0.650 in. Min, 0.663 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 6320-01-567-9792
NSN 5930-01-467-2488
NSN 5960-00-172-7889
NSN 6240-01-564-7698
NSN 5905-01-262-4597
NSN 5985-00-879-9680
NSN 6320-01-582-6668
NSN 5999-01-302-4823
NSN 6320-00-070-4544
NSN 6645-01-312-3558
NSN 5996-01-394-5768
NSN 5910-01-120-3820