T.O. 2j-j75-4; front compressor; 36 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 6150-00-341-3860
NSN 5975-01-100-1063
NSN 5930-01-477-5208
NSN 5905-01-519-8272
NSN 5945-01-361-3232
NSN 6685-00-314-4566
NSN 5935-01-446-6885
NSN 5965-01-623-8005
NSN 5855-00-147-2508
NSN 6150-01-249-7306
NSN 5965-00-900-8102
NSN 5920-01-633-6646