Honeywell KSN770 Aviation Communications Transceiver User Manual 006 10716 0000

Honeywell International Inc. Aviation Communications Transceiver 006 10716 0000

User Manual

DraftHoneywell International Inc.23500 West 105th StreetOlathe, Kansas 66061-8425U.S.A.CAGE: 22373Telephone: (800) 601-3099 (Toll Free U.S.A./Canada)Telephone: (602) 365-3099 (International Direct)Telephone: 00-800-601-30999 (EMEA Toll Free)Telephone: 420-234-625-500 (EMEA Direct)Website: www.myaerospace.comPage T-1Publication Number 006-10716-0000, Revision 0 Initial 6 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited.ECCN: 7E994, NLR Eligible.System Installation ManualKSN 765/770 Safety NavigatorPart Number CAGE066-01204-0101 22373066-01204-1101 22373066-01213-0101 22373066-01213-1101 22373Legal NoticeExport ControlDraft as of 10/15/2012
DraftPage T-26 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Proprietary InformationHoneywell – ConfidentialTHIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., CONTAIN TRADE SECRETS AND MAY NOT, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC. ALL RIGHTS RESERVED.Honeywell Materials License AgreementThe documents and information contained herein (“the Materials”) are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc. (collectively “Honeywell”). These Materials are provided for the exclusive use of Honeywell Service Centers; Honeywell-authorized repair facilities; operators of Honeywell aerospace products subject to an applicable product support agreement, their wholly owned-subsidiaries or a formally designated third party service provider; and direct recipients of Materials from Honeywell’s Aerospace Technical Publication Distribution. The terms and conditions of this License Agreement govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the operation, maintenance, or repair of Honeywell aerospace products conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. However, this License Agreement will govern in the event of a conflict between its terms and conditions and those of a purchase order or acknowledgement.1. License Grant - If you are a party to an applicable product support agreement, a Honeywell Service Center agreement, or an authorized repair facility agreement, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to operate, maintain, or repair Honeywell aerospace products only in accordance with that agreement.If you are a direct recipient of these Materials from Honeywell’s Aerospace Technical Publication Distribution and are not a party to an agreement related to the operation, maintenance or repair of Honeywell aerospace products, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to maintain or repair the subject Honeywell aerospace products only at the facility to which these Materials have been shipped ("the Licensed Facility"). Transfer of the Materials to another facility owned by you is permitted only if the original Licensed Facility retains no copies of the Materials and you provide prior written notice to Honeywell.2. Rights In Materials - Honeywell retains all rights in these Materials and in any copies thereof that are not expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets. No license to use any Honeywell trademarks or patents is granted under this License Agreement.3. Confidentiality - You acknowledge that these Materials contain information that is confidential and proprietary to Honeywell. You agree to take all reasonable efforts to maintain the confidentiality of these Materials.4. Assignment And Transfer - This License Agreement may be assigned to a formally designated service designee or transferred to a subsequent owner or operator of an aircraft containing the subject Honeywell aerospace products. However, the recipient of any such assignment or transfer must assume all of your obligations under this License Agreement. No assignment or transfer shall relieve any party of any obligation that such party then has hereunder. 5. Copies of Materials - Unless you have the express written permission of Honeywell, you may not make or permit making of copies of the Materials. Notwithstanding the foregoing, you may make copies of only portions of the Material for your internal use. You agree to return the Materials and any copies thereof to Honeywell upon the request of Honeywell.Draft as of 10/15/2012
DraftPage T-36 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.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. Upon termination of this License Agreement, you will return these Materials to Honeywell without retaining any copies and will have one of your authorized officers certify that all Materials have been returned with no copies retained.7. Remedies - Honeywell reserves the right to pursue all available remedies and damages resulting from a breach of this License Agreement.8. Limitation of Liability - Honeywell does not make any representation regarding the use or sufficiency of the Materials. THERE ARE NO OTHER WARRANTIES, WHETHER WRITTEN OR ORAL, EXPRESS, IMPLIED OR STATUTORY, INCLUDING, BUT NOT LIMITED TO, (i) WARRANTIES ARISING FROM COURSE OF PERFORMANCE, DEALING, USAGE, OR TRADE, WHICH ARE HEREBY EXPRESSLY DISCLAIMED, OR (ii) WARRANTIES AGAINST INFRINGEMENT OF INTELLECTUAL PROPERTY RIGHTS OF THIRD PARTIES, EVEN IF HONEYWELL HAS BEEN ADVISED OF ANY SUCH INFRINGEMENT. IN NO EVENT WILL HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES, SPECIAL DAMAGES, INDIRECT DAMAGES, LOSS OF PROFITS, LOSS OF REVENUES, OR LOSS OF USE, EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES. TO THE EXTENT PERMITTED BY APPLICABLE LAW, THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHER LIABILITY ARISES FROM BREACH OF CONTRACT, WARRANTY, TORT (INCLUDING BUT NOT LIMITED TO NEGLIGENCE), BY OPERATION OF LAW, OR OTHERWISE.9. Controlling Law - This License shall be governed and construed in accordance with the laws of the State of New York without regard to the conflicts of laws provisions thereof. This license sets forth the entire agreement between you and Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties.Safety AdvisoryWARNING: BEFORE THE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED, KNOW THE HANDLING, STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE MANUFACTURER OR SUPPLIER. FAILURE TO OBEY THE MANUFACTURERS’ OR SUPPLIERS’ RECOMMENDATIONS CAN RESULT IN PERSONAL INJURY OR DISEASE.This publication describes physical and chemical processes which can make it necessary to use chemicals, solvents, paints, and other commercially available materials. The user of this publication must get the Material Safety Data Sheets (OSHA Form 174 or equivalent) from the manufacturers or suppliers of the materials to be used. The user must know the manufacturer/ supplier data and obey the procedures, recommendations, warnings and cautions set forth for the safe use, handling, storage, and disposal of the materials.Warranty/Liability AdvisoryWARNING: HONEYWELL ASSUMES NO RESPONSIBILITY FOR ANY HONEYWELL EQUIPMENT WHICH IS NOT MAINTAINED AND/OR REPAIRED IN ACCORDANCE WITH HONEYWELL’S PUBLISHED INSTRUCTIONS AND/OR HONEYWELL’S FAA/SFAR 36 REPAIR AUTHORIZATION. NEITHER DOES HONEYWELL ASSUME RESPONSIBILITY FOR SPECIAL TOOLS AND TEST EQUIPMENT FABRICATED BY COMPANIES OTHER THAN HONEYWELL.WARNING: INCORRECTLY REPAIRED COMPONENTS CAN AFFECT AIRWORTHINESS OR DECREASE THE LIFE OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL TOOLING OR TEST EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS OR GIVE UNSATISFACTORY RESULTS.Draft as of 10/15/2012
DraftPage T-46 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Copyright - NoticeCopyright 2012 Honeywell International Inc. All rights reserved.Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies.Draft as of 10/15/2012
DraftPage TI-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.TRANSMITTAL INFORMATIONTHIS IS AN INITIAL RELEASE OF THE KSN 765/770 SAFETY NAVIGATOR SIM PUB. NO. 006-10716-0000 AND IS ISSUED FOR USE IN SUPPORT OF THE FOLLOWING:Table TI-1 shows the applicable components.Revision HistoryTable TI-2 shows the revision history of this SIM.Table TI-1. Applicable Components Component PN Nomenclature066-01204-0101 KSN 770 Safety Navigator066-01204-1101 KSN 770 Safety Navigator066-01213-0101 KSN 765 Safety Navigator066-01213-1101 KSN 765 Safety NavigatorTable TI-2. Revision History Revision Number Revision Date0 6 Dec 2012Draft as of 10/15/2012
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DraftPage RR-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell. RECORD OF REVISIONSFor each revision, write the revision number, revision date, date put in the manual, and your initials in theapplicable column.NOTE: Refer to the Revision History in the TRANSMITTAL INFORMATION section for revision data.Revision Number Revision Date Date Put In Manual By Revision Number Revision Date Date Put In Manual By Draft as of 10/15/2012
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DraftPage RTR-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.RECORD OF TEMPORARY REVISIONSInstructions on each page of a temporary revision tell you where to put the pages in your manual. Removetemporary revision pages only when discard instructions are given. For each temporary revision, put theapplicable data in the record columns on this page.Definition of Status column: TR may be active, cancelled, or incorporated. If TR is incorporated list the revisionnumber. For example enter: INC Rev 7. If TR is replaced by another TR then put “Cancelled”. For example:Cancelled by TR NN-NN. “Active” is entered by the holder of manual.TemporaryRevision Number Status PageNumber IssueDate Date Put in Manual ByDateRemovedFrom Manual ByDraft as of 10/15/2012
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DraftPage SBL-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.SERVICE BULLETIN LISTService Bulletin/Revision Number Title Modification Date Put inManualDraft as of 10/15/2012
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DraftPage LEP-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Subheading and Page Date Subheading and Page DateLIST OF EFFECTIVE PAGES* indicates a changed or added page.F indicates a foldout page.TitleT-1 6 Dec 2012T-2 6 Dec 2012T-3 6 Dec 2012T-4 6 Dec 2012T-4 6 Dec 2012Transmittal InformationTI-1 6 Dec 2012TI-2 6 Dec 2012Record of RevisionsRR-1 6 Dec 2012RR-2 6 Dec 2012Record of Temporary RevisionsRTR-1 6 Dec 2012RTR-2 6 Dec 2012Service Bulletin ListSBL-1 6 Dec 2012SBL-2 6 Dec 2012List of Effective PagesLEP-1 6 Dec 2012LEP-2 6 Dec 2012LEP-3 6 Dec 2012LEP-4 6 Dec 2012Table of ContentsTC-1 6 Dec 2012TC-2 6 Dec 2012TC-3 6 Dec 2012TC-4 6 Dec 2012TC-5 6 Dec 2012TC-6 6 Dec 2012TC-7 6 Dec 2012TC-8 6 Dec 2012TC-9 6 Dec 2012TC-10 6 Dec 2012IntroductionINTRO-1 6 Dec 2012INTRO-2 6 Dec 2012INTRO-3 6 Dec 2012INTRO-4 6 Dec 2012INTRO-5 6 Dec 2012INTRO-6 6 Dec 2012INTRO-7 6 Dec 2012INTRO-8 6 Dec 2012Section IGeneral Information1-1 6 Dec 20121-2 6 Dec 20121-3 6 Dec 20121-4 6 Dec 20121-5 6 Dec 20121-6 6 Dec 2012Section IIInstallation2-1 6 Dec 20122-2 6 Dec 20122-3 6 Dec 20122-4 6 Dec 20122-5 6 Dec 20122-6 6 Dec 20122-7 6 Dec 20122-8 6 Dec 20122-9 6 Dec 20122-10 6 Dec 20122-11 6 Dec 20122-12 6 Dec 2012F 2-13 6 Dec 2012F 2-14 6 Dec 2012F 2-15 6 Dec 2012F 2-16 6 Dec 2012F 2-17 6 Dec 2012F 2-18 6 Dec 2012F 2-19 6 Dec 2012F 2-20 6 Dec 20122-21 6 Dec 20122-22 6 Dec 20122-23 6 Dec 20122-24 6 Dec 20122-25 6 Dec 20122-26 6 Dec 20122-27 6 Dec 20122-28 6 Dec 20122-29 6 Dec 20122-30 6 Dec 20122-31 6 Dec 20122-32 6 Dec 20122-33 6 Dec 20122-34 6 Dec 2012F 2-35 6 Dec 2012Draft as of 10/15/2012
DraftPage LEP-26 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Subheading and Page Date Subheading and Page Date* indicates a changed or added page.F indicates a foldout page.F 2-36 6 Dec 2012F 2-37 6 Dec 2012F 2-38 6 Dec 2012F 2-39 6 Dec 2012F 2-40 6 Dec 2012F 2-41 6 Dec 2012F 2-42 6 Dec 2012F 2-43 6 Dec 2012F 2-44 6 Dec 20122-45 6 Dec 20122-46 6 Dec 2012F 2-47 6 Dec 2012F 2-48 6 Dec 20122-49 6 Dec 20122-50 6 Dec 2012Section IIISystem Interconnects3-1 6 Dec 20123-2 6 Dec 20123-3 6 Dec 20123-4 6 Dec 2012F 3-5 6 Dec 2012F 3-6 6 Dec 20123-7 6 Dec 20123-8 6 Dec 2012F 3-9 6 Dec 2012F 3-10 6 Dec 20123-11 6 Dec 20123-12 6 Dec 2012F 3-13 6 Dec 2012F 3-14 6 Dec 2012F 3-15 6 Dec 2012F 3-16 6 Dec 20123-17 6 Dec 20123-18 6 Dec 20123-19 6 Dec 20123-20 6 Dec 20123-21 6 Dec 20123-22 6 Dec 2012F 3-23 6 Dec 2012F 3-24 6 Dec 2012F 3-25 6 Dec 2012F 3-26 6 Dec 20123-27 6 Dec 20123-28 6 Dec 20123-29 6 Dec 20123-30 6 Dec 2012F 3-31 6 Dec 2012F 3-32 6 Dec 20123-33 6 Dec 20123-34 6 Dec 20123-35 6 Dec 20123-36 6 Dec 2012F 3-37 6 Dec 2012F 3-38 6 Dec 2012F 3-39 6 Dec 2012F 3-40 6 Dec 2012F 3-41 6 Dec 2012F 3-42 6 Dec 20123-43 6 Dec 20123-44 6 Dec 20123-45 6 Dec 20123-46 6 Dec 20123-47 6 Dec 20123-48 6 Dec 20123-49 6 Dec 20123-50 6 Dec 2012F 3-51 6 Dec 2012F 3-52 6 Dec 2012F 3-53 6 Dec 2012F 3-54 6 Dec 2012F 3-55 6 Dec 2012F 3-56 6 Dec 2012F 3-57 6 Dec 2012F 3-58 6 Dec 20123-59 6 Dec 20123-60 6 Dec 20123-61 6 Dec 20123-62 6 Dec 20123-63 6 Dec 20123-64 6 Dec 2012F 3-65 6 Dec 2012F 3-66 6 Dec 2012F 3-67 6 Dec 2012F 3-68 6 Dec 2012F 3-69 6 Dec 2012F 3-70 6 Dec 2012F 3-71 6 Dec 2012F 3-72 6 Dec 20123-73 6 Dec 20123-74 6 Dec 2012F 3-75 6 Dec 2012F 3-76 6 Dec 2012F 3-77 6 Dec 2012F 3-78 6 Dec 2012Draft as of 10/15/2012
DraftPage LEP-36 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Subheading and Page Date Subheading and Page Date* indicates a changed or added page.F indicates a foldout page.F 3-79 6 Dec 2012F 3-80 6 Dec 20123-81 6 Dec 20123-82 6 Dec 20123-83 6 Dec 20123-84 6 Dec 20123-85 6 Dec 20123-86 6 Dec 20123-87 6 Dec 20123-88 6 Dec 2012F 3-89 6 Dec 2012F 3-90 6 Dec 2012F 3-91 6 Dec 2012F 3-92 6 Dec 2012F 3-93 6 Dec 2012F 3-94 6 Dec 2012F 3-95 6 Dec 2012F 3-96 6 Dec 2012F 3-97 6 Dec 2012F 3-98 6 Dec 2012F 3-99 6 Dec 2012F 3-100 6 Dec 20123-101 6 Dec 20123-102 6 Dec 2012F 3-103 6 Dec 2012F 3-104 6 Dec 20123-105 6 Dec 20123-106 6 Dec 2012F 3-107 6 Dec 2012F 3-108 6 Dec 20123-109 6 Dec 20123-110 6 Dec 2012F 3-111 6 Dec 2012F 3-112 6 Dec 2012F 3-113 6 Dec 2012F 3-114 6 Dec 20123-115 6 Dec 20123-116 6 Dec 20123-117 6 Dec 20123-118 6 Dec 2012F 3-119 6 Dec 2012F 3-120 6 Dec 2012F 3-121 6 Dec 2012F 3-122 6 Dec 20123-123 6 Dec 20123-124 6 Dec 2012F 3-125 6 Dec 2012F 3-126 6 Dec 2012F 3-127 6 Dec 2012F 3-128 6 Dec 20123-129 6 Dec 20123-130 6 Dec 2012F 3-131 6 Dec 2012F 3-132 6 Dec 20123-133 6 Dec 20123-134 6 Dec 20123-135 6 Dec 20123-136 6 Dec 2012F 3-137 6 Dec 2012F 3-138 6 Dec 20123-139 6 Dec 20123-140 6 Dec 2012F 3-141 6 Dec 2012F 3-142 6 Dec 20123-143 6 Dec 20123-144 6 Dec 20123-145 6 Dec 20123-146 6 Dec 2012F 3-147 6 Dec 2012F 3-148 6 Dec 2012F 3-149 6 Dec 2012F 3-150 6 Dec 2012F 3-151 6 Dec 2012F 3-152 6 Dec 2012F 3-153 6 Dec 2012F 3-154 6 Dec 20123-155 6 Dec 20123-156 6 Dec 2012Section IVTBD4-1 6 Dec 20124-2 6 Dec 2012Draft as of 10/15/2012
