Ch 47 Turbine Engine (rotary Wing Aircraft) Parts

(Page 3) End item NSN parts page 3 of 4
Part Number
NSN
NIIN
2-300-001-05 Annular Ball Bearing
004002789
2-300-034 Cylindrical Roller Bearing
000189654
2-300-034-01 Cylindrical Roller Bearing
000189654
2-300-035 Cylindrical Roller Bearing
001165534
2-300-035-01 Cylindrical Roller Bearing
001165534
2-300-812-01 Pressure Indicator
011177303
2-300-828-01 Thermocouple Harness Assembly
011110797
2-300-842 Fluid Filter
011083652
2-300-842-01 Fluid Filter
011083652
2-310-052 Immersion Thermocouple
013330805
2-310-052-02 Immersion Thermocouple
013330805
2-310-054 Immersion Thermocouple
013330803
2-310-054-02 Immersion Thermocouple
013330803
2-310-086-01 Immersion Thermocouple
013330805
2-310-088-01 Immersion Thermocouple
013330803
2-310-143 Wiring Harness
014171714
2-310-143-01 Wiring Harness
014171714
2250-4005 Fluid Filter
001796990
26452-0 Carrier Assembly
000158611
26486-0 Metal Tube Assembly
011794136
Page: 3

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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