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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 Availability
SAT Static Air Temperature
SBAS Satellite-Based Augmentation System
SCIT Storm Cell Identification and Tracking
SD Secure Digital
sec second(s)
SEL, SLCT select
SFC surface
SIAP Standard Instrument Approach Procedures
SID Standard Instrument Departure
SIGMET Significant Meteorological Information
Sim simulator
SLP/SKD slip/skid
SMBL symbol
SPD speed
SPI Special Position Identification
SPKR speaker
SQ squelch
SRVC, SVC service
STAL stall
STAR Standard Terminal Arrival Route
STATS statistics
STBY standby
STD standard
SUA Special Use Airspace
SUSP suspend
SVS Synthetic Vision System
SW software
SYS system
T true
TA Traffic Advisory
TACAN Tactical Air Navigation System
TAF Terminal Aerodrome Forecast
TAS True Airspeed
TAS Traffic Advisory System, true airspeed
TAT Total Air Temperature
TAWS Terrain Awareness and Warning System
TCA Terminal Control Area
TCAS Traffic Collision Avoidance System
TEL telephone
TEMP temperature
TERM terminal
TF Track Between Two Fixes
TFR Temporary Flight Restriction
T HDG True Heading
TIS Traffic Information System
TIT Turbine Inlet Temperature
TKE Track Angle Error
TMA Terminal Maneuvering Area
TMR/REF Timer/Reference
Topo topographic
Track Direction of aircraft movement relative to a ground position; also ‘Ground Track’
Track Angle Error The angle difference between the desired track and the current track.
TRG target
TRK track
TRSA Terminal Radar Service Area
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES 518
Appendix C
TRUNC truncated
TTL total
TURN procedure turn
TX transmit
UNAVAIL unavailable
USR user
UTC Coordinated Universal Time
UTM/UPS Universal Transverse Mercator / Universal Polar Stereographic Grid
V, Vspeed velocity (airspeed)
VA Heading Vector to Altitude
VAPP VOR approach
VAR variation
VD Heading Vector to DME Distance
Vdc volts, direct current
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 Receiver
VM Heading Vector to Manual Termination
VMC Visual Meteorological Conditions
VNAV, VNV vertical navigation
VOL volume
VOR VHF Omni-directional Range
VORTAC very high frequency omnidirectional range station and tactical air navigation
VPL Vertical Protection Level
VPROF VNV profile, vertical profile
VPTH VNV path, vertical path
VR Heading Vector to Radial
VS vertical speed
VSI Vertical Speed Indicator
VSR Vertical Speed Required
VTF vector to final
W watt(s), west
WAAS Wide Area Augmentation System
WARN warning (GPS position error)
WGS-84 World Geodetic System - 1984
WPT waypoint(s)
WW world wide
WX weather
XFER, XFR transfer
XPDR transponder
XTALK cross-talk
XTK cross-track
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
519
Appendix D
Frequentlyuently 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 WAAS?
The Wide Area Augmentation System (WAAS) uses a system of ground stations to correct any GPS signal errors. These ground stations correct for errors caused by ionospheric disturbances, timing, and satellite orbit errors. It also provides vital integrity information regarding the health of each GPS satellite. The signal correction is then broadcast through one of two geostationary satellites. This correction information can then be received by any WAAS-enabled GPS receiver.
　
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