User Manual Part 3

Page 3-4
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
A. Aircraft ID
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 3-33.
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 3-1 to change the AES aircraft ID
information.
To just view the aircraft tail number information, the user level is required.
(1) At the GUI login, the username is "User" and there is no password.
The GUI AES status summary screen lets the user navigate to all applicable options. At the User
level, the Other Information & Control has an option to display the current Aircraft ID stored in the
AES Configuration data. Refer to Figure 3-1 for the AES aircraft ID information page.
132 Yes True heading Hybrid 110 50 0.0055
degrees
324 Yes Pitch angle INS 50 20 0.011
degrees
325 Yes Roll angle INS 50 20 0.01 degrees
330 Yes Yaw rate INS 50 20 0.015
degrees/sec
326 Yes Pitch rate INS 50 20 0.015
degrees/sec
327 Yes Roll rate INS 50 20 0.015
degrees/sec
331 Yes Body longitudinal
acceleration
INS 60 20 0.001 g
332 Yes Body lateral
acceleration
INS 60 20 0.001 g
333 Yes Body vertical
Acceleration
INS 60 20 0.001g
Secondary
Label
Same accuracy as Primary
110 GNSS latitude GNSS 1000 20 0.000172
degrees
111 GNSS longitude GNSS 1000 20 0.000172
degrees
76 GNSS altitude
(MSL)
GNSS 1000 20 0.125 ft