Honeywell International Inc. 9PGTPL-100A 사용자 설명서
Page 2004
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.
When the cables are installed in the aircraft, they must be supported firmly enough to
prevent movement and carefully protected from abrasion. Additional protection must
be supplied in all locations where the cables may be subject to abuse. In wire bundles,
the cables must not be tied tightly together because this increases the possibility of
noise pickup and similar interference. When routing cables through the airframe, the
cables must cross high-level lines at a right angle.
prevent movement and carefully protected from abrasion. Additional protection must
be supplied in all locations where the cables may be subject to abuse. In wire bundles,
the cables must not be tied tightly together because this increases the possibility of
noise pickup and similar interference. When routing cables through the airframe, the
cables must cross high-level lines at a right angle.
The installer must be knowledgeable of system variations that are unique to the
installation, such as system strapping requirements. The installer must use ARINC
Characteristic 718 and 735 as a guide and reference throughout the fabrication and
installation of the cables in the aircraft.
installation, such as system strapping requirements. The installer must use ARINC
Characteristic 718 and 735 as a guide and reference throughout the fabrication and
installation of the cables in the aircraft.
Antenna cabling with unique requirements is described in paragraph 3.C.(5).
(2) Interface Capability and Requirements
The Description and Operation section of this manual lists the types of external
avionics equipment that can be connected to the MILACAS-FR Processor, TA/VSI, and
RA/VSI and describes the types of signals. Determine the types of aircraft equipment
to be connected to the MILACAS-FR system.
avionics equipment that can be connected to the MILACAS-FR Processor, TA/VSI, and
RA/VSI and describes the types of signals. Determine the types of aircraft equipment
to be connected to the MILACAS-FR system.
(3) Primary Power and Circuit Breaker Requirements
The MILACAS-FR system operates primarily from 115 V 400 Hz or 28 V dc power
supplied by the aircraft. The displays use 5 V 400 Hz, 5 V dc or 28 V dc lighting power.
A 26 V 400 Hz input is provided for reference for the synchro-to-digital converters.
Power dissipation varies with the system configuration. Power connections are shown
in the interwiring diagrams, Figure 2002.
supplied by the aircraft. The displays use 5 V 400 Hz, 5 V dc or 28 V dc lighting power.
A 26 V 400 Hz input is provided for reference for the synchro-to-digital converters.
Power dissipation varies with the system configuration. Power connections are shown
in the interwiring diagrams, Figure 2002.
(4) Suppression Pulse Requirements and Wiring
Connections for the suppression pulse from the MILACAS-FR Processor (see Figure
2002) are dependent on aircraft equipment and wiring. Typically, the suppression pin
is connected from the MILACAS-FR Processor to the suppression inputs on the
L-band equipment (i.e., transponder and DME equipment).
2002) are dependent on aircraft equipment and wiring. Typically, the suppression pin
is connected from the MILACAS-FR Processor to the suppression inputs on the
L-band equipment (i.e., transponder and DME equipment).