User's Manual Part 6

Page C-5
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
(b) OAE TMA
Installation Procedure
(Cont)
TMA install Refer to OAE TMA Installation
Procedure.
TMA radome
and radome
fairing
Depending on the airframe, there may
be a need to install radome fairing
which adapts to the tail empennage of
the aircraft, consult aircraft OEM.
Radome and fairing installation is
aircraft specific. Refer to aircraft
specific SDIM for details.
NOTE:
Before removing the Tail
Mount Radome, Honeywell
recommends manually
steering the TMA to a safe
antenna orientation position
using the JetWave™ GUI. The
TMA parking position is
included in the AES System
Configuration File, which can
be accessed through the GUI
web interface and by
navigating to Configuration
File page. Consult aircraft
specific SDIM for detailed
instructions.
TMA bonding Electrically bond in accordance with
Figure 4-30.
TMA
alignment
Automatic alignment, manual
alignment, or command, refer to TMA
Alignment on page 2-23 and Inspection
of Waveguide on page 4-43
Section Parameter Item NA √ Value
Draft as of 31 May 2017