22-06. AEROPLANE: AUTOMATIC FLIGHT CONTROL SYSTEMS
All questions: 100
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1. The control law in a fly-by-wire system is a relationship between:
2. To allow the coupling of a dual channel flight director:
3. The engagement of an autopilot is not possible when:
1) there is a fault in the electrical power supply.
2) the controlled-turn knob is not set to centre-off.
3) there is a synchronization fault in the pitch channel.
4) there is a fault in the attitude reference unit.
The combination re-grouping all the correct statements is:
4. If a pilot was to carry out a roll manoeuvre, on release of the control column with the autopilot in CWS mode, what does the autopilot do?
5. (Refer to figure 022-13)
The FD command bars on the ADI (illustration number 2) indicate that:
