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TF30-P-1 aircraft engine fuel control
ams 5616 stainless steel w/ROCKWELL-C 35 to 40 hardness, o/a dim. 0.665 in. min to 0.671 in. max dia by 0.478 in. min to 0.499 in. max lg, 0.100 in. min to 0.101 in. max dia by 0.128 in. min to 0.129 in. max lg middle section, 8 grooves equally spaced around each end on 0.560 in. min to 0.580 in. max dia surface
1EA
Schedule B number: 8481809050
nmfc 127220
Other taps, cocks, valves, etc.
FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers
Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.
Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.
Used on tf30-p-1 aircraft engine fuel control.