JCP3-001 Control Panel - NVG
Installation and Operating Manual
Rev A
Page B2
B1
Airworthiness Approval
Airworthiness approval of the JCP3-N01 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 JCP3-N01 Control Panel - NVG. 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 JCP3-N01 Control Panel - NVG in
[aircraft location].
The JCP3-N01 is approved to CAN-TSO-C139. The JCP3-N01 meets RTCA DO-160G environmental qualifications
for this installation. See Section 1 of the JCP3-001 Installation and Operation Manual.
Installed in accordance with the JCP3-N01 Installation Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.
The JCP3-N01 interfaces with the Remote Audio Controller per the Installation Manual instructions.
The JCP3-N01 Installation Manual provides detailed installation instructions and wiring diagrams (Section 2, and
Appendices A and B).
Power is supplied to the JCP3-N01 from the Remote Audio Controller.
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 JCP3-N01 Control Panel - NVG is “on condition” only. Refer to the JCP3-N01 Maintenance
Manual. Periodic maintenance of the JCP3-N01 is not required.
The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the
Jupiter Avionics JCP3-N01 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 JCP3-N01 Control
Panel - NVG 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 JCP3-N01 installed in an [aircraft make and model].
Applicability
: Applies to a Jupiter Avionics JCP3-N01 installed in an [aircraft make and model].
Definitions/Abbreviations
: None, N/A.
Precautions
: None, N/A.
Units of Measurement
: None, N/A.
Referenced Publications
: JCP3-N01 Installation and Operating Manual
JCP3-N01 Maintenance Manual
JCP3-N01 Operating Manual
STC/TC # [applicable STC/TC number for the specific aircraft installation]
Distribution
: This document should be a permanent aircraft record.
