Titanium alloy, 0.8510 in. Min, 0.8635 in. Max lg
No other part numbers with same form, fit, and function found.
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 5985-01-279-2064
NSN 6130-01-611-9969
NSN 6320-01-006-6138
NSN 5930-00-932-9039
NSN 5910-01-257-8239
NSN 6645-01-381-6084
NSN 5975-01-216-0282
NSN 5945-01-325-7999
NSN 5985-01-032-1674
NSN 6620-00-064-7992
NSN 6645-00-296-8310
NSN 5835-01-250-2633