Serving our customers with quality and safety first.
unified fuel control for F100 aircraft eng
used with bimetal disk group, part of pb actuator assy
scres, 1.10 in. l o/a; 0.65 in. l stem 0.09 in. dia one end; 0.04 in. thk flange 0.19 in. dia 0.41 in. from other end, no. 8-32UNJC-3A rolled thd 0.332 in. l, end fluted socket spline maj dia 0.09 in. max, spline width 0.02 in. max
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 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).