Garmin 695 Manual De Usuario

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Garmin GPSMAP 695/696 Owner’s Manual
190-00919-00  Rev. G
Appendix E
222
Overview
GPS Navigation
Flight Planning
Hazar
d A
voidance
Additional F
eatur
es
Appendices
Index
TIS-A LIMITATIONS
TIS-A relies on surveillance of the Mode-S radar system, which is a “secondary 
surveillance” radar system similar to that used by ATCRBS.  Many limitations are 
inherent in secondary radar surveillance.  Information provided by TIS-A is neither 
better nor more accurate than the information used by ATC.  TIS-A is intended only to 
assist in visual acquisition of other aircraft in visual meteorological conditions (VMC).  
While TIS-A is a useful aid for visual traffic avoidance, system limitations must be 
considered to ensure proper use.  No recommended avoidance maneuvers are given, 
nor authorized, as a direct result of a TIS-A intruder display or TIS-A advisory.
• TIS-A operation may be intermittent during turns or other maneuvering.
• TIS-A is dependent on two-way, line-of-sight communications between the aircraft
and the Mode-S radar antenna.  Whenever the structure of the aircraft comes 
between the transponder antenna and the ground-based radar antenna, the signal 
may be temporarily interrupted.
 NOTE: Refer to the TIS-A Limitations section of the Aeronautical Information 
Manual (AIM) for a more comprehensive explanation of limitations and 
anomalies associated with TIS-A.
 NOTE: TIS-A is unavailable at low altitudes in many area of the United States.  
This is often the case in mountainous regions.
 NOTE: Garmin is not responsible for Mode S geographical coverage.  Operation 
of the ground stations is the responsibility of the FAA.  Refer to the AIM for a 
Terminal Mode S radar site map.
TIS-A information is collected during a single radar sweep.  Collected information 
is then sent through the Mode S uplink on the next radar sweep.  Because of this, the 
surveillance information is approximately five seconds old.  TIS-A ground station tracking 
software uses prediction algorithms to compensate for this delay.  These algorithms 
use track history data to calculate expected intruder positions consistent with the time 
of display.  Occasionally, aircraft maneuvering may cause variations in this calculation 
and create slight errors on the Map Page which affect relative bearing information and