, 166 were produced under licence in France by Sud-Aviation for the French Air Force.

The CH-34 was also built and developed under license from 1958 in the United Kingdom by Westland Aircraft as the turboshaft engined Wessex which was used by the Royal Navy and Royal Air Force. The RN Wessex was fitted out with weapons and ASW equipment for use in an antisubmarine role. The RAF used the Wessex, with turboshaft engines, as an air/sea rescue helicopter and as troop transporter. Wessexes were also exported to other countries and produced for civilian use.

Operational history

[edit]
CH-37C and UH-34D of the United States Marine Corps. The H-34 was complementary to other types in US service. Nevertheless, it showed how a versatile and reliable medium helicopter could be adapted to many roles.

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

The type was internationally and commercially.

Algerian War

[edit]

The helicopters used by the French Air Force, including the Sikorsky H-34, aggregated over 190,000 flying hours in Algeria (over 87,000 for the H-21 alone) and helped to evacuate over 20,000 French combatants from the combat area, including nearly 2,200 at night. By the time the war in Algeria had ended, eight officers and 23 non-commissioned officers had been killed.

The use of armed helicopters during the Algerian War, coupled with helicopter transports which can insert troops into enemy territory, gave birth to some of the modern tactics of airmobile warfare.[5]

Vietnam War

[edit]
U.S. Marine Corps UH-34Ds over Mekong Delta
USMC helicopter in Vietnam

French evaluations on the reported ground fire vulnerabilities of the CH-34 may have influenced the U.S. Army's decision to deploy the CH-21 Shawnee to Vietnam instead of the CH-34, pending the introduction into widespread service of the Bell UH-1 Iroquois. U.S. Army H-34s did not participate in Vietnam, and did not fly in the assault helicopter role, but a quantity were supplied to the Republic of Vietnam Air Force (RVNAF). These saw little use due to a lack of spare parts and maintenance.[6]

U.S. Marine Corps UH-34Ds over Vietnam, 1965.

Its higher availability and reliability due to its simplicity compared to the newer helicopters led Marines to ask for it by name. The phrases "give me a HUS", "get me a HUS" and "cut me a HUS" entered the U.S. Marine Corps vernacular, being used even after the type was no longer in use to mean "help me out".[7]

USMC H-34s were also among the first helicopter gunships trialled in theatre, being fitted with the Temporary Kit-1 (TK-1), comprising two M60C machine guns and two 19-shot 2.75 inch rocket pods. The operations were met with mixed enthusiasm, and the armed H-34s, known as "Stingers" were quickly phased out. The TK-1 kit would form the basis of the TK-2 kit used on the UH-1E helicopters of the USMC.

An H-34 was featured in the famous early-Vietnam War Time-Life photo essay "One Ride With Yankee Papa 13", photographer Larry Burrows, which depicted stages of a disastrous combat mission in which several crew were wounded or killed.[8]

Post-Vietnam War

[edit]

The H-34 remained in service with United States Army and Marine Corps aviation units into the late 1960s; at this time it was also standard equipment in Marine Corps Reserve, Army Reserve and Army National Guard aviation units, eventually being replaced by the UH-1 Iroquois utility helicopter. Sikorsky terminated all production activities in 1968, a total of 1,821 having been built.[9] All H-34 helicopters were retired from service in the U.S. military by the early 1970s; the type having the distinction of being the last piston-engined helicopter to be operated by the Marine Corps. On 3 September 1973, the last flight of a USMC UH-34 occurred as Bureau Number 147191 which had been formally assigned to Headquarters Squadron, FMF Pacific was flown from Quantico, Virginia to MCAS New River to be placed on static display.[10][11]

France

[edit]

France purchased an initial batch of 134 Choctaws; these were shipped in kit-form from the United States and locally assembled by Sud-Aviation. Later, a further 166 were domestically manufactured by Sud-Aviation; these were operated by the[12]French Naval Aviation (Navy) and Air force.

United Kingdom

[edit]
Wessex at Ascension Island, 1982

The Wessex was used as an anti-submarine and utility helicopter with the Royal Navy and as a transport and search and rescue helicopter with the Royal Air Force. British Wessex saw action in several conflicts: Falklands, Oman, Borneo, Aden, etc.

The twin-turbine Wessex served into the 21st century, and was one of the longest serving and successful of the H-34 types.

South Vietnam

[edit]
RVNAF CH-34As at Tan Son Nhut.

Used by RVNAF 219th Squadron to insert MACV-SOG reconnaissance teams into Laos.[13] The H-34 was the primary RVNAF helicopter until replaced by the Bell UH-1 Huey.[14]

Israel

[edit]
Israeli Air Force Sikorsky S-58 (1967)

Israeli S-58s flew numerous combat missions after the end of the Six-Day War; these missions were mainly against Palestinians infiltrating Israel or against their bases in Jordan. On 21 March 1968, various S-58s participated in the Battle of Karameh, bringing Israeli troops in and out of the theatre as well as evacuating the wounded. This was the last operation of the S-58 as it was retired shortly later, having been replaced by the newer Bell 205 and Aérospatiale Super Frelon.[15]

Civilian use

[edit]
Civil S-58T powered by a Pratt & Whitney Canada PT6T Twin-Pac turbine power plant

The H-34's lift capacity was just sufficient to lift a Mercury space capsule. In 1961, the hatch of Mercury-Redstone 4 was prematurely detached and the capsule was filled with seawater. The extra weight was too much for the H-34 and the capsule, Liberty Bell 7, was emergency released and sank in deep water,[16] remaining on the ocean floor until 1999.

Sikorsky set up a production line in 1970 to remanufacture existing S-58 aircraft into the S-58T configuration, replacing the R-1820 engine with a pair of Pratt & Whitney Canada PT6T-3 Twin-Pac turboshafts; Sikorsky obtained a Federal Aviation Administration type certificate for the conversion in April 1971. The conversion enhanced safety, allowing the aircraft to continue flight after an engine failure, and greatly improved its hot and high performance; whereas the R-1820 could only provide full power up to an altitude of 700 ft (210 m), the paired PT-6s provide full power up to 6,000 ft (1,800 m), and an S-58T can fly at maximum gross weight up to 5,000 ft (1,500 m). The type certificate for the S-58T was sold to California Helicopter International in 1981.[17]

In the late 1980s and early 1990s, S-58T helicopters were operated by New York Helicopters in scheduled passenger airline service between JFK International Airport and East 34th Street Heliport, New York.[18]

S-58T of New York Helicopter at 34th Street Helicopter pad in 1987

In the early 1970s, Orlando Helicopter Airways developed a novel civil conversion of the S-55/H-19, the Heli-Camper, a campervan-like conversion—featuring a built-in mini-kitchen and sleeping accommodations for four.[19] Later in that decade, Orlando developed a larger version based on the S-58 and participated in a joint effort with popular American recreational vehicle (RV) manufacturer Winnebago Industries to market both aircraft as the Winnebago Heli-Home. The S-58 version featured a larger kitchenette, sleeping accommodations for six, a minibar, and an entertainment system; optional floats were offered for amphibious operations. The aircraft were featured in several American popular magazines and reportedly drew large crowds at RV shows and dealerships, but their high purchase price together with rising 1970s fuel prices resulted in very limited sales; production is not well documented but is estimated at only six or seven of the S-55 and S-58 versions combined.[20]

