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?

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
At what speed does the TAD system change from pre takeoff calculated inputs to one compensated for airspeed and power?
80kias
26
Are pilot trim inputs still required with TAD operational?
Yes
27
Are pilot trim inputs on top of (additive) the TAD?
Yes
28
Upon landing or during touch and go the TAD will set the rudder trim to ___________ position with aircraft on the _________ and airspeed below __________ KIAS.
Takeoff Ground 80 kias
29
Will the TAD system completely trim the aircraft in yaw?
No
30
Which switch activates the TAD system?
Trim Aid switch
31
What EICAS when TAD off?
TAD OFF
32
Which cockpit is the gust lock in?
Front cockpit
33
What position is the elevator in when gust lock in?
Nose down
34
How is the rudder locked with the gust lock when it attached to the control stick?
Through a latch assembly and barrel lock via a latch operating cable.