H 1 Iroquois Parts

(Page 27) End item NSN parts page 27 of 35
Part Number
NSN
NIIN
204-031-467-011 Access Door Hinge
007574846
204-031-467-012 Access Door Hinge
007574847
204-031-467-11 Access Door Hinge
007574846
204-031-467-11S Access Door Hinge
007574846
204-031-467-12 Access Door Hinge
007574847
204-031-467-8 Access Door Hinge
007574847
204-031-658-002 Access Door Hinge
008933441
204-031-658-2 Access Door Hinge
008933441
204-031-762-001 Hinge Plate Spring
007388354
204-031-762-002 Hinge Plate Spring
007388355
204-031-762-1 Hinge Plate Spring
007388354
204-031-762-2 Hinge Plate Spring
007388355
204-031-919-043 Retaining Clip
000898575
204-031-919-43 Retaining Clip
000898575
204-031-920-003 Support Pylon Damper
008396863
204-031-920-3 Support Pylon Damper
008396863
204-032-259-029 Cargo Strap Assembly
009275755
204-032-259-29 Cargo Strap Assembly
009275755
204-040-016-005 H Transmission Assembly
001830834
204-040-016-5 H Transmission Assembly
001830834
Page: 27 ...

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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