Avionic fundamental 4 Please provide little explanation or r

Avionic fundamental 4

Please provide little explanation or reason for the answer

thank you

1-10. Prior to engagement, the autopilot pitch channel servo motor loop maintains its synchro rotor
a. perpendicular to the field in the stator. b. perpendicular to ~e field in the rotor.
e. parallel to-the field inUre stator. d. parallel to the field in the rotor.

2-11. Versine lift compensation involves
a. lifting the nose while banking.
b. increasing engine thrust while banking.
c. using spoilers to achieve stability while banking.
d. lifting the tail while banking.

3-12. Which one ofthe following is NOT a factor in calculating track angle error?
a. airplane heading
b. actual ground path track
c. desired track
d. way points

4-13. The purpose of a CWS Force system is to
a. increase steering accuracy.
b. increase steering range.
c. decrease manual force needed to steer.
d. provide dual control.

Solution

4-13 (d) provide dual control..

because CWS is the acumen for Control Wheel Steering. Broadly speaking, it is a sub-set of the autopilot (A/P) system which can used on either System A or B. When engaged, CWS maneuvers the aircraft in response to control pressures applied to the control wheel or column.