SYS - Flight Controls Flashcards
Name the four T-6C secondary flight controls?
- aileron trim surface
- elevator trim tab
- rudder trim tab
- trim aid device
Aileron travel limits?
- 20deg up
- 11deg down
Should the adjustable aileron trim tab be used by aircrew?
No
What does mass balanced mean for the ailerons?
The centre of maps is along the hinge line
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.
Down springs
Bell crank
Neutral
Where are the elevator bobweights and what do they do?
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
Max travel of the elevator?
- 18deg up
- 16deg down
Purpose of rudder cemeteries springs?
Help centre the rudder and enhance feedback
Total travel of rudder pedal adjustment?
7 inches
Maximum deflection of rudder?
24deg
Which trim systems are controlled by the top of the control stick?
Pitch and roll
Which control stick trim switch has priority?
Rear seat
Where is the rudder trim switch and who has priority?
On the PCL, rear seat has priority
Where is the trim interrupt switch?
Top of the control stick
Which trim systems does the trim interrupt switch remove power from when held?(4)
Aileron, elevator, rudder, and TAD
Will the trim systems return to normal operation when the trim interrupt switch is released?
Yes, but the TAD will remain disengaged
Maximum aileron trim degrees?
6deg
Is the aileron trim a trim tab or control surface displacement?
Control surface displacement
Does the elevator trim system use a trim tab or control surface displacement?
A small tab in the centre of the elevator
Max degrees for elevator trim?
5.5 deg up
22 deg down
Does the rudder trim use a tab or control surface displacement?
Small rudder tab on trailing edge
Max travel of rudder trim tab?
9deg left or right
Purpose of the TAD system? (3)
- assist pilot in maintaining directional trim
- reduce out of trim rudder forces
- maintain coordinated flight
What inputs does the TAD computer calculate based on? (4)
- pitch rate
- altitude
- airspeed
- engine torque