Variants

[edit]

Pre-1962 USAF/Army designations

[edit]
H-34A
U.S. Army version of the HSS-1 powered by a 1,525 hp R-1820-84, re-designated CH-34A in 1962, 359 built and 21 transferred from the U.S. Navy.
JH-34A
Designation for H-34A used for weapon tests.
VH-34A
Staff transport conversions of H-34A.
H-34B
H-34As converted with detail changes, became CH-34B in 1962.
H-34C
H-34B design with detail changes converted from H-34As, became CH-34C in 1962.
Choctaw gunship armed with XM3 armament system, 1962

US Navy designations

[edit]
XHSS-1 Seabat
Three Sikorsky S-58s for evaluation by the U.S. Navy, re-designated YHSS-1 then YSH-34G in 1962.
HSS-1 Seabat
Production Anti-Submarine model for the U.S. Navy, re-designated SH-34G in 1962, 215 built
HSS-1F Seabat
One HSS-1 re-engined with two YT-58-GE as a flying test bed, re-designated SH-34H in 1962.
YHSS-1N Seabat
One HSS-1 converted as the HSS-1N prototype, re-designated YSH-34J in 1962.
HSS-1N Seabat
Night/Bad weather version of the HSS-1 with improved avionics and autopilot, re-designated SH-34J in 1962, 167 built (an addition 75 HSS-1 airframes were built to CH-34C standard for West Germany).
HUS-1 Seahorse
Utility transport version of the HSS-1 for the U.S. Marine Corps, re-designated UH-34D in 1962, 462 built
HUS-1A Seahorse
Forty HUS-1s fitted with amphibious pontoons, re-designated UH-34E in 1962.
HUS-1G Seahorse
United States Coast Guard version of the HUS-1, re-designated HH-34F in 1962, six built.
HUS-1L Seahorse
Four HUS-1s converted for Antarctic operations with VXE-6, re-designated LH-34D in 1962.
HUS-1Z Seahorse
Seven HUS-1s fitted with VIP interior for the Executive Flight Detachment, re-designated VH-34D in 1962.

Post-1962 Tri-Service designations

[edit]
CH-34A
H-34A re-designated in 1962
CH-34B
H-34B re-designated in 1962
CH-34C
H-34C re-designated in 1962
JH-34C
Designation for CH-34C used for weapon tests.
VH-34C
Staff transport conversions of CH-34C.
HH-34D
Designation applied to aircraft given USAF serials to be transferred under MAP and MDAP.
LH-34D
HUS-1L re-designated in 1962
UH-34D
HUS-1 re-designated in 1962 and 54 new build.
VH-34D
HUS-1Z re-designated in 1962
UH-34E
HUS-1A re-designated in 1962
HH-34F
HUS-1G re-designated in 1962
YSH-34G
YHSS-1 re-designated in 1962
SH-34G
HSS-1 re-designated in 1962
SH-34H
HSS-1F re-designated in 1962
SH-34Js on the USS Essex in 1962
A VH-34D presidential helicopter (BuNo 147201) on the South Lawn of the White House in 1961
YSH-34J
YHSS-1N re-designated in 1962
SH-34J
HSS-1N re-designated in 1962
UH-34J
SH-34J without ASW equipment for cargo and training purposes.
HH-34J
Ex-USN UH-34Js operated by the U.S. Air Force
VH-34J
Staff transport conversions of SH-34J.

Canadian designations

[edit]
CH-126
Canadian military designation for the S-58B.

Thai designations

[edit]
H.4
(Thai: ฮ.๔) Royal Thai Armed Forces designation for the H-34B.[21]
H.4A
(Thai: ฮ.๔ก) Royal Thai Armed Forces designation for the S-58T.[21]

Civil variants

[edit]
S-58A
Commercial designation for basic cargo variant, certified in 1956
S-58B
Commercial designation for improved cargo variant, certified in 1956
S-58C at Schreckhof airfield in warbird livery, 2016.
S-58C
Commercial passenger transport/airliner version, certified in 1956
An S-58T performing an external load operation in Dallas, Texas.
A retired S-58T Twinpac, with its distinctive squared "nostrils" on the nose. On display at an Indonesian aviation Museum
S-58D
Commercial airliner/freighter version, certified in 1961
S-58E
Certified in 1971
S-58F
Certified in 1972 an increased maximum weight variant of the S-58B.
S-58G
Certified in 1972 an increased maximum weight variant of the S-58C.
S-58H
Certified in 1972 an increased maximum weight variant of the S-58D.
S-58J
Certified in 1972 an increased maximum weight variant of the S-58E
S-58T
Commercial conversion to turboshaft power using Pratt & Whitney Canada PT6T-3 Twin-Pac turboshaft with special nose cowling featuring distinctive twin rectangular air intakes, designations relate to original model:
S-58BT
Turboshaft-powered conversion of the S-58B
S-58DT
Turboshaft-powered conversion of the S-58D
S-58ET
Turboshaft-powered conversion of the S-58E
S-58FT
Turboshaft-powered conversion of the S-58F
S-58HT
Turboshaft-powered conversion of the S-58H
S-58JT
Turboshaft-powered conversion of the S-58J
Orlando Heli-Camper / Winnebago Heli-Home
RV conversion by Winnebago Industries and Orlando Helicopter, fitted with a Wright Cyclone R-1820-24 engine[20]
Orlando Airliner
Commercial conversion. 18-seat passenger transport helicopter.
Wessex of the Royal Navy, 1980

Licensed variants

[edit]
Westland Wessex
Licence production and development in the United Kingdom.

