
Garmin G1000 Cockpit Reference Guide for the Piper PA-46 Meridian
190-00764-03 Rev. C
62
Annunciations & Alerts
Flight
InstrumentsEICAS
Nav/Com/
XPDR/AudioAFCSGPS Nav
Flight
PlanningProcedures
Hazard
Avoidance
Additional
Features
Abnormal
Operation
Annun/
AlertsAppendixIndex
Caution Messages
Caution Messages Description
BETA Propeller is operating in Beta mode
CABIN ALT 10000 Cabin altitude is above 10,000 feet
CHIP DETECT Chip detect
FEATHER Propeller is feathered or a failure has occurred in the feather system
FIRE DETECT FAIL Fire detection system has failed
FUEL FILTER Fuel filter approaching bypass and requires maintenance
FUEL IMBALANCE Fuel imbalance is over 40 lbs
FUEL QTY LOW Fuel quantity is less than 180 lbs
HYDR PUMP ON Hydraulic pump is on. Caution has 20 sec. delay
OXYGEN Oxygen system has been turned on (aircraft is in the air)
L/R* PITOT HEAT FAIL Left or right pitot heat has failed. Displayed as warning if both fail.
PITOT HEAT OFF Pitot heat is off
PROP HEAT FAIL Propeller heat failure (aircraft is on the ground)
STALL WARN FAIL Failure detected in stall warning system
STARTER ENGAGED Starter engaged when Ng is more than 56% for more than 10 sec.
STBY BAT HT FAIL Standby attitude battery heater failure
SURF DE-ICE FAIL Surface de-ice fail
VACUUM LOW Vacuum is low
* Only affected side (L, R) displayed in CAS message; noted CAS messages display L/R as an example.
Advisory Messages
Advisory
Messages
Description
ALTERNATOR OFF Alternator is off
BETA Propeller is operating in Beta mode
DOOR AJAR Door is ajar (aircraft is on the ground)
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 (aircraft is on the ground)
STARTER ENGAGED Starter engaged when Ng is less than 56%
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.
Kommentare zu diesen Handbüchern