User's Manual Part 1

Page 4-21
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
The FMA may be installed anywhere on the top of the aircraft, Honeywell recommends not installing
the FMA at the mid fuselage station near the wing or slightly aft of the wing due to higher aero loads.
.
Figure 4-8. FMA Install Location
The fuselage antenna assembly and K
RFU (if installed outside the aircraft) will be mounted on the
antenna interface mount and it supplies a means to secure all equipment and wiring mounted on it.
Depending on the airframe, the AIM/LAIM is installed to provide a firm flat base for installation of
the FMA and KRFU. These are detailed in the next sections. For customers who want to build their
own AIM, please reference the third-party OAE specification, SP-90405087.
H. FMA Bonding
The bonding straps are installed before proceeding with installation
of FMA assembly on the A791
based AIM or LAIM.
The FMA assembly and KRFU must be bonded to the airframe.
Consult the airframe manufacturer for the correct torque values.
I. FMA Installation Procedure
Following installation activities are detailed in subsequent sections:
• Installation of the FMA.
• Connecting the waveguide, RF coax interface to the FMA.
• Installation of KRFU and bonding straps.
• Installation of waveguide and coax between FMA and KRFU.
Draft as of 31 May 2017