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turbine engine main fuel control model no. AJ-E1
scres, immunized, 0.630 in. o/a lg, 0.340 in. od, 0.270 in. id, 90 deg countersink both ends, 0.066 in. min 0.0690 in. max dia of rivet hole drilled 0.310 in. from each end through both walls, 36 straight side serrations entire length
5EA
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 turbine engine main fuel control model no. aj-e1.