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aug control, F100-PW-220 eng
cres 1.52 in. l o/a; 0.19 in. dia end w/0.31 in. dia flange 0.17 in. from end, 0.0469 in. dia hole thru side of head; 0.13 in. dia shank 0.23 in. l; double flange 0.27 in. od, 0.20 in. w, spaced 0.08 in. apart; 0.18 in. od other end w/0.09 in. hex socket, hole thru both walls 0.08 in. C-TO-End; 0.2500-20Unified form spcl thd, 0.2450 max maj dia, 0.1837 max minor dia
Schedule B number: 8803300060
nmfc 133300
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 aug control,f100-pw-220 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).