User's Manual Part 1

Page 4-23
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Figure 4-10. FMA Assembly Lifting Fixture Removal
(d) The orientation of the FMA assembly is defined with re
spect to the principal axes of the
aircraft.
(e) Attach the FMA to the AIM with screws and flat washer
s. The AIM is provisioned with
captive nuts. Refer to the airframe specific kits and assembly for fastener specifications
and required torque. Mounting holes in base are accessed from the top between the
antenna and turntable by rotating the assembly in azimuth.
(f) Remove protective cap from disconnect plug on harness.
1 Visually inspect connector and make sure that there are no debris in cavities.
2 Visually inspect the center conductor and verify that it is still straight and the finish
is intact.
(2) FMA Bonding Requirements
(a) Install one end of bonding straps to AIM at labe
led bonding points with screw and
washers.
(b) Install the other end of bonding straps to bonding
points on the FMA base. Refer to the
airframe specific kits and assembly for fastener specifications and required torque.
Refer to Figure 4-1 for the FMA ground strap connection.
(3) Waveguide and RF Coax Interconnection to FMA Assembly
(a) A common RF component kit exists for each
installation type. The ARINC 791 style
installation uses PN 90404243-02. The non ARINC 791 style installation uses PN
90404243-01. Installation drawings specific to each kit are available.
Draft as of 31 May 2017