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 6240-01-397-8713
NSN 5905-00-870-4464
NSN 5950-01-321-6178
NSN 6240-01-242-9138
NSN 4140-01-360-0594
NSN 6220-01-298-6836
NSN 5835-00-257-2852
NSN 5996-01-364-0207
NSN 6110-00-621-3475
NSN 6320-01-029-2196
NSN 5920-00-091-9435
NSN 5930-00-464-9776