Garmin G1000 Piper PA-46 Meridian - Manual (Page 104)

Garmin G1000 Pilot’s Guide for the Piper PA-46 Meridian 190-00763-01 Rev. A 90
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
CAbIN PRESSURIZATION
Cabin pressurization information (cabin altitude, rate of change, and differential cabin pressure) is shown at
the top of the right EICAS column. Only readouts for cabin altitude and pressure differential are displayed in
Reversionary Mode.
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.
Figure 3-10 Cabin Pressurization Display
Pressure
Altitude
Pressure
Change
Rate
Pressure
Differential
FUEL INFORMATION
The fuel display is located beneath the differential pressure scale and shows the fuel quantity in each tank
(pounds, lbs), fuel flow (pounds per hour, pph), and fuel temperature (°C). Fuel quantity for each tank is
normally shown along a slider scale. Only readouts appear for all fuel information in Reversionary Mode.
Fuel
Flow
Fuel
Temperature
Figure 3-11 Fuel Display
Tank Fuel
Quantities