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 5835-01-406-7633
NSN 6240-00-160-0786
NSN 5945-01-212-7152
NSN 5965-00-356-3838
NSN 5999-00-807-8104
NSN 6320-01-582-6668
NSN 6320-01-384-7079
NSN 6645-01-064-3711
NSN 5925-00-491-2363
NSN 5998-00-067-3319
NSN 5915-01-126-4529
NSN 5910-01-076-3644