Operators

[edit]

Accidents and incidents

[edit]
  • 27 July 1960 Chicago Helicopter Airways Flight 698 a S-58C registered N879 crashed into Forest Home Cemetery, Forest Park, Illinois, United States with the loss of 11 passengers and two crew. The investigation concluded that the helicopter became uncontrollable as a result of structural disintegration in flight caused by a fatigue failure of the main rotor blade.[46]
  • 14 November 1971 Sikorsky SH-34J, A-062 of the Uruguayan Navy lost control after trying to lift a ground vehicle in an airshow, the helicopter fell to the ground hitting another Sikorsky SH-34J Helicopter. The broken blades flew directly into the audience of the airshow killing 8 people and severely injuring and mutilating at least 40 more. Due to the unstable political situation of the country at the time, no investigation followed the accident. Several years later, many irregularities came to light: The helicopter condition was not good when it was purchased by the Uruguayan Navy, fuel used was not appropriate, temperature on the day of the accident was too high to attempt a heavy lift, and the co-pilot of the helicopter was a fixed wing pilot with no experience in rotary wing aircraft.[47]
  • 10 July 2002 Sikorsky S-58ET, N580US (S/N 58-1673, built 1963), struck power transmission lines with its tailwheel, ripping the aircraft in two, over Brookville Lake, Indiana. One crew member was killed; the other two crew members were rescued by boaters. The aircraft was operated by Midwest Helicopter Airways of Hinsdale, Illinois, and registered to Midwest Truxton International of Burr Ridge, Illinois. "Based on interviews with witnesses and the surviving pilots, there was no indication of any mechanical failure," said SGT. Steve Comer of the Indiana State Police. NTSB Accident Report #CHI02FA189 [48]
  • 13 March 2011 Sikorsky S-58ET, N33602, suffered an engine failure, descended and veered off the side of an office building in El Segundo, California while lifting an external air conditioning unit from the roof. The commercial pilot was seriously injured and the helicopter was substantially damaged and consumed by a post-impact fire. The helicopter was registered to Heli Flight, Inc., and operated by Aris Helicopters.[49]

Aircraft on display

[edit]
Sikorsky UH-34D Seahorse in National Air and Space Museum

Canada

[edit]

Chile

[edit]

France

[edit]
  • HSS-1, No. 182, is on display at the Base d'aéronautique navale d'Hyères, the military part of the Toulon–Hyères Airport in France.[53] Serving until 1977 with 31F squadron, it was one of the last operational H-34's in French Naval Aviation. Now restored, No. 182 is displayed in the typical navy blue color of the French navy's helicopters of this time period.[54]
H-34 of the Heer

Germany

[edit]

Indonesia

[edit]

Netherlands

[edit]
  • A former Royal Netherlands Navy SH-34J Seabat bearing the markings of number 134 operating from Valkenburg naval air station is on display with folded rotor blades and tail in the newly opened "Nationaal Militair Museum" situated at the former airbase of Soesterberg. Previously the aircraft was displayed in the National Air Force museum at Kamp Zeist which has since closed down.[64]

Thailand

[edit]

Philippines

[edit]
A Sikorsky H-34 helicopter on display at the Philippine Air Force Aerospace Museum in Manila.

United States

[edit]
UH-34D at the Cavanaugh Flight Museum, Texas
VH-34C of the Presidential Fleet. In service with the head-of-state it would have gone by callsign "Army One"; since 1976 only "Marine One" is used.
Another view of the VH-34C at Pima Museum
H-34 at Pacific Coast Air Museum, in California, USA

Specifications (H-34 Choctaw)

[edit]

Data from Jane's All the World's Aircraft 1958-59[121]

General characteristics

  • 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[citation needed]
  • Height: 14 ft 3.5 in (4.356 m)
  • Empty weight: 7,646 lb (3,468 kg)
  • Gross weight: 11,867 lb (5,383 kg)
  • 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)
  • Main rotor area: 2,463 sq ft (228.8 m2) *Blade section:NACA 0012[122]

Performance

  • Maximum speed: 122 mph (196 km/h, 106 kn) [123]
  • Cruise speed: 97 mph (156 km/h, 84 kn) [123]
  • 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)
  • Hover ceiling OGE: 5,500 ft (1,676 m) (H-34A)
  • Rate of climb: 1,500 ft/min (7.6 m/s) at sea level
  • Vertical rate of climb: 600 ft/min (3.05 m/s) at sea level

Armament

Notable appearances in media

[edit]

See also

[edit]
The ill-fated Piasecki PA-97, used 4 modified H-34s with a blimp

Related development

Aircraft of comparable role, configuration, and era

Related lists

Notes

[edit]

Bibliography

[edit]

Further reading

[edit]
[edit]
Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
The Sikorsky H-34 (company designation S-58) is a piston-engined military developed by the American manufacturer in the early , initially designed to meet a requirement for an advanced platform. Powered by a single Wright R-1820-84 Cyclone nine-cylinder delivering 1,525 horsepower, it features a four-bladed main rotor with a 56-foot and an anti-torque three-bladed , enabling a maximum speed of approximately 123 and a service ceiling of 12,400 feet. The helicopter has a fuselage length of 47 feet 2 inches, a height of 14 feet 4 inches, an empty weight of 7,900 pounds, and a of 14,000 pounds, with capacity for a crew of two (pilot and co-pilot/observer) plus up to 16 troops, 12 stretchers for , or equivalent cargo loads such as 8,000 pounds externally. Its range extends to about 350 miles with standard fuel, though auxiliary tanks could increase this for specific missions. Development of the H-34 began as a private venture by Sikorsky in 1952, evolving from the earlier S-55 design but with a larger and more powerful engine to address limitations in anti-submarine capabilities of prior models like the HO4S. The prototype, designated XHSS-1 Seabat, conducted its maiden flight on March 8, 1954, at Sikorsky's facility in , demonstrating improved stability and payload over predecessors. Initial production orders followed in 1955, with the U.S. adopting it as the HSS-1 for shipboard ASW operations equipped with and depth charges, while the U.S. Marine Corps received the HUS-1 variant for utility and assault roles. The U.S. Army designated it the H-34 for troop transport and cargo duties, and it was also produced under license in by Sud-Aviation starting in 1958, leading to a total of 2,108 units built worldwide between 1953 and 1970. The H-34's operational history spans multiple conflicts and roles, marking it as one of the last major piston-powered helicopters before the era dominated designs. It saw early combat with French forces during the and its first U.S. deployment in in 1962, where the UH-34D became the Marine Corps' primary medium-lift for troop insertions, resupply, medevac, and support armed with machine guns or pods. Hundreds of H-34s, primarily UH-34Ds, served with U.S. Marine Corps units in , logging thousands of flight hours despite vulnerabilities like magnesium skin prone to corrosion and fire; it was gradually phased out by models such as the UH-1 and CH-46 Sea Knight by the late 1960s. Beyond U.S. service, the was exported to more than 25 nations, including operations in the , , and various Cold War-era missions, with some variants adapted for search-and-rescue (HH-34) or VIP transport (VH-34). Key variants include the naval HSS-1/HSS-1N Seabat for ASW, the Marine HUS-1/HUS-1A for amphibious assault, the Army CH-34C for , and international models like the French SA 321 Super Frelon precursor or Japanese S-58J. While its piston engine limited performance compared to later helicopters, the H-34's robust all-metal construction, amphibious capabilities in some versions, and versatility established it as a foundational utility platform, influencing subsequent Sikorsky designs like the SH-3 . Production ceased in 1970, but preserved examples remain in museums and occasional civilian use, underscoring its historical significance in rotary-wing aviation.

