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.
Classification: Aircraft turbines (engines), except for use in civil aircraft, of a power not exceeding 5000 kw
NSN 5935-00-623-3579
NSN 5965-01-509-0926
NSN 5996-00-199-9303
NSN 6320-00-894-1644
NSN 5975-00-522-2711
NSN 6220-00-145-1423
NSN 5920-01-537-0684
NSN 5996-01-161-6296
NSN 5950-01-606-9819
NSN 5935-01-315-7448
NSN 5915-00-816-9056
NSN 2925-01-106-8871