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DraftPage TC-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.TABLE OF CONTENTSTitle PageINTRODUCTION1. How to Use This Manual .......................................................................................................INTRO-1A. General ........................................................................................................................ INTRO-1B. Observance of Manual Instructions ............................................................................. INTRO-1C. Symbols ....................................................................................................................... INTRO-1D. Units of Measure ......................................................................................................... INTRO-2E. Standard Practices Manual ......................................................................................... INTRO-2F. Electrostatic Discharge ................................................................................................ INTRO-22. Customer Support .................................................................................................................INTRO-2A. Honeywell Aerospace Online Technical Publications Website ................................... INTRO-2B. Global Customer Care Center ..................................................................................... INTRO-23. References ........................................................................................................................... INTRO-3A. Honeywell/Vendor Publications ................................................................................... INTRO-3B. Other Publications ....................................................................................................... INTRO-34. Acronyms and Abbreviations ............................................................................................... INTRO-3A. General ........................................................................................................................ INTRO-35. Process Verification .............................................................................................................. INTRO-7A. Verification Data .......................................................................................................... INTRO-76. Software History ................................................................................................................... INTRO-7A. Software Data .............................................................................................................. INTRO-77. History of Changes ............................................................................................................... INTRO-7A. Modification/Configuration History ............................................................................... INTRO-7B. Change History for Parts List ...................................................................................... INTRO-7SECTION I - GENERAL INFORMATION1.1 Introduction .................................................................................................................................... 1-11.2 Applicability of the Installation Manual ........................................................................................... 1-11.3 Description of the Equipment ......................................................................................................... 1-11.3.1 KSN 7xx Safety Navigator ..................................................................................................1-11.3.2 GPS Antenna ..................................................................................................................... 1-21.3.3 KCM 200 Configuration Module ......................................................................................... 1-21.4 Technical Characteristics ............................................................................................................... 1-21.5 Units Supplied ................................................................................................................................ 1-41.5.1 KSN 7xx Safety Navigator ..................................................................................................1-41.5.2 GPS Antennas ................................................................................................................... 1-41.6 License Requirements ................................................................................................................... 1-41.7 Recommendations for IFR Approval .............................................................................................. 1-4A. Aircraft Logbook Entry .......................................................................................................... 1-4B. Aircraft Installation Requirements ........................................................................................ 1-4C. Approved Airplane Flight Manual Supplement ..................................................................... 1-5D. Pilot’s Guide ......................................................................................................................... 1-5Draft as of 10/15/2012
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Do not copy without express permission of Honeywell.TABLE OF CONTENTS (CONT)Title PageSECTION II - INSTALLATION2.1 Overview ........................................................................................................................................ 2-12.2 Unpacking and Inspecting Equipment ............................................................................................ 2-12.3 KSN 7xx Installation ....................................................................................................................... 2-12.3.1 General .............................................................................................................................. 2-12.3.2 Minimum System Configuration ......................................................................................... 2-22.3.3 Installation Materials .......................................................................................................... 2-22.3.4 KSN 7xx Installation Considerations .................................................................................. 2-72.3.5 KSN 7xx Cooling Requirements ...................................................................................... 2-112.3.6 KSN Pinouts ..................................................................................................................... 2-212.3.7 KSN Wiring and Cable Harness Fabrication .................................................................... 2-322.3.8 KSN Power Distribution ................................................................................................... 2-452.3.9 Placards and Labels ........................................................................................................ 2-452.3.10 Weight and Balance ......................................................................................................... 2-452.4 Antenna Installation ..................................................................................................................... 2-462.4.1 GPS/WAAS Antenna Location Considerations ................................................................ 2-462.4.2 COM and NAV Antenna Installation Considerations ........................................................ 2-492.5 Optional Accessory Installation .................................................................................................... 2-502.5.1 External Annunciators ...................................................................................................... 2-502.5.2 External Switches ............................................................................................................ 2-502.6 Magnetic Compass Recalibration ................................................................................................ 2-50SECTION III - SYSTEM INTERCONNECT3.1 Introduction .................................................................................................................................... 3-13.2 Standard Interface Definitions ........................................................................................................ 3-13.2.1 Discrete Input ..................................................................................................................... 3-13.2.2 Discrete Output .................................................................................................................. 3-13.2.3 EIA Standard Serial Interfaces ........................................................................................... 3-23.2.4 ARINC 429 Standard Serial Interfaces .............................................................................. 3-23.2.5 ARINC 453 Interface .......................................................................................................... 3-23.3 Power System Interface ................................................................................................................. 3-33.3.1 General .............................................................................................................................. 3-33.3.2 Electrical Characteristics .................................................................................................... 3-33.3.3 Panel Lighting Inputs ......................................................................................................... 3-43.3.4 Interconnect Diagram ......................................................................................................... 3-43.4 Position Interface ........................................................................................................................... 3-73.4.1 Applicable Part Numbers ...................................................................................................3-73.4.2 Function ............................................................................................................................. 3-73.4.3 Requirements and Limitations ........................................................................................... 3-73.4.4 Electrical Characteristics .................................................................................................... 3-73.4.5 Interconnect Diagram ......................................................................................................... 3-73.5 WX RDR Interface ....................................................................................................................... 3-113.5.1 Applicable Part Numbers ................................................................................................. 3-11Draft as of 10/15/2012
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Do not copy without express permission of Honeywell.TABLE OF CONTENTS (CONT)Title Page3.5.2 Function ........................................................................................................................... 3-113.5.3 Requirements and Limitations .......................................................................................... 3-113.5.4 Electrical Characteristics .................................................................................................. 3-113.5.5 Interconnect Diagram ....................................................................................................... 3-113.6 EGPWS Interface ......................................................................................................................... 3-173.6.1 Applicable Part Numbers ................................................................................................. 3-173.6.2 Function ........................................................................................................................... 3-183.6.3 Requirements and Limitations .......................................................................................... 3-183.6.4 Electrical Characteristics .................................................................................................. 3-183.6.5 Interconnect Diagram ....................................................................................................... 3-213.7 Traffic Interface ............................................................................................................................ 3-273.7.1 Applicable Part Numbers ................................................................................................. 3-273.7.2 Function ........................................................................................................................... 3-273.7.3 Requirements and Limitations .......................................................................................... 3-273.7.4 Electrical Characteristics .................................................................................................. 3-283.7.5 Interconnect Diagram ....................................................................................................... 3-293.8 Heading/AHRS Interface .............................................................................................................. 3-333.8.1 Applicable Part Numbers ................................................................................................. 3-333.8.2 Function ........................................................................................................................... 3-333.8.3 Requirements and Limitations .......................................................................................... 3-343.8.4 Electrical Characteristics .................................................................................................. 3-343.8.5 Interconnect Diagram ....................................................................................................... 3-353.9 Altitude/Airdata/Fuel Interface ...................................................................................................... 3-433.9.1 Applicable Part Numbers ................................................................................................. 3-433.9.2 Functions .......................................................................................................................... 3-433.9.3 Requirements and Limitations .......................................................................................... 3-453.9.4 Electrical Characteristics .................................................................................................. 3-463.9.5 Interconnect Diagrams ..................................................................................................... 3-49 3.10 Flight Control Interface ................................................................................................................. 3-593.10.1 Applicable Part Numbers .................................................................................................3-593.10.2 Function ........................................................................................................................... 3-593.10.3 Requirements and Limitations .......................................................................................... 3-593.10.4 Electrical Characteristics .................................................................................................. 3-613.10.5 Interconnect Diagram ....................................................................................................... 3-643.11 DME Interface .............................................................................................................................. 3-733.11.1 Applicable Part Numbers .................................................................................................3-733.11.2 Function ........................................................................................................................... 3-733.11.3 Requirements and Limitations .......................................................................................... 3-733.11.4 Electrical Characteristics .................................................................................................. 3-733.11.5 Interconnect Diagram ....................................................................................................... 3-743.12 NAV Indicator Interface ................................................................................................................ 3-813.12.1 Applicable Part Numbers .................................................................................................3-813.12.2 Function ........................................................................................................................... 3-813.12.3 Requirements and Limitations .......................................................................................... 3-81Draft as of 10/15/2012