Design and development

Origins and requirements

Following , the U.S. Navy and sought a versatile medium to succeed early models like the Sikorsky S-55 (H-19 ), focusing on roles in (ASW), troop transport, and general utility operations. The Navy, in particular, initiated a competition in January 1950 for a dedicated ASW helicopter capable of carrying a pilot, copilot, equipment, and ordnance while operating from small deck ships. This requirement emphasized reliable piston-engine performance over nascent turbine technology, prioritizing proven radial engines for durability in maritime environments. The shared similar needs for enhanced troop and cargo lift in tactical scenarios, driving demand for a design that could handle greater payloads and longer ranges than predecessors. Igor Sikorsky's team at initiated the S-58 as a private venture in early 1952, building on the S-55's success to anticipate military needs. Development proceeded with company funds until the U.S. Navy awarded a contract on 30 June 1952 for four XHSS-1 prototypes under the ASW program, following the 1950 competition where Sikorsky's design was selected after issues with Bell's competing HSL. Sikorsky's design philosophy favored a single main with a configuration over tandem rotors, as outlined in his 1949 paper, arguing that the single- layout offered superior efficiency, simpler mechanics, and better scalability for medium-sized helicopters across all operational sizes. After evaluating tandem options, the team selected a four-bladed main (56 feet in diameter) and a four-bladed for improved lift and stability. The powerplant chosen was the radial piston engine, valued for its reliability and marine-adapted heritage from aircraft, rated at 1,525 shaft horsepower. The design achieved an internal payload of up to 16 troops or equivalent , with external load capacity reaching 4,000 pounds via sling, and a range exceeding 300 miles—significant advancements over the H-19 Chickasaw's roughly 10-troop limit and shorter under load. These improvements addressed the military's push for a that could transport combat-equipped squads or sustain ASW patrols without frequent refueling, with a maximum gross weight of 14,000 pounds.

Prototype development and testing

In June 1952, the U.S. Navy awarded a contract to develop four prototypes of a new , designated the XHSS-1, as a more capable successor to the HO4S. Construction of the prototypes began shortly thereafter at in , with the first aircraft completing assembly by late 1953. The maiden flight of the first XHSS-1 prototype occurred on March 8, 1954, at Bridgeport Municipal Airport, piloted by Sikorsky's chief Dimitry D. ("Jimmy") Viner. Viner, a veteran Sikorsky and nephew of , conducted the initial 20-minute flight, during which the aircraft demonstrated stable handling with its single Wright R-1820-84 Cyclone rated at 1,525 shaft horsepower driving a four-bladed main rotor. The prototypes featured an all-metal fuselage, landing gear, and a pylon-mounted , designed for shipboard operations with folding rotors and tail boom. Over the following year, the four XHSS-1 prototypes accumulated extensive flight hours in company and government testing to validate performance, stability, and anti-submarine capabilities, including dunking sonar integration and hovering accuracy. These evaluations confirmed the design's suitability for naval service, leading to production approval and the first production HSS-1 Seabat entering U.S. Navy service in 1955 for anti-submarine warfare roles. Parallel to Navy development, the U.S. evaluated the S-58 design and placed an initial order in 1955, designating it the H-34 for utility transport duties. The 's early adopters received the first H-34A aircraft in April 1955, featuring modifications such as reinforced cabin flooring for troop and cargo carrying, external rescue hoists, and provisions for mounts to support search-and-rescue, , and general utility missions. These adaptations emphasized the helicopter's versatility beyond its naval origins, with over 400 H-34As ultimately delivered to units by the late 1950s.

Production history and upgrades

Serial production of the Sikorsky H-34, designated S-58 by the manufacturer, commenced in 1954 at the company's primary facility in , following the successful testing of prototypes. Sikorsky manufactured approximately 1,800 units through January 1970, serving U.S. military branches including the , , Marine Corps, and , as well as export orders. Licensed production expanded the type's availability internationally; Sud-Aviation in assembled 135 kits from U.S. components and built an additional 166 units locally, primarily for French forces. In the , produced nearly 400 examples under license, though these were adapted as the turbine-powered variant, sharing the core airframe design. Overall, the H-34 family exceeded 2,300 units, reflecting its role as a versatile during the piston-engine era. Mid-life improvements enhanced the H-34's capabilities amid evolving operational demands through the 1950s and . Early production models featured the Wright R-1820-84 radial engine rated at 1,525 shaft horsepower, an uprating from prototype configurations that improved payload and performance for transport and anti-submarine roles. In 1957, Sikorsky tested an HSS-1F prototype with two engines, demonstrating the potential for turbine power in future designs. During the , several H-34s underwent conversions for VIP transport, including the VH-34D equipped with executive interiors for presidential and staff duties, such as those operated by the Executive Flight Detachment. U.S. production wound down in the late as turbine-powered successors like the SH-3 Sea King entered service, marking the shift to more efficient designs. However, export deliveries and civilian conversions persisted into the 1970s, with airframes adapted for commercial utility, , and passenger services by modifying surplus units. Economic factors included a of approximately $250,000 in mid-1950s dollars, making it a cost-effective option for medium-lift requirements at the time.

Operational history

U.S. military service

The Sikorsky H-34 entered service in 1955 as the HSS-1 Seabat, primarily for (ASW) operations. Equipped with the AN/AQS-4 dipping , it enabled detection and tracking of submerged submarines by lowering the sonar transducer into the water from hovering positions, marking a significant advancement in shipborne ASW capabilities. The HSS-1 operated from carriers in both the Atlantic and Pacific fleets, typically in squadrons of four to six aircraft alongside fixed-wing S-2 Tracker aircraft, and could carry two homing torpedoes (such as the Mk 43 or Mk 44) for attack roles, with a crew of four including two pilots and two sonar operators. Over 385 HSS-1 and HSS-1N variants were delivered to the , serving until the early when they began to be phased out in favor of the more capable , though some remained in utility roles (redesignated SH-34G/J) until 1974. The U.S. Marine Corps adopted the H-34 as the UH-34D Seahorse starting in 1962, deploying it extensively in for assault support, troop transport, and during the war's early years through 1969. The UH-34D served as the primary medium-lift for Marine squadrons like HMM-362, which arrived at Soc Trang in the in April 1962 as part of Operation Shufly, the first major U.S. Marine commitment to . In operations such as —the first major U.S. offensive of the war in August 1965 near Van Tuong—the UH-34Ds conducted critical troop insertions and extractions under intense enemy fire, supporting the in amphibious assaults and resupply missions. These s frequently encountered ground fire, resulting in battle damage to nearly every UH-34 involved in high-threat insertions and occasional losses, contributing to the type's high operational tempo and vulnerability in contested environments. The U.S. designated its H-34 as the H-21 Shawnee's successor in and roles under the name , employing it from the mid-1950s through the mid-1960s for transport, reconnaissance, and humanitarian missions. A notable deployment occurred during the 1964 , where H-34s supported evacuation operations amid the , conducting challenging s in remote jungle areas to extract American and European civilians from hostage situations. By 1965, the began transitioning frontline duties to the more versatile (Huey), particularly for Vietnam-bound units, relegating the H-34 primarily to reserve and units into the late 1960s. The U.S. operated the H-34 as the HH-34D (initially HUS-1G) from 1959 onward, focusing on medium-range search-and-rescue (SAR) missions along coastal and offshore areas. With its amphibious capabilities and ability to carry rescue equipment, the HH-34D extended SAR coverage for maritime distress calls, including responses to severe weather events like the hurricanes of the , where it facilitated hoist operations and personnel recoveries in rough seas and flooded regions. The helicopter's service in SAR emphasized its reliability in adverse conditions, contributing to numerous lifesaving efforts before being supplemented by newer models in the late .

