Titanium alloy, 2.929 in. Lg, 0.720 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 7035-00-117-0418
NSN 6610-01-457-1974
NSN 5930-00-369-1645
NSN 5935-01-506-5231
NSN 5945-00-180-1234
NSN 5835-00-794-7500
NSN 6150-00-126-8936
NSN 6135-01-223-3869
NSN 5990-00-644-3365
NSN 5905-01-451-4205
NSN 6220-01-392-8376
NSN 5920-00-140-1492