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 5915-01-357-9468
NSN 5835-01-357-9235
NSN 7035-00-417-2967
NSN 6610-00-010-9714
NSN 7035-01-392-9838
NSN 6610-01-462-5980
NSN 6145-00-138-4658
NSN 5998-01-022-5836
NSN 5965-01-243-5494
NSN 6620-01-183-5329
NSN 5999-01-566-8008
NSN 5930-01-098-1896