Honeywell BENDIX/KING KCS55 - SECTION I GENERAL INFORMATION; System Component Description; Functional Description; Technical Characteristics

BENDIX/KING KCS 55/55A
Rev 11, Apr/2007
©Honeywell International Inc. Do not print without express permission of Honeywell Page i
SECTION I
GENERAL INFORMATION
PARAGRAPH PAGE
1.1 SYSTEM COMPONENT DESCRIPTION 1-1
1.2 FUNCTIONAL 1-1
1.3 TECHNICAL CHARACTERISTICS 1-2
1.3.1 KCS 55/55A 1-2
1.3.2 KI 525/525A 1-3
1.3.3 KG 102/102A 1-4
1.3.4 KMT 112 1-5
1.3.5 KA 51/51A 1-5
1.3.6 KA 51B 1-6
1.3.7 KA 52 1-6
1.3.8 KA 57 1-7
1.4 UNITS AND ACCESSORIES SUPPLIED 1-7
1.4.1 KI 525/525A PICTORIAL NAVIGATION INDICATOR 1-7
1.4.2 KG 102/102A DIRECTIONAL GYRO 1-8
1.4.3 KMT 112 MAGNETIC AZIMUTH TRANSMITTER 1-9
1.4.4 KA 51/51A/51B SLAVING ACCESSORY 1-9
1.4.5 KA 52 AUTOPILOT ADAPTER 1-10
1.4.6 KA 57 AUTOPILOT ADAPTER 1-10
1.5 INSTALLATION KITS 1-11
1.6 COMPENSATOR KIT (OPTIONAL) 1-13
1.7 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 1-13
SECTION II
INSTALLATION
PARAGRAPH PAGE
2.1 UNPACKING AND INSPECTING EQUIPMENT 2-1
2.2 PREINSTALLATION CHECK 2-1
2.3 KI 525/525A INDICATOR INSTALLATION 2-2
2.3.1 GENERAL 2-2
2.3.2 MOUNTING 2-2
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
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