T.O. 2j-f110-14, fig 62 ind 5; inlet guide vane near 1st vane, compressor
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 5975-01-353-8395
NSN 6110-00-788-1521
NSN 5999-01-295-8115
NSN 5895-00-111-1560
NSN 5985-00-392-8078
NSN 5930-01-065-4041
NSN 5835-01-105-6545
NSN 5945-01-383-8377
NSN 6150-00-205-6775
NSN 5935-01-337-3351
NSN 6105-01-658-4191
NSN 5905-01-037-3558