International military service

The French military was an early and extensive adopter of the H-34, acquiring 261 units for the Aéronavale () and Armée de l'Air (French Air Force), primarily in the HSS-1 and HUS-1 variants. These helicopters played a pivotal role in the from 1956 to 1962, marking one of the first large-scale uses of rotary-wing in operations. Assigned to squadrons such as 20S, 31F, 32F, and 33F, the H-34s conducted (ASW) patrols, (SAR), and troop transport missions, accumulating over 190,000 flight hours in rugged terrain. They provided critical logistical support, including rapid insertion of paratroopers and supplies during urban engagements like , where armed H-34s offered fire support and air cover for ground forces, influencing modern helicopter tactics. The licensed production of the H-34 through , developing the turbine-powered variant from the base S-58 design starting in 1959. Over 380 helicopters were built, with the Royal Navy's operating more than 140 in anti-submarine, utility, and SAR roles through the 1970s. These aircraft supported naval operations worldwide, including troop transport and ASW from carriers, and remained in service during the 1982 , where they performed vital SAR and logistical tasks amid harsh South Atlantic conditions. The (IAF) employed over 30 SH-34 helicopters, a locally designated variant of the H-34, primarily for and transport during major conflicts. In the 1967 , the SH-34s facilitated rapid casualty evacuation under intense combat, contributing to the IAF's operational tempo despite Arab air threats. During the 1973 , they achieved approximately 90% availability rates, enabling medevac missions across front lines even as Arab forces targeted Israeli assets, underscoring the type's reliability in high-threat environments. Other nations integrated the H-34 into their forces for diverse military applications. South Vietnam's Air Force (VNAF) received over 140 H-34 Choctaws, which supported operations throughout the until the 1975 , including troop and with the 219th Special Operations Squadron. In , the Royal Thai Air Force operated 63 H-34s from 1962 to 1980, employing them in anti-insurgency campaigns against communist forces in the and 1970s. ’s acquired 145 H-34G models in the early for and medevac across its army, air force, and navy branches, retiring them by 1975 after routine duties. briefly utilized a small number of H-34s in the for utility roles before phasing them out, with surviving examples now in museums.

Civilian operations

The Sikorsky S-58, the civilian designation for the H-34, received FAA certification for commercial airline service in August 1956, enabling its initial use in passenger and utility transport roles. Following military retirement, numerous surplus airframes were converted for non-military applications, with Sikorsky establishing a production line in 1970 to remanufacture them into the turbine-powered S-58T configuration under a issued in April 1971. Over 100 such conversions were performed across various operators, primarily for heavy-lift tasks including oil rig personnel transport, , and in the United States and ; for instance, Keystone Helicopters employed S-58s for log extraction in rugged terrain. By the 1970s, the S-58 had been adapted for , with modifications including internal or belly-mounted tanks for water or retardant delivery. Helicopters retrofitted several units with 270-U.S. (1,022-liter) internal tanks equipped with gating systems for precise drops, while earlier U.S. Marine Corps tests in 1958 demonstrated 150-U.S. (568-liter) external tanks on H-34 variants for forest fire suppression. These adaptations supported operations in wildfire-prone areas, including , where S-58s contributed to suppression efforts through the 1990s before larger helicopters assumed primary roles. In offshore oil support, the S-58T proved reliable for crew transport and light cargo in challenging marine environments from the to the , particularly in the where early operations utilized surplus military models. Turbine conversions enhanced performance, with operators like Chevron employing dedicated units; stability was improved through aftermarket kits addressing dynamic rollover risks during deck landings. In the during the 1970s, UK-based firms such as integrated S-58s into emerging oilfield logistics, supporting rig access amid harsh weather. Into the 2020s, a small number of airworthy S-58Ts continue niche civilian operations under FAA Part 135 regulations for on-demand charter services, including stunts—such as reenactments in productions like those documented in the Internet Movie Plane Database—and occasional museum demonstration flights. Examples include flyable examples at the , maintained for educational flights while complying with commercial airworthiness standards.

Variants

U.S. military variants

The U.S. employed the Sikorsky H-34 (S-58) in various configurations prior to the 1962 Tri-Service designation system, primarily for utility, transport, and roles across the Army, , and Marine Corps. These early variants featured the radial engine and were adapted for specific service needs, with production emphasizing durability for amphibious and troop-carrying operations. The HSS-1 Seabat served the U.S. as an helicopter, entering service in 1954 with dipping and capabilities; 215 units were built. The U.S. Army's H-34 , introduced in 1955, functioned as a utility transport capable of carrying 16 troops or cargo, with 359 examples produced and an additional 21 transferred to the . For the U.S. Marine Corps, the HUS-1 provided assault support and troop transport, with 462 units constructed, some fitted with amphibious pontoons as the HUS-1A. Following the 1962 redesignation to unify aircraft nomenclature across services, H-34 variants received updated prefixes reflecting their roles: U for utility, S for anti-submarine, H for , and V for staff transport. The Marine Corps' UH-34D, a redesignation of the HUS-1 (totaling 462 units), became the primary troop transport in Vietnam, with enhancements including reinforced airframes and improved for the conflict. The Navy's SH-34G, derived from the HSS-1, continued in reserve units for through the 1970s, allocated for training and operational support. The U.S. operated the HH-34F (redesignated from HUS-1G) for missions starting in the 1960s, acquiring 6 units equipped with rescue hoists, auxiliary fuel tanks for extended range, and night-flying provisions. Specialized modifications expanded the H-34's versatility in combat and executive roles. The UH-34J, an upgraded UH-34D variant, incorporated door-mounted machine guns for and defensive fire during Vietnam troop extractions, serving with Marine squadrons like HMM-364. For VIP transport, the VH-34 (based on the H-34A/HUS-1) equipped the U.S. Army's Executive Flight Detachment and Marine HMX-1 squadron from 1958, carrying presidents Eisenhower and Kennedy with luxurious interiors; 8 units were produced and redesignated VH-34A in 1962. Overall, U.S. military procurement totaled around 1,100 H-34s across services, with most retired by 1973 in favor of turbine-powered successors like the UH-1 and SH-3, though reserves retained some into the late 1970s.
VariantServiceRoleQuantityKey Features
HSS-1 SeabatASW215Dipping , torpedoes; entered service 1954
H-34 Utility transport359Troop/cargo carrier; 1955 introduction
HUS-1 Assault support462Amphibious options; troop capacity 16
UH-34DTroop transport462 (redesignated from HUS-1)Vietnam enhancements; redesignated 1962
SH-34G ReservesASWN/A (derived from HSS-1)/weapons; phased out 1970s
HH-34FSAR6Rescue hoist, extended range; 1960s service
UH-34JArmed transportN/A (modified from UH-34D)Door guns for Vietnam
VH-34A/VIP8Presidential interiors; 1958-1960s

