Pilot's Guide

Garmin G1000 Pilot’s Guide for the Piper PA-44-180 Seminole
190-01461-00 Rev. A
84
ENGINE INDICATION SYSTEM
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICESINDEX
ELECTRICAL
DC current for the left and right alternators (pointers labeled “L” and “R”) and voltage for the DC bus are
shown along color-coded horizontal scales, with readouts above the scale. The ammeter displays the battery
load in amperes (amps) along a horizontal scale, with a white tick mark indicating zero amps. The horizontal
scales and pointers will not appear in Reversionary Mode.
Figure 3-6 Electrical Group
Bus Voltage
Ammeter
Alternator
Current
EXHAUST GAS TEMPERATURE BAR GRAPH
Exhaust Gas (EGT) temperatures in degrees Fahrenheit are displayed for each cylinder using a bar graph on
the Engine Page. A temperature readout for each cylinder is shown at the top of the graph. Cylinders whose
EGTs are in the normal range appear in white. The temperature readout is replaced with white dashes if the
temperature exceeds the normal range.
Exhaust Gas
Temperatures
Normal
Temperature
Range Exceeded
Figure 3-7 Exhaust Gas Temperature