Boeing 777 Flight Controls
1 / 15
The PRI FLIGHT COMPUTERS EICAS message indicates?
2 / 15
When do the alternate pitch trim levers move the stabilizer?
3 / 15
When are pitch trim changes required with the 777 'fly-by-wire' system?
4 / 15
When do the control wheel stabilizer trim switches control stabilizer movement directly?
5 / 15
Which statement is true when the primary flight computer disconnect dwitch is positioned to DISC?
6 / 15
What can you say about the FLAPS DRIVE EICAS message?
7 / 15
What does the PRI FLIGHT COMPUTERS EICAS message indicate?
8 / 15
What is the meaning of the EICAS advisory message STABILIZER CUTOUT?
9 / 15
When does TAC automatically add rudder to minimize yaw?
10 / 15
In direct mode, which of the following components of fly-by-wire are NOT operating?
11 / 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?
12 / 15
What is the maximum speed of wheel to rudder cross-tie operation?
13 / 15
Do the ailerons increase lift for takeoff?
14 / 15
In the normal mode, a control column input or trim change is required to maintain a constant flight path:
15 / 15
Which spoilers will be locked out in secondary and direct modes?
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