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Do not copy without express permission of Honeywell.TABLE OF CONTENTS (CONT)Title Page3.12.4 Electrical Characteristics .................................................................................................. 3-823.12.5 Interconnect Diagram ....................................................................................................... 3-853.13 RMI/OBI Interface ...................................................................................................................... 3-1013.13.1 Applicable Part Numbers ............................................................................................... 3-1013.13.2 Function ......................................................................................................................... 3-1013.13.3 Requirements and Limitations ....................................................................................... 3-1013.13.4 Electrical Characteristics ................................................................................................ 3-1013.13.5 Interconnect Diagram .....................................................................................................3-1013.14 Dual System Interface (Cross-Fill) ............................................................................................. 3-1053.14.1 Applicable Part Numbers ............................................................................................... 3-1053.14.2 Function ......................................................................................................................... 3-1053.14.3 Requirements and Limitations ....................................................................................... 3-1053.14.4 Electrical Characteristics ................................................................................................ 3-1053.14.5 Interconnect Diagram .....................................................................................................3-1053.15 Audio Interface ........................................................................................................................... 3-1093.15.1 Applicable Part Numbers ............................................................................................... 3-1093.15.2 Function ......................................................................................................................... 3-1093.15.3 Requirements and Limitations ....................................................................................... 3-1093.15.4 Electrical Characteristics ................................................................................................ 3-1093.15.5 Interconnect Diagram .....................................................................................................3-1093.16 Annunciations - Suspend/Dead Reckoning/NAV Interface ......................................................... 3-1153.16.1 Applicable Part Numbers ............................................................................................... 3-1153.16.2 Function ......................................................................................................................... 3-1153.16.3 Requirements and Limitations ....................................................................................... 3-1163.16.4 Electrical Characteristics ................................................................................................ 3-1183.16.5 Interconnect Diagram .....................................................................................................3-1183.17 Miscellaneous Interface ............................................................................................................. 3-1233.17.1 Applicable Part Numbers ............................................................................................... 3-1233.17.2 Function ......................................................................................................................... 3-1233.17.3 Requirements and Limitations ....................................................................................... 3-1233.17.4 Electrical Characteristics ................................................................................................ 3-1243.17.5 Interconnect Diagram .....................................................................................................3-1243.18 XM Receiver Interface ............................................................................................................... 3-1293.18.1 Applicable Part Numbers ............................................................................................... 3-1293.18.2 Function ......................................................................................................................... 3-1293.18.3 Requirements and Limitations ....................................................................................... 3-1293.18.4 Electrical Characteristics ................................................................................................ 3-1293.18.5 Interconnect Diagram .....................................................................................................3-1293.19 Maintenance Interface ............................................................................................................... 3-1333.19.1 Applicable Part Numbers ............................................................................................... 3-1333.19.2 Function ......................................................................................................................... 3-1333.19.3 Requirements and Limitations ....................................................................................... 3-1333.19.4 Electrical Characteristics ................................................................................................ 3-1343.19.5 Interconnect Diagram .....................................................................................................3-135Draft as of 10/15/2012
DraftPage TC-56 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.TABLE OF CONTENTS (CONT)Title Page3.20 Stormscope Interface (WX-500) ................................................................................................. 3-1393.20.1 Applicable Part Numbers ............................................................................................... 3-1393.20.2 Function ......................................................................................................................... 3-1393.20.3 Requirements and Limitations ........................................................................................ 3-1393.20.4 Electrical Characteristics ................................................................................................ 3-1393.20.5 Interconnect Diagram .....................................................................................................3-1393.21 NAV/COM Interface (KSN 7x0 Only) .......................................................................................... 3-1433.21.1 Applicable Part Numbers ............................................................................................... 3-1433.21.2 Function ......................................................................................................................... 3-1433.21.3 Requirements and Limitations ........................................................................................ 3-1433.21.4 Electrical Characteristics ................................................................................................ 3-1443.21.5 Interconnect Diagram .....................................................................................................3-1463.22 Data Bus Information ................................................................................................................. 3-155SECTION IV - TBDDraft as of 10/15/2012
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DraftPage TC-76 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.LIST OF FIGURESFigure PageINTRO-1 Symbols ............................................................................................................................. INTRO-22-1 Field of View - CDI Source Selection .......................................................................................... 2-92-2 Field of View - GPS Annunciation ............................................................................................. 2-102-3 Field of View - TAWS ................................................................................................................ 2-112-4 KSN 7xx Safety Navigator Outline Drawing .............................................................................. 2-132-5 KSN 7xx Back Panel ................................................................................................................. 2-212-6 Coaxial Right Angle Connector Instruction Sheet ..................................................................... 2-352-7 TNC Antenna Coax with Straight Connector ............................................................................. 2-372-8 Quadraxial Cable Preparation ................................................................................................... 2-393-1 Power System Interface Interconnect Diagram .......................................................................... 3-53-2 Position Interface Interconnect Diagram .....................................................................................3-93-3 WX RDR Interface Interconnect Diagram ................................................................................. 3-153-4 EGPWS Interface - Internal (Growth) Interconnect Diagram .................................................... 3-233-5 EGPWS Interface - External Interconnect Diagram .................................................................. 3-253-6 Traffic Interface Interconnect Diagram ......................................................................................3-313-7 Heading Interface - XYZ Interconnect Diagram ....................................................................... 3-373-8 AHRS Interface Interconnect Diagram ..................................................................................... 3-413-9 Altitude Interface Interconnect Diagram ................................................................................... 3-513-10 Airdata/OAT Interface Interconnect Diagram ........................................................................... 3-533-11 Fuel Flow/Airdata Interface Interconnect Diagram ................................................................... 3-553-12 Flight Control Interface - Roll Composite Steering Interconnect Diagram ................................ 3-653-13 Flight Control Interface - Deviation/Course Datum Interconnect Diagram ................................ 3-673-14 Flight Control Interface - DC Interconnect Diagram (Sheet 1 of 1) ........................................... 3-693-15 Flight Control Interface - ARINC 429 Interconnect Diagram .................................................... 3-713-16 DME Interface - Remote Interconnect Diagram ....................................................................... 3-753-17 DME Interface - Panel Mount Interconnect Diagram ............................................................... 3-773-18 DME Interface - ARINC 429 Interconnect Diagram ................................................................. 3-793-19 NAV Indicator Interface - OBS 1 Interconnect Diagram ........................................................... 3-893-20 NAV Indicator Interface - OBS 2 Interconnect Diagram ........................................................... 3-913-21 NAV Indicator Interface - Deviation and Flag Interconnect Diagram ....................................... 3-933-22 NAV Indicator Interface - ARINC 429 Interconnect Diagram .................................................... 3-95Draft as of 10/15/2012
DraftPage TC-86 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.LIST OF FIGURES (CONT)Figure Page3-23 NAV Indicator Interface - Composite Interconnect Diagram (KSN 7x0 Models Only) ............... 3-993-24 RMI/OBI Interface Interconnect Diagram ............................................................................... 3-1033-25 Dual System Interface Interconnect Diagram ......................................................................... 3-1073-26 Audio Interface 1 Interconnect Diagram ................................................................................ 3-1113-27 Audio Interface 2 Interconnect Diagram ................................................................................ 3-1133-28 Annunciations - Suspend/Dead Reckoning Interconnect Diagram ........................................ 3-1193-29 Annunciations - NAV Interface Interconnect Diagram ............................................................. 3-1213-30 Miscellaneous Interface 1 Interconnect Diagram ................................................................... 3-1253-31 Miscellaneous Interface 2 Interconnect Diagram ................................................................... 3-1273-32 XM Receiver Interface Interconnect Diagram ........................................................................ 3-1313-33 Maintenance Interface Interconnect Diagram ........................................................................ 3-1373-34 Stormscope Interface (WX-500) Interconnect Diagram .......................................................... 3-1413-35 COM Interface Interconnect Diagram ..................................................................................... 3-1473-36 NAV Interface Interconnect Diagram ..................................................................................... 3-1493-37 NAV Interface - Remote DME Channeling Interconnect Diagram ......................................... 3-1513-38 NAV Interface - Panel Mount DME Channeling Interconnect Diagram .................................. 3-153Draft as of 10/15/2012
