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1.1775 in. min, 1.838 in. max o/a lg, 0.620 in. min, 0.625 in. max od 1st step 1st end, 0.335 in. min lg 1st step, 0.810 in. min, 0.820 in. max od 4th step 1st end, 0.755 in. min, 0.765 in. max od 5th step 1st end, hex 1.008 in. min, 1.046 in. max distance from 1st end, 1.052 in. min, 1.062 in. max w across flats, 0.4375 in.-20 unf class 3a thd 2nd end
1EA
Schedule B number: 8803300060
nmfc 030660
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.
1.1775 in. min, 1.838 in. max o/a lg, 0.620 in. min, 0.625 in. max od 1st step 1st end, 0.335 in. min lg 1st step, 0.810 in. min, 0.820 in. max od 4th step 1st end, 0.755 in. min, 0.765 in. max od 5th step 1st end, hex 1.008 in. min, 1.046 in. max distance from 1st end, 1.052 in. min, 1.062 in. max w across flats, 0.4375 in.-20 unf class 3a thd 2nd end
1. | 5233333 | Cage 71934 |
2. | 23077086 | Cage 63005 |
Nothing similar to this part number was found in our inventory
A spring loaded nozzle designed to meter and inject fuel at specific pressure(s) to engine fuel combustion chambers.