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Installation; General Information; Kn 62a; Kn 62 And Kn 64 - Honeywell BendixKing KN 62A Installation Manual

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BENDIX/KING
2.1

GENERAL INFORMATION

This section contains information relative to the installation and wiring of the KN 62/62A/64 DME.
A close adherence to methods and procedures discussed herein is required.
2.1.1
KN 62A ONLY
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.
2.1.2

KN 62 AND KN 64

The conditions and tests performed on this article are minimum performance standards. It is the
responsibility of those desiring to install this article either on or within a specifice type or class of
aircraft to determine that the aircraft installation conditions are within these perfomrance 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 care when unpacking the equipment. Make a visual inspection of the unit for
evidence of damage incurred during shipment. If a claim for damage is to be made, save the ship-
ping container to substantiate the claim. The claim should be promptly filed with the transportation
company. It would be advisable to retain the container and packaging material after all equipment
has been removed in the event that equipment storage or reshipment should become necessary.
2.3

EQUIPMENT INSTALLATION

2.3.1

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. While modern day individual circuit designs
consume much less electrical energy, the watts per cubic inch dissipated within avionics units re-
mains much the same due to high density packaging techniques utilized. Consequently, the im-
portance of providing avionics stack cooling is still with us.
Rev 7, November/2004
SECTION II

INSTALLATION

00144I06.TDC
KN 62/62A/64
Page 2-1

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