Garmin G1000 Piper PA-46 Matrix - Manual (Page 106)

Garmin G1000 Pilot’s Guide for the Piper PA-46 Mirage/Matrix 190-01108-00 Rev. B 92
ENGINE INDICATION AND CREW ALERTING SYSTEM
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL FEA
TURES
APPENDICES
INDEX
OIL PRESSURE AND TEMPERATURE GAUGES
Engine oil pressure and temperature (Figure 3-10) are shown along horizontal bar indicators above the CAS
display. Oil pressure is shown in pounds per square inch (psi) and temperature in degrees Fahrenheit (°F).
If the oil pressure pointer enters the yellow band, a caution is issued. If the oil pressure or oil temperature
pointers enter the red band, a warning is issued.
Figure 3-10 Oil Pressure and Temperature Gauges
CAbIN PRESSURIZATION (MIRAGE ONLY)
Cabin pressurization information (cabin altitude, rate of change, and differential cabin pressure) is shown at
the upper right area of the Mirage EICAS column (Figure 3-11).
Cabin altitude (ALT FT) is shown on a color-coded vertical scale with a readout (in feet) displayed below.
Cabin altitude change rate (RATE FPM) is also shown on a vertical scale with a readout (in fpm) displayed
below. Cabin pressure differential (DIFF PSI) is shown on a color-coded horizontal scale with a readout (in
pounds per square inch; psi) displayed above. Warnings are issued for excessive cabin altitude or differential
pressure. In Reversionary Mode, only readouts for cabin altitude and differential pressure are displayed.
Figure 3-11 Cabin Pressurization Display (Mirage)
Cabin
Altitude
Pressure
Change
Rate
Pressure
Differential