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 5950-00-420-0803
NSN 5930-00-274-1308
NSN 5935-00-171-0362
NSN 5905-00-005-4874
NSN 6105-01-240-3606
NSN 5950-00-462-1792
NSN 5910-00-919-3318
NSN 6620-00-905-6590
NSN 5835-01-459-7428
NSN 7035-01-502-6764
NSN 6320-01-523-4954
NSN 7035-01-209-6325