0.669 in. Min, 0.682 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 5895-00-560-1707
NSN 6105-01-043-0959
NSN 5915-00-334-9606
NSN 5855-01-371-5645
NSN 2925-01-326-0908
NSN 6685-01-263-7054
NSN 5935-00-826-9291
NSN 5998-01-050-0885
NSN 6150-01-649-3598
NSN 6130-01-515-0399
NSN 5910-01-452-2504
NSN 5975-00-406-1662