Garmin ADS-B Out Installation du système - Page 13

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Elliott Aviation Technical Products Development, Inc.

6601 74

Ave Building A

Milan, IL 61264

Instructions for Continued Airworthiness For Garmin ADS-B System Installation

3.1

Overview:

The information contained herein supplements the basic Maintenance Manuals only in those areas listed, when the

aircraft is modified in accordance with Elliott Aviation drawings and diagrams specified in Section 1.3 of this

document.

3.1.1 GTX 3000s are located in the forward right avionics bay upper equipment shelf. A configuration module is

also located inside the J3302 connectors.

3.1.2 GDL 88 is located in the forward right avionics bay upper equipment shelf. A configuration module is also

located inside the J811 connector.

3.1.3 AMCs are located in the forward right and left avionics bays upper equipment shelf.

3.1.4 Flight Stream 110 (if installed) is located on the outboard side of the Co-Pilot's chart holder cabinet.

3.1.5 ADS-B 1/2 annunciator is located in the cockpit panel

3.1.6 GA 36 GPS Antenna is located on top of the aircraft fuselage above the cabin headliner FS 172.00-187.00

left of center line

3.1.7 UAT Antenna is located on the belly of the aircraft fuselage below the left forward avionics bay FS 67.10-

75.80

3.1.8 Wiring follows existing aircraft wire routes in the nose and cockpit area.

3.2

Equipment and wiring access:

No new access is required from the installation of this modification. Access to all equipment and wiring is gained

using existing aircraft maintenance manual techniques.

Chapter 3

ACCESS:

Report No.: ICA-3832-560

Revision: IR

Dated 01/23/2018

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