Actuator Overload Protection Quiz

Loss of valid pitch trim communication from the FCCs to the HSCU.

The flaps will remain in their last position, held by the no-back devices integral with each actuator, when power was lost.

It disables the flap system for the remainder of the flight by de-energizing the HCM SOV.

<p>It responds to electrical commands received from the FECU and provides directional control, extend/retract, and low/high speed rate control of the PDU.</p> Signup and view all the answers

<p>Automatically controlled by the Flight Control Computers (FCCs)</p> Signup and view all the answers

<p>GND SPOILER Switch: ARMED AND Both Throttles at idle AND specific wheel speed and/or radar altimeter conditions met</p> Signup and view all the answers

<p>The ground spoilers will deploy when the throttles are retarded to idle, if the flight crew elects to abort the takeoff.</p> Signup and view all the answers

<p>The GND SPOILER switch in the cockpit center pedestal must be ARMED, and the activation logic is similar to that used for the ground spoilers, including weight-on-wheels or wheel speed, and both throttles at the idle position.</p> Signup and view all the answers

<p>Incorrect position of FLAP Handle, SPEED BRAKE Handle, PARK / EMERG BRAKE Handle, Landing Gear Control Handle, Thrust Reverser Lever(s), GPWS/GND SPLR FLAP ORIDE Switch</p> Signup and view all the answers

<p>Speed brakes are not approved for extension with flaps at 39o (DOWN) or with landing gear extended in flight</p> Signup and view all the answers

<p>Speed brakes automatically retracted with speed brake handle not in stowed position and TLA �90%, or AOA limiting encountered</p> Signup and view all the answers

<p>GND SPLR switch must be OFF and manual spoiler landing distances must be taken into account</p> Signup and view all the answers