DraftPage TC-96 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.LIST OF TABLESTable PageINTRO-1 Verification Data .............................................................................................................. INTRO-71-1 Installation Manual Applicability ............................................................................................... 1-11-2 KSN 765 Safety Navigator Leading Particulars ....................................................................... 1-21-3 KSN 770 Safety Navigator Leading Particulars ....................................................................... 1-32-1 KSN 765 Safety Navigator Installation Kit, PN PL050-03727-0000 ......................................... 2-22-2 KSN 770 Safety Navigator Installation Kit, PN PL050-03727-0001 ......................................... 2-32-3 Accessories Required But Not Supplied .................................................................................. 2-42-4 Accessories Required But Not Supplied .................................................................................. 2-52-5 Operational Software ............................................................................................................... 2-62-6 Americas Database .................................................................................................................. 2-62-7 Atlantic Database ..................................................................................................................... 2-62-8 Pacific Database ...................................................................................................................... 2-72-9 Special Tools Required ............................................................................................................ 2-72-10 Connector List ........................................................................................................................ 2-212-11 Signals Assigned to the I/O 1 Connector (J1) ........................................................................ 2-222-12 Signals Assigned to the I/O 2 Connector (J2) ........................................................................ 2-252-13 Signals Assigned to the Power Supply Interface Connector (J3) .......................................... 2-282-14 Signals Assigned to the Main Processor Board Interface Connector (J4) ............................. 2-282-15 Signals Assigned to the GPS Antenna Connector (J5) .......................................................... 2-302-16 Signals Assigned to the Video Connector (J6) ...................................................................... 2-302-17 Signals Assigned to the Rear Panel USB Connector (J8) ..................................................... 2-302-18 Signals Assigned to XM WX Datalink Antenna Connector (J10) ........................................... 2-312-19 Signals Assigned to the VHF Transceiver Antenna Connector (J11) (KSN 7x0 Only) .......... 2-312-20 Signals Assigned to the Navigation Radio (VOR/LOC) AntennaConnector (J12) (KSN 7x0 Only) ........................................................................................... 2-312-21 Signals Assigned to the Navigation Radio (GS) AntennaConnector (J13) (KSN 7x0 Only) ........................................................................................... 2-312-22 Signals Assigned to the WX RDR/EGPWS Connector (J14) ................................................. 2-312-23 Component Weights .............................................................................................................. 2-452-24 GPS Antenna Cable Information ............................................................................................ 2-472-25 Cable Vendor Contact Information ......................................................................................... 2-47Draft as of 10/15/2012
DraftPage TC-106 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.LIST OF TABLES (CONT)Table Page3-1 Discrete Input States ............................................................................................................... 3-13-2 High Current Discrete Output States ....................................................................................... 3-13-3 Superflag Output States .......................................................................................................... 3-23-4 TBD .......................................................................................................................................... 3-33-5 TBD .......................................................................................................................................... 3-43-6 WX RDR Requirements and Limitations ................................................................................ 3-133-7 ARINC 429 Label 017 Control Function Availability in EGPWS Units ................................... 3-203-8 AHRS Labels ......................................................................................................................... 3-343-9 ARINC 429 Serial Airdata Labels .......................................................................................... 3-473-10 ARINC 429 Serial Airdata Labels .......................................................................................... 3-483-11 ARINC 429 Label ................................................................................................................... 3-743-12 TBD......................................................................................................................................... 3-823-13 ARINC 429 Labels ................................................................................................................. 3-853-14 NAV Annunciators by Installation Type ............................................................................... 3-117Draft as of 10/15/2012
DraftPage INTRO-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.INTRODUCTION1. How to Use This ManualA. General(1) This publication gives maintenance instructions for the equipment shown on the Title page.(2) Standard maintenance procedures that technicians must know are not given in this manual.(3) This publication is written in agreement with the ATA Specification.(4) Warnings, cautions, and notes in this manual give the data that follows:• A WARNING gives a condition or tells personnel what part of an operation or maintenance procedure, which if not obeyed, can cause injury or death• A CAUTION gives a condition or tells personnel what part of an operation or maintenance procedure, which if not obeyed, can cause damage to the equipment• A NOTE gives data, not commands. The NOTE helps personnel when they do the related instruction.(5) Warnings and cautions go before the applicable paragraph or step. Notes follow the applicable paragraph or step.B. Observance of Manual Instructions(1) Make sure that you carefully obey all safety, quality, operation, and shop procedures for the unit.(2) All personnel who operate equipment and do maintenance specified in this manual must know and obey the safety precautions.C. Symbols(1) The symbols and special characters are in agreement with IEEE Publication 260 and IEC Publication 27. Special characters in text are spelled out.(2) The signal mnemonics, unit control designators, and test designators are shown in capital letters.(3) The signal names followed by an “*” show an active low signal.(4) The symbols in Figure INTRO-1 show ESDS and moisture sensitive devices.Draft as of 10/15/2012
DraftPage INTRO-26 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Figure INTRO-1. Symbols (Sheet 1 of 1)D. Units of Measure(1) Measurements, weights, temperatures, dimensions, and other values are expressed in the USMS followed by the appropriate SI metric units in parentheses. Some standard tools or parts such as drills, taps, bolts, nuts, etc. do not have an equivalent.E. Standard Practices Manual(1) Standard cleaning, check, repair, and assembly procedures applicable to multiple models can be found in a standard practices manual. Refer to Paragraph 3, References.F. Electrostatic Discharge(1) Touch the items susceptible to electrostatic discharge in accordance with MIL-HDBK-263. Refer to MIL-STD-1686 for definition of the standards and conditions.2. Customer SupportA. Honeywell Aerospace Online Technical Publications Website(1) Go to the Honeywell Online Technical Publications Website at (www.myaerospace.com).• To download or see publications online• To order a publication• To tell Honeywell of a possible data error in a publication.B. Global Customer Care Center(1) If you do not have access to the Honeywell Technical Publications Website, or if you need to speak to personnel about non-Technical Publication matters, the Honeywell Aerospace Global Customer Care Center gives 24/7 customer service to Air Transport & Regional, Business & General Aviation, and Defense & Space customers around the globe.• Telephone: 800-601-3099 (Toll Free U.S.A./Canada)• Telephone: 602-365-3099 (International)• Telephone: 00-800-601-30999 (EMEA Toll Free)• Telephone: 420-234-625-500 (EMEA Direct).Draft as of 10/15/2012
DraftPage INTRO-36 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3. ReferencesA. Honeywell/Vendor Publications(1) Related Honeywell publications in this manual are shown in the list that follows:• ATA No. 34-70-07 (Pub. No. 006-15716-0000), CMM, KSN 765/770 Safety Navigator• Pub. No. A09-1100-004, Standard Repair Procedures for Honeywell Avionics Equipment Instruction Manual.B. Other Publications(1) These publications are standard references. Check for latest version of publication.• The United States GPO Style Manual 2000 (available at http://www.gpoaccess.gov/stylemanual/browse.html)• IEEE Std 260, Standard Letter Symbols for Units of Measurement (available from the American National Standards Institute, New York, NY)• ASME Y14.38, Abbreviations for Use on Drawings and in Text (available from the American National Standards Institute, New York, NY)• ANSI/IEEE Std 91, Graphic Symbols for Logic Functions (available from the American National Standards Institute, New York, NY)• H4/H8 CAGE Codes (available at http://www.logisticsinformationservice.dla.mil)• IEEE 315/ANSI Y32.2, Graphic Symbols for Electrical and Electronics Diagrams (available from the American National Standards Institute, New York, NY)• MIL-HDBK-263, Electrostatic Discharge Control Handbook for Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric) (available from any military standards database)• MIL-STD-1686, Electrostatic Discharge Control Program for Protection of Electrical and Electronic Parts, Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric) (available from any military standards database).4. Acronyms and AbbreviationsA. General(1) The abbreviations are used in agreement with ASME Y14.38.(2) Acronyms and non-standard abbreviations used in this publication are as follows:List of Acronyms and Abbreviations Term Full TermAC alternating currentAHRS attitude heading reference systemDraft as of 10/15/2012
DraftPage INTRO-46 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.AMP ampereANSI American National Standards InstituteARTCC air route traffic control centerARINC Aeronautical Radio, IncorporatedASME American Society of Mechanical EngineersATA Air Transport AssociationAWG American wire gaugeC celsiusCAGE commercial and government entityCDI course deviation indicatorCOM communicationcm centimeterCMM component maintenance manualdB decibelDC direct currentDME distance measuring equipmentDPL detailed parts listEB engineering bulletinEGPWS enhanced ground proximity warning systemEIA Electronic Industries AssociationELT emergency locator transmitterEMEA Europe, the Middle East, and AfricaESDS electrostatic discharge sensitiveEZ electrically zeroedF fahrenheitFMS flight manual supplementFSS flight service stationGND groundGPO Government Printing OfficeGPS ground positioning satelliteHSI horizontal situation indicatorHz HertzList of Acronyms and Abbreviations (Cont)Term Full TermDraft as of 10/15/2012
DraftPage INTRO-56 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.ICAO International Civil Aviation OrganizationIEC International Electrotechnical CommissionIEEE Institute of Electrical and Electronics EngineersIFIS electronic flight information systemIFR instrument flight ruleI/O input/outputINS inertial navigation systemIRU inertial reference unitkg kilogramKRC King Radio CompanyLCD liquid crystal displayLPV localizer performance with vertical guidanceLOC localizermA milliampereMAX maximumMFD multifunction displayMOD modificationmm millimeterMMDS multimode digital sensormW milliwattN/A not applicableNAV navigationNAVAID navigational aidNBD non-directional beaconnm nautical mileNo. numberOBS omni-bearing selectorORZ omni-range zeroedPN part numberPub. publicationRAIM receiver autonomous integrated monitorRDR radarList of Acronyms and Abbreviations (Cont)Term Full TermDraft as of 10/15/2012
DraftPage INTRO-66 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.REF referenceRF radio frequencyRX receiveSB service bulletinSBAS satellite based augmentation systemSID standard instrument departureSIM system installation manualSSM sign status matrixSTAR standard terminal arrival routeSTC supplemental type certificateSUA special-use airspaceTAS traffic awareness systemTAWS terrain awareness and warning systemTCAS traffic collision avoidance systemTHD TBD BY ENGINEERINGTIS traffic information serviceTR temporary revisionTSO Technical Standard OrderTX transmitVHF very high frequencyVOR very high frequency omnidirectional rangeUSB universal serial busUSMS United States Measurement SystemVAC volt, alternating currentVDC volt, direct currentVLOC very high frequency omni-range localizerVNAV vertical navigationVOR very high frequency omni-rangeWAAS wide area augmentation systemWOW weight on wheelsVrms volt, root-mean-squareWX weatherList of Acronyms and Abbreviations (Cont)Term Full TermDraft as of 10/15/2012
DraftPage INTRO-76 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.5. Process VerificationA. Verification Data(1) Honeywell does a verification of these technical instructions by performance or by simulation of the necessary procedures. Performance shows that the procedures were checked by the use of the manual. Simulation shows that the applicable personnel looked at the procedure in the manual and that the procedure is technically correct. The dates of verification for this manual are given in Table INTRO-1.6. Software HistoryA. Software Data(1) Not applicable.7. History of ChangesA. Modification/Configuration History(1) Not applicable.B. Change History for Parts List(1) Not applicable.XM satellite based flight information services weather sourceTable INTRO-1. Verification DataSection Method DateTBD TBD TBDTBD TBD TBDTBD TBD TBDList of Acronyms and Abbreviations (Cont)Term Full TermDraft as of 10/15/2012
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DraftPage 1-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.SECTION I - GENERAL INFORMATION1.1 IntroductionThis manual contains information relative to the physical, mechanical, and electrical characteristics of the KSN 7xx Safety Navigator. Installation and operating procedures are also included.Operating instructions are provided in KSN 7xx Pilot’s Manual, Pub. No. 006-18324-0000. Information relative to the maintenance, alignment, and procurement of the replacement parts can be found in the ATA No. 34-70-07 (Pub. No. 006-15716-0000), CMM, KSN 765/770 Safety Navigator.1.2 Applicability of the Installation ManualThis manual is applicable only to the KSN 7xx integrated avionics systems with the part numbers as shown in Table 1-1.1.3 Description of the Equipement1.3.1 KSN 7xx Safety NavigatorThe KSN 7xx product family feature is a full featured WAAS, integrated GPS navigator capable of LPV approaches. Some of the system features include:A. A TSO, GPS based, long range airborne database driven navigation. The primary purpose of the KSN 7xx is to provide the pilot with present position information, to display guidance information with respect to a flight plan defined by the pilot, and to provide communications functions to the pilot. Flight plan information is entered by the pilot via the concentric knobs and buttons on the front panel.B. A front loading pilot updateable database using a USB 2.0 thumb drive. Databases contain worldwide information on NAVAID, intersections, low altitude airways, terrain, obstructions and minimum safe altitudes. Database also includes public use and military airports with runways at least 3000 feet (914.4 meters) in length, airport communication frequencies, runway information, air route traffic control center data, flight service station frequencies, and SUA. SID and STAR waypoints and approaches are also included. The information can be selected by airport and procedure name.Table 1-1. Installation Manual ApplicabilitySystem PN DescriptionKSN 765 300-10940-0000 Top level assembly066-01213-0101 Safety Navigator066-01213-1101 Safety Navigator with RDR/EGPWS SupportKSN 770 300-10694-0000 Top level assembly066-01204-0101 Safety Navigator NAV/COM066-01204-1101 Safety Navigator NAV/COM with RDR/EGPWS SupportDraft as of 10/15/2012765/770 - would prefer to see this throughout the manual
