Beechcraft Baron G58 Pilot Operating Handbook page 383

Model G58
2. Disengages the autopilot.
3. Cancels all armed modes including Altitude Hold.
4. Cycles the flight plan to Missed Approach (software ver-
sion 0857.05 or 0857.06).
The autopilot may be re-engaged after GO AROUND is
selected.
The GO AROUND Mode can be cancelled using one of the fol-
lowing methods:
1. Select another roll mode such as HDG or NAV.
2. Adjust the pitch attitude using the CWS.
3. Adjust the pitch using the NOSE UP / NOSE DN keys.
CONTROL WHEEL STEERING (CWS) - Pressing the CWS
switch on the pilot's control wheel disengages the control sur-
face servos without disengaging the autopilot as long as the
switch is depressed. The servos are re-engaged when the
switch is released and the system will synchronize to the exist-
ing airspeed, vertical speed, pitch angle or roll angle depend-
ing upon the mode selected. If the autopilot and flight director
have not previously been engaged, pressing the CWS button
will activate the flight director in the pitch and roll hold modes.
When the CWS mode is active, a white [CWS] replaces the
green [AP] in the AFCS status bar.
MANUAL ELECTRIC PITCH TRIM - When the autopilot is not
engaged, the electric pitch trim system may be operated with
the split trim switch located on the left side of the pilot's control
wheel. The switches must be moved together in order to acti-
vate the trim system. If either side is independently activated
for more than 3 seconds, a red [PTRM] is displayed in the
AFCS System Status Field. The annunciator will extinguish
shortly after the switch is released. The red [PTRM] will also
illuminate when a failure of the pitch trim system occurs. If the
autopilot is engaged when this occurs, it will remain engaged.
See ELECTRIC PITCH TRIM FAILURE in Section 3.
Refer to Section 2, LIMITATIONS, Section 3, EMERGENCY
PROCEDURES, Section 3A, ABNORMAL PROCEDURES,
May, 2015
Section 7
Systems Description
7-83