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 5930-01-657-5319
NSN 6610-00-734-5976
NSN 5990-00-872-1312
NSN 5998-01-462-4159
NSN 5935-01-218-7938
NSN 6145-01-066-9481
NSN 6645-01-099-4322
NSN 5990-00-518-0684
NSN 5855-01-258-5161
NSN 6320-01-021-6633
NSN 6650-01-599-7717
NSN 5950-01-141-7019