DraftPage 1-26 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.C. Information on the KSN 7xx is displayed on a large, easy-to-read color LCD. Pilot information is input to the unit via flexible combination of touchscreen and graphics interface combined with cursor control and by the 16 push buttons on the front panel.D. An optional NAV receiver and COM transceiver that will allow integrated navigation and communications on KSN 7xx units so equipped.The KSN 7xx can use its present position information to determine crosstrack error, distance-to-waypoint, ground speed, track angle, time-to-waypoint and bearing to waypoint.The KSN 7xx can provide navigation data to external displays and autopilots. Some of this data is output to external devices.The internal database of the KSN 7xx contains information concerning airports, VOR, NDB, SUAs, airport runways and frequency location information, and nearest FSS and ARTCC names and frequencies. Waypoints are stored in the database by their ICAO identifiers. The ICAO identifiers are (in most cases) taken directly from Jeppesen or government aeronautical charts.1.3.2 GPS AntennaThe KA 96 GPS antenna, PN 071-01620-0001 or equivalent is the designated antenna for the KSN 7xx.1.3.3 KCM 200 Configuration ModuleThe configuration module is used to store some installation specific information, which is used by the KSN 7xx. The KCM 200 configuration module used with the KSN 7xx, is supplied with the KSN 7xx and is also available under PN 071-00188-1101.1.4 Technical CharacteristicsRefer to Table 1-2 for the KSN 765 Safety Navigator leading particulars.Refer to Table 1-3 for the KSN 770 Safety Navigator leading particulars.Table 1-2. KSN 765 Safety Navigator Leading Particulars Characteristic SpecificationTSO compliance TSO C146c, TSO-C165, TSO-C113, TSO-C63c, TSO-C147, TSO-C118, TSO-C157a, TSO-C110a, TSO-C151b, ETSO-2C63cLength 11.80 inches (299.8 mm)Width 6.25 inches (158.8 mm)Height 5.40 inches (137.2 mm)Weight Refer to SECTION II - INSTALLATIONMounting Panel mountEnvironmental conditions RTCA/DO-160GTemperature 4 to 131°F (20 to +55°C)Altitude 25,000 feet (7,620 meters)Draft as of 10/15/2012
DraftPage 1-36 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Vibration Category S, curves B & M; Category R curve GElectrical:Operating voltage +11 to +33 VDCOperating current:+28 VDC 4.9 AMP MAX+14 VDC 8.6 AMP MAXSoftware RTCA/DO-178B Levels B and CHardware RTCA/DO-254 Levels B and CTable 1-3. KSN 770 Safety Navigator Leading Particulars Characteristic SpecificationTSO compliance TSO C146c, TSO-C165, TSO-C113, TSO-C63c, TSO-C147, TSO-C118, TSO-C157a, TSO-C110a, TSO-C151b, ETSO-2C63c, TSO-C169a, TSO-C128a, TSO-C34e, TSO-C36e, TSO-C40c, ETSO-2C34f, ETSO-2C36F, ETSO-2C169a, ETSO-2C40c, and ETSO-2C128Length 11.80 inches (299.8 mm)Width 6.25 inches (158.8 mm)Height 5.40 inches (137.2 mm)Weight Refer to SECTION II - INSTALLATIONMounting Panel mountEnvironmental conditions RTCA/DO-160GTemperature 4 to 131°F (20 to +55°C)Altitude 25,000 feet (7,620 meters)Vibration Category S, curves B & M; Category R curve GElectrical:Operating voltage +11 to +33 VDCOperating current:+28 VDC 4.9 AMP MAX Steady State, 12.4 AMP TX+14 VDC 8.6 AMP MAX Steady State, 15.6 AMP TXSoftware RTCA/DO-178B Levels B and CTable 1-2. KSN 765 Safety Navigator Leading Particulars (Cont)Characteristic SpecificationDraft as of 10/15/2012
DraftPage 1-46 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.1.5 Units Supplied1.5.1 KSN 7xx Safety NavigatorRefer to Table 1-1 for the available configurations.1.5.2 GPS AntennasThe KA 96 GPS active antenna, PN 071-01620-0001 is the designated antenna for the KSN 770 Safety Navigator, and must be ordered separately.1.6 License RequirementsAn aircraft radio station license is no longer required for the KSN 7xx models that transmit for domestic (US) operations. For international travel, forms can be obtained from your nearest FCC field office or found online at http://transition.fcc.gov/Forms/Form605/605.html/ (See the regulatory authority for all countries in which the KSN 7xx will be operated for more information).1.7 Recommendations for IFR ApprovalThe following functions are required for IFR certification of the KSN 7xx.A. Aircraft Logbook EntryB. Aircraft Installation Requirements(1) TSO’d AntennaThe antenna must be a TSO’d KA 96 GPS antenna, PN 071-01620-0001 or equivalent.(2) NAV InstrumentationThe navigation information (D-Bar, NAV Flag, and TO-FROM) must be displayed on an instrument in the pilot’s panel within the pilot’s field of view. Electromechanical indicators are capable of displaying the variable scale factors of enroute, terminal, and approach modes. If the NAV information is displayed on an EFIS system, it must be capable of displaying variable D-Bar scaling required for GPS approaches. This may require a modification to the EFIS system. Refer to SECTION III - SYSTEM INTERCONNECT for the typical indicator usage.(3) OBS InterfaceFor approach approval, the OBS resolver must be interfaced so that selected course through the HSI/CDI indicator will be sent to the KSN 7xx for D-Bar resolution. In mechanical indicators, it will be accomplished by switching the OBS resolver lines; in EFIS installations, it will usually be through the serial busses. Some EFIS applications may require an adapter. Refer to SECTION III - SYSTEM INTERCONNECT for further information regarding OBS resolver characteristics.Hardware RTCA/DO-254 Levels B and CTable 1-3. KSN 770 Safety Navigator Leading Particulars (Cont)Characteristic SpecificationDraft as of 10/15/2012
DraftPage 1-56 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.(4) Switch/AnnunciatorsRefer to SECTION III - SYSTEM INTERCONNECT for specific information regarding switch/annunciator characteristics.(5) Altitude SourceAn altitude source is required for IFR certification. The altitude may be derived from a compatible encoding altimeter, some RS 232 air data systems, and most ARINC 429/575 air data systems. Refer to SECTION III - SYSTEM INTERCONNECT for further information regarding altitude source characteristics.C. Approved Airplane Flight Manual SupplementA flight manual supplement will need to be prepared and approved. The supplement may be prepared based on the sample. Refer to the FMS Appendix and the STC Appendix (TBD BY ENGINEERING), for further information.D. Pilot’s GuideThe KSN 770 Pilot’s Guide must be placed in the aircraft in a location that is accessible to the pilot. The Pilot’s Guide is PN 006-18324-0000.Draft as of 10/15/2012
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DraftPage 2-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.SECTION II - INSTALLATION2.1 OverviewThis section contains suggestions and factors to consider before installing the KSN 7xx Safety Navigator. Close adherence to these suggestions will assure satisfactory performance from the equipment.NOTE: The conditions and tests performed on this article are minimum performance standards. It is the responsibility of those desiring to install this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within these performance standards. The article may be installed only if further evaluation by the applicant documents an acceptable installation and is approved by the Administrator.2.2 Unpacking and Inspecting EquipmentExercise extreme caution when unpacking equipment. Perform a visual inspection of the unit for evidence of damage incurred during shipment. If a damage claim must be filed, save the shipping container and all packing materials to substantiate your claim. The claim must be filed as soon as possible. The shipping container and all packing materials must be retained in the event that storage or reshipment of the equipment is necessary.2.3 KSN 7xx Installation2.3.1 GeneralThe following paragraphs contain information pertaining to the installation of the KSN 7xx, including instructions concerning the location and mounting of the antenna.The equipment must be installed in the aircraft in a manner consistent with acceptable workmanship and engineering practices, and in accordance with the instructions set forth in this publication. To ensure the system has been properly and safely installed in the aircraft, the installer must make a thorough visual inspection and conduct an overall operational check of the system, on the ground, prior to flight.CAUTION: AFTER INSTALLATION OF THE CABLING AND BEFORE INSTALLATION OF THE EQUIPMENT, A CHECK MUST BE MADE WITH THE AIRCRAFT PRIMARY POWER SUPPLIED TO THE MOUNTING CONNECTOR TO ENSURE THAT POWER IS APPLIED ONLY TO THE PINS SPECIFIED IN THE INTERWIRING DIAGRAMS IN SECTION III.The KSN 7xx system installation will conform to standards designated by the customer, installing agency, and existing conditions as to the unit location and type of installation. However, the following suggestions must be carefully considered before installing your KSN 7xx system.Draft as of 10/15/2012
DraftPage 2-26 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.2 Minimum System Configuration2.3.3 Installation Materials2.3.3.1 Installation Kit Contents2.3.3.1.1 KSN 765 Safety NavigatorRefer to Table 2-1 for the KSN 765 Installation Kit, PN PL050-03727-0000.Table 2-1. KSN 765 Safety Navigator Installation Kit, PN PL050-03727-0000 Description Qty Bendix/King PNConnector, D-SUB, 27 mixed size crimp contacts, straight 1 53500239-2Contact, female, 10 AMP power, combo-D, 16 AWG, crimp, female 4 030-01454-0002Connector, 2-row, 50 sockets, board to cable - 0.156, crimp, straight 1 53502330-1Contact, socket, crimp, 20 AWG 42 030-01157-0011Connector, SUB-D HSG 37 contact, female sockets 1 030-01175-0000Connector, contact, board to cable, crimp, 20-24 AWG socket 24 53502674-1Connector, 25 contact subd hood 1 030-01447-0000Connector, 37 contact subd hood 1 030-01447-0001Contact, D-sub, 22 AWG, crimp, female 156 030-01466-0001Connector, high density subd, 78 contact 2 030-03296-0001Connector, 50 ohms BNC jack to push-on adaptor 1 030-03589-0001Connector, 75 ohms BNC jack to push-on adapter 1 030-03589-0002Rack chassis assembly with finish 1 047-11434-0004Nut plate, 50 pos as finish 2 073-01158-0003Nut plate, 25 pos as finishing 1 073-01159-0003Rear panel with hardware 1 073-01160-0004Nut plate, 37 pos as finish 1 073-01161-0003Spacer as finish 2 076-03228-0002Nut clip, 6-32 10 089-02353-0001Screw, pan head, #4-40 x 3/8 4 089-05903-0006Screw, pan head, #4-40 x 7/16 2 089-05903-0007Screw, pan head, #4-40 x 13/16 6 089-05903-0013Screw, flat head, #4-40 x 3/8 4 089-06008-0006Screw, flat head, #6-32 x 3/8 10 089-06012-0006Draft as of 10/15/2012
DraftPage 2-36 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.3.1.2 KSN 770 Safety NavigatorRefer to Table 2-2 for the KSN 70 Installation Kit, PN PL050-03727-0001.Cable assembly, fan 1 155-12514-0001Metal backshell kit, deep straight, DD shell size (kit consists of 1 shell, 2 cable clamps, 2 screws and 2 hex nuts) 2 53002878-1Connector, board to cable - 3 mm, crimp, 1-row, sockets-004, straight, receptacle housing, latch 1 53500258-1Connector contact, (board to cable, crimp, 20-24 AWG socket 4 53500259-1Fan gasket 2 57000118-001Shoulder screw, #4-40 6 57000119-001KCM 200 KSN 7xx configuration module 1 071-00188-0201KSN 7xx installation drawing 1 155-01812-0000Connector, sub-D HSG 25 contact, female pins 1 030-01173-0000Table 2-2. KSN 770 Safety Navigator Installation Kit, PN PL050-03727-0001 Description Qty Bendix/King PNConnector, D-sub, 27 mixed size crimp contacts, straight 1 53500239-2Contact, female, 10 AMP power, combo-D, 16 AWG, crimp, female 4 030-01454-0002Connector, 2-row, 50 sockets, board to cable - 0.156, crimp, straight 1 53502330-1Contact, socket, crimp, 20 AWG 42 030-01157-0011Connector, sub-D HSG 37 contact, female sockets 1 030-01175-0000Connector, contact, board to cable, crimp, 20-24 AWG socket 24 53502674-1Connector, 25 contact subd hood 1 030-01447-0000Connector, 37 contact subd hood 1 030-01447-0001Contact, D-sub, 22 AWG, crimp, female 156 030-01466-0001Connector, high density subd, 78 contact 2 030-03296-0001Connector, 50 ohms BNC jack to push-on adaptor 1 030-03589-0001Connector, 75 ohms BNC jack to push-on adapter 1 030-03589-0002Rack chassis assembly with finish 1 047-11434-0004Nut plate, 50 pos as finish 2 073-01158-0003Nut plate, 25 pos as finishing 1 073-01159-0003Table 2-1. KSN 765 Safety Navigator Installation Kit, PN PL050-03727-0000 (Cont)Description Qty Bendix/King PNDraft as of 10/15/2012REF
DraftPage 2-46 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.3.2 Accessories Required But Not SuppliedTable 2-3 list the available equipment (but not supplied) to assist in installation of the KSN 7xx. Other equipment may be acceptable; refer to the appropriate section in this manual for other options.Rear panel with hardware 1 073-01160-0004Nut plate, 37 pos as finish 1 073-01161-0003Spacer as finish 2 076-03228-0002Nut clip, 6-32 10 089-02353-0001Screw, pan head, #4-40 x 3/8 4 089-05903-0006Screw, pan head, #4-40 x 7/16 2 089-05903-0007Screw, pan head, #4-40 x 13/16 6 089-05903-0013Screw, flat head, #4-40 x 3/8 4 089-06008-0006Screw, flat head, #6-32 x 3/8 10 089-06012-0006Cable assembly, fan 1 155-12514-0001Metal backshell kit, deep straight, DD shell size (kit consists of 1 shell, 2 cable clamps, 2 screws and 2 hex nuts) 2 53002878-1Connector, board to cable - 3 mm, crimp, 1-row, sockets-004, straight, receptacle housing, latch 1 53500258-1Connector contact, board to cable, crimp, 20-24 AWG socket 4 53500259-1Fan gasket 2 57000118-001Shoulder screw, #4-40 6 57000119-001KCM 200 KSN 7xx configuration module 1 071-00188-0201KSN 7xx installation drawing 1 155-01812-0000Connector, sub-D HSG 25 contact, female pins 1 030-01173-0000Table 2-3. Accessories Required But Not Supplied Description Qty Source PN 1Circuit breaker (pull to open, 10 AMP main power in) 1 Klixon MS26574-10Circuit breaker (pull to open, 7.5 AMP MMDS TX power in) 1 Klixon MS26574-7.5Wire (single strand, 20, 22, 24 AWG) AR commercially available MIL-W-22759/16Wire (shielded, 22 AWG) AR commercially available MIL-C-27500Table 2-2. KSN 770 Safety Navigator Installation Kit, PN PL050-03727-0001 (Cont)Description Qty Bendix/King PNDraft as of 10/15/2012REF
DraftPage 2-56 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.3.3 Optional Accessories - Not SuppliedRefer to Table 2-4 for the accessories required but not supplied. Screw (flat head, #6-32) 26 commercially available MS24693-S30Wire (coaxial cable) AR commercially available MIL-DTL-17Nut (locknut, #6-32) 26 commercially available MS21044N06Washer (#6) 26 commercially available NAS1149FN632PAntenna (broadband communications, 50 ohms) 1 Dorne DM C70-1/AAntenna (VHF NAV, 50 ohms) 1 Comant CI-158C-2 3Antenna (GPS) 1 CAGE: 22373 KA 96Configuration module 1 CAGE: 22373 KGS 200adhesive commercially available RTV3145Alumiprep No. 33 Turco 594015Alodine No. 1001 Henkel 594417Electrical insulating compound Dow Corning DC-4Misc. screws, washers, cable ties, etc. commercially available Installer suppliedNOTE:1. Equivalent substitute can be used.2. Use to mount the tray.3. Must also order PN 0900532 for gasket and template.Table 2-4. Accessories Required But Not Supplied Description Qty Source PNAnnunciator panel 1 Mid-Continent MD41CDI 1 Various Refer to Paragraph 3.12 NAV Indicator InterfaceRemote swap switch - NAV 1Remote swap switch - COM 1Remote switch - Next FREQ 1Thumb drive 1Table 2-3. Accessories Required But Not Supplied (Cont)Description Qty Source PN 1Draft as of 10/15/2012Table 2-3 We should not be calling out specific brands and models of antennas, except in the case of Honeywell specific. Comm and Nav antennas should be generically described I don't like the term commercially available. We will be asked for Honeywell P/N's or equivalent. Table 2-4 We want to be more flexible about the callout of Annunciator Panels. There are a lot of vendors that shops will want to use. The Remote swap switches, remote switch and Thumb drives need to be better described. We should not be calling out specific brands and models of Antenna splitter, NAV. There are many that are suitable.
