NATO Stock Number
4810-00-016-1021
Sold in multiples of
1 EA
DEMIL
NO
Overall Length
Between 2.440 inches and 2.460 inches
Overall Diameter
Between 1.790 inches and 1.810 inches
End Application
Aircraft type c-141
Criticality Code Justification
Test
Material
Aluminum alloy
Surface Treatment
Anodize
Test Data Document
99193-664417 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
Matl per ww-t-789, 6061-s0; surface per mil-a-8625; 1.029 in. Inside dia; flanged one end with 4 holes 0.124 in. Diameter thru; part of 4810-00-974-2847, pneumatic system tf33 turbojet engine
Fsc Application Data
Valve, butterfly
