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 6320-01-442-8604
NSN 6320-01-189-6891
NSN 5975-01-247-4053
NSN 5905-00-265-1659
NSN 6610-00-081-2365
NSN 6645-01-360-0293
NSN 5999-00-348-9213
NSN 5960-00-249-5005
NSN 6110-00-231-0776
NSN 5920-00-408-4423
NSN 6320-01-207-9038
NSN 6645-01-492-5304