User Manual Part 1

Page 2-24
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
(6) Airframe Structural Modifications
For the installation of OAE-FMA, structural modifications to the airframe m
ay be required in
the region where the OAE-FMA is to be mounted to accommodate the additional mass of the
antenna assembly and resulting aerodynamic loads.
The aerodynamic loads are dependent on the aircraft type as well as the installation location
of the OAE-FMA on the aircraft, and are therefore installation specific.
Bird strike and rapid decompression need to be considered for analysis and structural
substantiation.
The appropriately qualified personnel should derive the loads and do a structural analysis to
make sure of the suitability of the modifications.
The installer is responsible for all structural modifications to the aircraft.
(7) Mounting Guidelines
This section describes the mounting g
uidelines
for fuselage mount OAE.
Physical Placement:
The aircraft fuselage mount OAE is installed on top of the fuselage for clear satellite
communications.
Figure 2-9 shows a typical installation location for the fuselage mount OAE on an aircraft.
Honeywell recommends not installing the FMA at the mid fuselage station location of the
aircraft near the wings or slightly aft of the wings.
90404243 RF component kit (KRFU to FMA waveguide
and RX coax cable FMA to KRFU)
Table 2-7. FMA installation Kits(Cont)
PN Description