Original name vane, compressor stator, turbine engine
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 6220-00-426-6340
NSN 5998-01-227-4839
NSN 6145-01-548-2758
NSN 6320-00-313-9114
NSN 5915-01-143-2482
NSN 6110-01-504-4377
NSN 6105-00-684-6807
NSN 6620-00-088-8795
NSN 5998-01-246-0128
NSN 6105-01-034-7689
NSN 6610-00-633-4338
NSN 4140-00-132-2061