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B
2.1
GENERAL INFORMATION
This section contains suggestions and factors to consider before installing the KT 76C ATCRBS
Transponder. Close adherence to these suggestions will assure a more satisfactory performance
from the equipment.
The conditions and tests required for TSO approval of this article are minimum performance stan-
dards. It is the responsibility of those desiring to install this article either on or within a specific
type or class of aircraft to determine that the aircraft installation conditions are within TSO stan-
dards. The article may be installed only if further evaluation by the applicant documents an ac-
ceptable installation and is approved by the Administrator.
2.2
UNPACKING AND INSPECTING EQUIPMENT
Exercise extreme caution when unpacking the unit. Make a visual inspection of the unit for evi-
dence of damage incurred during shipment. If a claim for damage is to be made, save the shipping
container to substantiate the claim. Save all packing materials for use in unit storage or reship-
ment.
2.3
EQUIPMENT INSTALLATION
2.3.1
GENERAL
The following paragraphs contain information pertaining to the initial installation of the KT 76C AT-
CRBS Transponder, including instructions concerning the location and mounting of the supporting
antenna.
The equipment should be installed in the aircraft in a manner consistent with acceptable workman-
ship and engineering practices and in accordance with the instructions set forth in this publication.
To ensure that the system has been properly and safely installed in the aircraft, the installer should
make a thorough visual inspection and conduct an overall operational check of the system on the
ground prior to flight.
The KT 76C system installation will conform to standards designated by the customer, installing
agency and existing conditions as to the unit location and type of installation. However, the fol-
lowing suggestions should be considered before installing your KT 76C system.
2.3.2
AVIONICS COOLING REQUIREMENTS FOR PANEL MOUNTED EQUIPMENT
The greatest single contributor to increased reliability of all modern day avionics is to limit the max-
imum operating temperature of the individual units whether panel or remote mounted. While mod-
ern day individual circuit designs consume much less electrical energy, the watts per cubic inch
Rev 3, May 2004
ATCRBS TRANSPONDER
SECTION II
INSTALLATION
CAUTION
AFTER INSTALLATION OF THE CABLING AND
BEFORE INSTALLATION OF THE EQUIPMENT, A
CHECK SHOULD BE MADE WITH THE AIRCRAFT
PRIMARY POWER SUPPLIED TO THE MOUNT-
ING CONNECTOR TO ENSURE THAT POWER IS
APPLIED ONLY TO THE PINS SPECIFIED IN THE
INTERCONNECT DIAGRAM,
IM 006-10545-0003.dwd
FIGURE 2-2
.
KT 76C
Page 2-1
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