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 6145-01-415-3763
NSN 5925-01-160-7609
NSN 5998-01-120-7278
NSN 5999-01-506-9722
NSN 5905-00-906-3138
NSN 5996-01-030-9694
NSN 6645-01-076-4655
NSN 6145-00-113-6278
NSN 6145-01-610-1963
NSN 6650-01-556-3508
NSN 5930-01-048-0596
NSN 5960-01-287-4187