Boeing 777 Flight Controls
1 / 15
What power source is used for the actuation of all primary flight controls?
2 / 15
What happens if uncommanded stabilizer motion is sensed?
3 / 15
What is wheel to rudder cross-tie?
4 / 15
Which statement is true when the primary flight computer disconnect dwitch is positioned to DISC?
5 / 15
What is the effect of placing a stabilizer cutout switch to cutout?
6 / 15
Which one of the following statements is false?
7 / 15
Which trim control is inhibited when the autopilot is engaged?
8 / 15
When does TAC automatically add rudder to minimize yaw?
9 / 15
Which one of the following statements is incorrect?
10 / 15
What does stall warning consist of?
11 / 15
In direct mode, which of the following components of fly-by-wire are NOT operating?
12 / 15
Auto speed-brakes protection is provided for which phases of flight?
13 / 15
A wheel to rudder cross-tie function provides the capability of being able to control the initial effects of an engine failure using control wheel inputs only. How many degrees of rudder deflection can be obtained from control wheel inputs?
14 / 15
Which of these flight control surfaces droop when the trailing edge flaps extend?
15 / 15
When are pitch trim changes required with the 777 'fly-by-wire' system?
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