Flight Controls Flashcards

1
Q

Pitch/Roll Disconnect is used by the flight crew for what?

A

To physically separate the connection between the ailerons and spoilers, and between the left and right elevator

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2
Q

How is the rudder controlled and actuated?

A

Electronically controlled (Fly by wire), hydraulically actuated

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3
Q

Variable Differential Transformers on each rudder pedal send what?

A

Electronic signals to the (SECU)
Smart Electronic Control Units which correspondingly deflects the rudder

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4
Q

The Flaps are operated by…

A

Main DC electrical power

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5
Q

If hydraulic pressure is lost, hydraulic accumulators will do what for the spoilers?

A

Maintain pressure so that all six panels will function as ground spoilers upon landing.

*Speedbrake and Roll Spoiler functionality will be disabled

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6
Q

Ground Spoilers deploy…

A

Automatically during landing rollout or aborted takeoffs

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7
Q

What panels are used as speed brakes?

A

Panels 1,2,5 and 6

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8
Q

The AFCS Trim, when engaged, the autopilot provides…

A

Pitch Trim Only

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9
Q

Aileron Trim System is electrical. The actuator is installed in the _____ wing and is connected to the _____ trim tab

A

Right
Right

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10
Q

The Left Aileron Trim Tab is a…

A

Geared Servo Tab

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11
Q

Horizontal Stabilizer Trim is provided by primary and secondary trim systems. Primary Pitch Trim consists of an A and B motor. A is powered by _____ ______ bus, B and Secondary Trim are powered by the ______ ________
bus

A

Left Mission Bus

Right Emergency Bus

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12
Q

The Mach Trim System is designed to compensate for…

A

The nose down pitching moment as Mach increases

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13
Q

Rudder trim is provided by an ____________ actuator attached to the rudder pedals

A

Electromechanical

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14
Q

Can you takeoff with the control lock on?

A

No, the throttles can be moved to taxi with the control lock engaged, but the left throttle cannot be advanced for takeoff

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