DraftPage 2-66 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.3.4 Software Options2.3.3.4.1 Operational Software, refer to Table 2-5.2.3.3.4.2 Aviation DatabaseThe Aviation Databases that are updated on a 28 day cycle are identified with a part number specified with the following notation:YY = Last two digits of the current yearCC – Cycle Number (01-13)2.3.3.4.2.1 Americas Database, refer to Table 2-6.2.3.3.4.2.2 Atlantic Database, refer to Table 2-7. Antenna splitter, NAV 1 Comant CI-1125Table 2-5. Operational SoftwareSoftware Description PNKSN 765 Safety Navigator 206-0476-0101KSN 770 Safety Navigator 206-00454-0101Table 2-6. Americas DatabaseDatabase Description Part NumberAmericas aviation database 723-429YY-00CCAmericas navigation database 723-432YY-00CCAmericas cartography database 723-435YY-00CCAmericas terrain database 723-43800-0000Americas database data File 723-440YY-00CCTable 2-7. Atlantic DatabaseDatabase Description Part NumberAmericas aviation database 723-430YY-00CCAmericas navigation database 723-433YY-00CCAmericas cartography database 723-436YY-00CCAmericas terrain database 723-43800-0001Americas database data File 723-441YY-00CCTable 2-4. Accessories Required But Not Supplied (Cont)Description Qty Source PNDraft as of 10/15/2012Table 2-5 Do we really want to call out Operational Software in an Install Manual. 206-xxxxx-yyyy's belong in the CMM? Table 2-6, 2-7 & 2-8 Databases Are 723 Numbers appropriate for the install manual? Aren't these Engineering drawing numbers?
DraftPage 2-76 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.3.4.2.3 Pacific Database, refer to Table 2-8.2.3.3.5 Special Tools Required, refer to Table 2-9.2.3.4 KSN 7xx Installation ConsiderationsCare must be exercised to avoid mounting components near equipment operating with high pulse current or high power outputs such as radar and satellite communications equipment. In general, the equipment must be installed in a location convenient for operation, inspection, and maintenance, and in an area free from excessive vibration, heat, and noise generating sources.2.3.4.1 KSN 7xx Mounting ConsiderationsThe KSN 7xx installation will conform to standards designated by the customer, installing agency, and existing conditions as to the unit location and type of installation. However, the following suggestions will assure more satisfactory performance from the equipment.A. Plan a location on the aircraft so that the KSN 7xx is plainly visible to the pilot, and so that the pilot has complete access to all front panel controls (refer to Paragraph 2.3.4.2 Field of View Considerations for more information).NOTE: Care must be taken in selecting the optimum location for the KSN 7xx. In some potential mounting locations, glare and reflections may cause the display to be nearly unreadable. Therefore, careful considerations of these effects must be made before choosing the final mounting location.B. Check to be sure that there is adequate depth behind the unit for connectors and cabling.Table 2-8. Pacific DatabaseDatabase Description Part NumberAmericas aviation database 723-431YY-00CCAmericas navigation database 723-432YY-00CCAmericas cartography database 723-435YY-00CCAmericas terrain database 723-43800-0002Americas database data File 723-440YY-00CCTable 2-9. Special Tools Required Number 1Description Source9507 Crimp tool (D-Sub) commercially available9502-3 Crimp tool positioner (D-Sub) commercially available4811-1-0-0 Insertion/Extraction Tool (D-Sub) commercially availableNOTE:1. Equivalent substitute can be used.Draft as of 10/15/2012same question as Table 2-6 & 2-7Table 2-9 Special Tools We need much better information about the tools and how to get them
DraftPage 2-86 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.C. Ensure there is at least 1.0 inch (25.4 mm) (minimum), unobstructed from the muffin fan.D. Be sure that the mounting location is not close to heater vents or other sources of high heat.E. Refer to Figure 2-4 for the cutout dimensions. Mark and cut the opening.F. Mount the rails on either side of the cutout. Ensure that the rails are electrically bonded (less than 10 milliohms to aircraft GND).G. Attach the cable harness to the rear connectors. The KSN 7xx must be wired according to the interconnect diagrams in Section III of this manual.H. Attach the coaxial cables to the rear antenna connectors. Refer to Figure 2-6 for the details for mounting the coaxial connectors to the coaxial cable.I. Prior to installing any equipment, make a continuity check of all wires and cables associated with the system. Then apply power and check for proper voltages at system connectors, and then remove power before completing the installation.J. Slide the unit in, and secure it.2.3.4.2 Wiring Harness ConsiderationTo allow for inspection or repair of the wiring of the connector assembly itself, sufficient lead length must be left so that when the mounting hardware for the rear connectors and antenna coaxial cable is removed the assembly may be pulled forward several inches. Also, a bend must be made in the harness (at the rear connectors) to allow water droplets that might form on the harness due to condensation, to drip off at the bend and not collect in the connection.The length of cables from the KSN 7xx connector to other system units is not generally critical because unit interfaces are designed with high impedance inputs, low impedance outputs, and low noise susceptibility characteristics. The exceptions are the wires from the KSN 7xx to the KCM 200 Configuration Module (refer to Paragraph 3.17 Miscellaneous Interface).2.3.4.3 Field of View ConsiderationsTBD BY ENGINEERING – See AC 20-138A, TSO-C146c, FAA Issue Paper clarifying “…on or near the affected display”.2.3.4.3.1 Centerline DeterminationThe centerline of the acceptable field of view is determined in the following order:(1) The centerline of the Basic T.(2) For aircraft without the Basic T configuration, use the centerline of the pilot side control yoke or stick, unless it is offset from the center position of the pilot’s seat (such as with a side stick or Beech Bonanza style throw over style yoke).(3) For aircraft without a centered yoke or control stick, an imaginary line from the center of the pilot’s seat through the instrument panel may be used.Draft as of 10/15/2012
DraftPage 2-96 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.4.3.2 CDI Source SelectionIf the KSN 7xx is mounted in the field of view as shown in Figure 2-1, then no external annunciator showing CDI source is required. If the KSN 7xx is mounted outside of this area, then an external annunciator indicating whether VLOC or GPS is selected must be mounted in close proximity to the CDI and within the field of view as shown in Figure 2-1.Figure 2-1. Field of View - CDI Source SelectionDraft as of 10/15/2012
DraftPage 2-106 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.4.3.3 GPS AnnunciationThe GPS annunciations as shown in Figure 2-2 must be in the pilot’s field of view. If the KSN 7xx is not mounted with the boarders defined in Figure 2-2, then an external annunciation must be mounted within this field of view.Figure 2-2. Field of View - GPS Annunciation2.3.4.3.4 TAWSRefer to Figure 2-3 for the TAWS.Draft as of 10/15/2012
DraftPage 2-116 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Figure 2-3. Field of View - TAWS2.3.4.4 Pressurized Aircraft ConsiderationsIn pressurized aircraft, any wiring that penetrates the pressure vessel must be installed in accordance with the Type Design of the aircraft. Considerations for penetrating the pressure vessel of the aircraft for installation are beyond the scope of this manual.2.3.5 KSN 7xx Cooling RequirementsExternal forced air cooling is not required for the KSN 7xx. Cooling fans are provided internal to the unit.The KSN 7xx complies with DO 160C Paragraph 4.5.4 Category V for 30 minutes operation after in flight loss of cooling at 104°F (40°C) ambient temperature and sea level pressure.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-136 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-4. KSN 7xx Safety Navigator Outline Drawing(Dwg. No. 155-01812-0000 Rev. E) (Sheet 1 of 4)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-156 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-4. KSN 7xx Safety Navigator Outline Drawing(Dwg. No. 155-01812-0000 Rev. E) (Sheet 2 of 4)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-176 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-4. KSN 7xx Safety Navigator Outline Drawing(Dwg. No. 155-01812-0000 Rev. E) (Sheet 3 of 4)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-196 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-4. KSN 7xx Safety Navigator Outline Drawing(Dwg. No. 155-01812-0000 Rev. E) (Sheet 4 of 4)Draft as of 10/15/2012
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DraftPage 2-216 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.6 KSN Pinouts2.3.6.1 Refer to Figure 2-5 for the back panel connector locations.Figure 2-5. KSN 7xx Back PanelRefer to Table 2-10 for the connector list.Table 2-10. Connector ListConnector Type Signal DescriptionsJ1 78 Pin D High Density Refer to Table 2-11.J2 78 Pin D High Density Refer to Table 2-12.J3 13 Pin D Refer to Table 2-13.J4 37 Pin D Refer to Table 2-14.J5 RF Refer to Table 2-15.J6 Video Refer to Table 2-16.J7 - -Draft as of 10/15/2012
DraftPage 2-226 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.6.2 Connector PinoutsRefer to Table 2-11 for the signals assigned to the I/O 1 connector (J1).J8 Mini B USB (not used) Refer to Table 2-17.J9 - -J10 RF Refer to Table 2-18.J11 RF Refer to Table 2-19.J12 RF Refer to Table 2-20.J13 RF Refer to Table 2-21.J14 25 Pin D Refer to Table 2-22.Table 2-11. Signals Assigned to the I/O 1 Connector (J1) Function Description Signal Type I/O Interface Pin No.AHRS AHRS 429 RX A 429 Input 66AHRS AHRS 429 RX B 429 Input 46AHRS Heading REF HI Analog Input 6AHRS Heading REF LO Analog Input 7AHRS Heading Valid Discrete Input 21AHRS Heading X Synchro Input 77AHRS Heading Y Synchro Input 58AHRS Heading Z Synchro Input 59ALT Airdata/Fuel/Heading 232 RX RS-232 Input 61NAV/IND LNAV/VNAV Approach Active Annunciate High Current Discrete Output 15DME 1DME Channel Request KRC Input 76DME 1DME Common KRC Input 56DME 1DME Serial Clock KRC Output 75DME 1DME Serial Data KRC Output 57EGPWS(E) Legacy PXPRESS 232 GND RS-232 REF 43EGPWS(E) Legacy PXPRESS 232 TX RS-232 Output 63Table 2-10. Connector ListConnector Type Signal DescriptionsDraft as of 10/15/2012
