User Manual Part 1

Page 2-13
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
CAUTION: THE TAIL MOUNT OAE ASSEMBLY IS ELECTROSTATIC-SENSITIVE. STANDARD
ELECTROSTATIC-SENSITIVE HANDLING PROCEDURES MUST BE OBSERVED.
(6) TMA Airframe Structural Modifications
Fo
r the installation of TMA, structural modifications to the
tail empennage of the airframe may
be required to accommodate the additional mass of the antenna assembly and aerodynamic
loads.
The aerodynamic loads are dependent on the aircraft type as well as the installation location
of the tail mount antenna assembly and KRFU on the aircraft, and are therefore installation
specific.
The appropriately qualified personnel should derive the loads and perform a structural
analysis to verify the suitability of the modifications.
The installer is responsible for all structural modifications to the aircraft.
(7) TMA Mounting Guidelines
This section describes the mounting guid
elines for th
e tail mount OAE.
The radome installation is aircraft specific.
The airframe manufacturer can be consulted to determine the torque requirements for
mounting the TMA assembly, KRFU, radome, and radome fairing for each unique installation.
(8) TMA Physical Placement
The TMA and KRFU must be mounted on the top of the tail empennage for clear satellite
comm
unications. Figure 2-2 shows a typical installation location for the tail mount antenna
assembly on an aircraft.
Figure 2-2. TMA Installation Location
Table 2-5. TMA Installation Kits
PN Description
SCD-90402677 WR42 to 2.92 mm coax adapter