User Manual Part 3

Page 3-22

16 Sep 2015

23-15-29

SYSTEM DESCRIPTION AND INSTALLATION MANUAL

JetWave™ System

429 interface through which the required ARINC 429 labels as defined in APM configuration file are

made available.

Navigate to the AES Summary and Link Status page and scroll down to see the aircraft status.

Refer to Figure 3-13.

This page will be updated with current latitude and longitude position of the aircraft.

Once the JetWave™ system starts receiving the valid navigational input from aircraft IRS system,

make sure that the values are correct as compared to the aircraft navigational system outputs.

Figure 3-13. Aircraft Statuses

D. Manual Steering of the Antenna

To do a commanded test to manually steer the antenna, navigate to "Manual Antenna Steering"

under the commanded test menu. Monitor the antenna movement in accordance with the

commanded test fed through the GUI tool. Refer to Figure 3-14.

NOTE:

In order to see the antenna movement, the radome can be removed. If it is an OAE-TMA,

Honeywell recommends manually steering the TMA through GUI to a safe antenna

orientation position before removal. The TMA parking position is included in the AES

System Configuration File, which can be accessed through the GUI web interface and by

navigating to Configuration File page. Consult aircraft specific SDIM for detailed

instructions.