Garmin ADS-B Installation du système - Page 10

Parcourez en ligne ou téléchargez le pdf Installation du système pour {nom_de_la_catégorie} Garmin ADS-B. Garmin ADS-B 22 pages.

Elliott Aviation Technical Products Development, Inc.

6601 74

Ave Building A

Milan, IL 61264

Instructions for Continued Airworthiness For Garmin ADS-B System Installation

GTX 3000 Configuration Status Sample Page:

2.3.2.10 For troubleshooting an in-service system, GPS activity may be confirmed using this "Info / ADS-B

Out" page. Lack of GPS position may be due to GDL 88 issues such as disconnect antenna coax,

faulty antenna or faulty GDL 88. See 2.5 above. If the GDL 88 is not suspect, suspect RS 232

interface, configuration or GTX 3000 transponder. The GTX 3000 is not field serviceable. If faulty,

the GTX 3000 line replaceable unit may only be repaired by Garmin.

2.3.2.11 For troubleshooting an in-service system, heading activity may be confirmed using this "Info / EHS"

page. Lack of heading may be due to suspect 429 interface or configuration. The GTX 3000

heading source is the same as is used for the Flight Crew presentations The GTX 3000 is not field

serviceable. If faulty, the GTX 3000 line replaceable unit may only be repaired by Garmin.

2.3.2.12 For troubleshooting an in-service system, the above may be confirmed using this "Status" page:



2.3.2.13 The GTX 3000 is not field serviceable. If faulty, the GTX 3000 line replaceable unit may only be

repaired by Garmin.

Weight on wheels is operating correctly. (squat switch, wiring and config).

ADS-B mode indicated. (GDL 88, valid 429 data, wiring and config).

4096 code agrees with RMU ATC settings. Access the Pro Line control display unit and

exercise the squawk codes, the GTX 3000 should indicate correctly almost immediately.

(wiring and config).

Flight ID agrees with RMU ATC settings. Select reversionary mode on the associated

instrument panel to enable off-side control display unit GTX 3000 control. (RMU, wiring and

config).

TCAS status correct for aircraft. Most aircraft will have TCAS installed. Confirm TCAS by

visual observation of directional antennas and / or Pro Line control display unit TCAS page.

Confirm no faults if TCAS installed and the ADS-B system is interfaced properly. (wiring and

config).

Report No.: ICA-3832-560

Revision: IR

Dated 01/23/2018

10 of 21