User's Manual Part 6

Page C-9
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 (Cont) Waveguide -
KRFU to FMA
(Cont)
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 4-35 or
Figure 4-37, depending on the
configuration being used.
Electrical
bonding
Electrically bond in accordance with
page 4-18.
N. FMA Installation
Procedure
Physical
Examine the FMA AIM for physical
damage.
Examine the FMA assembly for
physical damage.
Examine the radome for physical
damage. Refer to Figure 4-32.
Environmental conditions, refer to
Figure 4-31.
Positioning
The aircraft fuselage mount OAE must
be mounted on the top of the fuselage.
FMA AIM Refer to Fuselage Mount Antenna (If
applicable) (8).
FMA Install Refer to Fuselage Mount Antenna (If
applicable) (8).
FMA radome Attach the radome assembly onto the
AIM.
FMA bonding Electrically bond in accordance with
page 4-16.
FMA
alignment
Automatic alignment, manual
alignment, or command, refer to FMA
Alignment on page 2-39 and Inspection
of Waveguide on page 4-43.
Section Parameter Item NA √ Value
Draft as of 31 May 2017