Monitoring The Chts And Egts; Avionics; Autopilot/Flight Director; General - Beechcraft Baron G58 Pilot Operating Handbook

Model G58
MONITORING THE CHT
Specific EGT and CHT values for each cylinder are found on
the MFD.
1. ENGINE Soft Key . . . . . . . . . . . . . . . . . . . . . . . . PRESS
2. LEAN Soft Key . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
3. CYL SLCT Soft Key . . . . . . . . . . . . . . . . . . . . . . PRESS
(Each press of the key cycles the display to the next cyl-
inder. The selected cylinder display number changes
color from white to cyan and the digital displays show the
absolute temperature and deviation from Peak tempera-
ture for the selected cylinder.)
4. MFD Softkeys . . . . . RETURN TO MAIN ENGINE PAGE

AVIONICS

AUTOPILOT/FLIGHT DIRECTOR

GENERAL

It is the responsibility of the Pilot to monitor
the autopilot when it is engaged. The pilot
should be prepared to immediately discon-
nect the autopilot and take prompt correc-
tive action in the event of unexpected or
unusual autopilot behavior.
Do not attempt to manually fly the airplane with the autopilot
engaged except when using the Control Wheel Steering
(CWS) button. The autopilot pitch servo will oppose pilot pitch
inputs and will trim the elevator in the opposite direction of the
pilot input. This could lead to a significant out-of-trim condition
in the pitch axis. Disconnect the autopilot using the AP DISC
switch, the left side of the trim switch, or the AP key if manual
control is desired.
June, 2011
Normal Procedures
AND EGT
S S
Section 4
4-31