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
piston 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 it
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 significantly
greater comfort.
A total of 135 H-34s
were built in the U.S. and assembled by
Sud-Aviation in France, 166 were produced
under licence in France by Sud-Aviation for
the French Air Force, Navy and Army Aviation
(ALAT).
The CH-34 was
also built and developed under license from
1958 in the United Kingdom by Westland
Aircraft as the turbine 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.
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Variants
- 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.
- 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
- 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.
- 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.
- S-58
- Commercial designation for basic
cargo variant
- S-58B
- Commercial designation for improved
cargo variant
- S-58C
- Commercial passenger
transport/airliner version
- S-58D
- Commercial airliner/freighter
version
- S-58T
- Commercial conversion to turboshaft
power by Sikorsky, Orlando Helicopter,
and California Helicopter. Kit uses
Pratt & Whitney Canada PT6T-3 Twin-Pac
turboshaft with special nose cowling
featuring distinctive twin rectangular
air intakes.
- S-58 Heli-Camper
- Commercial conversion, fitted with a
Wright Cyclone R-1820-24 engine.
- Orlando Airliner
- Commercial conversion. 18-seat
passenger transport helicopter.
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SPECIFICATIONS: |
PERFORMANCE:
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Rotor Span:
56 ft 0 in (17.07 m)
Length:
56 ft 8.5 in (17.28 m)
Height:
15 ft 11 in (4.85 m) Empty Weight:
7,900 lb (3,583 kg)
Gross Weight:
14,000 lb (6,350 kg)
Crew:
2 plus
16 troops or 8 stretchers |
Maximum
speed:
123 mph (107 kn, 198 km/h)
Cruising
speed:
Range:
293 km (182 mi)
Service
ceiling:
4,905 ft (1,495 mi) |
Engines:
1 × Wright R-1820-84 radial engine,
1,525 hp (1,137 kW) |
Armament:
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SOURCE:
Wikipedia |
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