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2915-01-1332467, p/n 781111
cres per AMS5630, hardness 53-58Hrc; 1.228 in. lg o/a; 0.622 in. maj od; first end flange dia 0.410 in., bore 0.2213 in., 0.635 in. lg; second end dia 0.497 in. chamfered 0.04 x 0.04, cbore 0.393 in., 0.593 in. dp; groove 0.110 in. w x 0.104 in. dp on shank and on shoulder; nha p/n 782110
1EA
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 2915-01-1332467,p/n 781111.