0.659 in. Min, 0.672 in. Max lg
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 5985-01-552-1413
NSN 6645-00-153-3834
NSN 5950-01-029-2133
NSN 4140-00-189-0235
NSN 5975-00-671-3528
NSN 5835-00-457-9528
NSN 6130-00-396-1118
NSN 5855-00-631-4565
NSN 5965-01-447-8821
NSN 5985-01-370-2419
NSN 5975-01-461-3120
NSN 5975-00-273-0790