User's Manual Part 2

Page 4-38
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
This is not detailed in this document as the requirement of antenna interface mount is air frame
specific.
J. TMA Radome and Radome Fairing
Depending on the airframe, there may be a need to install radome fairing which adapts to the tail
empennage of the aircraft.
Th
is is not detailed in this document as the requirement of radome fairing is airframe specific.
K. TMA Assembly
The tail mount OAE assembly is typically mounted in the same location
as the Ku SA
TCOM radio
slot on the top of the aircraft tail/empennage.
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 4-19.
Figure 4-19. TMA Assembly Isometric View
The TMA assembly attaches to the base in five (05) locations. Refer to Figure 4-19 and Figure 4-30
for details.
L. 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 4-19.
4.9 Radome
The radome installation is aircraft specific. See aircraft specific SDIM for details.
Depending on the AIM selected, the radome gets installed differently.
With the A791 based AIM, the Radome will be installed on the A791 based AIM.
Draft as of 31 May 2017