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Garmin G1000 Manual

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Page 661

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 647
APPENDIX C
ACC accuracy
ACT, ACTV active,  activate
ADC air data computer
ADF Automatic Direction Finder
ADI Attitude Direction Indicator
AF Arc to fix
AFCS Automatic Flight Control System
AFM Airplane Flight Manual
AFMS Airplane Flight Manual Supplement
AFRM airframe
AGL Above Ground Level
AHRS Attitude and Heading Reference System
AIM Aeronautical Information Manual
AIRMET Airman’s Meteorological Information
ALRT alert
ALT...

Page 662

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A648
APPENDIX C
DCLTR, DECLTR declutter
DEC FUEL decrease fuel
deg degree
DEIC, DEICE de-icing
DEP departure
Desired Track The desired course between the active 
“from” and “to” waypoints.
DEST destination
DF Direct to Fix
DFLT default
DGRD degrade
DH decision height
Dilution of Precision A measure of GPS satellite geometry 
quality on a scale of one to ten (lower 
numbers equal better geometry, where 
higher numbers equal poorer...

Page 663

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 649
APPENDIX C
G/S, GS glideslope
GA go-around
gal, gl gallon(s)
GBOX gearbox
GDC Garmin Air Data Computer
GDL Garmin Satellite Data Link
GDU Garmin Display Unit
GEA Garmin Engine/Airframe Unit
GEO geographic
GFC Garmin Flight Control
GIA Garmin Integrated Avionics Unit
GLS Global Navigation Satellite Landing 
System
GMA Garmin Audio Panel System
GMC Garmin Mode Controller
GMT Greenwich  Mean Time
GMU Garmin Magnetometer Unit
GND...

Page 664

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A650
APPENDIX C
Left Over Fuel Reserve The amount of flight time remaining, 
based on the amount of fuel on board 
after the completion of one or more legs 
of a flight plan or direct-to, and a known 
consumption rate.
Leg The portion of a flight plan between two 
waypoints.
LIFR Low Instrument Flight Rules
LNAV Lateral Navigation
LO low
LOC localizer
LOI loss of integrity (GPS)
LON longitude
LPV Localizer Performance with Vertical...

Page 665

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 651
APPENDIX C
REF reference
REM remaining (fuel remaining above 
Reserve)
REQ required
RES reserve (fuel reserve entered by pilot)
REV reverse, revision, revise
RF Constant Radius Turn to Fix
RMI Radio Magnetic Indicator
RMT remote
RNG range
RNWY runway
ROL roll
ROM read only memory
rpm revolutions per minute
RST FUEL reset fuel
RSV reserve (fuel reserve entered by pilot)
RT right
RVRSNRY reversionary
RX receive
S south
SA Selective...

Page 666

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A652
APPENDIX C
VERT vertical
Vertical Figure of Merit A measure of the uncertainty in the 
aircraft’s vertical position.
Vertical Speed Required The vertical speed necessary to descend/
climb from a current position and altitude 
to a defined target position and altitude, 
based upon current groundspeed.
VFOM Vertical Figure of Merit
VFR Visual Flight Rules
VHF Very High Frequency
VI Heading Vector to Intercept
VLOC VOR/Localizer...

Page 667

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 653
APPENDIX D
FREQUENTLY ASKED QUESTIONS
If	a	particular	 aspect	of	G1000	 operational	 capability	is	not	 addressed	 by	these	 commonly	 asked	questions	 or	in	
the	 index,	 contact	 Garmin	 (see	the	copyright	 page	or	back	 cover	 for	contact	 information)	 or	a	Garmin-authorized	
dealer.		Garmin	is	dedicated	to	supporting	its	products	and	customers.
What is sB as?
The	 Satellite	 Based	Augmentation	 System	(SBAS)	uses	a	system	 of...

Page 668

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A654
APPENDIX D
For	RAIM	 to	work	 correctly,	 the	GPS	 receiver	 must	track	 at	least	 five	satellites.		 A	minimum	 of	six	 satellites	 is	
required	to	allow	RAIM	to	eliminate	a	single	corrupt	satellite	from	the	navigation	solution.
RAIM	ensures	 that	satellite	 geometry	 allows	for	a	navigation	 solution	calculation	 within	a	specified	 protection	
limit	(2.0	nm	for	oceanic	 and	en	route,	 1.0	nm	 for	terminal,	 and	0.3	nm	 for...

Page 669

190-00709-04  Rev. AGarmin G1000 Pilot’s Guide for the Socata TBM 850 655
APPENDIX D
Normal (OBS not activated)
•	Automatic sequencing of waypoints 
•	 Manual
When	 OBS	mode	 is	active,	 the	G1000	 allows	the	pilot	 to	set	 a	desired	 course	to/from	 a	waypoint	 using	the	
CRS/BARO Knob	and	HSI	(much	like	a	VOR).
The	most	 common	 application	 for	using	 the	OBS	Softkey	 is	the	 missed	 approach.	 	 The	G1000	 suspends	
automatic	 waypoint	sequencing	 (indicated	by	a	‘SUSP’	 annunciation	 placed	on	the...

Page 670

Garmin G1000 Pilot’s Guide for the Socata TBM 850190-00709-04  Rev. A656
APPENDIX D
When DOes the cDi scale change?
Once	a	departure	 is	activated,	 the	G1000	 Course	 Deviation	 Indicator	(CDI)	full	scale	 deflection	 is	set	 to	0.3	
nm.	 	 The	CDI	 scale	 changes	 to	1.0	 nm	 (terminal	 mode)	then	ramps	 up	to	2.0	 nm	 (enroute	 mode)	at	30	 nm	
from	 the	departure	 airport.		When	31	nm	 from	 the	destination,	 the	CDI	 scale	 smoothly	 transition	 from	2.0	nm		
back	 to	1.0	 nm	 (terminal	 mode).		At...
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