Engine indication and crew alerting system – Garmin G1000 Piper PA-46 Meridian User Manual

Page 112

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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

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