INSTALLATION MANUAL KNI 582 RADIO MAGNETIC INDICATOR Manual Number 006-00193-0003 Revision 3, March/2007
Honeywell - Confidential THIS DOCUMENT AND ALL INFORMATION AND EXPRESSION CONTAINED HEREIN ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., ARE PROVIDED IN CONFIDENCE, AND MAY BE USED BY PERSONS REQUIRED BY FEDERAL AVIATION REGULATION PART 21.50 TO COMPLY WITH ANY OF THE TERMS OF THESE INSTRUCTIONS. EXCEPT AS SET FORTH ABOVE, NO PERSON MAY, IN WHOLE OR IN PART, USE, DUPLICATE OR DISCLOSE THIS INFORMATION FOR ANY PURPOSE WITHOUT THE PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC.
KNI 582 Honeywell Materials License Agreement The documents and information contained herein ("the Materials") are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc (collectively "Honeywell").
KNI 582 6. Term - This License Agreement is effective until terminated as set forth herein. This License Agreement will terminate immediately, without notice from Honeywell, if you fail to comply with any provision of this License Agreement or will terminate simultaneously with the termination or expiration of your applicable product support agreement, authorized repair facility agreement, or your formal designation as a third party service provider.
KNI 582 REVISION HIGHLIGHTS Part Number 006-00193-0003 Rev 3 Date Mar/2007 Description Replace all pages of the manual. This is a complete reprint. Removed NVG versions from the manual. Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
KNI 582 TABLE OF CONTENTS SECTION 1 GENERAL INFORMATION 1.1 1.2 1.3 1.4 1.4.1 1.4.2 1.5 1.6 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EQUIPMENT DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TECHNICAL CHARACTERISTICS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UNITS AND ACCESSORIES SUPPLIED . . . . . . . . . . . . . . . . . . . . . . . . . . . KNI 582 RMI CONFIGURATIONS . . . . . . . . .
KNI 582 LIST OF FIGURES Figure 2-1 Figure 2-2 Figure 2-3 Figure 2-4 Figure 2-5 Figure 2-6 Figure 2-7 Figure 2-8 Figure 2-9 Figure 2-10 Figure 3-1 KNI 582 Outline and Mounting Drawing . . . . . . . . . . . . . . . . . . . . . . . 2-5 Connector Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-7 KNI 582 Pin Functions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-8 KNI 582/KDF 805/KNR 665A/KNR 615 Interconnect . . . . . . . . . . . . .
KNI 582 LIST OF TABLES Table 1-1 - KNI 582 RMI Technical Characteristics. . . . . . . . . . . . . . . . . . . . . . . . . . . Table 1-2 - KNI 582 RMI Configurations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 1-3 - KNI 582 RMI Installation Kit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Table 1-4 - Additional Equipment, Compatible with KNI 582 RMI . . . . . . . . . . . . . . . . Rev 3, March/2007 ©Honeywell International Inc.
KNI 582 SECTION 1 GENERAL INFORMATION 1.1 INTRODUCTION This manual contains information relative to the physical, mechanical, and electrical characteristics of the KNI 582 Radio Magnetic Indicator. General installation instructions are also included. 1.2 EQUIPMENT DESCRIPTION The KNI 582 Radio Magnetic Indicator (PN 066-3060-00/01/02/03/04/10/11/12/13) provides bearing information to either ADF or VOR stations by means of two pointers, each of which is read against the compass card.
KNI 582 SPECIFICATION CHARACTERISTIC POWER REQUIREMENTS Primary: 11.33VDC 0.4A maximum 26VAC 400Hz 6VA Lighting: 28V at 80mA maximum 5V at 460mA maximum Note: 14V Installations may use 5V Versions with dropping resistor. COMPASS HEADING INPUT Operates from any slaved magnetic compass with ARINC X, Y, and Z outputs. Z grounded externally. COMPASS VALID Valid = +27.5VDC Invalid = 0VDC 2mA maximum VOR/LOC COMPOSITE INPUT (-04 Version TACAN Compatible) 0.
KNI 582 SPECIFICATION CHARACTERISTIC B. Receiver 1. Input resistance = 1K ± 5% returned to +V 2. +V = 9.0V ± 15% C. Interconnecting Lines 1. Maximum Shunt Capacity = 2000 pF II Waveform Timing A. Data 1. Data Rate - Approx. 1KHz 2. Negative Logic (“Low True”) B. Clock 1. The negative going edge of the clock waveform will be greater than 10us and less than 250us from any data transistors point. 2. The minimum time that the clock spends in either the high or low state will be greater than 10us. C.
