JUPITER AVIONICS UJAC2-001 Panel Mount USB-C Charger User Manual

www.jupiteravionics.com

Copyright 2021 Jupiter Avionics Corp.
All rights reserved

Jupiter Avionics Corporation (JAC) permits a single copy of this manual to be printed or downloaded for the express use of an installing agency. Any such electronic or printed copy of this manual must contain the complete text of this copyright notice. Any unauthorized commercial distribution of this manual is strictly prohibited. Except as described above, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded, or stored in any storage medium for any purpose without the express prior written consent of JAC.

IMPORTANT:
Information in this document is subject to change without notice.
To confirm the current revision status of this manual, visit the JAC website:
www.jupiteravionics.com

RECORD OF REVISIONS

Revision| Rev Date| Description| ECR
A| Feb 2021| Initial release, Serial number 1001 and higher.| 7574
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Prepared: DGB| Checked:

JAC 02-10-21 SDB

| Approved:

JAC 02-10-21 KDV

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SECTION 1 – DESCRIPTION

1.1 System Overview

**** The UJAC2-001 Panel Mount USB-C Charger allows the aircraft power to charge USB devices.
The UJAC2-001 provides a USB PD Type C receptacle with an auto-adjustable supply which can deliver 5 Vdc @ 3 A, 9 Vdc @ 3 A, 12 Vdc @ 3 A, 15 Vdc @ 3 A, or 20 Vdc @ 2.25 A.
The UJAC2-001 can be mounted in any orientation.

1.2  Features Overview

**** The UJAC2-001 faceplate has a baked-on flat black urethane finish to resist scratches and nicks during use. The UJAC2-001 provides a single USB PD Type C receptacle with up to 45 Watts of output power.

The UJAC2-001 provides a flexible urethane cover to protect the USB port when not in use. The UJAC2-001 supports USB Power Delivery (PD) revision 2.0.

1.3 Inputs and Outputs

**** Refer to the UJAC2-001 connector map for the mating connector designators and pin assignments for the input and output signals.

1.3.1 Inputs

1.3.2 Outputs

1.3.3  Grounds/Spares

1.4 Specifications

**** 1.4.1 Electrical Specifications

![JUPITER AVIONICS UJAC2-001 Panel Mount USB-C Charger User Manual -

Electrical Specifications](https://manuals.plus/wp-content/uploads/2022/03 /JUPITER-AVIONICS-UJAC2-001-Panel-Mount-USB-C-Charger-User-Manual-Electrical- Specifications.jpg)   1.4.2  Mechanical Specifications

SECTION 2 – INSTALLATION

2.1 Introduction

**** This section contains unpacking and inspection procedures, installation information, and post-installation checks.

2.2 Continued Airworthiness

**** Maintenance of the UJAC2-001 is on condition only. Scheduled inspection and/or periodic maintenance of this unit is not required.

2.3 Unpacking and Inspecting Equipment

**** Unpack the equipment carefully. Check for shipping damage and report any problems to the relevant carrier. Confirm that the Authorized Release Certificate or Certificate of Conformance is included. Complete the on-line warranty card from the Jupiter Avionics Corporation (JAC) website – www.jupiteravionics.com/warranty

2.3.1 Warranty

This product manufactured by JAC is warranted to be free of defects in workmanship or performance for 2 years from the date of installation by an approved JAC dealer or agency. This warranty covers the cost of all materials and labour to repair or replace the unit, but does not include the cost of transporting the defective unit to and from JAC or its designated warranty repair centre, or of removing and replacing the defective unit in the aircraft. This warranty does not cover failures due to abuse, misuse, accident, or unauthorized alteration or repairs.

THIS WARRANTY IS VOID IF THE PRODUCT IS NOT INSTALLED BY AN AUTHORIZED JAC DEALER. If the on-line warranty card is not completed, the product will be warranted from the date of manufacture.

Contact JAC for return authorization, and for any questions regarding this warranty and how it applies to your unit(s). JAC is the final arbiter concerning warranty issues.

