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 6145-01-114-5593
NSN 6645-01-193-9839
NSN 6145-00-188-3657
NSN 6645-01-578-6815
NSN 5965-00-161-1512
NSN 2925-01-655-4455
NSN 6145-01-108-0150
NSN 6150-00-162-4211
NSN 5975-00-401-5365
NSN 6145-01-293-5463
NSN 5835-00-532-5910
NSN 5950-01-051-6081