H 1 Iroquois Parts

(Page 20) End item NSN parts page 20 of 35
Part Number
NSN
NIIN
204-001-295-5 Throttle Control Lever
007800883
204-001-298-001 Pilot Collective Box Assembly
007318091
204-001-298-1 Pilot Collective Box Assembly
007318091
204-001-328-043 Cycli Boot Assembly
007406486
204-001-328-047 Dust And Moisture Seal Boot
007406485
204-001-328-43 Cycli Boot Assembly
007406486
204-001-328-47 Dust And Moisture Seal Boot
007406485
204-001-358-001 Cyclic Arm Assembly
000857370
204-001-358-1 Cyclic Arm Assembly
000857370
204-001-366-005 Cyclic Frict Linear
000898234
204-001-366-5 Cyclic Frict Linear
000898234
204-001-373-001 Bell Crank
007583668
204-001-373-1 Bell Crank
007583668
204-001-376-003 Magnetic Brake
009098716
204-001-376-3 Magnetic Brake
009098716
204-001-600-009 Aircraft Control Stick
000222344
204-001-600-9 Aircraft Control Stick
000222344
204-001-617-001 Slide Stick Tube
007577150
204-001-617-1 Slide Stick Tube
007577150
204-001-701-001 Pedal Support Assembly
006246738
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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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