Iroquois Uh-1 Helicopter Parts

(Page 38) End item NSN parts page 38 of 41
Part Number
NSN
NIIN
205-070-764-1 Seat Assembly Fitting
000140717
205-070-773-001 Litter Guide Support
007585700
205-070-773-1 Litter Guide Support
007585700
205-072-204-001 Drip Pan
001135794
205-072-204-1 Drip Pan
001135794
205-072-231-1 Rescue Post Support
000203838
205-075-135 Nonmetallic Tubing
000539154
205-075-135-19 Nonmetallic Tubing
000539154
205-706-082-3 Aircraft Fairing
000072566
2061K72P011 Dust And Moi Protective Cap-plug
001059454
20630-20-20 Tube To Hose Straight Adapter
000178233
20630-20-20-20 Tube To Hose Straight Adapter
000178233
20641 Plain Encased Seal
002856378
2069900046 Electrical Insulation Tape
008324298
206M5 Hexagon Self-locking Nut
001984759
20AS111-1 Connector Adapter
005390203
20P101-10 Electrical Plug Connector
005527699
20RT353-1 Diode Semiconductor Device
009224818
21-006-7-11 Sleeve Bushing
009902634
21-007-9-14-5 Sleeve Bushing
000892880
Page: 38

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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