Garmin GPSMAP 800 Series Manuel de l'opérateur - Page 13

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Également pour Garmin GPSMAP 800 Series : Manuel de démarrage rapide (17 pages), Addendum au manuel du pilote (22 pages), Manuel du propriétaire (40 pages), Manuel de démarrage rapide (4 pages), Manuel du propriétaire (46 pages), Manuel d'instructions d'installation (6 pages), Manuel d'instructions d'installation (34 pages), Manuel d'instructions d'installation (6 pages)

Garmin GPSMAP 800 Series Manuel de l'opérateur
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2-1. General

Traffic alerts are automatic. The GTS 800 sends all the
data to the display system. Pilot control of the GTS 800 is
through the interfaced control and display unit, the GDU
1040H.
The traffic system must be in Operating Mode for traffic to
be displayed and for traffic advisories (TA) to be issued.
After power up, the traffic system is in Standby Mode. The
GTS 800 must be in Operating Mode for traffic to be
displayed and for TAs to be issued.
Check that the remote TAS ON/OFF switch is
switched ON. If set to OFF, the NO DATA
annunciation will be displayed. (The switch may
be left ON during engine starting as it is
interfaced with the avionics master switch.)
The GTS 800 will automatically transition from
STANDBY to OPERATE mode or from OPERATE
to STANDBY mode based on input received from
the G1000H.
Switching from Standby Mode to Operating Mode:
1. On the Traffic Page, select the OPERATE SoftKey, or
press the MENU Key and turn the small FMS knob to
select 'Operate Mode'.
2. Press the ENT Key.
Switching from Operating Mode to Standby Mode:
1. On the Traffic Page, select the STANDBY SoftKey, or
press the MENU Key and turn the small FMS knob to
select 'Standby Mode'.
2. Press the ENT Key.
FAA Approved:
Report No. 28-AC-061
This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment
Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision
ENSTROM 480B RFM SUPPLEMENT
CHAPTER 2. NORMAL PROCEDURES
level of this Rotorcraft Flight Manual Supplement.
NOTE
NOTE
2-1
Rev. 1
Mar 21/17