Ch 47 Turbine Engine (rotary Wing Aircraft) Parts

(Page 2) End item NSN parts page 2 of 4
Part Number
NSN
NIIN
2-101-321-09 Aircraft Gas T Turbine Blade Set
011878729
2-101-322-05 Aircraft Gas T Turbine Blade Set
011878730
2-101-331-02 Aircraft Gas Tur Compressor Disk
011167330
2-101-332-02 Aircraft Gas Turbin Turbine Disk
011093098
2-103-024-03 Compressor Rotor Spacer
010233163
2-103-024X01 Compressor Rotor Spacer
010233163
2-121-134-09 Aircraft Gas Turbin Turbine Case
010979837
2-131-090-14 Combustio Atomizing Housing Assembly
001523779
2-131-110-63 Aircraf Combustion Chamber Liner
011286611
2-141-050-08 Torquemeter Shaft
013535057
2-141-337-06 Headed Straight Pin
011094923
2-160-010-21 Assem Starter Drive
014619195
2-160-980-03 Branched Metal Tube Assembly
010127709
2-161-620-68 Turbine Engine Main Fuel Control
011692563
2-161-690-02 Turbine Engine Speed Sensor
014614684
2-170-580-02 Turbine Engine Main Fuel Control
013719305
2-171-110-01 Metallic Particle Detector
011430049
2-200-071-27 Parts Kit
013474930
2-300-001 Annular Ball Bearing
004002789
2-300-001-02 Annular Ball Bearing
004002789
Page: 2

Ch 47 Turbine Engine (rotary Wing Aircraft)

Picture of Ch 47 Turbine Engine (rotary Wing Aircraft)

The Allison Model 250, now known as the Rolls-Royce M250, (US military designations T63 and T703) is a highly successful turboshaft engine family, originally developed by the Allison Engine Company in the early 1960s. The Model 250 has been produced by Rolls-Royce since it acquired Allison in 1995.

In 1958, the Detroit Diesel Allison division of General Motors was chosen by the US Army to develop a new light turbine engine to power a Light Observation Aircraft (LOA), to replace the Cessna O-1A Bird Dog. At this stage the US Army were unsure whether to have a fixed- or rotary-wing aircraft, so Allison was instructed to consider both applications. Design studies undertaken considered a wide range of possible mechanical configurations for the turboprop/turboshaft. These studies culminated in the testing of the first prototype engine, designated YT63-A-3, in April 1959. In 1960 the US Army settled for a rotary wing platform. The YT63-A-3 first flew in a variant of the Bell 47 helicopter in 1961. A modified version of the engine (YT63-A-5) with the exhaust pointing upwards (to avoid grass fires) soon followed. This version, rated at 250 hp, passed the Model Qualification Test in September 1962. Thus was born the Model 250. Incidentally, the Hughes OH-6 design was selected for the US Army LOH platform in May 1965,

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