KNI 582 1.4 UNITS AND ACCESSORIES SUPPLIED 1.4.1 KNI 582 Configurations The KNI 582 RMI is available in the following versions: PART NUMBER DESCRIPTION 066-3060-00 Black Bezel, 27.5 VDC/26VAC Lights 066-3060-01 Black Bezel, 5 VDC/5VAC Lights 066-3060-02 Black Bezel, 27.5 VDC/26VAC Lights 066-3060-03 Black Bezel, 5 VDC/5VAC Lights 066-3060-04 Black Bezel, 5 VDC/5VAC Lights (TACAN Compatible) 066-3060-10 Black Bezel, 27.
KNI 582 PART NUMBER DESCRIPTION -00 -01 -02 -03 089-05115-0012 Scr. FHP 6-32 x 3/4 4 0 4 0 089-06461-0012 Scr. FHP 6-32 x 3/4 0 4 0 4 030-01157-0011 Socket Crmp 20G 0 0 49 49 030-01176-0000 HSG Conn 50S 0 0 1 1 030-01188-0000 Pin Polrzin Female 0 0 1 1 030-02350-0015 Conn Sub-Min F 50P 1 1 0 0 030-02414-0001 Hood & Lvr Mdfd 1 1 1 1 Table 1-3 - KNI 582 RMI Installation Kit (Cont) 1.
KNI 582 1.6 LICENSE REQUIREMENTS None. 1.7 CONTINUED AIRWORTHINESS INSTRUCTIONS 1.7.1 Equipment The instructions for continued airworthiness given in the TC or STC approvals for this product supplements or supersedes the instructions for continued airworthiness in this manual. Most Honeywell products are designed and manufactured to allow "on condition maintenance". On condition maintenance is described as follows; There are no periodic service requirements necessary to maintain continued airworthiness.
KNI 582 SECTION 2 INSTALLATION 2.1 GENERAL This section contains the suggestions and information to consider before installation of the KNI 582 Radio Magnetic Indicator into the aircraft. Close adherence to these suggestions will assure optimum performance from the equipment. 2.2 UNPACKING AND INSPECTING EQUIPMENT Exercise extreme care when unpacking the equipment. Make a visual inspection of the unit for evidence of damage during shipment.
KNI 582 2. The above step should be repeated for at least one additional heading 90° from the first. B. ADF Accuracy 1. Depending on the application, the KNI 582 RMI can be tested for either DC SIN/COS ADF or X, Y, Z, ADF by tuning in a station on the appropriate ADF. 2. In the DC SIN/COS Mode the needles should position the direction of the station +5°. Repeat for at least one more station. 3. Repeat Step 2 for X, Y, Z, ADF +5°. C. VOR Accuracy 1.
KNI 582 TEST DATA Compass Card Accuracy (Magnetic Heading) minus (KNI 582 RMI Indication) = Error (±2° Max.) (±2° Max.) ADF (D.C. SIN/COS) Accuracy (Station Heading) minus (KNI 582 RMI Indication) = Error (±5° Max.) (±5° Max.) ADF (X, Y, and Z) Accuracy (Station Heading) minus (KNI 582 RMI Indication) = Error (±5° Max.) (±5° Max.) VOR (OBI DIGITAL) Accuracy (Station Bearing) minus (KNI 582 RMI Indication) = Error (±5° Max.) (±5° Max.
KNI 582 Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
KNI 582 Figure 2-2 Connector Assembly Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
KNI 582 Figure 2-3 KNI 582 Pin Functions Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
KNI 582 Figure 2-8 KNI 582 Cable Assembly (Dwg No 155-02114-0000, R-AA) Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
KNI 582 Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.
KNI 582 SECTION 3 OPERATION 3.1 GENERAL The KNI 582 RMI display is discussed below: A. Compass Card/Lubber Line: This rotating card repeats gyro stabilized magnetic compass information. Aircraft heading is read from the compass card under the orange lubber line. B. Compass Flag: This flag comes into view whenever the compass system determines that the heading is invalid or the indicated heading has an error of 5° or more. C.
KNI 582 Figure 3-1 KNI 582 Control Functions Rev 3, March/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.