Jupiter Avionics JA74-001 Installation And Operating Manual

Jupiter Avionics JA74-001 Installation And Operating Manual

Dual usb charging port

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JA74-001
Dual USB Charging Port
Installation and Operating Manual
Rev A
Jupiter Avionics Corporation
1959 Kirschner Road
Kelowna BC
Canada V1Y 4N7
Tel: +1 778 478 2232
Toll-Free: 1 855 478 2232
www.jupiteravionics.com
Rev B
Page i

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Summary of Contents for Jupiter Avionics JA74-001

  • Page 1 JA74-001 Dual USB Charging Port Installation and Operating Manual Rev A Jupiter Avionics Corporation 1959 Kirschner Road Kelowna BC Canada V1Y 4N7 Tel: +1 778 478 2232 Toll-Free: 1 855 478 2232 www.jupiteravionics.com Rev B Page i...
  • Page 2 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.
  • Page 3: Table Of Contents

    JA74-001 Dual USB Charging Port Installation and Operating Manual Table of Contents SECTION 1 - DESCRIPTION ..............................1 System Overview ..............................1 Features Overview ..............................1 Inputs and Outputs ..............................1 1.3.1 Inputs ................................1 1.3.2 Bi-Directional Ports ............................1 1.3.3...
  • Page 4: Section 1 - Description

    The JA74-001 Dual USB Charging Port allows the aircraft owner /operator to use an unused portion of the instrument panel for charging portable devices such as cell phones. The JA74-001 includes two USB 2.0 Type A receptacles with a power supply (5 Volt, up to 2.1 Amp per port). Features Overview The JA74-001 is painted in a baked-on flat black urethane finish to resist scratches and nicks during use.
  • Page 5: Mechanical Specifications

    2 Dzus fasteners Bonding ≤ 2.5 mΩ Installation kit part number INST-JA74 1.4.3 Flammability of Materials The JA74-001 complies with the requirements of RTCA/DO-160G Sec 26.3.3 "Flammability", through equivalent flammability testing of materials and the Small Parts Exemption. Rev A Page 2...
  • Page 6: Section 2 - Installation

    Introduction This section contains unpacking and inspection procedures, installation information, and post-installation checks. Continued Airworthiness Maintenance of the JA74-001 is on condition only. Scheduled inspection and/or periodic maintenance of this unit are not required. 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.
  • Page 7: Mechanical Installation

    Unless otherwise noted, all wiring shall be a minimum of 20 AWG. Refer to the Interconnect drawing for additional specifications. 2.4.3 Mechanical Installation The JA74-001 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 2.4.4.1...
  • Page 8: Section 3 - Operation

    Introduction This section contains the operating instructions for the JA74-001. The JA74-001 allows an unused portion of the instrument panel to be utilized for charging phones or other devices. Front Panel Connectors The JA74-001 has two front panel USB Power output connectors.
  • Page 9: Appendix A - Installation Drawings

    JA74-001 Dual USB Charging Port Installation and Operating Manual Appendix A - Installation Drawings Introduction The drawings necessary for installation and troubleshooting of the JA74-001 Dual USB Charging Port are in this Appendix, as listed below. Installation Drawings DOCUMENT JA74-001 Connector Map...
  • Page 10 View is from side of mating connector PREPARED 05-03-16 CHECKED TITLE Dual USB Charging Port P1, P2, P3 and P4 Connector Map APPROVED 05-03-16 NCAGE CODE PART NO. SHEET L00N3 JA74-001 DOC NO. JA74-001 Connector Map Rev A.dwg JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT...
  • Page 11 CONNECTION TO AIRFRAME GROUND SHOULD BE MADE WITH 20 AWG WIRE. LENGTH NOT TO EXCEED 3 FT (0.91 M). CABLE SHIELDS AT THE JA74-001 CONNECTOR PINS MAY BE TERMINATED TO AIRFRAME GROUND USING A TAG RING P/N: MS27741-5 OR EQUIVALENT.
  • Page 12 2ND RING AUDIO LO AUDIO LO AUDIO RIGHT AUDIO LEFT PREPARED 05-03-16 CHECKED TITLE Dual USB Charging Port APPROVED 05-03-16 NCAGE CODE PART NO. SHEET L00N3 JA74-001 DOC NO. JA74-001 Interconnect Rev A.dwg JUPITER AVIONICS TEMPLATE AUTOCAD PORTRAIT SIZEA REV B.DWT...
  • Page 13 ANGLES: 0.5 DEG NCAGE CODE PART NO. SHEET APPROVED 05-04-16 L00N3 JA74-001 CONFIDENTIAL & PROPRIETARY DOC. NO. MATERIAL: TO JUPITER AVIONICS CORP. JA74-001 Mechanical Installation Rev A.SLDDRW FINISH: DRAWING NOT TO SCALE JUPITER AVIONICS TEMPLATE SOLIDWORKS LANDSCAPE SIZEB REV B.DRWDOT...
  • Page 14: Appendix B - Installation Documents

    JA74-001 Dual USB Charging Port Installation and Operating Manual Appendix B - Installation Documents Rev A Page B1...
  • Page 15: B1 Airworthiness Approval

    [aircraft location]. See Section 1 of the JA74-001 Installation Manual. Installed in accordance with the JA74-001 Installation Manual, Revision [ ], and AC 43.13-2, Chapters 2, and 3. The JA74-001 interfaces with existing aircraft systems per the Installation Manual instructions.
  • Page 16 Refer to the JA74-001 Maintenance Manual. 7. Removal and Replacement Information Refer to Section 2 of this manual - the JA74-001 Installation and Operating Manual. If the unit is removed and reinstalled, a functional check of the equipment should be conducted.

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