Iroquois Uh-1 Helicopter Parts

(Page 23) End item NSN parts page 23 of 41
Part Number
NSN
NIIN
204-001-256-5 Collective Stick Friction Shoe
009369253
204-001-328-047 Dust And Moisture Seal Boot
007406485
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
204-001-701-001 Pedal Support Assembly
006246738
204-001-701-1 Pedal Support Assembly
006246738
204-010-132-001 Pylon Assembly Mast Nut Lock
006250039
204-010-132-1 Pylon Assembly Mast Nut Lock
006250039
204-010-132-1-18608 Pylon Assembly Mast Nut Lock
006250039
204-010-318-001 Bearing Housing Liner
007853624
204-010-457-005 Sleeve Spacer
008309727
204-010-457-5 Sleeve Spacer
008309727
204-010-526-001 Strap Retainer Nut Lock
006702959
Page: 23 ...

Helicopter, Iroquois Uh-1

Picture of Iroquois 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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