Honeywell BENDIX/KING KRA 405 - Page 6

B TABLE OF CONTENTS KRA 405
Rev 6, June 2003 IM 006-00104-0006.dwd TOC-2
2-2 KRA 405 Installation Drawing...................... (Dwg 155-05153-0000)....2-17
2-3 Typical Antenna Installation For a Dual Radar Altimeter System..........2-19
2-4 KA 54 (Dorne Margolin Type DMPN 3-3/A) Antenna ...................................
Outline and Mounting................................... (Dwg 155-05159-0000)....2-21
2-5 UBC (Type AD 43013-1) and Comant (Type 01-34-04531)..........................
Antenna Outline and Mounting .................... (Dwg 155-05166-0000)....2-23
2-6 Dorne Margolin (Type DMPN 3-4/A) Antenna ..............................................
Outline and Mounting................................... (Dwg 155-05167-0000)....2-25
2-7 KA 54A (Sensor Systems Type S67-2002) Antenna.....................................
Outline and Mounting................................... (Dwg 071-01501-0000)....2-27
2-8 Aircraft Installation Delay (AID) and Installation Cable Length Chart ....2-29
2-9 TNC Coax/ Connector Assembly (RG393/U) ........................................2-30
2-10 Connector Pin Locations.............................. .........................................2-31
2-11 KRA 405 Altitude Trip Test Point and Adjustment Locations.................2-32
2-12 KRA 405 Test Equipment Setup.................. .........................................2-33
2-13 External Sonalert w/15 Second DH Audio Fader...................................2-34
2-14 KRA 405 Radar Altimeter System Interconnect(Dwg 155-01153-0000)2-35
SECTION III
OPERATION
Paragraph Page
3.1 General....................................................................................................3-1
3.2 Normal Operation ....................................................................................3-1
3.3 Emergency Operation..............................................................................3-3
LIST OF ILLUSTRATIONS
Figure Page
3-1 KNI 415 Control Functions........................... ...........................................3-4
3-2 KNI 416 Control Functions........................... ...........................................3-5
RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
UP536434