Secondary Flight Controls Flashcards

1
Q

What are the secondary flight controls?

A

Hydraulically actuated spoilers, horizontal stabilizer, flaps

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2
Q

When the adjustable horizontal stabilizer is trimmed properly, what is the position of the control column?

A

Centered

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3
Q

The stabilizer trim is measured in the cockpit as _____ to _____ units of trim.

A

-3 to 11

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4
Q

How can you move the stabilizer?

A

Electrically, manually, or through the autopilot.

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5
Q

During preflight, what is the correct setting of the stabilizer trim prior to checking the elevator?

A

6 to 11 nose-up

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6
Q

The left_____ switch and the right______ switch when pressed simultaneously, move the horizontal stab leading edge at a rate of _____________.

A

Clutch; motor; ½ degree per second

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7
Q

The _____________ flaps determine the deflection of the leading edge flaps.

A

Outboard

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8
Q

The warning horn sounds if the No. 3 throttle is near OPEN and the flap lever is near the ________ detent.

A

0, 40 or 50

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9
Q

When will the warning horn sound on the ground?

A

No 3 throttle near fully open and: speed brake is aft of 2 degrees, leading edge flaps not fully extended and flaps lever is 0, 40 or 50 degrees

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10
Q

Only the _______ flaps can be manually extended or retracted

A

Main

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11
Q

After an unscheduled rudder deflection, one of the first steps is to determine whether the rudder pedals moved. What does this step determine?

A

Whether the potential cause of the problem is Power Control Unit (PCU)/mechanical (rudder pedals moved), powered rudder, or EFAS/SYD (did not move rudder pedals)

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12
Q

Maximum available spoiler deflection using the speed brake lever is _______ degrees.

A

60

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13
Q

A speed brake lever position of less than ________ degrees is not recommended due to a tendency to overcontrol at these settings.

A

40

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14
Q

If EFAS is inoperative, Vmcg can increase by as much as _______ KIAS

A

25

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15
Q

If you experience an unscheduled rudder deflection, after S1, you should immediately:

A

Turn off the rudder power

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16
Q

The inboard elevator tabs improve control characteristics by reducing the tendency to ___________at higher speeds.

A

Overcontrol

17
Q

Prior to performing the Flap and Speed Brake Warning Horn check, ensure the _______ are fully extended.

A

Leading edge flaps

18
Q

After an unscheduled rudder deflection, EFAS and SYD turn off as a direct result of:

A

Turning off the rudder power (remember when pressure drops below 1,000 PSI, EFAS/SYD turn off

19
Q

After turning off the rudder power due to an unscheduled rudder deflection, check _______ bleeds down, _____ disengages, and the ______ disengages.

A

Rudder power hydraulic pressure bleeds down, EFAS/SYD

20
Q

If the rudder pedals didn’t move during an unscheduled rudder deflection, what is the possible cause?

A

EFAS/SYD

21
Q

The main flaps operate by either ___ or ____

A

Hydraulic or manual movement