Garmin ADS-B Instalación del sistema - Página 17
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Elliott Aviation Technical Products Development, Inc.
th
6601 74
Ave Building A
Milan, IL 61264
Instructions for Continued Airworthiness For Garmin ADS-B System Installation
10.1 Structural inspection requirements and intervals:
.
Structural Element (skin)
Location: Between FS 172.00 and 187.00 over cabin headliner LH of centerline
GPS Antenna, connector hole
GPS Antenna, fastener hole
Location: Between FS 67.10 and 75.80 lower fuselage LBL: 10.0
UAT Antenna, connector hole
UAT Antenna, fastener hole
10.1.1
Definition of "flight":
One flight within the context of this damage tolerance assessment is
The inspection intervals take effect from the date of installation. Any existing inspection requirements established by the
manufacturer for the affected structure are also applicable.
The connector and fastener holes should be inspected using eddy current inspection techniques, according to the
intervals outlined in the tables above.
10.2 Inspection Procedures:
The inspection should include the following structural details:
Modification
Affected
GPS Antenna,
Skin
UAT Antenna
When inspecting the antenna installations, accomplish the following:
1.
For the GPS antenna, remove cabin headliner panel for access to coax, disconnect the coax. For the
UAT antenna, remove the LH nose avionics compartment door. Remove the antenna attach screws and
the antenna. Carefully remove any remaining old sealant from airplane skin and attachment hardware. .
FEB 09 2018
FAA Approved Date:_________________
Antenna Installations: 237-3832-M0560-010
Antenna Installations: 237-3832-M0560-010
one takeoff and landing.
Structural Detail
Connector hole
Doubler fastener
holes
Threshold (flights)
10,271
4,835
13,016
7,466
Inspection Notes
Inspect edge of hole in skin.
Inspect fastener holes in skin.
Cracks are most likely around fastener holes
closest to the edges of the doubler.
Report No.: ICA-3832-560
Dated 01/23/2018
Recurring (flights)
10,271
4,835
13,016
7,466
Revision: IR
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