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F-35A "at rest" Flap Position?

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I don't think that they are strictly electric, at least not totally.   I know that the horizonal tail uses a self contained hydraulic system, that is, all of the hydraulic fluid used in the actuator is recycled within the actuator assembly via a motor attached to it.  I am pretty confident that the flap system uses the same type of setup.  Each actuator assembly does have it own electrical control unit.   It would make sense that the units wouldn't bleed down with this system.

Actuation components of the primary flight control system of the F-35 multirole combat aircraft. The aircraft’s rudder, flaperon and horizontal tail are powered by electrohydrostatic actuators. Source: Moog (Click image to enlarge)

Edited by fasteagle12
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