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 5975-00-009-8718
NSN 5975-00-732-1289
NSN 5998-00-373-7728
NSN 6150-01-657-6774
NSN 6240-01-147-5424
NSN 6645-00-498-6869
NSN 5835-01-424-4577
NSN 6130-01-400-6123
NSN 5835-00-422-1441
NSN 5985-01-607-0291
NSN 7035-00-445-9657
NSN 6645-00-056-1580