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 5965-00-959-4910
NSN 6145-00-984-7739
NSN 6320-01-359-3921
NSN 6320-01-349-2131
NSN 6650-00-334-5901
NSN 5990-01-425-2175
NSN 6145-00-485-6812
NSN 5835-00-315-3797
NSN 5935-00-216-7435
NSN 6650-00-113-4102
NSN 6620-01-106-3553
NSN 5985-01-465-1950