Garmin G1000 Manual

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A607
ADDITIONAL FEATURES
 Or:
1) Press the MENU Key to display the Page Menu.
2) Turn either FMS Knob to place the cursor on ‘Sort By Address’.
3) Press the ENT Key.  The sorting selection is indicated at the bottom center of the list windo\
w.
Viewing the content of a text message:
1) While viewing the AUX-TEXT MESSAGING Page, select the desired message box.
2) Press the FMS Knob to activate the cursor.
3) Turn either FMS Knob to select...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A608
ADDITIONAL FEATURES
 Or:
a) Press the MENU Key to display the Page Menu.
b) Turn either FMS Knob to place the cursor on ‘Close Message’.
c) Press the ENT Key.
Marking selected message as read:
1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the FMS Knob to activate the cursor.
2) Turn either FMS Knob to select the desired message.
3) Select the MRK READ Softkey.
 Or:
a) Press the MENU Key to display the Page Menu....

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A609
ADDITIONAL FEATURES
8.11 ABNORMAL OPERATION
SVS TROUBLESHOOTING
SVS	is	intended	 to	be	 used	 with	traditional	 attitude,	heading,	 obstacle,	 terrain,	and	traffic	 inputs.	 	 SVS	is	
disabled	 when	valid	attitude	 or	heading	 data	is	not	 available	 for	the	 display.		 In	case	 of	invalid	 SVS	data,	 the	PFD	
display	reverts	to	the	standard	blue-over-brown	attitude	display.
SVS	becomes	disabled	without	the	following	data...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A610
ADDITIONAL FEATURES
UNUSUAL ATTITUDES
Unusual attitudes are displayed with red chevrons overlaid on the display indicating the direction to fly to 
correct	the	unusual	 attitude	condition.	 	 The	display	 shows	either	a	brown	 or	blue	 colored	 bar	at	the	 top	 or	
bottom	 of	the	 screen	 to	represent	 earth	or	sky.		 This	is	intended	 to	prevent	 losing	sight	of	the	 horizon	 during	
extreme	pitch	attitudes.
Figure 8-106  Unusual...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A611
ADDITIONAL FEATURES
GDL 69/69A DATA LINK RECEIVER TROUBLESHOOTING
Some	quick	troubleshooting	steps	listed	below	can	be	performed	to	find	the	possible	cause	of	a	failure.
•	 Ensure	the	owner/operator	 of	the	 aircraft	 in	which	 the	Data	 Link	 Receiver	 is	installed	 has	subscribed	 to	
SiriusXM
•	 Ensure	the	SiriusXM	subscription	has	been	activated
•	 Perform	a	quick	check	of	the	circuit	breakers	to	ensure	that	power	is	applied	to...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A612
ADDITIONAL FEATURES
If	a	failure	still	exists,	the	following	messages	may	provide	insight	as	to	the	possible	problem:
MessageMessage LocationDescription
CHECK ANTENNAXM Radio Page - active channel fieldData Link Receiver antenna error; service required
UPDATINGXM Radio Page - active channel fieldData Link Receiver updating encryption code
NO SIGNALXM Radio Page - active channel field
Weather Datalink Page - center of pageLoss of...

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 613
APPENDIX A
ANNUNCIATIONS AND ALERTS
CAS MESSAGES
See the Pilot’s Operating Handbook (POH) for recommended pilot actions.
•	Warning (red) – Immediate crew awareness and action required; Master Warning triggered
•	Caution (yellow) – Immediate crew awareness and possible future corrective action required; Master Caution 
triggered
Inhibits prevent certain CAS messages from being displayed during the following conditions:
•	 Engine...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A614
APPENDIX A
Inhibits
MessagesComments
ENGINE OFFENGINE ONGROUNDTOPIAIRLOPI
AUTO SELFuel timer off or out of serviceX
AUX BOOST PMP ONElectric fuel pump running (manual or automatic mode)
BAT AMPBattery current over 50 A while on groundXXX
BAT OFFBattery offX
BLEED OFFFlow control and shut-off valve/shut-off valve closedXXX
CHIPOil chip detector on (if installed)XX
FRONT CARGO DOORForward baggage door openX
FUEL IMBALANCEFuel tanks...

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 615
APPENDIX A
COMPARATOR ANNUNCIATIONS
The	Comparator monitors critical values generated by redundant sensors.  If differences in the sensors exceed 
a specified amount, this discrepancy is annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare) 
as seen in Figure A-1.  If one or both of the sensed values are unavailable, it is annunciated as a ‘NO COMP’ (no 
compare).		The	following	is	a	list	of	the	possible	annunciations:...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A616
APPENDIX A
REVERSIONARY SENSOR ANNUNCIATIONS
Reversionary	sensor	selection	 is	annunciated	 in	the	 Reversionary	Sensor Window, as shown in Figure A-2.  
These	 annunciations	 reflect	reversionary	 sensors	selected	 on	one	 or	both	 PFDs.	 	 Selecting	 the	SENSOR Softkey 
gives access to ADC1, ADC2, AHRS1, and AHRS2	Softkeys.		 These	softkeys	 allow	manual	 switching	 of	sensors.		 In	
the	 case	 of	certain	 types	of	sensor...