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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
as differentiated by source control dwg N0. 114PS401
Schedule B number: 8803300060
nmfc 013120
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.
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
1. | 114PS401-1 | Cage 77272 |
2. | AV16B1568D | Cage 73760 |
Nothing similar to this part number was found in our inventory
An item specifically designed to automatically/manually maintain outlet/inlet fuel.