Titanium alloy, 2.426 in. Lg, 0.651 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 5998-00-134-0084
NSN 5965-01-512-1985
NSN 5999-01-043-9875
NSN 5985-01-403-2835
NSN 6610-00-049-6497
NSN 5930-00-827-6154
NSN 5855-00-688-9954
NSN 5925-01-121-8074
NSN 5999-00-837-6785
NSN 5925-00-337-8138
NSN 6145-01-010-4665
NSN 6150-01-577-9802