No other part numbers with same form, fit, and function found.
A continuous combustion type engine. consists primarily of a compressor, aircraft gas turbine engine, chamber, combustion, aircraft gas turbine engine and a turbine assembly, aircraft gas turbine engine. it may have an afterburner, turbine engine and/or a fan section. air is compressed and heated by a combustible fuel and expanded through the turbine. it is designed to furnish a source of rotary shaft, pneumatic power or thrust power. the pneumatic power is obtained by a bleedoff of the engine compressor. for a complete operating power unit, mounted on a base, see power unit, gas turbine engine.
NSN 6220-00-281-3822
NSN 5965-00-246-5612
NSN 6650-00-170-5095
NSN 6110-01-491-4207
NSN 5998-00-626-8719
NSN 6650-01-421-2762
NSN 5975-01-064-2868
NSN 6110-01-327-3670
NSN 6145-01-098-3899
NSN 6220-00-915-7731
NSN 6135-01-286-9563
NSN 5985-00-550-8750