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 5935-00-435-9712
NSN 4140-01-462-5901
NSN 5996-01-085-5031
NSN 5915-01-345-9070
NSN 6240-01-016-2172
NSN 5985-01-625-0998
NSN 6220-01-460-6677
NSN 5975-01-260-9972
NSN 5855-01-285-3483
NSN 5975-00-228-9161
NSN 6240-01-573-7036
NSN 2925-00-241-5244