User Manual Part 3

Page 3-32
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
(2) JetWave™ AES system status can be viewed through the GUI. Refer to Checking Status
Information section for description.
(3) On the Modman LRU the status indicator LED is on the Modman front panel. The various
Modman status indications are shown in Table 3-14.
H. Repair Requirements
(1) The BITE functionality of JetWave™ AES system can identify the faulty LRU in case any
occurrence of functional problems and this can be accessed through Modman.
(2) In accordance with continued airworthiness instructions, if a JetWave™ AES system is
inoperative, use Standard Practices Chapter of the Aircraft Maintenance Manual to:
• Remove the unit
• Secure cables and wiring
• Collar applicable switches and circuit breakers, and placard them as “inoperative”.
Before flight, revise the equipment list and weight and balance data as applicable, and record the removal
of the unit in the log book. Refer to section 91.213 of the FAR or the aircraft’s minimum equipment list. All
repairs must be done at the Honeywell factory.
10. Troubleshooting
This section supplies troubleshooting procedures for JetWave™ system. Airline maintenance
engineers can troubleshoot JetWave™ system on the ground, with the Health Status Information
and Fault Details and Isolation assistance displayed on the AES GUI.
Table 3-13. Unscheduled Maintenance
Item Potential Damage Inspection
JetWave™ AES FMA
OAE/TMA OAE
Heavy rain / hail Paint erosion External visual
bird strike Paint damage/radome
puncture
External visual
JetWave™ AES
system Failure
NA NA Removal
Table 3-14. Modman LED Status Indications
Status LED Mode
Off No electrical power / electrical power is
supplied but prior to boot.
Flash green at a minimum
of 10 seconds
Modman initialization
On - green Modman in normal operation
On - red Modman in Fault Mode