User's Manual Part 6

Page C-13
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) Physical
(Cont)
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 FMA
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
thru Figure 4-37, depending on the
configuration being used.
Electrical
bonding
Electrically bond in accordance with
page 4-18.
I. 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
for clear satellite communications.
FMA LAIM Refer to Fuselage Mount Antenna (If
applicable) (8).
Install radome
skirt fairing
Install and attach the radome skirt
fairing to fuselage with 39 fasteners.
Section Parameter Item NA √ Value
Draft as of 31 May 2017