JA34-BT1 Universal Radio Adapter with Bluetooth
®
Installation and Operating Manual
Rev D
Page B2
B1
Airworthiness Approval
Airworthiness approval of the JA34-BT1 may require completion of a TCCA Major Modification Report per CAR STD
(AWM) 571 Appendix L, or a FAA Form 337. The sample wording for a description of the work is provided to assist
the Installing Agency in preparing Instructions for Continued Airworthiness (ICA) when replacing an existing radio
adapter with a Jupiter Avionics JA34-BT1 Universal Radio Adapter with Bluetooth. This sample may be modified
appropriately for new installations. It is the installer’s responsibility to determine the applicability of the method used.
Installations performed outside the USA and Canada must follow the applicable aviation authority’s regulations.
Sample Wording:
Removed the existing [model] radio adapter and replaced with a Jupiter Avionics JA34-BT1 Universal Radio Adapter
with Bluetooth in [aircraft location].
Installed in accordance with the JA34-BT1 Installation & Operating Manual, Revision [ ], and AC 43.13-2, Chapters 2,
and 3.
The JA34-BT1 interfaces with existing aircraft radios per the Installation & Operating Manual instructions.
The JA34-BT1 Installation & Operating Manual provides detailed installation instructions and wiring diagrams (Section
2, and Appendices A and B).
Power is supplied to the JA34-BT1 through a 1.0-Amp circuit breaker.
Aircraft equipment list, weights and balance amended. Compass compensation checked and found to conform to
applicable regulations.
B2
Instructions for Continued Airworthiness
Maintenance of the JA34-BT1 Universal Radio Adapter with Bluetooth is “on condition” only. Refer to the JA34-BT1
Maintenance Manual. Periodic maintenance of the JA34-BT1 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JA34-BT1 unit installation as part of a Type Certificate (TC) or Supplemental Type Certificate (STC)
project to comply with CAR STD (AWM) 523/527/525/529.1529 or FAR 23/25/27/29.1529 “Instructions for Continued
Airworthiness”.
Items that may vary by aircraft make and model are shown in brackets (“[ ]”) and should be filled in as appropriate.
Some of the checklist items do not apply, in which case they should be marked “N/A” (Not Applicable).
Instructions for Continued Airworthiness, Jupiter Avionics JA34-BT1
Universal Radio Adapter in an [Aircraft Make and Model]
1. Introduction
[Aircraft that has been altered: Registration number, Make, Model and Serial Number]
Content, Scope, Purpose and Arrangement
: This document identifies the Instructions for Continued
Airworthiness for a Jupiter Avionics JA34-BT1 installed in an [aircraft make and model].
Applicability
: Applies to a Jupiter Avionics JA34-BT1 installed in an [aircraft make and model].
Definitions/Abbreviations
: None, N/A.
Precautions
: None, N/A.
Units of Measurement
: None, N/A.
Referenced Publications
: JA34-BT1 Installation & Operating Manual
JA34-BT1 Maintenance Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution
: This document should be a permanent aircraft record.
2. Description of the System/Alteration
Jupiter Avionics JA34-BT1 Universal Radio Adapter with Bluetooth interfaces to external transceivers and [include
other equipment/systems as appropriate]. Refer to Appendix A of this manual for interconnect information. Refer
to aircraft manufacturer approved interconnect for actual installation.