DraftPage 2-236 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.GPS GPS Flight Plan 232 TX RS-232 Output 62GPS GPS GAMA 429 TX A 429 Output 71GPS GPS GAMA 429 TX B 429 Output 51GPS GPS/Airdata/Fuel 232 GND RS-232 REF 42Growth Spare 429 RX 3 A 429 Input 67Growth Spare 429 RX 3 B 429 Input 47Growth Spare 429 TX A 429 Output 70Growth Spare 429 TX B 429 Output 50Growth Spare 2 RS 232 RX RS-232 Input 23NAV/IND LNAV Approach Active Annunciate High Current Discrete Output 16NAV/IND CDI From Analog Output 8NAV/IND CDI GPS Annunciate High Current Discrete Output 18NAV/IND CDI Select In Discrete Input 3NAV/IND CDI To Analog Output 27NAV/IND CDI VLOC Annunciate High Current Discrete Output 38NAV/IND Dead Reckoning Annunciate High Current Discrete Output 17NAV/IND EFIS CTRL 429 RX A 429 Input 68NAV/IND EFIS CTRL 429 RX B 429 Input 48NAV/IND ILS Approach Energize High Current Discrete Output 40NAV/IND Lateral Deviation (CDI) FlagAnalog Output 9NAV/IND Lateral Deviation (CDI) Flag+ Analog Output 28NAV/IND Lateral Deviation (CDI) Left Analog Output 10NAV/IND Lateral Deviation (CDI) Right Analog Output 29NAV/IND Lateral Deviation Superflag Analog Output 13NAV/IND Loss of Integrity Annunciate High Current Discrete Output 19NAV/IND Message Annunciate High Current Discrete Output 20NAV/IND OBI Clock OBI Output 25NAV/IND OBI Data OBI Output 5NAV/IND OBI Select In Discrete Input 24Table 2-11. Signals Assigned to the I/O 1 Connector (J1) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-246 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.NAV/IND OBI Sync OBI Output 4NAV/IND OBS_C (REF LO) OBS I/O 74NAV/IND OBS_D (COS HI) OBS Input 54NAV/IND OBS_E (COS LO) OBS Input 55NAV/IND OBS_F (SIN HI) OBS Input 34NAV/IND OBS_G (SIN LO) OBS Input 33NAV/IND OBS_H (REF HI) OBS I/O 14NAV/IND OFF PATH Annunciate High Current Discrete Output 35NAV/IND Suspend Annunciate High Current Discrete Output 36NAV/IND Suspend In Discrete Input 2NAV/IND LP Approach Active Annunciate High Current Discrete Output 37NAV/IND Vertical Deviation Down Analog Output 12NAV/IND Vertical Deviation FlagAnalog Output 11NAV/IND Vertical Deviation Flag+ Analog Output 30NAV/IND Vertical Deviation Superflag Analog Output 32NAV/IND Vertical Deviation Up Analog Output 31NAV/IND 1VOR/ILS TX A 429 Output 72NAV/IND 1VOR/ILS TX B 429 Output 52NAV/IND 1VOR/LOC Composite Out Analog Output 60NAV/IND 1VOR/LOC Composite REF Analog REF 41NAV/IND 1Waypoint Annunciate High Current Discrete Output 39PWR GND1 Common GND REF 1PWR GND2 Common GND REF 78PWR KEY1 Key Key 26Traffic TA Aural Active Discrete Input 22Traffic Traffic Ctrl TX A 429 Output 73Traffic Traffic Ctrl TX B 429 Output 53Traffic Traffic Display 429 RX A 429 Input 69Traffic Traffic Display 429 RX B 429 Input 49Table 2-11. Signals Assigned to the I/O 1 Connector (J1) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-256 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Refer to Table 2-12 for the signals assigned to the I/O 2 connector (J2).WX WX-500 422 #2 RX A RS-422 Input 44WX WX-500 422 #2 RX B RS-422 Input 45WX WX-500 422 #2 TX A RS-422 Output 64WX WX-500 422 #2 TX B RS-422 Output 65NOTE: 1. KSN 7x0 Only.Table 2-12. Signals Assigned to the I/O 2 Connector (J2) Function Description Signal Type I/O Interface Pin No.ALT Airdata REF LO Analog I/O 67ALT Airdata REF HI Analog I/O 48ALT Baro ALT 429 A 429 Input 46ALT Baro ALT 429 B 429 Input 65ALT Baro Correction HI Analog Input 8ALT Baro Correction LO Analog Input 28ALT Gillham ALT A1 Discrete Input 18ALT Gillham ALT A2 Discrete Input 37ALT Gillham ALT A4 Discrete Input 57ALT Gillham ALT B1 Discrete Input 17ALT Gillham ALT B2 Discrete Input 36ALT Gillham ALT B4 Discrete Input 56ALT Gillham ALT C1 Discrete Input 16ALT Gillham ALT C2 Discrete Input 35ALT Gillham ALT C4 Discrete Input 55ALT Gillham ALT D4 Discrete Input 76EGPWS EGPWS Status 429 TX A 429 Output 45EGPWS EGPWS Status 429 TX B 429 Output 64EGPWS Landing Gear Discrete Input 34EGPWS OATAnalog Input 68Table 2-11. Signals Assigned to the I/O 1 Connector (J1) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-266 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.EGPWS OAT + Analog Input 69EGPWS OAT GND Analog Output 49EGPWS OAT REF Analog Output 50EGPWS Shared - Flaps or Tactical Select (Low ALT Mode) Discrete Input 15EGPWS Terrain Caution Annunciate High Current Discrete Output 24EGPWS Terrain Inhibit Discrete Input 74EGPWS Terrain Warn Annunciate High Current Discrete Output 4EGPWS Terrain Failure Annunciate High Current Discrete Output 3EGPWS WOW Discrete Input 54EGPWS Shared - Audio On or Low Altitude Mode Annunciate High Current Discrete Output 23EGPWS EGPWS Self Test Discrete Input 75Flight Control GPS Steering Select Discrete Output 77Flight Control GPS/LOC Approach Annunciate High Current Discrete Output 22Flight Control Remote Go Around Discrete Input 72Flight Control Roll SteerAnalog Output 9Flight Control Roll Steer+ Analog Output 10Flight Control Roll Steer REF HI Analog Input 30Flight Control Roll Steer REF LO Analog Input 29Flight Control Roll Steer Valid Discrete Output 59Connected Gateway XM WX 232 GND RS-232 REF 41Connected Gateway XM WX 232 RX RS-232 Input 60Connected Gateway XM WX 232 TX RS-232 Output 40Growth Spare 429 RX 1 A 429 Input 44Growth Spare 429 RX 1 B 429 Input 63Growth Spare 429 RX 2 A 429 Input 47Growth Spare 429 RX 2 B 429 Input 66Table 2-12. Signals Assigned to the I/O 2 Connector (J2) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-276 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Growth Spare In1 Discrete Input 12Growth Spare In2 Discrete Input 31Growth Spare In3 Discrete Input 51Growth Spare In4 Discrete Input 70Growth Spare In5 Discrete Input 11Growth Spare In6 Discrete Input 73Growth Spare Out1 High Current Discrete Output 38NAV/IND LPV Approach Active Annunciate High Current Discrete Output 58MAINT IOP 422 #4 RX A RS-422 Input 42MAINT IOP 422 #4 RX B RS-422 Input 43MAINT IOP 422 #4 TX A RS-422 Output 61MAINT IOP 422 #4 TX B RS-422 Output 62MISC FAN Return Common GND REF 19MISC KSN Fan Discrete Output 20MISC 1MMDS Fan Discrete Output 39NAV/COM 1COM Audio Out HI Audio Output 5NAV/COM 1COM Audio Out LO Audio Output 25NAV/COM 1COM Channel Decrement Discrete Input 14NAV/COM 1COM Channel Increment Discrete Input 13NAV/COM 1COM Mic Audio In HI Audio Input 6NAV/COM 1COM Mic Audio In LO Audio Input 26NAV/COM 1COM Mic Key Discrete Input 71NAV/COM 1COM Remote Transfer Discrete Input 52NAV/COM 1Emergency Frequency Discrete Input 33NAV/COM 1NAV Audio Out HI Audio Output 7NAV/COM 1NAV Audio Out LO Audio Output 27NAV/COM 1Transmit Interlock Discrete Input 53PWR GND3 Common GND REF 1Table 2-12. Signals Assigned to the I/O 2 Connector (J2) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-286 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Refer to Table 2-13 for the signals assigned to the power supply interface connector (J3).Refer to Table 2-14 for the signals assigned to the main processor board interface connector (J4).PWR GND4 Common GND REF 78PWR KEY2 Key Key 32Traffic Traffic Disc 1 Out Discrete Output 2Traffic Traffic Disc 2 Out Discrete Output 21NOTE: 1. KSN 7x0 Only.Table 2-13. Signals Assigned to the Power Supply Interface Connector (J3) Function Description Signal Type I/O Interface Pin No.MAINT 33V_BOOST_TEST Analog (Test Only) Output 1MAIN 5V_KSN_TEST Analog (Test Only) Output 4MAINT 5V7_STARTUP-TEST Discrete (Test Only) Output 5Main 112VPOS_MMDS_TEST Analog (Test Only) Output 3PWR MAIN_POWER_IN Aircraft Power Input A3PWR MAIN_POWER_IN _RTN Aircraft GND Input A1PWR 1MAIN_POWER_IN _RTN Aircraft GND Input A4PWR 1MMDS_TX_POWER_IN Aircraft Power Input A2MAINT ON_OFF_Status_N Discrete (Test Only) Output 2NOTE: 1. KSN 7x0 Only.Table 2-14. Signals Assigned to the Main Processor Board Interface Connector (J4) Function Description Signal Type I/O Interface Pin No.CONFIG MOD Config MOD Data I2C I/O 12CONFIG MOD Config MOD GND I2C Output 29CONFIG MOD Config MOD Power I2C Output 11Dual KSN 7XX 422 #1 RX A RS-422 Input 24Table 2-12. Signals Assigned to the I/O 2 Connector (J2) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-296 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Dual KSN 7XX 422 #1 RX B RS-422 Input 25Dual KSN 7XX 422 #1 TX A RS-422 Output 6Dual KSN 7XX 422 #1 TX B RS-422 Output 7GPS GPS Dataload 232 GND RS-232 REF 31GPS GPS Dataload 232 RX RS-232 Input 32GPS GPS Dataload 232 TX RS-232 Output 13GPS GPS Enhanced PXPRESS 232 GND RS-232 REF 21GPS GPS Enhanced PXPRESS 232 RX RS-232 Input 20GPS GPS Enhanced PXPRESS 232 TX RS-232 Output 2GPS GPS Time Mark HI RS-422 Output 10GPS GPS Time Mark LO RS-422 Output 28Growth Spare In8 Discrete Input 3Lighting Remote Dimming HI Analog Input 17Lighting Remote Dimming LO Analog Input 36MAINT Demo Mode Select Discrete Input 19MAINT Shop Mode Select Discrete Input 18MAINT/ AUDIO Shared - Maintenance or Voice Recognition 422 RX B RS-422 Input 23MAINT/ AUDIO Shared - Maintenance or Voice Recognition 422 TX B RS-422 Output 5MAINT/ AUDIO Shared - Maintenance or Voice Recognition 422 RX A RS-422 Input 22MAINT/ AUDIO Shared - Maintenance or Voice Recognition 422 TX A RS-422 Output 4PWR GND5 Common GND REF 1PWR GND6 Common GND REF 37WX Datalink Receiver 422 #3 RX A RS-422/RS-232 Input 26WX Datalink Receiver 422 #3 RX B RS-422/RS-232 Input 27WX Datalink Receiver 422 #3 TX A RS-422/RS-232 Output 8WX Datalink Receiver 422 #3 TX B RS-422/RS-232 Output 9WX Satellite Audio - Left HI Audio Output 15Table 2-14. Signals Assigned to the Main Processor Board Interface Connector (J4) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-306 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Refer to Table 2-15 for the signals assigned to the GPS antenna connector (J5).Refer to Table 2-16 for the signals assigned to the video connector (J6).Refer to Table 2-17 for the signals assigned to the rear panel USB connector (J8).WX Satellite Audio - Left LO Audio Output 34WX Satellite Audio - Right HI Audio Output 14WX Satellite Audio - Right LO Audio Output 33Table 2-15. Signals Assigned to the GPS Antenna Connector (J5) Function Description Signal Type I/O Interface Pin No.GPS GPS Antenna RF I/O CenterGPS GPS Antenna GND RF I/O ShellTable 2-16. Signals Assigned to the Video Connector (J6) Function Description Signal Type I/O Interface Pin No.Video Remote Video Video Input CenterVideo Remote Video GND Video Input ShellTable 2-17. Signals Assigned to the Rear Panel USB Connector (J8) Function Description Signal Type I/O Interface Pin No.Not Used USB2 DMini USB I/O 2Not Used USB2 D+ Mini USB I/O 3Not Used USB2 D GND Mini USB Output 5Not Used USB2 VBUS Mini USB Output 1Not Used USB2 ID Mini USB Output 4Table 2-14. Signals Assigned to the Main Processor Board Interface Connector (J4) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-316 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Refer to Table 2-18 for the signals assigned to the XM WX datalink antenna connector (J10).Refer to Table 2-19 for the signals assigned to the VHF transceiver antenna connector (J11).Refer to Table 2-20 for the signals assigned to the navigation radio (VOR/LOC) antenna connector (J12).Refer to Table 2-21 for the signals assigned to the navigation radio (GS) antenna connector (J13).Refer to Table 2-22 for the signals assigned to the WX RDR/EGPWS connector (J14).Table 2-18. Signals Assigned to XM WX Datalink Antenna Connector (J10) Function Description Signal Type I/O Interface Pin No.WX Datalink Antenna RF Input CenterWX Datalink Antenna GND RF Input ShellTable 2-19. Signals Assigned to the VHF Transceiver Antenna Connector (J11) (KSN 7x0 Only) Function Description Signal Type I/O Interface Pin No.NAV/COM COM Antenna RF I/O CenterNAV/COM COM Antenna GND RF I/O ShellTable 2-20. Signals Assigned to the Navigation Radio (VOR/LOC) Antenna Connector (J12) (KSN 7x0 Only) Function Description Signal Type I/O Interface Pin No.NAV/COM VOR/LOC Antenna RF Input CenterNAV/COM VOR/LOC Antenna GND RF Input ShellTable 2-21. Signals Assigned to the Navigation Radio (GS) Antenna Connector (J13) (KSN 7x0 Only) Function Description Signal Type I/O Interface Pin No.NAV/COM GS Antenna RF Input CenterNAV/COM GS Antenna GND RF Input ShellTable 2-22. Signals Assigned to the WX RDR/EGPWS Connector (J14) Function Description Signal Type I/O Interface Pin No.EGPWS(E) EGPWS CTRL 429 TX A 429 Output 13EGPWS(E) EGPWS CTRL 429 TX B 429 Output 12Draft as of 10/15/2012
