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 2925-00-838-7164
NSN 5920-01-640-9556
NSN 6610-01-459-8722
NSN 6130-01-558-6617
NSN 5905-01-630-3647
NSN 5996-01-189-6280
NSN 6645-01-168-8465
NSN 7035-01-027-1718
NSN 6645-01-563-2812
NSN 6685-00-854-7947
NSN 5855-00-323-0967
NSN 6105-00-161-8070