User's Manual Part 1
Table Of Contents
- TRANSMITTAL INFORMATION
- SECTION 1 INTRODUCTION
- SECTION 2 DESCRIPTION
- SECTION 3 SYSTEM PRE-CONFIGURATION
- SECTION 4 INSTALLATION
Page 4-1
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
SECTION 4
INSTALLATION
4.1 Overview
A. Installation Procedure Overview for the JetWave™ System
This section includes information about installing the equipment in the core JetWave™ system. Contact
VAR/DP/Honeywell about installation kits that include mating connectors and cables.
Honeywell recommends that LRUs be installed in accessible locations that are compatible with the
environmental levels that the equipment is certified to handle.
Refer to APPENDIX D for the installation reference checklist.
Complete the Airframe Specific Information sheet in APPENDIX D. For new configurations, provide
this sheet to Honeywell so an APM file can be generated.
NOTE:
ARINC 429 labels may be obtained from the aircraft ADIRU or MMR or other suitable
equipment, providing they meet the required update rate, latency and accuracy.
NOTE:
For FMA located in Non-ARINC791 defined positions, a structural blockage map will have
to be defined for the aircraft.
The JetWave™ system installation procedure includes:
• the Modman, APM, Maintenance Panel and Discrete wiring
• the KANDU
• the AIM or the LAIM
• the KRFU Thermal Pad and the KRFU
• the FMA or the TMA
•the Radome
• Cabling and drawings.
Refer to Table 4-3 for a detailed explanation of the discrete signal required for correct operation of
the GX system.
The overview of the installation procedure for the JetWave™ system is as follows:
(1) Install adapter plate for the FMA. For Fuselage Mount Configurations, install either the
ARINC 791 style antenna interface mount (AIM) or non ARINC 791 local antenna interface
mount (LAIM), depending on the selected installation option. Installation shall be per
instructions related to each configuration. The adapter plates required for mounting the OAE
are available in installation kits from Honeywell and various other suppliers.
or
The TMA tail configuration requires that the TMA and KRFU be installed on the aircraft tail tip
under a radome specific to the tail on that aircraft. Installation brackets and provisions are
specific to each tail platform.
Draft as of 31 May 2017