User Manual Part 3

Page D-9
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
C. Non-A791 Based OAE-FMA with the LAIM Checklist
E. KRFU (Cont) Waveguide -
KRFU to FMA
(Cont)
The RX in
terconnect 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 2-27, Figure 2-28, or Figure 2-29
and interconnect drawing Figure 2-34,
Figure 2-35, or Figure 2-36.
Electrical
bonding
Electrically bond in accordance with
page 2-9.
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 2-32.
Environmental conditions, refer to
Figure 2-31
Positioning
The aircraft fuselage mount OAE must
be mounted on the top of the fuselage.
FMA AIM Refer to Fuselage Mount Antenna (8).
FMA Install Refer to Fuselage Mount Antenna (8).
FMA radome Attach the radome assembly onto the
AIM.
FMA bonding Electrically bond in accordance with
page 2-29.
FMA alignment Automatic alignment, manual alignment,
or command, refer to FMA Alignment on
page 2-35 and TMA and FMA Antenna
Alignment Procedure on page 2-36.
Section Parameter Item NA √ Value