Ki 525/525A Indicator Installation; Mounting; General - Honeywell BENDIX/KING KCS55 Installation Manual

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Table of Contents

RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION

BENDIX/KING

THE FOLLOWING PRECAUTIONS MUST BE OB-

SERVED WHILE FABRICATING THE SYSTEM IN-

STALLATION HARNESS AND REMOVING/REIN-

STALLING UNITS FOR MAINTENANCE.

AVOID CONNECTOR DAMAGE:

1. WHEN FABRICATING THE INSTALLATION

HARNESS FOR THE KCS 55/KCS 55A SYSTEM,

SUFFICIENT STRAIN RELIEF SHOULD BE LEFT

IN THE HARNESS AT THE CONNECTORS SO AS

NOT TO APPLY ANY UNDUE STRESS TO THEM.

2. SYSTEM CONNECTORS SHOULD BE IN-

SPECTED FOR POSSIBLE DAMAGE DURING RE-

MOVAL AND REINSTALLATION.

3. CARE SHOULD BE TAKEN WHEN MATING THE

CONNECTORS TO INSURE THAT THE PINS EN-

GAGE WITHOUT UNDUE FORCE SO AS NOT TO

DAMAGE PINS IN EITHER CONNECTOR. DAM-

AGED CONNECTORS WILL COME UNDER

CLOSE INSPECTION TO DETERMINE THE VA-

LIDITY OF ANY WARRANTY CLAIMS.

4. AFTER INSTALLATION OF THE CABLING AND

BEFORE INSTALLATION OF THE EQUIPMENT, A

CHECK SHOULD BE MADE WITH AIRCRAFT PRI-

MARY POWER SUPPLIED TO THE MOUNTING

CONNECTOR. THIS WILL ENSURE THAT POW-

ER IS APPLIED ONLY TO THE PINS SPECIFIED

IN THE INTERCONNECTION DIAGRAMS.

The TSO identifies the minimum performance standards, tests, and other conditions applicable for

issuance of design and production approval of the article. The TSO does not specifically identify

acceptable conditions for installation of the article. The TSO applicant is responsible for docu-

menting all limitations and conditions suitable for installation of the article. An applicant requesting

approval for installation of the article within a specific type or class of product is responsible for

determining environmental and functional compatibility.

2.3