2.4  Installation Procedures

CAUTION: The power input circuitry of the unit may be damaged if the installation does not conform to the wiring instructions in this manual.

2.4.1 Installation Limitations

Those installing the UJAC2-001, on or in a specific type or class of aircraft, must determine that the aircraft installation conditions meet standards. The UJAC2-001 may be installed only by following the applicable airworthiness requirements.

2.4.2 Cabling and Wiring

All wire shall be selected in accordance with the original aircraft manufacturer’s maintenance instructions, or AC43.13- 1B Change 1, Paragraphs 11-76 through 11-78. Unshielded wire types shall qualify to MIL-W-22759 as specified in AC43.13-1B Change 1, Paragraphs 11-85, 11-86, and listed in Table 11-11. Follow the Connector Map in Appendix A of this manual.
Maintain wire segregation and route wiring in accordance with the original aircraft manufacturer’s maintenance instructions.
Unless otherwise noted, all wiring shall be a minimum of 22 AWG. Refer to the Interconnect drawing for additional specifications. Check that the ground connection is clean and well secured, and that it shares no path with any electrically noisy aircraft accessories such as blowers, turn-and-bank instruments, or similar loads.

2.4.3 Mechanical Installation

The UJAC2-001 can be mounted in any attitude and location with adequate space for the front panel and sufficient clearance for the connector and wiring harness. It requires no direct cooling.

2.4.4 Post Installation Checks

• Voltage/Resistance checks

Do not attach this unit until the following conditions are met:

• Check P1 pin 1 for +27.5 Vdc
• Check P1 pins 6 and 7 for continuity to ground (less than 5 Ω).
• Check all pins for shorts to ground or adjacent pins.

2.4.4.2 Power on Checks.

Power up the aircraft’s systems and confirm normal operation of all functions of the UJAC2-001. Refer to Section 3 (Operation) for specific operational details.
When all performance checks are satisfied, complete the necessary regulatory documentation before releasing the aircraft for service. Refer to Appendix B.

2.5 Installation Kit

The kit required to install this unit is not included with the unit. The installation kit (Part # INST-UJAC) consists of the following:

2.5.1 Recommended Crimp Tools

Standard D-Sub Crimp Tool Chart

Tool Type| Hand crimping tool| Positioner| Insertion/extractor tool
POSITRONIC| 9507-0-0-0| 9502-5-0-0| 4711-2-0-0
DANIELS| AFM 8| K13-1| 91067-2
MIL-SPEC| M22520/2-01| M22520/2-08| M81969/1-02

2.6 Installation Drawings

The drawings and documents required for Installation can be found in Appendix A of this manual.

SECTION 3 – OPERATION

3.1 Introduction

This section contains the operating instructions for the UJAC2-001.

3.2 Front Panel Connector

**** The UJAC2-001 has one front panel USB-C Power output connector.

3.2.1 USB-C Power Output

The UJAC2-001 Panel Mount USB-C Charger has a USB PD Type C receptacle with an auto-adjustable supply which can deliver 5 Vdc @ 3 A, 9 Vdc @ 3 A, 12 Vdc @ 3 A, 15 Vdc @ 3 A or 20 Vdc @ 2.25 A for charging cell phones and similar devices.

The USB connector has a black urethane dust cover.

 Note: This port is not designed to be used for data transfer

3.3 Compatibility

CAUTION: Attempting to connect an incompatible plug or device could damage the UJAC2-001, the attached device, or both. If in doubt, check with your installing agency.

