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Sikorsky S-62 / HH-52 Sea Guard


The forerunner of an entirely new generation of production models, the S-62 was the company 's first amphibious helicopter, with a boat hull and powered by a single General Electric T58 turbine.


S-62 prototype


The Sikorsky S-62 was the first turbine-powered helicopter to be granted a type approval certificate by the U.S. Federal Aviation Agency, and was also the first type to pass new regulations introduced by the FAA to govern the operation of commercial passenger-carrying helicopters.


The design, drawn up in 1957-58, was based on using identical main and tail rotors and transmission systems, and other dynamic and mechanical features, of the proven piston-engined S-55. The fuselage was entirely new, being designed for fully amphibious operation with a flying-boat hull and main undercarriage wheels semi-retractable within the two outrigged stabilising floats. Power was provided by a single General Electric shaft turbine engine, mounted centrally above the main cabin and accommodation provided for a 2-man flight crew and 10 airline passengers or 12 troops.




Two S-62 prototypes were completed, with 1050shp T58-GE-6 engines derated to 670shp. The maiden flight on 22 May 1958, and subsequent world-wide demonstration flights, were made by N880, while N972 carried out trials for the FAA type certificate which was awarded on 30 June 1960; and a few days later the first production machine, designated S-62A, was delivered to a commercial customer.




Later S-62A's have CT58-100 or -110 engines of 1250 (derated to 730) shp. The S-62B is essentially similar to the A model, but employs the rotor system of the Sikorsky S-58 with the main blades shortened by 0.33m.


February 1962, after service trials with a modified S-62A, the U.S. Navy ordered four of these aircraft on 21 June 1962 as HU2S-1G's (later as HH52A’s) for the U.S. Coast Guard. Initial deliveries, under the designation HH-52A and named Seaguard, were made in January 1963. This version powered by a 932kW CT58-GE-8 engine was replaced by the HH-3 Pelican.
Sikorsky HH-52A
In all, ninety-nine were built; 1352 to 1379, 1382 to 1413, 1415 to 1429, 1439 to 1450, and 1455 to 1466.


The HH-52A can carry six litters and can hoist 600 pounds on a cable at-tached to an electric winch with an explosive guillotine cutter. The engine is a GE turbine that generates 1,250 shaft horsepower, de-rated, on this Coast Guard version to only 830 shp by limiting the size of the fuel-flow orifices.




HH-52s based at Houston, Texas, frequently practised recovery of the NASA Apollo astronauts. One US Coast Guard machine was used in the film Airport '77.


Subsequent naval orders for the HH-52A had raised the total to eighty-four by mid-1968 and it has been in use since early 1963. The HH-52A has the T58-GE-8 engine, military version of the CT58-110, and automatic stabilisation equipment. Additional features for coastal search and rescue work include a fold-down rescue platform and boat-towing gear. A rescue hoist can be mounted above the starboard cabin door to lift a maximum load of 272kg, or the S-62A can lift a 1361kg slung load by means of an under-fuselage hook.


The S-62C is the equivalent of the HH-52A for commercial and foreign military customers. Apart from the U.S. Coast Guard, which remains the largest user of the type, the biggest single operator of S-62's is Petroleum Helicopters Inc, which has a fleet of six for work in support of offshore oil-drilling operations in the Gulf of Mexico. Of the forty-six S-62 type helicopters ordered, up to summer 1968, other than those of the USCG, nearly half were for customers in Japan, where Mitsubishi hold the licence. Nine examples were built under licence for service with Japanese Maritime Self- Defence Force (JMSDF).


By mid-1993, no military, and only a very small number of civilian, S-62s remain in use.




Engine: 1 x General Electric CT58-110-1 turboshaft
Accommodation: 11 passengers


Engine: 1 x General Electric CT-58-100-1 turboshaft, rated at 990kW
Main rotor diameter: 16.15m
Length with rotors turning: 18.86m
Fuselage length: 13.58m
Height: 4.33m
Width: 4.8m
Max take-off weight: 3630kg
Empty weight: 2248kg
Cruising speed: 163km/h
Rate of climb: 5.8m/s
Service ceiling: 3570m
Range: 743km
Crew: 2
Passengers: 10












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