Titanium alloy, 0.8510 in. Min, 0.8635 in. Max lg
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 5960-01-453-6170
NSN 7035-00-890-7649
NSN 6130-01-184-6758
NSN 4140-01-073-7436
NSN 6620-01-235-3752
NSN 4140-00-974-5055
NSN 5925-00-259-2098
NSN 5910-01-339-9055
NSN 6320-01-255-2096
NSN 5835-00-170-5238
NSN 6105-01-236-1379
NSN 6620-00-028-3370