Titanium, 0.250-28 unjf-3a external thd
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 6685-00-186-0190
NSN 6130-01-148-6511
NSN 5999-01-484-9059
NSN 5920-00-155-2173
NSN 5835-01-508-2528
NSN 6240-00-954-7853
NSN 5895-01-157-4741
NSN 5965-00-560-1760
NSN 6685-01-507-7268
NSN 5835-01-123-8305
NSN 6145-01-081-8586
NSN 5950-00-448-3126