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main fuel pump, p/n 024891-116, for TF39 acft eng
relief valve adjusting nut
cres per AMS5640; 2.084 - 2.104 in. l; one end 1.125 in. od flatted 1.00 in. across, 0.875 in. bore 0.656 in. dp, 1.250-12UNJF-3A thd 0.157 in. from end 1.189 in. l; 1.123 in. od other end w/O-Ring seal groove 0.972 in. dia, 0.141 in. w, 0.067 in. from end, 0.875 in. bore 1.125 in. dp
1EA
Schedule B number: 8803300060
nmfc 133320
Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts the
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 main fuel pump,p/n 024891-116,for tf39 acft eng.
Nothing similar to this part number was found in our inventory
A regulating device threaded or unthreaded for the purpose of tuning the mechanism for which it is specifically designed. it may have a limiting collar, shoulder or slot. the rotating facility may be a hex head or collar, a slot or socket end. excludes bolt (as modified); screw (as modified); stud (as modified).