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 6110-01-158-0968
NSN 5930-00-756-0439
NSN 4140-01-580-1224
NSN 5915-01-090-1057
NSN 5965-01-481-6957
NSN 5895-01-513-6691
NSN 5835-01-218-9340
NSN 5965-00-752-5823
NSN 5965-01-167-8513
NSN 5985-00-526-3469
NSN 6135-01-346-0851
NSN 4140-00-860-9142