User Manual Part 1

Page 2-14
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
(9) TMA Interface Mount Brackets (if Required)
Depending on the airframe, there may be a need to install a TMA to
airframe interface mount
brackets, which adapts to the tail empennage of the aircraft and in turn supplies a firm flat
base for the TMA assembly.
This is not detailed in this document as the requirement of antenna interface mount is air
frame specific.
(10) TMA Radome and Radome Fairing
Depending on the airframe, there may be a need to install radome fairing which adapts to the
tail empenna
ge of the aircraft.
This is not detailed in this document as the requirement of radome fairing is airframe specific.
(11) TMA Assembly
The tail mount OAE assembly is typically mounted on the Ku SATCOM ra
dio slot on top of
empennage of the aircraft vertical stabilizer.
Consult the airframe manufacturer for identification of appropriate airframe specific
installation slots on the empennage.
The isometric rear and front views of the TMA assembly is shown in Figure 2-3.
Figure 2-3. TMA Assembly Isometric View
The TMA assembly attaches to the base in five (05) locations. Refer to Figure 2-3 and Figure
2-
30 for deta
ils.
(12) TMA Assembly Orientation
Orientation of the TMA assembly is defined with respect to the
principal axes of the aircraft.
The TMA assembly is to be installed such that the TMA J2 connector side is located towards
the front of aircraft as indicated by the arrow as shown in Figure 2-3.
(13) KRFU Installation Location with the TMA
The KRFU install location at the top of aircraft tail empennage is airframe specific.