User's Manual Part 6

Page C-4
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
4.6 KRFU Physical Examine for physical damage.
Environmental conditions, refer to
Figure 4-27, Figure 4-28, or Figure 4-29
depending on configuration used.
Install the thermal pad in accordance
with KRFU on page 4-16.
The KRFU is installed with the TMA,
refer to OAE TMA Installation Procedure
on page 4-30.
The KRFU feet are configured differently
depending on the part number ordered.
Make sure feet are in the correct
configuration for the aircraft application.
Waveguide Make sure the waveguide is connected
before powering the KRFU.
Waveguide -
KRFU to TMA
Connection must be WR28 for TX and
coaxial cable for RX.
The TX interconnect path loss
The RX interconnect path loss
RX connection at the KRFU requires a
WR42 to coax transition adapter at the
KRFU J4
Electrical
wiring
Electrically wire and interconnect in
accordance with outline drawing
Figure 4-27, Figure 4-28, or Figure 4-29
and interconnect drawing Figure 4-34.
Electrical
bonding
Electrically bond in accordance with
page 4-18.
(b) OAE TMA
Installation Procedure
Physical Refer to OAE TMA Installation
Procedure.
TMA mounting Refer to OAE TMA Installation
Procedure.
TMA interface
mount
brackets
Refer to OAE TMA Installation
Procedure.
Section Parameter Item NA √ Value
Draft as of 31 May 2017