User's Manual Part 6

Page 6-10
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
C. Discrete Input Testing
(1) If wired, activate the Modman Reset by toggling Modman reset sw
itch on the JetWave™ AES
control panel.
(2) If the Modman Reset is not wired, then reset
the system from the GUI.
(3) Monitor the Modman ”power” and “status” LEDs flash continuously.
(4) Toggle the Modman Reset switch on the Satcom test panel to the open/non-grounded
position
.
(5) Monitor the “status” LED on the front of the Modman, progresses from red color to steady
state gre
en as seen during initial power-on.
(6) Check for the Aircraft Tail number page and make sure that the aircraft tail number page is
update
d with the aircraft Tail number.
Navigate to the AES Summary and Link Status page and scroll
down to see the ARINC 791
Discrete input and output state of the JetWave™ system. Refer to Figure 6-8.
For illustration, the figure that follows shows the AES discrete signal state. Use the wired aircraft
interfaces to toggle and see if the applicable discrete are asserted or de-asserted.
Figure 6-8. Discrete I/O State
D. ARINC 429 Input Interface Testing
For the operation of the JetWave
TM
system, the aircraft must have a functional IRS providing
ARINC 429 labels to the KANDU. Functional IRS is interfaced with the KANDU through Receive
only ARINC 429 interface through which the required ARINC 429 labels as defined in the APM
configuration file are made available.
Navigate to the Link Status page and scroll down to see the aircraft status. Refer to Figure 6-9.
NOTE: GUI displays roll, pitch, and yaw information in the Aircraft Summary and Link status
page. The aircraft yaw information is calculated from True Heading and True Track
ARINC 429 labels from the aircraft. If True Track label is not configured, yaw value in
the GUI page will indicate as “Unavailable”. There will be no other effects if True
Track is not configured, other than that GUI status.
This page will be updated with current latitude and longitude position of the aircraft.
Draft as of 31 May 2017