Garmin G1000 Manual

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 85077
FLIGHT INSTRUMENTS
WIND DATA
Wind	direction	 and	speed	 in	knots	 can	be	displayed	 relative	to	the	 aircraft	 in	a	window	 to	the	 upper	 left	of	
the	HSI.		 When	 the	window	 is	selected	 for	display,	 but	wind	 information	 is	invalid	 or	unavailable,	 the	window	
shows	NO	WIND	DATA.		Wind	data	can	be	displayed	in	three	different	ways.
Figure 2-35  Wind Data
No Data
Option 2
Option 1
Option 3
Displaying wind data:
1) Press the PFD...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A78
FLIGHT INSTRUMENTS
VERTICAL NAVIGATION (VNV) INDICATIONS
When	a	VNV	 flight	 plan	has	been	 activated,	 VNV	indications	 (VNV	Target	 Altitude,	 RVSI,	VDI)	appear	 on	the	
PFD	 in	conjunction	 with	the	“TOD	 within	 1	minute	 message”	 and	“Vertical	 track”	voice	alert.	 	 See	the	Flight	
Management	 and	AFCS	 sections	 for	details	 on	VNV	 features.	 	 VNV	indications	 are	removed	 from	the	PFD	
according	to	the	criteria	listed	in...

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 85079
FLIGHT INSTRUMENTS
2.3 PFD ANNUNCIATIONS AND ALERTING FUNCTIONS
The	 following	 annunciations	 and	alerting	 functions	 are	displayed	 on	the	 PFD.	 	 Refer	to	the	 Engine/Airframe	
Systems	 Section	for	information	 on	the	 Crew	 Alerting	 System	(CAS)	and	to	Appendix	 A	for	 more	 information	 on	
alerts and annunciations.
SYSTEM ALERTING
The System Messages Window conveys messages to the flight crew regarding problems with the...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A80
FLIGHT INSTRUMENTS
MARKER BEACON ANNUNCIATIONS
Marker	Beacon	Annunciations	 are	displayed	 on	the	 PFD	 to	the	 left	of	the	 Selected	 Altitude.	 	 Outer	marker	
reception	 is	indicated	 in	blue,	 middle	 in	amber,	 and	inner	 in	white.		 Refer	to	the	 Audio	 Panel	and	CNS	 Section	
for	more	information	on	Marker	Beacon	Annunciations.
Figure 2-38  Marker Beacon Annunciations
Outer Marker
Middle Marker
Inner Marker
Altimeter
TRAFFIC...

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 85081
FLIGHT INSTRUMENTS
TERRAIN ANNUNCIATIONS
Terrain	Awareness	 and	Warning	 System	(TAWS)	or	TERRAIN-SVS	 annunciations	appear	on	the	 PFD	 to	the	
upper	 left	of	the	 altimeter.		 Refer	to	the	 Hazard	 Avoidance	 Section	and	Appendix	 A	for	 information	 on	terrain	
alerts and annunciations.
Figure 2-40  Traffic and Example Terrain Annunciations  

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A82
FLIGHT INSTRUMENTS
ALTITUDE ALERTING
The	Altitude	Alerting	function	provides	visual	alerts	when	approaching	the	Selected	Altitude,	and	visual	and	
aural	alerts	when	deviating	from	the	selected	altitude.		Whenever	the	Selected	Altitude	on	the	PFD	is	changed,	
Altitude	Alerting	is	reset.		Altitude	Alerting	is	independent	of	the	AFCS.
The	following	occur	when	approaching	the	Selected	Altitude:
•	 Upon	passing	through	 1000	feet	of	the...

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 85083
FLIGHT INSTRUMENTS
MINIMUM DESCENT ALTITUDE/DECISION HEIGHT ALERTING
For	altitude	 awareness,	 a	Minimum	 Descent	Altitude	 (MDA)	or	Decision	 Height	(DH),	based	on	barometric	
altitude or radar altitude, can be set.  When active, the altitude setting is displayed to the lower left of the 
altimeter and with a bug at the corresponding altitude along the altimeter (once the altitude is within the\
 visible 
range	of	the	tape).		The...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A84
FLIGHT INSTRUMENTS
RADAR ALTIMETER
When the radar height (the aircraft altitude above ground level detected by the radar altimeter) is between 
zero	and	2500	 feet,	the	current	 value	is	displayed	 in	green	 to	the	 upper	 right	of	the	 HSI	 (Figure	 2-45).	Display	
of	radar	height	becomes	more	sensitive	as	the	height	above	ground	decreases	(Table	2-3).
Figure 2-45 Current Radar Height
Radar Altimeter
Radar Height Range Shown to...

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 85085
FLIGHT INSTRUMENTS
A	ground	 line	(Figure	 2-48)	is	shown	 on	the	 Altimeter	 to	display	 the	aircraft’s	 height	relative	 to	the	 ground.		
If	the	 data	 becomes	 invalid,	the	message	 “RA	FAIL”	 is	displayed	 in	yellow	 in	place	 of	the	 current	 radar	height	
(Figure	 2-49).	 	The	Radar	 Altimeter	 test	is	done	 on	the	 MFD	 but	is	displayed	 on	the	 PFD	 directly	 above	the	
Radar	Altimeter	box	(Figure	2-50).
Figure 2-48...

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A86
FLIGHT INSTRUMENTS
2.4 ABNORMAL OPERATIONS
ABNORMAL GPS CONDITIONS
The	 annunciations	 listed	in	Table	 2-4	can	 appear	 on	the	 HSI	 when	 abnormal	 GPS	conditions	 occur	(Figure	
2-52).		Refer	to	the	Flight	Management	Section	for	more	information	on	Dead	Reckoning	Mode.
AnnunciationLocationDescription
LOILower left of 
aircraft symbol
Loss of Integrity Monitoring–GPS integrity is insufficient for the \
current 
phase of flight...