SYS - Flight Controls Flashcards

1
Q

Name the four T-6C secondary flight controls?

A
  • aileron trim surface
  • elevator trim tab
  • rudder trim tab
  • trim aid device
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2
Q

Aileron travel limits?

A
  • 20deg up

- 11deg down

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3
Q

Should the adjustable aileron trim tab be used by aircrew?

A

No

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4
Q

What does mass balanced mean for the ailerons?

A

The centre of maps is along the hinge line

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5
Q

The two elevator ___________ are attached to the AFT elevator ____________ to provide a balanced control feel and tendency to return the control stick to the ___________ position.

A

Down springs
Bell crank
Neutral

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6
Q

Where are the elevator bobweights and what do they do?

A

At the base of the front of the control stick and designed to put on heavier stick force when pulling G to enhance control feedback and help prevent overstressing

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7
Q

Max travel of the elevator?

A
  • 18deg up

- 16deg down

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8
Q

Purpose of rudder cemeteries springs?

A

Help centre the rudder and enhance feedback

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9
Q

Total travel of rudder pedal adjustment?

A

7 inches

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10
Q

Maximum deflection of rudder?

A

24deg

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11
Q

Which trim systems are controlled by the top of the control stick?

A

Pitch and roll

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12
Q

Which control stick trim switch has priority?

A

Rear seat

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13
Q

Where is the rudder trim switch and who has priority?

A

On the PCL, rear seat has priority

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14
Q

Where is the trim interrupt switch?

A

Top of the control stick

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15
Q

Which trim systems does the trim interrupt switch remove power from when held?(4)

A

Aileron, elevator, rudder, and TAD

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16
Q

Will the trim systems return to normal operation when the trim interrupt switch is released?

A

Yes, but the TAD will remain disengaged

17
Q

Maximum aileron trim degrees?

A

6deg

18
Q

Is the aileron trim a trim tab or control surface displacement?

A

Control surface displacement

19
Q

Does the elevator trim system use a trim tab or control surface displacement?

A

A small tab in the centre of the elevator

20
Q

Max degrees for elevator trim?

A

5.5 deg up

22 deg down

21
Q

Does the rudder trim use a tab or control surface displacement?

A

Small rudder tab on trailing edge

22
Q

Max travel of rudder trim tab?

A

9deg left or right

23
Q

Purpose of the TAD system? (3)

A
  • assist pilot in maintaining directional trim
  • reduce out of trim rudder forces
  • maintain coordinated flight
24
Q

What inputs does the TAD computer calculate based on? (4)

A
  • pitch rate
  • altitude
  • airspeed
  • engine torque
25
Q

At what speed does the TAD system change from pre takeoff calculated inputs to one compensated for airspeed and power?

A

80kias

26
Q

Are pilot trim inputs still required with TAD operational?

A

Yes

27
Q

Are pilot trim inputs on top of (additive) the TAD?

A

Yes

28
Q

Upon landing or during touch and go the TAD will set the rudder trim to ___________ position with aircraft on the _________ and airspeed below __________ KIAS.

A

Takeoff
Ground
80 kias

29
Q

Will the TAD system completely trim the aircraft in yaw?

A

No

30
Q

Which switch activates the TAD system?

A

Trim Aid switch

31
Q

What EICAS when TAD off?

A

TAD OFF

32
Q

Which cockpit is the gust lock in?

A

Front cockpit

33
Q

What position is the elevator in when gust lock in?

A

Nose down

34
Q

How is the rudder locked with the gust lock when it attached to the control stick?

A

Through a latch assembly and barrel lock via a latch operating cable.