H 1 Iroquois Parts

(Page 24) End item NSN parts page 24 of 35
Part Number
NSN
NIIN
204-011-304-1 Stabilizer Support Assembly
008309741
204-011-428-003 Bearing Retaining Plate
008762410
204-011-428-3 Bearing Retaining Plate
008762410
204-011-428-3-10000 Bearing Retaining Plate
008762410
204-011-428-3-17772 Bearing Retaining Plate
008762410
204-011-443-001 Ball Bearing Unit
008309756
204-011-443-1 Ball Bearing Unit
008309756
204-011-443-1-17 Ball Bearing Unit
008309756
204-011-443-1-17772 Ball Bearing Unit
008309756
204-011-443-3 Bearing Retaining Plate
008309757
204-011-446-003 Headless Shoulder Pin
007186798
204-011-446-3 Headless Shoulder Pin
007186798
204-011-726-001 Thrust Plug
001136175
204-011-726-1 Thrust Plug
001136175
204-012-016-001 Rotor Blade Plate
004016189
204-012-016-1 Rotor Blade Plate
004016189
204-012-103-001 Hub Assembl Fitting
002007454
204-012-103-1 Hub Assembl Fitting
002007454
204-012-105-001 Static Stop Assembly
002007815
204-012-105-1 Static Stop Assembly
002007815
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H 1 Iroquois

Picture of H 1 Iroquois

The Bell UH-1 Iroquois (nicknamed "Huey") is a military helicopter powered by a single turboshaft engine, with two-blade main and tail rotors. The first member of the prolific Huey family, it was developed by Bell Helicopter to meet a United States Army's 1952 requirement for a medical evacuation and utility helicopter, and first flew in 1956. The UH-1 was the first turbine-powered helicopter to enter production in 1960 for the United States military, and more than 16,000 have been built since.

The Iroquois was originally designated HU-1, hence the Huey nickname, which has remained in common use, despite the official redesignation to UH-1 in 1962. The UH-1 first saw service in combat operations during the Vietnam War, with around 7,000 helicopters deployed. The Bell 204 and 205 are Iroquois versions developed for the civil market.

In 1952, the Army identified a requirement for a new helicopter to serve as medical evacuation (MEDEVAC), instrument trainer, and general utility aircraft. The Army determined that current helicopters were too large, underpowered, or complex to maintain easily. In November 1953, revised military requirements were submitted to the Department of the Army.

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