User's Manual Part 1

Page 3-2
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
The AES system configuration includes the aircraft installation information.
NOTE:
The AES System configuration file update is not a field activity. This is done by the
equipment supplier as part of production process. On completion of AES system installation
activities, the installer can view and verify the AES configuration settings through the GUI
as described in this section.
To view and make sure the AES configuration data is correct, navigate to the “Configuration Files”
information pages under the “Other Information & Control” menu. Figure 6-4 shows the typical
configuration file Information page.
NOTE:
The AES system does not lose its configuration data because of the loss of its primary
power. The validity of the AES configuration content is determined by the AES system with
a checksum process. The checksum is done at the time of each power-up. An invalid
checksum results in the AES system reverting to the default values.
255
/111
Yes Present Position –
Longitude
/GNSS Longitude
Hybrid
/GNSS
160
/1000
100
/20
0.000172°
261
/76
Yes Altitude
/GNSS Altitude (MSL)
Hybrid
/GNSS
65
/1000
40
/20
0.125 ft
132
/314
Yes
/No
True Heading Hybrid
/INS
110 50 0.0055°
/0.4°
324 Yes Pitch Angle INS 50 20 0.011°
325 Yes Roll Angle INS 50 20 0.01°
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
175
/112/312
Yes Ground Speed
/GNSS Ground Speed
Hybrid
/GNSS/
INS
110
/Nil
40 0.125 knots
(kn)
Label
Acceptable Replacement to Primary
125 UTC Time INS 1200 200 0.1 min.
Table 3-1. ARINC 429 Label List
Draft as of 31 May 2017