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The Fairchild C-123 Provider is an American military transport aircraft designed by Chase Aircraft and built by Fairchild Aircraft for the U.S. Air Force.In addition to its USAF service, which included later service with the Air Force Reserve and the Air National Guard, it went on to serve the U.S. Coast Guard and various air forces in Southeast Asia.
The 606th Special Forces Squadron was composed of two sections, the Fairchild C-123 Provider section which was under the call sign of "Candlestick", and the U-10 Helio Courier section which was under the call signs of "Loudmouth" and "Litterbugs" (and "Clown" for Civil Action missions).
In 1949, the Hagerstown, Maryland, Fairchild Engine and Airplane Corporation developed the Chase XCG-20 glider into the C-123 Provider transport which entered service in 1955. In 1954 Fairchild purchased the American Helicopter Company, incorporating it and the XH-26 Jet Jeep as a division. [ 7 ]
The Stroukoff YC-134, designed in 1956, was based heavily on the Fairchild C-123 Provider, itself designed by Michael Stroukoff.The United States military contracted with Stroukoff Aircraft Corporation to develop an improved version of the aircraft, combining features that the company had developed for the YC-123D and YC-123E.
It was activated flying the Chase YC-122 Avitruc, then the Fairchild C-123 Provider as the United States Air Force's first assault airlift group. It deployed to Europe, but was inactivated in 1957 and its components transferred to another unit. It was activated as a maintenance wing in 2005.
On February 5, 1982, a Republic of Korea Air Force Fairchild C-123J crashed while on approach to Jeju International Airport, Jeju, South Korea. All 47 passengers and 6 crew were killed in the impact. It remains the fourth-worst accident in South Korean aviation history. [1]
Data from "C-123 Provider in action" General characteristics Crew: 3 Length: 77 ft 1 in (23.50 m) Wingspan: 110 ft 0 in (33.53 m) Height: 33 ft 10 in (10.31 m) Wing area: 1,222.78 sq ft (113.600 m 2) Airfoil: NACA 23017 Max takeoff weight: 70,000 lb (31,751 kg) limited by tow aircraft to 40,000 pounds (18,000 kg) See also Aviation portal Related development Chase XC-123A Fairchild C-123 ...
This page was last edited on 7 September 2010, at 01:02 (UTC).; Text is available under the Creative Commons Attribution-ShareAlike 4.0 License; additional terms may apply.