Tag Archives: 65001

14 October 1964

Prototype Sikorsky YCH-53A Sea Stallion, Bu. No. 151613, 14 october 1964. (Sikorsky Archives)
Prototype Sikorsky YCH-53A Sea Stallion, Bu. No. 151613, 14 October 1964. (Sikorsky Archives)

14 October 1964: The first prototype Sikorsky YCH-53A Sea Stallion, Bu. No. 151613, made its first flight at the Sikorsky plant at Stratford, Connecticut. (Sikorsky Model S-65, serial number 65001.)

The Bridgeport Telegram reported:

Brief First Flight Made By CH-53A at Sikorsky

     The Sikorsky-Marine Corps CH-53A, designed as the free world’s largest and fastest transport helicopter, took off for the first time Wednesday at the Sikorsky Aircraft plant here. The aircraft was hovered within the flight field in its preliminary phase of the test program.

     The brief flight exceeded expectations and project engineers and pilots expressed satisfaction with the CH-53A’s overall performance. More than twice the forces expected in actual high-performance flight were induced during ground tests prior to flight with far better results than ever before experienced at this early stage of a test program. Tie-down tests, started during the summer to check for components, structure and systems function, also provided “very satisfactory” results.

     The CH-53A will be capable of speed of more than 200 miles an hour and will carry payloads of up to nine tons. It is powered by two General Electric T-64-6 turboshaft engines of 2,850 horsepower each. It will be flown by a three-man crew and will carry 38 fully-equipped troops. For medical evacuation duties, the CH-53A will carry 24 patients.

The Bridgeport Telegram, Vol. LXXIII, No, 250, Saturday, 17 October 1964, Page 3, Columns 6–7

The fuselage of the YCH-53A was similar in configuration to the smaller CH-3C (S-61R). It used the dynamic components from the CH-37 Mojave (S-56) and CH-54A Tarhe (S-64).

U.S. Marine Corps Sikorsky CH-53A Sea Stallion (Wikimedia)

The Sikorsky CH-53A Sea Stallion is a twin-engine heavy-lift transport helicopter operated by two pilots. It is 88 feet, 2.4 inches (26.883 meters) with rotors turning. The fuselage is 67 feet, 2.4 inches (20.483 meters) long  and 8 feet, 10 inches (2.692 meters) wide. The six-blade fully articulated main rotor is 72 feet, 2.7 inches (22.014 meters) in diameter and turns counterclockwise as seen from above. (The advancing blade is on the helicopter’s right.) Main rotor speed is 185 r.pm. The four-blade semi-articulated tail rotor has a diameter of 16 feet (4.877 meters) and is placed on the left side of the tail rotor pylon in a pusher configuration. It turns clockwise as seen from the helicopters left. (The advancing blade is below the axis of rotation.) Overall height (rotors turning) of the Sea Stallion is 24 feet, 10.8 inches (7.599 meters). The tail rotor speed is 792 r.p.m.

The CH-53A is powered by two General Electric T64-GE-6 turboshaft engines rated at 2,850 shaft horsepower, each. Performance of the CH-53D (T64-GE-413, 3,925 s.h.p) has a maximum speed (Vne) of 130 knots (241 kilometers per hour) service ceiling of 16,750 feet (5,105 meters) and range with maximum payload of 540 miles (870 kilometers)

Two YCH-53A prototypes were built, followed by 139 CH-53A Sea Stallion production models.

The CH-53 was developed into the three-engine CH-53E Super Stallion. The current production variant is the CH-53K King Stallion.

Sikorsky HH-53B 66-14428, Super Jolly Green Giant, first flight at Stratford, Connecticut, 15 March 1967. (Sikorsky Historical Archives)
Sikorsky CH-53E Super Stallion at Mojave, California, 9 September 2007. (Alan Redecki/Wikipedia)
This photograph by Alan Radecki of a Sikorsky CH-53E Super Stallion taking off at Mojave, California, 20 September 2007, is too exciting not to include. (Akradecki/Wikipedia)
Sikorsky CH-53K King Stallion at West Palm Beach, Florida, 2 March 2017. (Lance Corporal Molly Hampton, United States Marine Corps)

© 2017 Bryan R. Swopes