Engine indication and crew alerting system – Garmin G1000 Piper PA-46 Meridian User Manual
Page 111

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