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

Page 111

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190-00763-01 Rev. A

Garmin G1000 Pilot’s Guide for the Piper PA-46 Meridian

97

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

Caution Messages

Description

ESDI ESI GROUND TOPI AIR LOPI

BETA

Propeller is operating in Beta mode

X

CABIN ALT 10000

Cabin altitude is above 10,000 feet

CHIP DETECT

Chip detect

X

X

FEATHER

Propeller is feathered or a failure has occurred in the feather
system

FIRE DETECT FAIL

Fire detection system has failed

X

X

FUEL FILTER

Fuel filter approaching bypass and requires maintenance

X

X

FUEL IMBALANCE

Fuel imbalance is over 40 lbs

X

X

FUEL QTY LOW

Fuel quantity is less than 180 lbs

HYDR PUMP ON

Hydraulic pump is on. Caution has 15 sec. delay

OXYGEN

Oxygen system has been turned on

X X

X

L/R* PITOT HT FAIL

Left or right pitot heat has failed. Displayed as warning if both
fail

X

X

PITOT HEAT OFF

Pitot heat is off

PROP HEAT FAIL

Failure detected in propeller heat system

X

X

STALL WARN FAIL

Failure detected in stall warning system

STARTER ENGAGED

Starter engaged when Ng is more than 56% for more than 10
sec.

X

X

STBY BAT HT FAIL

Standby attitude battery heater failure

X

X

SURF DE-ICE FAIL

Surface de-ice fail

X X

X

X

VACUUM LOW

Vacuum is low

X X

X

X

* Only affected side (L, R) displayed in CAS message; noted CAS messages display L/R as an example

Table 3-4 CAS Caution Messages

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