User Manual Part 3

Page E-1
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
APPENDIX E
1. List of Airframe Specific Information Required for JetWave™ System Configuration
A Honeywell proprietary configuration tool is used to generate the JetWave™ configuration files. Information
as listed in the tables below is to be provided to Honeywell for generation of JetWave™ configuration files.
Aircraft Information:
Aircraft Model/Type
Tail Number:
Serial Number:
Value Added Reseller (VAR/DP)
Name of the Service Provider
ARINC 429 Labels
ARINC 429 Interface Speed Interface Bus Speed
ARINC
429
Label
No. ARINC 429 Label Name Accuracy
ARINC 429
Label
Latency
Total
Latency
(in
Msec)
ARINC 429
Minimum
Transmission
Rate (in
Msec)
Jitter
(Uncert
ainty in
Delay)
150 UTC Time
260 Date
270 Status
254 Present Position – Latitude
255 Present Position –
Longitude
261 Altitude
132 True Heading
324 Pitch Angle
325 Roll Angle
330 Yaw rate
326 Pitch rate
327 Roll rate
331 Body longitudinal
Acceleration
332 Body lateral Acceleration
333 Body vertical Acceleration
110 GNSS Latitude
111 GNSS Longitude
76 GNSS Altitude (MSL)