Honeywell International Inc. 9PGTPL-100A 사용자 설명서
Page 2002
1 Mar 2006
34-45-54
MAINTENANCE MANUAL
TPL-100A Processor / Part No. 940-0530-001
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
Install the MILACAS-FR in the aircraft in a manner consistent with acceptable
workmanship and engineering practices. Follow the instructions in this
publication. To make sure that the system has been properly and safely installed
in the aircraft, the installer must make a thorough visual inspection. The installer
must perform the post-installation/operational check of the system on the ground
prior to flight.
workmanship and engineering practices. Follow the instructions in this
publication. To make sure that the system has been properly and safely installed
in the aircraft, the installer must make a thorough visual inspection. The installer
must perform the post-installation/operational check of the system on the ground
prior to flight.
CAUTION: AFTER INSTALLATION OF THE CABLING AND BEFORE
INSTALLATION OF THE EQUIPMENT, APPLY AIRCRAFT PRIMARY
POWER TO THE UNIT CONNECTORS AND MAKE SURE THAT
POWER GOES ONLY TO THE PINS SPECIFIED IN THE
INTERCONNECT DIAGRAMS, FIGURE 2002.
POWER TO THE UNIT CONNECTORS AND MAKE SURE THAT
POWER GOES ONLY TO THE PINS SPECIFIED IN THE
INTERCONNECT DIAGRAMS, FIGURE 2002.
B. Location of Equipment
(1) TCAS Antenna Location
The system uses a top-mounted directional antenna and either a bottom-mounted
directional or omnidirectional antenna.
directional or omnidirectional antenna.
Refer to directional antenna outline drawings in Figure 2001, and if applicable,
manufacturer's documentation for the omnidirectional antenna.
manufacturer's documentation for the omnidirectional antenna.
The top directional ANT-81A TCAS antenna is mounted within 5 degrees of the
centerline of the aircraft and as far forward on the constant radius portion of the
fuselage as possible.
centerline of the aircraft and as far forward on the constant radius portion of the
fuselage as possible.
Obstructions, including other antennas, must not be present in the forward direction of
either the top or bottom ANT-81A TCAS antenna.
either the top or bottom ANT-81A TCAS antenna.
The bottom ANT-81A TCAS antenna (directional or omni) is located within 5 degrees
of the centerline of the aircraft and as close as possible to the vertical frame station
location of the top directional antenna (but can vary up to a maximum of 25 feet
longitudinally from the top antenna).
of the centerline of the aircraft and as close as possible to the vertical frame station
location of the top directional antenna (but can vary up to a maximum of 25 feet
longitudinally from the top antenna).
The ANT-81A TCAS top and bottom antenna must not be mounted closer than 30
inches from any other antenna on the aircraft. This provides 20 dB of isolation or 2.5
wavelengths at 1090 MHz.
inches from any other antenna on the aircraft. This provides 20 dB of isolation or 2.5
wavelengths at 1090 MHz.