Iroquois Hh/uh-1 Helicopter Parts

(Page 14) End item NSN parts page 14 of 21
Part Number
NSN
NIIN
204-040-929 Cover And Lift Plat
009084853
204-040-929-029 Cover And Lift Plat
009084853
204-040-929-29 Cover And Lift Plat
009084853
204-040-968 Cover And Lift Plat
009084853
204-050-151-005 Skid Gear Nut Assembly
008980002
204-050-151-5 Skid Gear Nut Assembly
008980002
204-050-170-001 Rod End Clevis
008959345
204-050-170-1 Rod End Clevis
008959345
204-060-767-001 Boot Control Rod Retainer
007082253
204-060-767-1 Boot Control Rod Retainer
007082253
204-060-767-1-17772 Boot Control Rod Retainer
007082253
204-061-606 Liquid Quantity Transmitter
008687028
204-061-606-1 Liquid Quantity Transmitter
008687028
204-061-717-3 Rod End Bearing
008973758
204-070-032-003 Aircraft Safety Belt
007874299
204-070-032-3 Aircraft Safety Belt
007874299
204-070-371-7 Cabin Heat Duct Flapper Assembly
008588421
204-070-450-019 Tail Webbing Strap
009671821
204-070-450-19 Tail Webbing Strap
009671821
204-070-540-3 Air Dis Suppressor
000100423
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Helicopter, Iroquois Hh/uh-1

Picture of Iroquois Hh/uh-1 Helicopter

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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