body, aluminum alloy, alloy 356, temper T6, anodized, motor operated, m 8 to p 60 psi operating pressure, 1/2 sec min, to 1 sec max operating time at 28 vdc, 70 deg f at operating pressure, fuel per mil-h-5572 or mil-j-5624, oil per mil-l-7808, fluid connection, MS33786-16, electrical connector, MS3112e-14s-5p, acceleration factor 12g, seat, synthetic rubber, fluid temp, m 65 to p 160 deg f, max internal actuator pressure 15 psi, functional test in accordance with general controls spec e-850-AV16B1568d
Used on awacs 411l fuel system; c135 aircraft. designed for partially submerged operation; control handle, two position on/off; 120 psig operating pressure; thermal relief valve; 12.730 in long, including handle; 5.000in wide; 3.750 in high
body, aluminum alloy, alloy 356, temper T6, anodized gray, mil-a-8625, type 1, functional test per general controls spec. E850-AV16B1456c, motor operated, 0 to 30 psi operating pressure, 1/2 second min, 1 second max operating time at 28 v at 70 deg f at operating pressure, oil per mil-l-6082a, electrical connector, AND10066c-14s-5p, acceleration factor 12g, seat, synthetic rubber, fluid temp m 65 to p 160 deg f
Used on f/rf 104g aircraft engine fuel control. electrically operated, 28 volts, direct current, 48 watts, 0 to 60 psi operating pressure at 70 deg f temp, 130 gpm rating, 2.500 lbs max wt, o/a dim. approx 7.380 in. min to 7.429 in. max lg by 3.190 in. w by 5.660 in. h, 2 ports w/o-rings
