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valve p/n AV17A1052 for B-1B aircraft fuel system
alum aly per QQ-A-250/4, 0.302 - 0.322 in. thk, 3.044 in. l, 1.764 in. w; along one side 2 holes thru 0.187 in. dia 0.969 in. apart C-TO-C, corners angled 0.425 in. x 45 deg; other side 2 holes 10-32UNF-3B thd thru 0.792 in. CEN-TO-End, 2 holes thru 0.187 in. dia 0.210 CEN-TO-End, corners angled 0.125 in. x 45 deg; hole 0.260 in. dia thru 0.585 in. CEN-TO-Side, 1.522 CEN-TO-End
1EA
Schedule B number: 8481909090
nmfc 190500
Parts of taps, cocks, valves and similar appliances
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 valve p/n av17a1052 for b-1b aircraft fuel system.