Honeywell KI 209, KI 208 Installation Manual

RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
h
INSTALLATION MANUAL
KI 208, KI 209
NAVIGATION INDICATORS
MANUAL NUMBER 006-00140-0004
Revision 4, August 2002
UP536434
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
PRIOR TO EXPORT OF THIS DOCUMENT, REVIEW FOR EXPORT LICENSE REQUIREMENT IS NEEDED.
COPYRIGHT NOTICE
©1988, 1996, 2002 HONEYWELL INTERNATIONAL INC.
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REPRODUCTION OF THIS PUBLICATION OR ANY PORTION THEREOF BY ANY MEANS WITHOUT THE EXPRESS WRITTEN PERMISSION OF HONEYWELL IS PROHIBITED. FOR FURTHER INFORMATION CONTACT THE MANAGER, TECHNICAL PUBLICATIONS, HONEYWELL, ONE TECHNOLOGY CENTER, 23500 WEST 105TH STREET OLATHE KS 66061 TELEPHONE: (913) 782-0400.
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
BENDIX/KING KI 208, KI 209
REVISION HISTORY
INSTALLATION MANUAL
BENDIX/KING
KI 208, KI 209
Navigation Indicators
PART NUMBER REV DATE DESCRIPTION
--------------------------------------------------------------------------------------------------------------------­006-00140-0004 4 Aug/2002 Replaces P/N 006-00140-0003.
006-00140-0003 3 Oct/1996 Replaces P/N 006-00140-0002.
006-00140-0002 2 Mar/1988 Replaces P/N 006-00140-0001.
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RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
BENDIX/KING KI 208, KI 209
THIS PAGE RESERVED
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BENDIX/KING TABLE OF CONTENTS KI 208, KI 209

SECTION I
GENERAL INFORMATION
Paragraph Page
1.1 Introduction .............................................................................................1-1
1.2 Equipment Description.............................................................................1-1
1.3 Technical Characteristics.........................................................................1-1
1.4 Units and Accessories Supplied ..............................................................1-2
1.5 Accessories Required, But Not Supplied.................................................1-3
1.6 License Requirements.............................................................................1-3
1.7 Requirements for TSO’d VOR/ ILS/ Glideslope System..........................1-3
LIST OF TABLES
Table Page
1-1 Technical Characteristics KI 208, KI 209.................................................1-1
SECTION II
INSTALLATION
Paragraph Page
2.1 General....................................................................................................2-1
2.2 Unpacking and Inspecting Equipment .....................................................2-1
2.3 Installation KI 208, KI 209 .......................................................................2-1
2.4 Post Installation Checkout .......................................................................2-2
LIST OF TABLES
Table Page
2-1 ILS Deflection ..........................................................................................2-3
2-2 Glideslope Deflection...............................................................................2-3
LIST OF ILLUSTRATIONS
Figure Page
2-1 KI 208 Pinout List.....................................................................................2-5
2-2 KI 209 Pinout List.....................................................................................2-6
2-3 Crimping Tool ..........................................................................................2-7
2-4 KI 208, KI 209 Connector Assembly .......................................................2-8
2-5 KI 208, KI 209 Outline and Mounting .....(Dwg 155-05235-0000)...........2-9
2-6 KI 208, KI 209 Typical Interconnect ....... ..............................................2-11
2-7 KI 208 Non-TSO’d System Interconnect.(Dwg 155-01223-0000).........2-13
2-8 KI 209 System Interconnect....................(Dwg 155-01241-0000).........2-15
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BENDIX/KING TABLE OF CONTENTS KI 208, KI 209
SECTION III
OPERATION
Paragraph Page
3.1 Equipment Operation ..............................................................................3-1
3.2 Indicator Control Functions KI 208, KI 209..............................................3-2
LIST OF ILLUSTRATIONS
Figure Page
3-1 KI 208 Control Functions .........................................................................3-3
3-2 KI 209 Control Functions .........................................................................3-4
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BENDIX/KING KI 208, KI 209

SECTION I

GENERAL INFORMATION

1.1 INTRODUCTION

This manual contains information relative to the physical, mechanical and electrical characteristics of the Bendix/King Silver Crown KI 208 and KI 209.

1.2 EQUIPMENT DESCRIPTION

The Bendix/King KI 208 VOR Indicator is designed to operate with VHF navigational equipment (such as the KX 155, KX 155A, KX 165A) to provide OMNI (VOR) or LO­CALIZER (LOC) information. The VHF navigational receiver receives and detects the omni or localizer information. The KI 208 converts this information to DC signals which drive the LEFT-RIGHT needle and the TO-OFF-FROM flag of the visual indicator.
The KI 209 ILS Indicator performs the same functions as the KI 208. In addition, it contains an UP-DOWN glideslope needle with an OFF warning flag.
An anti reflective lens coating is also available on some models of the KI 208 and KI 209.

1.3 TECHNICAL CHARACTERISTICS

TABLE 1-1 Technical Characteristics KI 208, KI 209
SPECIFICATION CHARACTERISTIC
KI208, KI209 TSO COMPLIANCE: C40a, C36c Class C Cat 2.
DO-138 Environmental Cat. DAPAAAXXXXXX.
ADDITIONAL TSO COMPLIANCE FOR KI 209 ONLY:
SIZE: See Figure 2-5 (P/N 155-05235-0000).
WEIGHT: See Figure 2-5 (P/N 155-05235-0000).
POWER REQUIREMENTS:
KI 208, KI 209 Indicator
C34c Class D Cat 2.
14 Vdc at 50 mA, 28 Vdc at 50 mA.
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KI 208 Lighting
KI 209 Lighting
KI 208, KI 209 Lighting
Rev 4, Aug 2002 IM 006-00140-0004 Page 1-1
14 Vdc at 80 ±20 mA. 14 Vdc at 160 ±45 mA. 28 Vdc at 80 ±20 mA.
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
BENDIX/KING KI 208, KI 209
TABLE 1-1 Technical Characteristics KI 208, KI 209
SPECIFICATION CHARACTERISTIC
VOR/LOC:
Input Impedance:
Nominal Composite Input Level:
Localizer Sensitivity:
OMNI Accuracy:
OMNI Sensitivity:
External Load:
GLIDESLOPE DEVIATION METER:
Input Impedance:
Deflection Sensitivity:
GLIDESLOPE FLAG:
Input Impedance:
50 k ohms, nominal.
LOC: 0.33 ±10% Vrms. VOR: 0.50 ±10% Vrms ARINC phased.
4 dB tone ratio will give 3 dot scale deflection.
±2° max error, ±1° typical.
±10° off course gives full scale deflection.
ARINC autopilot deviation (two 1 k loads).
1 k ±5% ohms.
150 ±5% uA for full scale deflection.
1 k ±5% ohms minimum.
Deflection Sensitivity:
125 uA for flag to leave stop. 260 uA maximum for fully concealed flag.

1.4 UNITS AND ACCESSORIES SUPPLIED

1.4.1 KI 208 VOR Indicator
066-3056-00 066-3056-02 Antireflective lens
1.4.2 KI 209 ILS Indicator
066-3056-01 066-3056-03 Antireflective lens
1.4.3 Bendix/King Equipment Installation Kit (P/N 050-01550-0000) which includes mating connectors, mounting hardware, etc., is as follows:
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