190-01115-01 G3X™/G3X Touch™ Avionics Installation Manual
Rev. AV Page 20-16
20.6 ARINC 743 Footprint Antenna Installation (GA 36, GA 37, GA 55A, GA 57X)
This section describes the structural mounting of the ARINC 743 footprint antenna (GA 36, GA 37, GA
55A, GA 57X) installation. One acceptable method is to use Garmin P/N: 115-00846-00 doubler plate.
Another acceptable method is to fabricate and install one of three doublers, Figure 20-14
, Figure 20-15, or
Figure 20-16
, depending on the thickness of the skin. The three doubler designs vary only by number of
rivets and hole preparation for installation with flush rivets. Figure 20-24
shows installation of the ARINC
743 footprint antenna.
Table 20-6 provides a summary of design and installation details for the antenna doubler. Figure 20-17
shows an example of the doubler installed between stringers on the top fuselage skin, just off centerline.
The location should be flat, with no gaps between the skin and doubler, to keep from deforming the skin
during installation.
20.6.1 Preparation of Doubler
1. Use Garmin P/N: 115-00846-00, or refer to Table 20-6 for guidance on selecting the appropriate
doubler drawing based on the thickness of skin at the antenna location. Make the doubler from
2024-T3 Aluminum (AMS-QQ-A-250/5), 0.063” sheet thickness.
2. For installation in aircraft skins of thickness less than 0.051”, countersink the rivet holes in the
doubler for use with flush head rivets (MS20426AD4-x).
3. When using Garmin P/N: 115-00846-00 doubler, sixteen rivet holes exist in the part. For
installation of Garmin P/N: 115-00846-00 in skins of thickness between 0.032” and 0.049”, only
the rivets identified for use through the skin cutout detail (Figure 20-18
) and doubler installation
(Figure 20-21
) are required.
Table 20-6 ARINC 743 Footprint Antenna Doubler Design and Installation
Skin Thickness 0.032” to 0.049” 0.049” to 0.051” 0.051” to 0.063”
Doubler Design (Figure) Figure 20-14 Figure 20-15 Figure 20-16
Number of Rivets Required 12 16 16
Type of Rivets Required
1
MS20426AD4-x MS20426AD4-x MS20426AD4-x
Skin Preparation for Rivets Dimple Dimple Countersink
Doubler Preparation for Rivets Countersink Countersink None
Skin Cutout Detail (GA 55A) Figure 20-18 Figure 20-19 Figure 20-20
Doubler Installation (Figure) Figure 20-21 Figure 20-22 Figure 20-23
1
Rivet length determined at installation, dependent on thickness of material (rivet length = grip length +
1.5 * rivet diameter)
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