Alerting System - Beechcraft Baron G58 Pilot Operating Handbook

Model G58
Oil temperature is indicated on a linear scale and is sensed as
it enters each engine from the oil cooler. The sensors are
wired to the left and right GEA for display. Numeric tempera-
ture value is displayed on the SYSTEM engine page.
Oil pressure is sensed at the back of each engine off a port
below the oil coolers and wired to the left and right GEA for dis-
play. The display is liner, with a numeric pressure value avail-
able on the SYSTEM engine page.
The ALT LOAD and BUS VOLTS displays are described in the
electrical systems description and the FUEL QTY GAL display
is described in the fuel systems description. See the Garmin
G1000 Engine Indication System Pilot's guide for more
detailed information.

ALERTING SYSTEM

The G1000 provides an Annunciation window and an Alerts
window on the PFD to inform the pilots of Warning Alerts, Cau-
tions Alerts, Advisory Alerts, and Messages that may occur
during the operation of the airplane. Both windows are also
available on the MFD to provide the same notifications when
the MFD is operating in the reversionary mode. The available
alerts and selected messages are shown in the table below.
When an alert occurs, three things occur simultaneously.
1. The ALERTS softkey will assume a new label and color
depending on the level of alert. The softkey label will
change to a red WARNING label for warning alerts, a
yellow CAUTION label for caution alerts, and a white
ADVISORY label for advisory alerts. The label will also
assume a flashing mode.
May, 2015
Section 7
Systems Description
7-71