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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36

SECTION 6 – AUTOMATIC

FLIGHT CONTROL

6-1

SECTION 6: AUTOMATIC FLIGHT

CONTROL

In addition to the AFCS (Automatic Flight Control Sys-

tem) keys on the MFD, as discussed in the System Over-

view section, the following buttons and switches used by

the AFCS are located in the cockpit separately from the

PFD and MFD.

• AP DISC (Autopilot Disconnect) Button —

Located on the pilot’s control wheel, pressing this

button disengages the autopilot. Pressing it also

acknowledges an autopilot disconnect.

• CWS (Control Wheel Steering) Button —

Located on the pilot’s control wheel, pressing and

holding the CWS button disengages the control

surface servos without disengaging the autopi-

lot. If the ﬂight director has not been activated,

pressing the CWS button will activate the ﬂight

director in the default pitch and roll hold modes.

• GA (Go Around) Button — Located on the sub-

panel or throttle lever, the GA button disengages

the autopilot and selects the Go Around Pitch and

Roll (wings level) modes.

• MET (Manual Electric Trim) Switch — This

switch is used to operate manual electric pitch

trim. Moving both switches forward simultane-

ously trims the aircraft nose down. Moving both

switches aft simultaneously trims the aircraft nose

up. The left switch is the ARM contact and the

right switch controls the up/down trim. Pressing

the ARM switch disengages the autopilot, if cur-

rently engaged. If one side of the switch is active

for more than three seconds without the other

side also being active, ‘PTRM’ is displayed in the

AFCS System Status ﬁeld on the PFD. Pressing

the MET ARM switch also acknowledges an auto-

pilot disconnect.

Figure 6-1 AFCS Keys

Pressing the FD key activates only the ﬂight director in

the default Pitch Hold/Roll modes without engaging the

autopilot. Pressing the AP key activates the ﬂight director

and yaw damper, and engages the autopilot. When only

the ﬂight director is engaged, pressing the FD key disen-

gages the ﬂight director.

Upon activation of the autopilot and/or ﬂight director,

command bars are displayed on the PFD. If the attitude

information being sent to the ﬂight director becomes in-

valid or unavailable, the command bars are removed from

the display.

Figure 6-2 Command Bars

6.1 MODE ANNUNCIATIONS

Mode annunciations are displayed on the PFD. Figure

6-3 shows the AFCS Status Bar ﬁelds. Modes associated

with aircraft movement about the roll axis are displayed

on the left side. Modes associated with aircraft movement

about the pitch axis are displayed on the right. Armed

modes are displayed in white and active modes are dis-

played in green.

1 2 ... 36 37 38 39 40 41 42 43 44 45 46 ... 115 116

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