Garmin Pilatus PC_6 Guide de l'utilisateur Page 391

  • Télécharger
  • Ajouter à mon manuel
  • Imprimer
  • Page
    / 404
  • Table des matières
  • MARQUE LIVRES
  • Noté. / 5. Basé sur avis des utilisateurs
Vue de la page 390
190-00870-00 Rev. B
Garmin G950 Pilot’s Guide for the Pilatus PC-6
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EIS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES INDEX
379
APPENDIX E
GENERAL TIS INFORMATION
NOTE
: Aircraft without an operating transponder are invisible to TIS.
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 meterorlogical conditions (IMC) or when there is no visual contact with the intruder aircraft.
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 G950 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 G950
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.
The main difference between the Traffic Information System (TIS) and Traffic Advisory (TAS) or Traffic Collision
Avoidance Systems (TCAS) is the source of surveillance data. 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 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.
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.
NOTE
: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in
mountainous regions.
Vue de la page 390
1 2 ... 386 387 388 389 390 391 392 393 394 395 396 ... 403 404

Commentaires sur ces manuels

Pas de commentaire