Flight Controls Flashcards

1
Q

What is the Speed Trim System

A

Speed stability augmentation system designed to improve flight characteristics during
- low gross weight
- aft center of gravity
- high thrust with autopilot disengaged

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2
Q

What is the purpose of the Speed Trim System

A

To return the airplane to a trimmed speed by commanding the stabilizer in a direction opposite the speed change

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3
Q

What are the conditions for the Speed Trim System to be engaged

A

Airspeed: 100kias - 0.6M
10 sec after TO
5 sec after release of trim switch
Autopilot OFF
Sensing of trim requirement

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4
Q

How are flight spoilers powered

A

Hydraulic systems A and B

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5
Q

Why can’t you move the speed brake lever past the flight detent

A

It will cause airplane buffeting

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6
Q

Which hydraulic systems power which flight spoilers?

A

A and B each power 2 flight spoilers on each side.

BABA ABAB

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7
Q

What does SPEED BRAKE DO NOT ARM light mean

A

Indicates an abnormal condition or test inputs to the system. This is deactivated with the speed brake in the down position.

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8
Q

What does SPEED BRAKE DO NOT ARM light mean when illuminated during landing?

A

Indicates wheel speed below 60kts and the speed brake lever is not in the down position.

Essentially….you forgot to stow them while getting off the runway

(3CM-PX)

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9
Q

SPEEDBRAKES EXTENDED light illuminates to indicate

A

Flight Spoilers are still extended at radio altitude below 800ft or Trailing edge flaps are extended more than 10 degrees

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10
Q

How are the ground spoilers actuated

A

Hydraulic system A

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11
Q

When will the Auto speed brake system operate?

A

Speed brake lever ARMED + light
RA less than 10 ft
Thrust Levers IDLE
MLG spin up + 60kts
MLG strut compression (WOW)

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12
Q

Which MLG strut must compress to deploy ground spoilers

A

RIGHT MLG

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13
Q

How does the Auto Speed Brake system work during an RTO

A

MLG spin up + 60kts
Thrust Levers IDLE
Reverse Thrust Levers deployed

All flight and ground spoilers will AUTOMATICALLY deploy until a thrust lever is moved out of idle or the handle is manually stowed

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14
Q

Describe the Load Alleviation System

A

Conditions: Gross weights above 155,000lbs
And speed above 320kias
3AA-3CL

Flight spoilers limited to 50%.
Must hold lever if wishing to override.

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15
Q

How are trailing edge flaps operated

A

Hydraulic System B

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16
Q

Normal flap landing configurations

A

15, 30 and 40

17
Q

What does LE FLAPS TRANSIT amber light indicate

A

-LE devices in Transit
-LE devices not in programmed position
-LE slat skew condition exists

18
Q

How are LE flaps and Slats actuated

A

Hydraulic System B

19
Q

What is the AUTOSLAT system

A

The SMYD will automatically move the slats to the “full extended” position when the airplane approaches a stall condition. This only occurs at flap positions 1, 2 and 5

20
Q

What indications are present when the AUTOSLAT system is activated

A

None.

21
Q

How is the autoslat system operated.

A

Hydraulic system B.
Alternate: PTU from system A

22
Q

What is the Flap Load Relief System

A

Automatic flap retraction if airspeed exceeds VLE.

AA-LB
Only available at 30 and 40

LC +
Available at 10, 15, 25, 30 and 40

23
Q

What indications exist when the Flap Load Relief System is operating

A

The flap position indicator will be the only indication

24
Q

Describe the Alternate Flaps extension

A

An electric motor will operate when the alternate flaps toggle switch is held in the down position.

25
Q

What does arming the ALTERNATE FLAPS master switch do

A

Closes the Flap bypass valve (prevents hydraulic lock of flap drive unit)
Activates standby pump
Arms the position switch

26
Q

How are the LE devices moved during alternate flap extension

A

Hydraulic power from the standby system drives LE flaps and slats to the full extend position

27
Q

Once placed down, how do the LE devices retract in alternate mode

A

They cannot be retracted. They can only be extended

28
Q

Which leading edge devices are Not monitored for skew conditions

A

Slats 1 and 8

29
Q

Mach Trim systems automatically functions above what speed

A

.615 M