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turbine engine fuel control model no. AJ-H1
scres ams 5610, immunize per bendix ES-091, rockwell c 35-45 hardness, 0.840 in. o/a od, 0.240 in. thk, plate has 0.085 min 0.095 in. max flange thk, flange end has 0.3000 in. min 0.3005 in. max id, other end counterbored 0.500 in. id
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 turbine engine fuel control model no. aj-h1.