AlliedSignal KAP 140 Manual de Instalação descarregar pdf (Página 21)

BENDIX/KING

KAP 140

Page 2--1

Revision 6, Oct 2002

CS:00991I06.IDU

SECTION II

INSTALLATION

2.1 GENERAL INFORMATION

This section contains general suggestions and information to consider before installation of the

KAP 140 Flight Control System. Close adherence to these suggestions will assure optimum

performance from the equipment. Specific installation requirements are contained in the STC

Installation Manual that pertains to the particular type of aircraft which the equipment is to be

installed.

NOTE

“The conditions and tests required for TSO approval of this article are

minimum performance standards. It is the responsibility of those

desiring to install the article either on or within a specific type or class

of aircraft to determine that the aircraft installation conditions are

within the TSO standards. If not within the TSO standards, the article

may be installed only if further evaluation by the applicant documents

an acceptable 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

shipping 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

maximum operating temperature of the individual units whether panel mounted or remote mounted.

While modern day individual circuit designs consume much less electrical energy, watts per cubic

inch dissipated within the avionics unit remains much the same due to high density packaging

techniques utilized. Consequently, the importance of providing cooling to the avionics stack is still

with us today.

While the KC140 does not require forced air cooling, the combined heat load of several units

operating in a typical avionics location will significantly degrade the reliability of the avionics if

provisions for cooling are not incorporated in the initial installation. Failure to provide cooling to the

equipment will lead to increased avionics maintenance costs and may also void the AlliedSignal Inc

warranty.

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AlliedSignal KAP 140 Manual de Instalação Página 21