B TABLE OF CONTENTS KRA 405
Rev 6, June 2003 IM 006-00104-0006.dwd TOC-1
SECTION I
GENERAL INFORMATION
Paragraph Page
1.1 Introduction..............................................................................................1-1
1.2 Description of Equipment.........................................................................1-1
1.3 Technical Characteristics.........................................................................1-1
1.4 Units and Accessories Supplied ..............................................................1-6
1.5 Accessories Required But Not Supplied..................................................1-8
1.6 License Requirements.............................................................................1-8
1.7 Continued Airworthiness..........................................................................1-8
LIST OF TABLES
Table Page
1-1 KRA 405 Radar Altimeter Technical Characteristics ...............................1-1
1-2 KNI 415, KNI 416 Indicator Technical Characteristics.............................1-4
1-3 KA 54 Antenna Technical Characteristics ...............................................1-5
1-4 KA 54A Antenna Technical Characteristics.............................................1-6
SECTION II
INSTALLATION
Paragraph Page
2.1 General Information.................................................................................2-1
2.2 Avionics Cooling Requirements for Panel Mounted Equipment ..............2-1
2.3 Altitude Trip Adjustment...........................................................................2-1
2.4 KRA 405 System Installation ...................................................................2-3
2.5 Post Installation Tests..............................................................................2-8
LIST OF TABLES
Table Page
2-1 Altitude Trip Set Test Equipment (Audio Generator) ...............................2-2
2-2 Approved Antennas .................................................................................2-4
2-3 RF Leakage Test Equipment (Microwave Absorber)...............................2-9
2-4 RF Output Test Equipment (Delay Line)................................................2-11
2-5 IF and Altitude Processor Test Equipment (Audio Generator) ..............2-12
2-6 Indicated KNI 415, KNI 416 Altitude (+/- 7%) ........................................2-13
LIST OF ILLUSTRATIONS
Figure Page
2-1 KNI 415, KNI 416 Installation Drawing ........ (Dwg 155-05160-0000)....2-15
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
UP536434