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turbine engine main fuel control model AJ-H1
ams 5610 cres w/ROCKWELL-C 26 to 33 hardness, immunized protective finish, o/a dim. 0.184 in. min to 0.190 in. max dia by 0.600 in. lg, thd portion size 0.190-32 NF-3A, small end 0.086 in. min to 0.090 in. max dia, basic bleed drill size no. 68, 0.0300 in. min to 0.0320 in. max dia
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 main fuel control model aj-h1.