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1.998 in. o/a lg, 1st end 1st shoulder, 0.240 in. min, 0.245 in. max od, 0.450 in. lg, 50 deg min 60 deg max angle of spray cone, 2nd shoulder, 0.367 in. min, 0.373 in. max od, 0.560 in. min, 0.600 in. max lg, 1 hole 0.094 in. dia thru one wall, 3rd shoulder, 0.285 in. min, 0.301 in. max lg, both ends chamfered 40 deg min, 50 deg max chamfer angle, 0.4375-20-UNJF-3A thd, 4th shoulder, 0.337 in. min, 0.347 in. max od, 0.079 in. min, 0.095 in. max lg, 2nd end, MS33656-2 style e, flared tube connection and gasket seal, thd 5/16-24-UNF-3A, 0.448 in. thd lg, 37 deg seat angle, hex nut, 0.563 in. w across flats, 3 head holes 0.047 in. dia
1EA
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.
1.998 in. o/a lg, 1st end 1st shoulder, 0.240 in. min, 0.245 in. max od, 0.450 in. lg, 50 deg min 60 deg max angle of spray cone, 2nd shoulder, 0.367 in. min, 0.373 in. max od, 0.560 in. min, 0.600 in. max lg, 1 hole 0.094 in. dia thru one wall, 3rd shoulder, 0.285 in. min, 0.301 in. max lg, both ends chamfered 40 deg min, 50 deg max chamfer angle, 0.4375-20-unjf-3a thd, 4th shoulder, 0.337 in. min, 0.347 in. max od, 0.079 in. min, 0.095 in. max lg, 2nd end, MS33656-2 style e, flared tube connection
1. | 24236 | Cage 71895 |
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3. | 2-300-216-02 | Cage 99193 |
4. | 24236DLN | Cage 71895 |
5. | 6660039 | Cage 09523 |
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.