190-01895-00 Rev. A
Garmin G1000 Pilot’s Guide for the Diamond DA62
SY
STEM
O
VER
VIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO P
ANEL
& CNS
FLIGHT
MANA
GEMENT
HAZARD
AV
OID
ANCE
AFCS
ADDITIONAL
FEA
TURES
APPENDICES
INDEX
603
APPENDIX E
GENERAL TIS INFORMATION
INTRODUCTION
NOTE
:
Aircraft without an operating transponder are invisible to TIS.
The Traffic Information Service (TIS) provides traffic advisory information to non-TAS/TCAS-equipped
aircraft. TIS is a ground-based service providing the relative locations of all ATCRBS Mode-A and Mode-C
transponder equipped aircraft within a specified service volume. The TIS ground sensor uses real-time track
reports to generate traffic notification. The G1000 System displays TIS traffic information on the Traffic Map
Page of the MFD. TIS information may also be displayed for overlay on the MFD Navigation Map Page, as
well as on the PFD Inset Map. Surveillance data includes all transponder-equipped aircraft within the coverage
volume. The G1000 System displays up to eight traffic targets within a 7.5 nm radius, from 3,000 feet below,
to 3,500 feet above the requesting aircraft.
TIS VS. TAS/TCAS
The Traffic Information System (TIS) requires contact with a ground station through a data link radio in
order to receive traffic information. Traffic Advisory (TAS) and Traffic Collision Avoidance Systems (TCAS) are
self-contained. TAS/TCAS uses an airborne interrogator with a half-second update rate, while TIS utilizes the
terminal Mode-S ground interrogator and accompanying data link to provide a five-second update rate. TIS
and TAS/TCAS have similar ranges.
TIS LIMITATIONS
NOTE
:
TIS is not intended to be used as a collision avoidance system and does not relieve the pilot of the
responsibility to “see and avoid” other aircraft. TIS should not be used for avoidance maneuvers during
instrument meteorological conditions (IMC) or when there is no visual contact with the intruder aircraft.
NOTE:
Refer to the TIS Limitations section of the Aeronautical Information Manual (AIM) for a more
comprehensive explanation of limitations and anomalies associated with TIS.
TIS 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 is neither better nor more accurate than the information used by ATC. TIS is intended only
to assist in visual acquisition of other aircraft in visual meteorological conditions (VMC). While TIS 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 intruder display or TIS advisory.
• TIS operation may be intermittent during turns or other maneuvering.
• TIS 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.
• Other limitations and anomalies associated with TIS are described in the AIM.
