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 6610-01-483-7874
NSN 6220-01-075-5884
NSN 6240-01-463-3132
NSN 5895-00-518-1593
NSN 5930-01-576-7812
NSN 5990-00-883-6364
NSN 6150-00-369-0376
NSN 5996-01-044-6958
NSN 5999-01-557-1940
NSN 6240-00-527-8614
NSN 5905-01-523-3797
NSN 6650-01-258-5871