Installation and Operating Manual

Appendix A – Installation Drawings

****A1                   Introduction

**** The drawings necessary for installation and troubleshooting of the UJAC2-001 are in this Appendix, as listed below.

A2                   Installation Drawings

MAIN CONNECTOR

UJAC2-001 INTERCONNECT WIRING NOTES

NOTES 1.ALL WIRE SIZE SHOULD BE 22 AWG MIN UNLESS OTHERWISE SPECIFIED. UNSHIELDED WIRE SHOULD BE SELECTED PER FAA AC43.13-1B CHANGE 1 PARA 11-76 TO 11-78. WIRE TYPES SHOULD BE IN ACCORDANCE WITH MIL-W-22759 AS DESCRIBED IN FAA AC43.13-1B CHANGE 1 PARA 11-85 AND 11-86 AND LISTED IN TABLE 11-11 OR 11-12. ALL SHIELDED CABLE SHOULD BE IN ACCORDANCE WITH MIL-DTL-27500 (REVISION H OR LATER).

CONNECTION TO AIRFRAME GROUND SHOULD BE MADE WITH 22 AWG WIRE. LENGTH NOT TO EXCEED 3 FT (0.91 M).
CABLE LENGTH NOT TO EXCEED 6 FT (1.82 M).

Installation and Operating Manual

Appendix B – Installation Documents

B1                   Airworthiness Approval

**** Airworthiness approval of the UJAC2-001 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 UJAC2-001 Panel Mount USB-C Charger. 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] panel mount charger and replaced with a Jupiter Avionics UJAC2-001 Panel Mount USB-C Charger in [aircraft location].

See Section 1 of the UJAC2-001 Installation & Operating Manual.

Installed in accordance with the UJAC2-001 Installation & Operating Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3.

The UJAC2-001 interfaces with existing aircraft systems per the Installation & Operating Manual instructions.

The UJAC2-001 Installation & Operating Manual provides detailed installation instructions and wiring diagrams (Section 2, and Appendices A and B).

Power is supplied to the UJAC2-001 through a [ ]-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 UJAC2-001 Panel Mount USB-C Charger is “on condition” only. Refer to the UJAC2-001 Maintenance Manual. Periodic maintenance of the UJAC2-001 is not required.

The following sample Instructions for Continued Airworthiness (ICA) provides assistance in preparing ICA for the Jupiter Avionics UJAC2-001 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 UJAC2-001 Panel Mount USB-C Charger 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 UJAC2-001 installed in an [aircraft make and model].
   Applicability : Applies to a Jupiter Avionics UJAC2-001 installed in an [aircraft make and model].
   Definitions/Abbreviations : None, N/A.
   Precautions : None, N/A.
   Units of Measurement : None, N/A.
   Referenced Publications : UJAC2-001 Installation & Operating Manual
   UJAC2-001 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 UJAC2-001 Panel Mount USB-C Charger with interface 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.

3. Control, Operation Information
   Refer to section 3 of this manual.

4. Servicing Information
   N/A

5. Maintenance Instructions
   Maintenance of the UJAC2-001 is ‘on condition’ only. Periodic maintenance is not required. Refer to the UJAC2-001 Maintenance Manual.

6. Troubleshooting Information
   Refer to the UJAC2-001 Maintenance Manual.

7. Removal and Replacement Information
   Refer to Section 2 of this manual – the UJAC2-001 Installation & Operating Manual. If the unit is removed and reinstalled, a functional check of the equipment should be conducted.

8. Diagrams
   Refer to Appendix A of this manual – the UJAC2-001 Installation & Operating Manual – for installation drawings and interconnect examples.

9. Special Inspection Requirements
   N/A

10. Application of Protective Treatments
    N/A

11. Data: Relative to Structural Fasteners
    UJAC2-001 and appropriate mounting hardware installation, removal and replacement should be in accordance with applicable provisions of AC 43.13-1B and AC 43.13-2A.

12. Special Tools
    N/A

13. This Section is for Commuter Category Aircraft Only
    A. Electrical loads : Refer to Section 1 of the UJAC2-001 Installation & Operating
    B.  Methods of balancing flight controls: N/A.
    C. Identification of primary and secondary structures : N/A.
    D. Special repair methods applicable to the airplane : N/A.

14. Overhaul Period
    No additional overhaul time limitations.

15. Airworthiness Limitation Section
    N/A

References

• Jupiter Avionics Corporation - Avionics design manufacturer

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