International and licensed variants

The was a British-licensed turbine-powered development of the Sikorsky H-34, produced by from 1958 to 1966, with approximately 140 units built primarily for and service. The Wessex HAS.1 variant, entering service in 1960, was adapted for with dipping and AS.12 wire-guided missiles, while the HCC.2 served in a VIP transport role for the royal family. Some later models incorporated the Rolls-Royce Gnome engine for improved performance over the original piston powerplant. In France, Sud-Aviation assembled 135 H-34s from U.S.-supplied kits starting in 1958 and produced an additional 166 under license through the , primarily for the and during the . These included the SA 158 designation for roles, with later developments like the S-58T turbine conversions featuring the Turboméca Turmo IIIC for enhanced reliability in hot climates; the SA 321 Super Frelon was developed as a successor to the H-34 in French service. Over 150 units were deployed in for troop and armed duties, often fitted with 20 mm cannons for . French designations evolved in the , with some reclassified as SA 181 for export and utility variants. Canada acquired three Sikorsky H-34A Choctaws, designated CH-126, for the Royal Canadian Air Force in the early , primarily for search-and-rescue and utility missions with No. 448 Squadron at RCAF Station Trenton. Thailand operated around 10 UH-34D Seahorses in the , designated AU-34 for anti-guerrilla operations against communist insurgents, with modifications for tropical environments including reinforced landing gear. Israel received 30 SH-34s in the , adapted with desert armor kits, sand filters, and reinforced undercarriages for operations in arid conditions during conflicts like the . Indonesia acquired approximately 10 H-34s, including S-58T models, in the for the , used in transport and reconnaissance roles during regional tensions. Overall, licensed production of H-34 derivatives totaled around 300 units across and the , supporting exports to over 20 nations for military utility roles.

Civilian variants

The civilian variants of the Sikorsky S-58 were adapted primarily from airframes for commercial , passenger transport, hauling, and specialized roles such as and offshore support, with FAA type certifications emphasizing safe operation in non-military environments. S-58B: This basic civil model received FAA type certification on August 2, 1956, and featured a standard configured for five to seven passengers on foldable benches or equivalent space, suitable for executive transport and general tasks. The variant retained the R-1820 but incorporated civil-specific modifications for service, with early operators including Chicago Helicopter Airways and . S-58C: Certified by the FAA on March 10, 1959, this cargo-oriented variant extended the cabin by 28 inches to increase internal volume, enabling configurations for up to eight passengers or additional freight while maintaining the utility focus of the S-58B. It was designed for heavy-lift commercial applications, including construction site material placement and external load transport. S-58T: Introduced as a (STC SH71EA) approved by the FAA on April 15, 1971, this turbine-powered conversion replaced the radial engine with a PT6T-3 Twin-Pac rated at 1,800 shp, enhancing hot-and-high performance and fuel efficiency for demanding civil operations. A total of 146 airframes underwent the upgrade through Sikorsky kits or third-party conversions between 1971 and 1977, with later models using the uprated PT6T-6 at 1,875 shp. Firefighting adaptations of the S-58T emerged in the and , including helitanker configurations developed by firms like Orlando Helicopter Airways, which added belly-mounted tanks for water or retardant drops and received FAA certification for roles. These modifications supported rapid response in wildland fire suppression, with several dozen S-58T variants active in such service by the early 2000s. S-58ET: This export civil turbine variant, based on the S-58E , incorporated the PT6T-3 Twin-Pac with a modified and was certified for international commercial use, particularly in offshore and heavy-lift tasks. It represented an adapted version of the S-58T for non-U.S. markets, emphasizing durability in remote and maritime environments. Overall, approximately 200 S-58 were converted or produced for civilian applications, drawing from , with the final major certifications occurring in the as upgrades extended the type's commercial viability.

Operators

Military operators

The Sikorsky H-34 helicopter was operated by numerous military organizations worldwide, primarily for utility, transport, , and roles. United States
  • United States Navy: Operated the HSS/SH-34 variants from 1955 to the 1970s, with 385 aircraft in service as the primary anti-submarine platform until the introduction of the SH-3 .
  • United States Marine Corps: Operated the UH-34 variant from 1955 to 1970, procuring 502 aircraft including 462 UH-34Ds and 40 UH-34Es for assault and utility missions.
  • United States Army: Operated the H-34 variant from 1955 to the early 1970s, with 369 aircraft in inventory by 1962 including 179 H-34As and 190 H-34Cs for troop transport.
  • United States Coast Guard: Operated the HH-34 variant from 1959 to 1962, with 6 aircraft acquired for operations.
France
  • French Navy (Aéronavale): Operated the HSS-1 variant from 1956 to 1979, with 61 aircraft used for and transport, including during the .
  • French Air Force (Armée de l'Air): Operated the H-34 variant in the , with approximately 200 aircraft for utility roles.
Other countries
  • : Operated the H-34 from 1958 to 1969, with 24 aircraft for transport and combat support.
  • : Operated the H-34 from 1963 to 1975, with 140 aircraft supplied under U.S. aid for operations.
  • : Operated the H-34 from 1962 to the 1980s, with 25 aircraft for utility and roles.
  • : Operated the H-34 in the , with 6 aircraft for training and transport.
  • : Operated the H-34 in the , with 10 aircraft for general utility.
  • Japan (Self-Defense Forces): Operated the S-58J variant from 1964, with 53 aircraft for utility and transport roles.
Former operators
  • Royal Canadian Air Force: Operated 3 aircraft, retired in the 1970s.
  • : Operated 4 aircraft in the .

Civilian operators

In the United States, () was a major civilian operator of the Sikorsky S-58, incorporating the type into its fleet in for offshore oil and gas support in the . By 1959, PHI had added multiple S-58 helicopters, expanding operations throughout the with bases along the Gulf Coast and internationally, serving the growing demands of the until at least the 1990s. New York Airways operated S-58 helicopters for urban passenger shuttle services between , , and Idlewild (now JFK) Airport starting in 1956, after purchasing seven units in 1955. The airline configured the aircraft for up to 12 passengers, marking an early commercial application of the type in short-haul commuter transport during the and , before ceasing operations in 1979. S-58 variants have also seen use by U.S.-based film production companies for aerial stunts and filming since the . For example, Helicopters operated an S-58T known as "Screaming Mimi" for the 1980s television series Riptide, performing dynamic flight sequences. Similar conversions continue in Hollywood productions through the , leveraging the helicopter's robust airframe for cinematic heavy-lift and utility shots. In Canada, Okanagan Helicopters (later part of ) utilized S-58 helicopters for provincial services, retrofitting at least one with an internal 270-U.S. gallon belly tank for in starting in the 1970s. The aircraft supported ongoing efforts, including water drops and crew transport, as demonstrated by operations at British Columbia Forest Service bases. In , Heli-Union in operated S-58ET conversions for utility missions, including an example registered F-BVJI based at in the early 1980s. The company maintained a small fleet of around five such for and support roles, with ongoing utility applications into recent years under its integration with technics. Globally, S-58 variants remain in limited civilian service as of 2025, primarily for heavy-lift and utility tasks with specialized operators, though exact numbers are not publicly detailed by authorities.

