Sikorsky CH-34 Choctaw
The CH-34 Choctaw had a single four-bladed main rotor and a four-bladed metal tail rotor. Although it was very robust and generally liked and respected by its crews, there were design flaws exposed by combat experience in Vietnam. The high cockpit made it an obvious target. The drive shaft created a partition that made it difficult for crew chiefs to come to the aid of injured cockpit crew. The H-34's magnesium skin resulted in very intense fires, and contributed to significant corrosion problems. The airframe was also too weak to support most of the weapons that allowed the UH-1 Huey to become an effective ad-hoc gunship.
Sikorsky CH-34 Choctaw Specifications and Performance
| Rotor diameter | 56 ft. |
| Length | 46 ft. 9 in. |
| Height | 15 ft. 11 in. |
| Weight | 13,000 lb. |
| Armament | None |
| Engine | 1425 hp Curtis-Wright R-1820-84C (radial pistons) |
| Maximum speed | 123 mph. |
| Cruising speed | 98 mph. |
| Range | 247 mi. |
| Service ceiling | 9,500 ft. |
Sikorsky CH-34 Choctaw helicopter.
CH-34 Choctaw helicopter, Fitzsimons Army Hospital, Aurora, CO, 13 September 1956.
Technicians work on a Marine HUS-1 / CH-34 Seahorse helicopter on the beach at Cua Viet, Vietnam, 1 October 1966.
Marine HUS-1 / CH-34 Seahorse helicopter on the runway at Dong Ha, Vietnam, 1 July 1967.
An air-to-air left front view of a Marine HUS-1 / CH-34 Seahorse helicopter over Cua Viet, Vietnam, 1967.