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turbine shaft, J-400 acft
material is 416 stainless steel, diameter 0.125 in., diameter 0.255 in., bevel 0.015 in. x 45 degrees, radii 0.005 in., depth 0.100 in. nom., item described on dwg as hago 7.5 g.p.h. 60 degree SEMI-Solid nozzle
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.
Used on turbine shaft,j-400 acft. material is 416 stainless steel, diameter 0.125 in., diameter 0.255 in., bevel 0.015 in. x 45 degrees, radii 0.005 in., depth 0.100 in. nom., item described on dwg as hago 7.5 g.p.h. 60 degree semi-solid nozzle
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.