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 5965-01-080-4021
NSN 5930-01-035-0406
NSN 6650-01-360-9691
NSN 5975-01-510-4355
NSN 5945-01-378-1880
NSN 5985-01-052-9757
NSN 5910-01-290-3769
NSN 6150-00-205-2490
NSN 5920-00-161-4564
NSN 5960-01-462-6267
NSN 7035-01-107-2811
NSN 5950-00-528-1446