JA95-N02 Audio Controller - Six Transceiver - NVG
Installation and Operating Manual
Rev B
Page B2
B1
Airworthiness Approval
Airworthiness approval of the JA95-N02 may require completion of a TCCA Major Modification Report per CAR STD
(AWM) 571 Appendix L. 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
JA95-N02 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 must follow the
applicable aviation authority’s regulations.
Sample Wording:
Removed the existing [model] audio panel and replaced with a Jupiter Avionics JA95-N02 Audio Controller in [aircraft
location].
The JA95-N02 is approved to CAN-TSO-C139 . The JA95-N02 meets RTCA DO-160F environmental qualifications
for this installation. See Section 1 of the JA95-N02 Installation Manual.
Installed in accordance with the JA95-N02 Installation Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.
The JA95-N02 interfaces with existing aircraft radios per the Installation Manual instructions.
The JA95-N02 Installation Manual provides detailed installation instructions and wiring diagrams (Section 2, and
Appendices A and B).
Power is supplied to the JA95-N02 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 JA95-N02 Audio Controller is “on condition” only. Refer to the JA95-N02 Maintenance Manual.
Periodic maintenance of the JA95-N02 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JA95-N02 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 JA95-N02 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 JA95-N02 installed in an [aircraft make and model].
Applicability
: Applies to a Jupiter Avionics JA95-N02 installed in an [aircraft make and model].
Definitions/Abbreviations
: None, N/A.
Precautions
: None, N/A.
Units of Measurement
: None, N/A.
Referenced Publications
: JA95-N02 Installation and Operating Manual
JA95-N02 Maintenance Manual
JA95-N02 Operating Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution
: This document should be a permanent aircraft record.
