Engine indication and crew alerting system – Garmin G1000 Piper PA-46 Meridian User Manual
Page 112
Garmin G1000 Pilot’s Guide for the Piper PA-46 Meridian
190-00763-01 Rev. A
98
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
Inhibits
Advisory Messages
Description
ESDI ESI GROUND TOPI AIR LOPI
ALTERNATOR OFF
Alternator is off
BETA
Propeller is operating in Beta mode
DOOR AJAR
Door is ajar
EMER BLEED ON
Emergency bleed is on
FEATHER
Propeller is feathered
L/R* FUEL PUMP ON
Left or right fuel pump is on. Inhibited if fuel pump is on for
fuel autobalance when imbalance is less than 40 lbs.
FUEL TEMP
Fuel temperature is low
GENERATOR OFF
Generator is off
IGNITION ON
Engine ignition is on
OXYGEN
Oxygen system has been turned on
X
X
STARTER ENGAGED
Starter engaged when Ng is less than 56%
X
X
STBY BAT TEST OK
Standby attitude battery test pass (standby attitude indicator
must be off)
* Only affected side (L, R) displayed in CAS message; noted CAS messages display L/R as an example
Table 3-5 CAS Advisory Messages