Titanium alloy, 1.231 in. Lg, 0.874 in. W, 0.552 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 5905-01-143-6503
NSN 5950-00-888-9673
NSN 5910-00-427-1731
NSN 5965-01-468-6186
NSN 6685-00-308-4204
NSN 6650-01-158-6888
NSN 5998-01-104-5462
NSN 2925-01-326-0908
NSN 6320-00-937-5625
NSN 5950-01-541-4659
NSN 6220-01-160-1738
NSN 6220-01-273-6024