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 5925-01-649-3392
NSN 2925-00-473-9532
NSN 4140-00-944-2557
NSN 5975-01-111-2665
NSN 6650-01-449-1413
NSN 5960-01-032-4229
NSN 6145-00-382-6199
NSN 5835-00-572-7445
NSN 6685-01-346-7677
NSN 5998-00-709-0613
NSN 6610-01-183-9141
NSN 5998-01-286-4261