Rev A
Page 3
JA74-001 Dual USB Charging Port
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 JA74-001 is on condition only. Scheduled inspection and/or periodic maintenance of this unit are
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 JA74, on or in a specific type or class of aircraft, must determine that the aircraft installation
conditions meet standards. The JA74 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.
Note that this unit has a ‘clamshell’ hood that is installed after the wiring is complete.
Maintain wire segregation and route wiring in accordance with the original aircraft manufacturer’s maintenance
instructions.
