T.O. 2j-j75-4; case-rear compressor front; compressor stator 9-14th stage; 178 units per assembly
A component of a vane assembly, compressor, aircraft gas turbine engine. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 6150-01-547-3061
NSN 5855-01-658-4510
NSN 5965-01-502-7006
NSN 5925-01-294-5707
NSN 5910-01-319-3342
NSN 5915-00-375-5000
NSN 5990-00-113-6137
NSN 6685-00-295-0824
NSN 5925-01-442-0650
NSN 5975-00-905-5194
NSN 5975-01-322-8515
NSN 4140-01-335-8992