Incidents and accidents

Notable military incidents

During the , the Sikorsky UH-34D served as a primary transport for U.S. Marine units, experiencing heavy exposure that resulted in significant losses. A total of 176 UH-34D helicopters were destroyed between 1962 and 1970, with many attributed to enemy fire during operations such as troop insertions and medical evacuations. One notable incident occurred on March 28, 1965, when UH-34D BuNo 148812 from Marine Medium Squadron 163 (HMM-163) was shot down by ground fire near the ; the pilot, Capt. William D. Reynolds, survived the crash but was fatally struck by the main rotor blade while fleeing the wreckage. These losses underscored the vulnerability of piston-engined helicopters to small-arms fire and prompted improvements in armored seating and tactics for subsequent missions. Overall, Marine records indicate 134 UH-34Ds downed by a combination of enemy action and operational accidents during the conflict. In the , French Air Force H-34s (designated HSS-1 or Pirate) pioneered roles but faced environmental challenges in desert operations. On May 12, 1958, H-34A serial 397 crashed at Djebel Bou Anouane near Batna, , resulting in the aircraft's destruction; the exact cause was not publicly detailed, but such incidents contributed to 31 French helicopter crew fatalities across the campaign. Another loss occurred on February 15, 1958, when H-34A SA-6 was destroyed by fire during a gunship mission, highlighting reliability issues with the in high-temperature conditions. The H-34 also saw demanding service in operations during the 1964 , where U.S. Army variants supported evacuations amid rebel threats, though specific losses were limited. A related example from British service involved the license-built Westland Whirlwind HAS.7 XN361, which ditched in the Eastern , approximately 1,150 miles west of , , on February 13, 1962, after a failure; all three crew members were rescued unharmed. These events collectively led to enhanced pilot training on mechanical failure responses and terrain avoidance.

Civilian accidents

The Sikorsky H-34 (S-58) has been involved in civilian accidents, with a common factor according to analyses of U.S. civil data. These mishaps often occurred during commercial passenger, offshore support, and utility operations, underscoring challenges with aging piston and turbine-converted airframes. A prominent early case of main failure took place on July 27, 1960, when Helicopter Airways Flight 698, an S-58C (N879), lost a due to metal fatigue during approach to Midway Airport in , . The helicopter disintegrated mid-air and crashed into Forest Home Cemetery in Forest Park, killing all 13 on board. The investigation revealed inadequate maintenance as the root cause, prompting the to mandate enhanced non-destructive testing and inspection intervals for S-58 rotor blades to prevent fatigue cracks. In offshore environments, an S-58ET (G-BCRU) operated by ditched near the BP Forties Charlie platform in the on April 21, 1976, after detachment due to tail gearbox failure. Of the 10 aboard, 9 survived, but 1 perished; the UK's recommended improvements to tail gearbox maintenance and design for S-58 variants supporting shuttles. Firefighting missions highlighted overload risks in turbine-converted models, as seen in the January 28, 1994, crash of an S-58T (N4995G) in San Jose, California, during external load operations. The external load became entangled in a power line, causing the pilot to lose control and collide with a high-rise building, resulting in a fatal impact that killed the sole occupant. The NTSB report emphasized the hazards of low-level operations near obstacles, influencing FAA updates to operational procedures for S-58T airframes in utility roles. More recently, on May 15, 2024, an S-58ET (C-GFXP) rolled onto its side during taxiing training at Burlington Executive Airport, , , after the right wheel hit a grass mound, resulting in substantial damage but no fatalities—the pilot sustained serious injuries. The Transportation Safety Board of 's investigation is ongoing for this ground handling incident on the aging turbine conversion. Turbine conversions like the S-58T have generally improved reliability over original engines but require vigilant to mitigate such risks.

Preservation

Surviving airframes

Sikorsky H-34 airframes remain extant worldwide, either airworthy or in storage, based on data from aviation registries including the FAA and EASA. Attrition has occurred through scrapping and failed restorations due to increasing parts scarcity for the aging design. Restoration efforts continue among private owners, particularly in the United States, where several projects involve converting piston-engined H-34s to turbine powerplants like the for improved reliability and use in flyable displays. Non-flying H-34 airframes serve roles such as ground-based instructional use at flight schools and technical training facilities. Preservation faces significant challenges from the obsolescence of the R-1820 , with aftermarket overhaul costs around $50,000 per unit due to limited availability of specialized components and expertise.

Aircraft on display

Several notable examples of the Sikorsky H-34 and its variants are preserved on static display or in flyable condition at museums and aviation sites around the world, showcasing its historical roles in military operations, , and .
The UH-34D , configured to depict its use during in in August 1965, is on display at the National Museum of the Marine Corps in . An HH-34J , originally a HSS-1 antisubmarine converted for Reserve , is exhibited at the Pacific Aviation Museum Pearl Harbor in , . Additional U.S. examples include a UH-34D at the USS Hornet Sea, Air & Space Museum in , highlighting its Vietnam-era personnel transport and assault capabilities, and a VH-34C at the in .

A Sikorsky S-58, assembled locally by Sud-Aviation and marked to represent service during the , is on static display at the Musée de l'Air et de l'Espace at Paris-Le Bourget Airport. An HSS-1 variant is preserved at the Musée de l'Aéronautique Navale in Rochefort, dedicated to history.

The Westland-built HAS.7, a licensed variant used by the for anti-submarine duties, is on display at the in Yeovilton, . An RAF HAR.10 example, employed for , was recently restored and relocated to the RAF Museum Midlands in Cosford, , after prior exhibition at the Midland Air Museum in .
Other Countries
In Canada, an H-34C is stored and displayed at the Reynolds-Alberta Museum in , . preserves an SH-34 variant at the on near . In , an AU-34 utility helicopter is exhibited at the Royal Thai Air Force Museum in Don Mueang, Bangkok. Additional examples, typically one or two per country, are held in military museums in (such as the H-34G at the Flugwerft Schleissheim near ), the , , , and the , often representing local licensed production or operational service. Dozens of H-34 airframes are on public display worldwide across these and other locations.

