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unified fuel control for F100 aircraft engine
micro adjustment for sequence valve body and piston assy
cres, 0.80 in. l o/a; 0.30 in. od one end w/internal hex socket 0.09 in. min across; fluted socket other end spline maj dia 0.09 in. max, spline width 0.03 in. max, thd 0.32 in. l from end 0.164-32UNJC-3A, apex thd 0.250-20 unified form 0.39 in. from end
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 unified fuel control for f100 aircraft engine.
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).