2-8 3rd Ed. Sep 30, 06
S–TEC
Table 2-2. Pre-Flight Test (continued from page 2-6)
ACTION RESPONSE
11. Press/Hold CWS Switch to arm
control wheel steering mode.
CWS, VS, and +0 (or ±1)
annunciations only appear on AP
display, as shown in Fig. 2-8.
12. Move A/C Control Wheel left and
right.
A/C Control Wheel’s increased
freedom of movement indicates that
Roll Servo is disengaged.
13. Move A/C Control Wheel forward
and aft.
A/C Control Wheel’s increased
freedom of movement indicates that
Pitch Servo is disengaged.
14. Release CWS Switch to engage
control wheel steering mode.
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15. Attempt movement of A/C
Control Wheel left and right.
A/C Control Wheel’s reduced
freedom of movement indicates that
Roll Servo is engaged.
16. Attempt movement of A/C
Control Wheel forward and aft.
A/C Control Wheel’s reduced
freedom of movement indicates that
Pitch Servo is engaged.
17. Rotate AP Modifier Knob CW
until +5 (500 FPM climbing) is
commanded, as shown in Fig. 2-9.
A/C Control Wheel moves in aft
directon.
18. Rotate AP Modifier Knob CCW
until -5 (500 FPM descending) is
commanded, as shown in Fig. 2-10.
A/C Control Wheel moves in forward
direction.
19. Rotate AP Modifier Knob CW
until +0 (0 FPM) is commanded.
A/C Control Wheel stops.
Note: If it is not possible to select a local VOR frequency on Navigation
Receiver, then proceed to step 30. Otherwise, proceed to step 20.
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