Instructions For Continued Airworthiness; Introduction; Description Of Alteration; Control, Operating Information - Garmin GDL 69 Instructions Manual

7) IAW: In Accordance With
8) ICA: Instructions for Continued Airworthiness
9) MFD: Multi-Function Display unit
10) PMI: Primary Manufacturing Inspector
11) POI: Primary Operations Inspector
12) STC: Supplemental Type Certificate
13) TC: Type Certification or Type Certificate
14) TSO: Technical Standard Order

2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

2.1 Introduction

Content, Scope, Purpose and Arrangement:
Applicability:
Definition of Abbreviations:
Precautions:
Units of measurement:
Referenced publications:
(or later revisions)
Retention:

2.2 Description of Alteration

The Garmin GDL 69/69A and optional GRT 10 Wireless Transceiver are installed in the aircraft as
remote-mount units. Pilot control of the GDL 69/69A is through the interfaced control and display unit,
such as a Garmin GMX 200 or other approved unit, for display and control of the weather data. The GDL
69A is also interfaced to the pilot through an audio panel, such as a Garmin GMA 347 for control of the
audio. The GDL 69A is also interfaced to the passengers through the GRC 10 Wireless Controller for
controlling audio features of the GDL 69A.

2.3 Control, Operating Information

The GDL 69/69A does not have a direct pilot interface. The GDL 69/69A is controlled via separately
installed device, such as the Garmin GMX 200 multi-function display. The GDL 69A audio features can
GDL 69/69A XM Satellite Radio
Instructions for Continued Airworthiness
This document identifies the Instruction for
Continued Airworthiness for the modification of the
aircraft by installation of the Garmin GDL 69/69A
remote XM Satellite Radio and optional GRT
10/GRC 10 Wireless Remote System.
Applies to aircraft altered by installation of the
Garmin GDL 69/69A XM Satellite Radio and
optional GRT 10/GRC 10 Wireless Remote
System.
See Section 1.6
None
None
190-00355-02 Rev. K GDL 69/69A XM Satellite
Radio Installation Manual
This document, or the information contained within,
will be retained in the aircraft's permanent records.
190-00355-00 Rev.E
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