Titanium alloy, 1.380 in. Lg, 0.879 in. W, 0.579 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 5905-01-521-3496
NSN 5999-01-040-0713
NSN 5996-01-552-7953
NSN 6150-01-429-4248
NSN 5996-00-823-8487
NSN 5990-00-932-3070
NSN 6685-01-319-6478
NSN 4140-00-152-7092
NSN 6240-01-459-9086
NSN 5920-00-276-8657
NSN 6610-01-327-3187
NSN 6145-01-158-8408