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 5905-01-265-0175
NSN 6110-01-122-5781
NSN 2925-01-217-0465
NSN 5905-00-399-4630
NSN 5925-00-948-0064
NSN 6620-00-193-9503
NSN 5996-01-213-5184
NSN 5935-00-246-2575
NSN 5990-00-179-2576
NSN 5910-00-144-4383
NSN 5920-00-149-1469
NSN 5996-00-296-9629