NATO Stock Number
4810-00-016-1026
Sold in multiples of
1 EA
DEMIL
NO
Overall Length
1.525 inches
Overall Diameter
Between 0.552 inches and 0.572 inches
End Application
Aircraft type c-141
Criticality Code Justification
Test
Material
Steel
Test Data Document
99193-664427 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)
General Description
Ams 5643, 17-4ph; one end 6-32 nc-3a threads per mil-s-7742, 0.280 in. Min to 0.370 in. Max length of threads; other end flanged; part of 4810-00-974-2847 and tf 33 turbojet engine
Fsc Application Data
Valve, butterfly