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Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36

SECTION 6 – AUTOMATIC

FLIGHT CONTROL

6-9

6.6 ROLL AXIS MODES

Mode annunciations for active roll axis modes are

shown in green during normal operation.

AFCS

Key

AFCS Mode Annunciation

FD/AP only Roll Hold (Default) ROL

HDG Heading Select HDG

NAV

VOR Enroute

Arm / Capture / Track

VOR

GPS Arm / Capture / Track GPS

BC Arm / Capture / Track BC

LOC Arm / Capture / Track;

(No Glideslope)

LOC

APR

GPS Arm / Capture / Track

GPS

VOR Approach

Arm / Capture / Track

VAPP

ILS Approach

Arm / Capture / Track

(Glideslope pitch mode

automatically armed)

LOC

GA Go Around (Wings Level) GA

The default roll axis mode is Roll Hold (ROL). When

no other roll axis modes are selected, this is the active

roll axis mode when the autopilot and/or ﬂight director

is engaged.

Roll Hold Mode (ROL)

1. Press the

key.

If the aircraft bank angle is

≥ 6 degrees when

the key is pressed, Roll Hold mode is selected

by default. Roll attitude at the time of activa-

tion is maintained by the autopilot. If only the

ﬂight director is active, command bars indicate

the proper roll attitude.

If the aircraft bank angle is

< 6 degrees when

the key is pressed, the aircraft will be main-

tained at wings level. If only the ﬂight direc-

tor is active, command bars give guidance to

maintain wings level.

Roll Hold mode is annunciated by ‘ROL’.

Figure 6-17 Roll Hold Mode

2. A new heading can be established by pressing

and holding the

CWS

button and manually

turning the aircraft to the desired new heading.

Release the

CWS

button and the aircraft will

maintain wings level at the new heading. The

same practice applies to holding roll attitude.

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