J301A-001 Audio Controller
Installation and Operating Manual
Rev A
Page B2
B1
Airworthiness Approval
Airworthiness approval of the J301A-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 J301A-001 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 J301A-001 Audio Controller in [aircraft
location].
Installed in accordance with the J301A-001 Installation and Operating Manual, Revision [ ], and AC 43.13-2, Chapters
2, and 3.
The J301A-001 interfaces with existing aircraft systems per the Installation and Operating Manual instructions.
The J301A-001 Installation and Operating Manual provides detailed installation instructions and wiring diagrams
(Section 2, and Appendices A and B).
Power is supplied to the J301A-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 J301A-001 Audio Controller is “on condition” only. Refer to the J301A-001 Maintenance Manual.
Periodic maintenance of the J301A-001 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics J301A-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 J301A-001 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 J301A-001 installed in an [aircraft make and model].
Applicability
: Applies to a Jupiter Avionics J301A-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
: J301A-001 Installation and Operating Manual
J301A-001 Maintenance Manual
J301A-001 Operating Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution
: This document should be a permanent aircraft record.
