User's Manual Part 6

Page 6-3

3 Mar 2017

23-15-29

SYSTEM DESCRIPTION AND INSTALLATION MANUAL

JetWave™ System

B. Terminal Activation

(1) To activate the terminal with your service provider you need to provide the ACM TPK.

(2) The TPK is written on the test report d

ocument delivered with the MODMAN.

(3) The TPK may be viewed using the MODMAN GUI.

6.2 Certification and Approvals

All antenna installations must obtain the approval of the appropriate government air/radio authority,

such as the FAA, EASA, or Transport Canada. Contact the authorities when you begin planning

your communication system in order to minimize approval and certification issues.

All system configurations are subject to Inmarsat type approval. New configurations (changes to

inter-LRU wiring losses, radome and/or IRS data sources) are subject to re-evaluation and must be

coordinated through Honeywell.

6.3 Post Installation System Checkout Procedures

A. General Overview

This section supplies the informatio

n required to determine the operational readiness of the

JetWave™ system, made up of the Modman, APM, KRFU, KANDU, and OAE FMA or OAE TMA.

The installed LRUs require operational and diagnostic testing for one of the reasons listed below:

• Operational verification tests that verify the operational readiness of the unit after installation on

an aircraft.

• Fault verification and diagnostics to verify that a fault exists and produce system reports for

trouble shooting purposes

• Operational verification of repairs that verify the operational readiness of units that have been

repaired before re-installation on an aircraft.

B. System Health and Configuration

This section describes the AES System configuration setting to be carried out on completion of LRU

installation activities for updating the aircraft tail number.

Aircraft tail number is the unique identifier used by the Inmarsat system to identify the user aircraft within

the network. The aircraft ID file contains aircraft identity information as follows (columns are Item, LRU,

Data):

To update the aircraft tail number in AES system, maintenance level access is required through the web

based GUI. Refer to Accessing the Maintenance Interface on page 7-1.

The GUI AES status summary screen lets the maintainer navigate to all applicable options. At the

maintenance level, the Other Information & Control has an option to display/update the current Aircraft ID

stored in the AES Configuration data. Refer to Figure 6-1 to change the AES aircraft ID information.

To just view the aircraft tail number information, the user level can be used.

At the GUI login, the username is "User" and there is no password.

Draft as of 31 May 2017