Specifications and performance

General characteristics

The Sikorsky H-34 Choctaw was a medium-lift typically operated by a crew of two, consisting of a pilot and co-pilot or observer. It had a capacity for 12 to 18 troops or up to eight stretchers for roles. The featured an all-metal construction with some magnesium skin components for weight reduction, and a four-bladed all-metal main rotor system along with a four-bladed . Overall length measured 56 feet 8.5 inches (17.28 m), with the length at 46 feet 9 inches (14.25 m); the main rotor diameter was 56 feet (17.07 m), and height to the rotor hub was 15 feet 11 inches (4.85 m). The helicopter had an empty weight of 7,900 pounds (3,583 kg) and a of 14,000 pounds (6,350 kg). Power was provided by a single R-1820-84 nine-cylinder air-cooled radial piston engine rated at 1,525 horsepower (1,137 kW). Internal fuel capacity totaled approximately 300 US gallons (1,135 liters), distributed across forward, center, and aft tanks. Optional armament included provisions for two 7.62 mm M60 machine guns mounted as door guns for defensive fire.

Armament and avionics

The Sikorsky H-34 military variants featured no standard fixed armament, but provisions allowed for defensive and offensive weaponry depending on the mission. Utility models like the UH-34 included mounts for two 7.62 M60 machine guns, each with 500 rounds per gun, typically positioned at side doors for during troop or search-and-rescue operations. In service with the U.S. Marine Corps, some UH-34Ds were adapted as gunships under the "Stinger" configuration, mounting two 2.75-inch rocket pods—each with seven tubes—alongside the M60 guns for , though these setups were phased out due to structural limitations. An external cargo hook with a 5,000-pound capacity was standard on utility variants, enabling sling-load of external loads such as or equipment. For (ASW) roles, primarily fulfilled by the U.S. Navy's HSS-1 Seabat, the H-34 incorporated specialized equipment including sonobuoy launchers for deploying passive acoustic sensors to detect submarines. These helicopters could carry two Mk 44 homing torpedoes (or earlier Mk 23 variants) in internal bays for engaging detected threats, supported by an system with automatic stabilization for precise hovering during weapon deployment. In the , the HSS-1N variant integrated the AN/AQS-4 dipping , a towed active/passive lowered into the water from a hovering position to localize submerged targets. Basic on early H-34 models supported (IFR) operations with an (ADF) for non-directional beacon navigation, (VOR) receivers for en-route guidance, and a gyroscopic for heading reference. Later upgrades, particularly on and Vietnam-era variants from the mid-1960s, added UHF/VHF communication radios for secure voice links and a for low-level height measurement during ASW or utility missions. Advanced electronic countermeasures (ECM) were absent until 1970s export models received retrofits for jamming enemy in conflict zones. Civilian S-58 derivatives, including the turboshaft-powered S-58T introduced in the 1970s, featured minimal focused on , with no provisions for armament. In the 2000s, many S-58T airframes underwent GPS retrofits, such as units, to enhance for and roles while maintaining compliance with modern airspace requirements.

Performance

The H-34 had a maximum speed of 123 miles per hour (108 knots, 198 km/h) and a cruise speed of 97 miles per hour (84 knots, 156 km/h). Its range was approximately 350 miles (300 nmi, 560 km) with standard fuel. The service ceiling was 12,400 feet (3,800 m), with a of 1,080 feet per minute (5.5 m/s).

Cultural depictions

In film and media

The Sikorsky H-34 has been depicted in various films, television series, and documentaries, typically highlighting its roles in military operations and early space recovery efforts. Archival footage of the helicopter appears in the 2011 miniseries , where it illustrates U.S. Marine Corps and South Vietnamese Air Force combat missions during the , including troop transport and medevac operations. It is also featured in (1987), portraying U.S. Marine Corps UH-34D helicopters in assault sequences, with used as stand-ins. Additional appearances include (1995), showing the H-34 in logistical support roles during Vietnam-era operations, and (1993), in comedic action scenes involving rescue missions. In cinematic portrayals, the H-34 features in The Right Stuff (1983), representing the utility helicopters used for spacecraft recovery in NASA's Mercury program during the late 1950s and early 1960s. The helicopter also appears in Thirteen Days (2000), providing visual context for U.S. military assets during the Cuban Missile Crisis, and in Universal Soldier (1992), as part of action sequences involving operations. These depictions emphasize the H-34's versatility as a medium-lift utility platform in Cold War-era scenarios. Television appearances include episodes of (1974–1980), where the H-34 serves as a background element in military-themed stories, and The Sixties (2014), a documentary series that incorporates historical footage to discuss aviation advancements and helicopter tactics. In video games, the H-34 is modeled as a playable in War Thunder (2012–present), allowing players to simulate its piston-engined performance in multiplayer battles based on mid-20th-century conflicts. The helicopter's cultural impact extends to scale modeling, with releasing a 1/48-scale UH-34D kit in the , which depicted the Marine Corps variant used for assault and recovery missions; this kit was reissued in later decades due to its popularity among enthusiasts.

In literature and models

The Sikorsky H-34 has been the subject of several specialized history books, primarily non-fiction works focusing on its , , and operational legacy. A comprehensive account is provided in Sikorsky H-34: An Illustrated History by Lennart Lundh, published by Schiffer in 1998, which draws on over a decade of research to detail the helicopter's development from its 1952 origins as a U.S. anti-submarine platform through its global deployments, including technical specifications, variants, and service with operators in over 20 countries. Similarly, Lundh's H-34 in Action, part of the Squadron/Signal Publications Aircraft in Action series (No. 146, 1993), emphasizes the H-34's combat roles in conflicts like the Korean and Wars, illustrated with period photographs, diagrams, and markings for modelers and historians. For operator-specific coverage, The Sikorsky H-34 in Service ( Publications, 2015) examines its adoption by the RCAF in the for search-and-rescue and transport duties, featuring over 120 images and technical data on modifications. Scale models of the H-34 remain popular among enthusiasts, with produced in multiple scales by established manufacturers to represent its diverse and configurations. In 1/48 scale, Italeri's kit depicts versions from the 1950s–1970s, including detailed rotor assemblies and interior components for assembly and painting. Gallery Models offers a modern tooling of U.S. Marine Corps UH-34D variants, noted for its accuracy over earlier reissues and inclusion of optional parts like folded rotors and gear. Trumpeter also produces 1/48 HH-34 models, emphasizing and schemes with etched metal details available from aftermarket suppliers. Smaller-scale options include Mark I Models' 1/144 injection-molded kits, which cover international operators such as U.S. Navy, Canadian Forces, Japanese Coast Guard, and examples, often bundled with decals for multiple schemes to highlight the H-34's worldwide use. Decal sets from Print Scale in 1/72 scale further support builds of U.S., French, and West German H-34s, providing stencils and national markings drawn from historical records. These kits underscore the helicopter's enduring appeal in modeling communities, with builds frequently documented in hobby publications for their representation of mid-20th-century rotary-wing technology.

References

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