Garmin G1000 Manual

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 85097
ENGINE & AIRFRAME SYSTEMS
ELECTRICAL SYSTEM
The Electrical Synoptics Page uses a diagram of the aircraft’s electrical system to display the system status.  The 
generators, ground power supply (GPU), batteries, and buses are shown in green to denote normal operation.    
Color of the units change depending on the condition.
Figure 3-16  Electrical Synoptics Page
1Standby Generator
2Main Generator
3Ground Power Unit Door
4Battery...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A98
ENGINE & AIRFRAME SYSTEMS
Active generator currents are displayed below the generator icons.  A disconnected generator is indi\
cated in 
gray; the current is removed from the display and the switch symbol is closed.
ConnectedDisconnectedConnectedDisconnected
Figure 3-17  Generator Status
GPU status information is removed from the electrical diagram when the GPU door is closed.  If the GPU door \
is open and selected, the GPU...

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 85099
ENGINE & AIRFRAME SYSTEMS
Battery and essential bus voltages are displayed using gauges.  DC buses are shown in green when energized.  
When not energized, the connection line to the main bus is removed and the bus label is displayed in red.
Figure 3-20  Battery and Essential Bus Low Voltage
Figure 3-21  DC Bus Status
Bus Not Energized
The Emergency Buses switch has two positions, UP (open) and DN (ground).  If the switch is in the...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A100
ENGINE & AIRFRAME SYSTEMS
FUEL SYSTEM
The Fuel Synoptics Page displays the status of the fuel tanks and feed s\
ystem.  Fuel quantity is depicted 
graphically; the color changes to yellow if the fuel quantity drops below the threshold level.
Figure 3-23  Fuel Synoptics Page
1Left Fuel Tank
2Left Fuel Line
3Fuel Pressure
4Engine Driven Boost Pump
5Auxiliary Boost Pump
6Fuel Selector
7Right Fuel Tank
8Right Fuel Line
9Fuel Flow Data...

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 850101
ENGINE & AIRFRAME SYSTEMS
Status of the fuel selector is indicated between the fuel tank symbols.  The mode, automatic (AUTO) or 
manual (MAN) is shown beneath the fuel selector symbol.
Left  Fuel Tank 
Selected
Switching Fuel 
Tank Selection
Right  Fuel Tank 
Selected
Manual or 
Unknown Fuel 
Tank Selection
Fuel Selector
Off
Table 3-1  Fuel Selector Status
If the auxiliary fuel boost pump is on, the symbol is displayed in green....

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A102
ENGINE & AIRFRAME SYSTEMS
GENERAL SYSTEMS
The General Synoptics Page aircraft diagram displays open doors in red (CAS messages also generated).  
Statuses of stall sensor, propeller, pitot probes, and windshield heat are also indicated on the diagram:
•	 White	indicates	that	heat	is	off	(propeller	and	windshield)
•	 Light	blue	indicates	heat	has	been	selected	(windshield)
•	 Green	indicates	heat	is	on
•	 Yellow	indicates	heat	has...

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 850103
ENGINE & AIRFRAME SYSTEMS
3.3 CREW ALERTING SYSTEM (CAS)
 NOTE: Refer to the Pilot’s Operating Handbook (POH) for emergency procedures.
 NOTE: Aural alerts associated with abnormal conditions and advisories are mana\
ged through the audio 
panels.  Refer to the Audio Panel and CNS Section for more information.
The Crew Alerting System (CAS) Display is located in the lower left corner of the EICAS Display (on the MFD) 
under normal...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A104
ENGINE & AIRFRAME SYSTEMS
CAS DISPLAY INHIBITS
Inhibits prevent certain CAS messages from being displayed during one or more of the following conditions:
•	 Engine
Takeoff and Landing Operation Phase inhibits (TOPI and LOPI) are implemented to reduce flight crew 
workload and distractions during takeoff and landing.  The following tables list the criteria which must be met\
 
to activate or deactivate TOPI or LOPI; only one...

190-00709-04  Rev.  AGarmin G1000 Pilot’s Guide for the Socata TBM 850105
ENGINE & AIRFRAME SYSTEMS
CAS MESSAGES AND PRIORITIZATION
 NOTE: Refer to the Pilot’s Operating Handbook (POH) for corrective pilot actions.
 NOTE: Red warning messages cannot be scrolled through and remain at the top of the \
CAS display.  The 
scroll bar changes to yellow if more than ten caution messages exist to \
be scrolled through.
CAS messages are grouped by criticality (warning, caution) and sorted by order of appearance...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev.  A106
ENGINE & AIRFRAME SYSTEMS
When a new yellow caution message appears on the CAS display, it flashes (inversely black on yellow)  
in conjunction with the Master Caution Indicator.  Pressing the Master Caution Indicator acknowledges all 
flashing yellow messages, extinguishes the master caution lights, and \
stops caution message flashing.  Messages 
are displayed until the issue is corrected.
Inhibits
MessagesComments
ENGINE...