JA98-001 Remote Mount Audio Controller
Installation and Operating Manual
Rev A
Page B2
B1
Airworthiness Approval
Airworthiness approval of the JA98-001 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
audio panel with a Jupiter Avionics JA98-001 Remote Mount Audio Controller. 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 Canada and the USA must follow the applicable aviation authority’s
regulations.
Sample Wording:
Removed the existing [model] audio controller and replaced with a Jupiter Avionics JA98-001 Remote Mount
Audio Controller in [aircraft location].
The JA98-001 is approved to CAN-TSO-C139 and FAA TSO-C139. The JA98-001 meets RTCA DO-160G
environmental qualifications for this installation. See Section 1 of the JA98-001 Installation Manual.
Installed in accordance with the JA98-001 Installation Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.
The JA98-001 interfaces with existing aircraft radios per the Installation Manual instructions.
The JA98-001 Installation Manual provides detailed installation instructions and wiring diagrams (Section 2, and
Appendices A and B).
Power is supplied to the JA98-001 through an existing [ ]-Amp circuit breaker that was previously used by the
original audio panel. The net electrical load is unchanged.
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 JA98-001 Remote Mount Audio Controller is “on condition” only. Refer to the JA98-001
Maintenance Manual. Periodic maintenance of the JA98-001 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JA98-001 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 JA98-001
Remote Mount Audio Controller 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 JA98-001 installed in an [aircraft make and model].
Applicability
: Applies to a Jupiter Avionics JA98-001 installed in an [aircraft make and model].
Definitions/Abbreviations
: None, N/A.
Precautions
: None, N/A.
Units of Measurement
: None, N/A.
Referenced Publications
: JA98-001 Installation and Operating Manual
JA98-001 Maintenance Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution
: This document should be a permanent aircraft record.
