Titanium alloy, 2.660 in. Lg, 0.650 in. W, 0.435 in.H
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 6610-01-189-0953
NSN 5905-01-626-6060
NSN 6135-00-947-0406
NSN 6620-01-529-6665
NSN 5935-01-456-4622
NSN 5935-00-349-8858
NSN 6145-01-473-7146
NSN 5999-01-654-8984
NSN 6150-01-589-9687
NSN 5910-01-622-5674
NSN 5999-01-053-5499
NSN 5998-01-459-8036