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Bell UH-1 Iroquois

Design & Development: - (Continued from Page 1)

UH-1B

The HU-1B was an improved model that was equipped with the Lycoming T53-L-5 engine of 960 shp, revised main rotor blades of 44 foot diameter and 21 inch chord, 13 inch higher rotor mast and a longer cabin that could accommodate seven passengers. This version was redesignated UH-1B in 1962.

Later production UH-1Bs were equipped with Lycoming T53-L-9 and L-11 engines of 1100 shp. Gross weight was 8,500 lbs and the standard empty weight was 4513 lbs.

Army testing of the "B" model started in November, 1960 with first production aircraft arriving in March, 1961. A total of 1010 "Bravo" models were delivered to the US Army. First deployment was in November 1963 when eleven were sent to Vietnam to join the "Alpha" models already in use by UTTCO.

One NUH-1B was produced for test purposes.

Bell certified a civil version of the UH-1B incorporating some minor safety improvements, such as improved door locks. The aircraft was marketed as the Bell 204B.

UH-1C The UH-1C was specifically developed as a gunship version until the "interim" attack helicopter, the Bell AH-1G Huey Cobra was available and to correct the deficiencies of the UH-1B when it was used in the armed role. The UH-1C was widely referred to as the "Huey Hog" in US Army service.


U.S. Army UH-1C "Huey". (Source: Unknown)

The "Charlie" model was fitted with the 1100 shp T53-L-9 or L-11 engine to provide the power needed to lift the weapons systems in use or under development at the time. It incorporated the new Bell 540 rotor system with 27 inch chord blades. The increased power lead Bell's engineers to design a new tailboom for the "C" which incorporated a wider chord fin on a longer boom and larger synchronized elevators. The "C" also introduced a dual hydraulic control system for redundancy in battle and an improved inlet filter system for the dusty conditions found in southeast Asia. Fuel was increased to 242 US gallons and gross weight to 9500 lbs, giving a nominal useful load of 4673 lbs.

Development on the "C" model had commenced in 1960, with production starting in June 1966. A total of 766 "C" models was completed, including five for the Royal Australian Navy, designated N9 and five for Norway. The balance went to the US Army.

Many UH-1Cs were later re-engined with the 1400 shp Lycoming T53-L-13 powerplant. With this engine they were redesignated UH-1M.

Continued on next page....


Sources:
Wikipedia: UH-1 Iroquois "Huey"