DraftPage 2-326 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.7 KSN Wiring and Cable Harness FabricationThe KSN MMDR receives primary power from the aircraft power source. A typical interface is shown in Paragraph 3.3 Power System Interface. Aircraft specific interfaces with more details are provided in separate EB or installation drawings.The length of the wires to parallel pins must be approximately the same length, so that the best distribution of current can be effected. Honeywell recommends that all wires (including spares) as provided with the interconnect definition information be included in the fabrication of the wiring harness. However, if full wiring is not desired, the installer must ensure that the minimum wiring requirements for the features and functions to be used have been incorporated.When cables are installed in the aircraft, they must be supported firmly enough to prevent movement and must be carefully protected against chaffing. Additional protection must also be provided in all locations where the cable may be subjected to abuse. In wire bundles, the cabling must not be tied tightly together as this tends to increase the possibility of noise pickup and similar interference.When routing cables through the aircraft the cables must cross high level RF lines at right angles.Prior to installing any equipment, make a continuity check of all wires and cables associated with the system. Then apply power and check for proper voltages at system connectors, and then remove power before completing the installation. The following guidelines are recommended:(1) The installing facility will supply and fabricate all external cables. The required connectors are supplied as part of the installation kit (refer to Table 2-1 or Table 2-2).EGPWS(E) External Audio Inhibit Discrete Input 24EGPWS(E) KCPB RX A 453 Input 9EGPWS(E) KCPB RX B 453 Input 22EGPWS(E) KCPB RX GND 453 Input 10Power GND10 Common GND REF 25Power GND9 Common GND REF 1WX WX RDR 708A 453 GND 453 Input 4WX WX RDR 708A 453 RX A 453 Input 5WX WX RDR 708A 453 RX B 453 Input 17WX WX RDR CTL 429 TX B 429 Output 14WX WX RDR CTL 429 TX A 429 Output 2WX WX RDR Power ON/OFF Discrete Output 15Table 2-22. Signals Assigned to the WX RDR/EGPWS Connector (J14) (Cont)Function Description Signal Type I/O Interface Pin No.Draft as of 10/15/2012
DraftPage 2-336 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.(2) The unit must be kept a minimum of 36 inches (914 mm) from all antennas. Additionally, the antenna coax cable must not be bundled with the other wiring harnesses to the unit. Coaxial cables must be routed separately and be kept a minimum of 1.0 inch (25.4 mm) from each other.(3) The length and routing of the external cables must be carefully planned before attempting the actual installation. Avoid sharp bends or locating the cable near aircraft control cables. The wiring cables must be of a length to allow for a “maintenance loop”; that is, the length must be adequate to access and extend the connectors aft of the panel for future maintenance purposes. Excess cabling must be secured and stowed by tie-wrapping until such maintenance is required.(4) The cables must be supported firmly enough to prevent movement. They must be carefully protected wherever one may chafe against another or against some other object (such as the aircraft structure). Extra protection must be provided in all locations where the cables may be subject to abuse. Shields on shielded wires must be grounded in accordance with the system interconnection information.(5) Shields must be carried through any obstruction via a thru-bulkhead connector. If shielding cannot be carried through by use of a bulkhead/connector pin, precautions must be taken to ensure each segment of the shielded lead be grounded at only one point. A GND connection of not more than two inches in length must be used. The preceding discussion does not apply to coaxial and quadraxial cable.(6) Avoid routing cabling near high noise and high power sources.2.3.7.1 Audio Electrical NoiseImproper installation of the audio lines to an audio panel can cause GND loops and degraded audio performance. Refer to your Audio Panel installation manual for guidance on proper installation of the audio lines.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-356 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-6. Coaxial Right Angle Connector Instruction Sheet (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-376 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-7. TNC Antenna Coax with Straight Connector (Sheet 1 of 1)Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-386 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-396 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-8. Quadraxial Cable Preparation (Sheet 1 of 3)Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-406 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-416 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-8. Quadraxial Cable Preparation (Sheet 2 of 3)Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-426 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-436 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 2-8. Quadraxial Cable Preparation (Sheet 3 of 3)Draft as of 10/15/2012
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DraftPage 2-456 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.3.8 KSN Power DistributionThe KSN 7xx is powered through two dedicated circuit breakers. A 10.0 AMP circuit breaker powers the MMDS radio system. A 7.5 AMP circuit breaker powers the rest of the KSN 7xx functions. These circuit breakers must be connected to the same power bus sources. The power bus can range from +11 to +33 VDC. For aircraft weighing less than 6000 pounds (2721.6 kg) with two KSNs, it is recommended that each KSN is powered from a separate power bus. For aircraft weighing more than 6000 pounds (2721.6 kg) with two KSNs, it is required that each KSN is powered from a separate power bus.2.3.9 Placards and LabelsAll placards and labels must be visible in all lighting conditions. Text must be a minimum of 0.10 inch (2.5 mm) in height, and must be a contrasting color to the background of the label/placard. Text must be permanent and not easily disfigurable. If the KSN is not configured for IFR operation, a placard stating “The KSN 7xx is limited to VFR use only” (or similar) must be installed in the pilots field of view.2.3.10 Weight and BalanceUsing component weights from Table 2-23 and the moment arm of the component mounting locations, perform a weight and balance calculation per AC 43-13-1B Chapter 10. Also account for equipment remove during the modification process.Table 2-23. Component WeightsComponent WeightKSN 770 (standard, includes KCM 200 and rack) 9.9 pounds (4.5 kg)KSN 770 (with WX RDR/EGPWS) 10.2 pounds (4.6 kg)KSN 765 (standard, includes KCM-200 and rack) 8.1 pounds (3.7 kg)KSN 765 (with WX RDR/EGPWS) 8.4 pounds (3.8 kg)GPS Antenna (KA-96) Refer to KA 96 IM (0.5 pounds [0.2 kg] nominal)Annunciator Panel Refer to the manufacturers dataNAV Antenna Refer to the manufacturers dataCOM Antenna Refer to the manufacturers dataIndicator Refer to the manufacturers dataDraft as of 10/15/2012
DraftPage 2-466 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.4 Antenna InstallationThe antenna(s) must be well removed from other antenna projections, the engine(s), and propeller(s). It must also be well removed from landing gear doors, access doors, or other openings which will break the GND plane for the antenna(s). On metal skinned aircraft, the antenna(s) must be bonded to the surface of the aircraft in a fore to aft location that provides the flattest GND plane. On composite aircraft, the antenna(s) must be located at the center of a conductive GND plane, contoured to the shape of the aircraft, having dimensions of at least 24.0 by 24.0 inches (610 by 610 mm). The antenna penetration must be designed such that the structural integrity of the fuselage is not compromised. The antenna(s) need to be within 5 degrees of the centerline.Where practical, plan the antenna location(s) to keep cable lengths as short as possible and avoid sharp bends in the cable to minimize the VSWR. Avoid running other cables or wires near the antenna cable(s).On pressurized aircraft, the antenna(s) must be sealed using an approved sealant, such as RTV No. 3145 (Honeywell PN 016-01082-0000) or equivalent, around the connector and mounting hardware.The antenna edge and mounting hardware recesses must be sealed from the outside for moisture protection using RTV or equivalent.Mount the antenna(s) in as clean as environment as possible, away from exhaust gases and oils. The antenna(s) must be kept clean. If left dirty (oil covered), the antenna performance may be affected.Antennas must be installed in accordance with their own installation manuals.2.4.1 GPS/WAAS Antenna Location ConsiderationsThe KA 96 GPS active antenna, PN 071-01620-0001 or equivalent is the designated antenna for the KSN 7xx.The antenna must be mounted on top of the fuselage near the cockpit. Avoid mounting the antenna near any projections, the propeller, or the T-tail of the aircraft, where shadows could occur. It is recommended that there be a separation of at least 36.0 inches (914 mm) between the GPS antenna and any VHF COM antenna on the aircraft.The antenna baseplate must be level within ±5 degrees in both axes when the aircraft is level (level is defined as the aircraft attitude required when weighing the aircraft for weight and balance) for optimum performance. If the antenna is tilted more than 5 degrees or is mounted close to other objects that shadow it, loss of some of the satellites will occur and system performance may be degraded. Antenna cable and connector information, including vendor information is listed below.Refer to Figure 2-7 for the cable/connector assembly instructions for the 0 to 40 feet (0 to 12.2 meters) category using RG 400/U or RG 142B/U.Refer to Table 16 GPS Antenna Cable Information (for both TNC and BMA) for the 0 to 80 feet (0 to 24.4 meters) and 0 to 100 feet (0 to 30.5 meters) categories. NOTE: The Nominal signal gain for the KA 96 is 27 to 31 dB, the noise figure is 1.9 dB at 77°F (25°C), 2.5 dB maximum. With 0.050 ice on the radome, gain will not decrease by more than 2.0 dB when viewing a satellite from 30 degrees above the horizon to zenith (as compared to a no ice condition).Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 2-476 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Table 2-24. GPS Antenna Cable InformationCable Length Cable PN TNC Connector (KSN 7xx) TNC Connector Antenna Maximum Allowable Loss(dB) @ 1.575 GHz0 to 40 feet (0 to 12.2 meters) PN: 024-00002-0000VPN: RG142B/U PN: 030-00134-0000VPN: TED Mfg. 5-10-30 PN: 030-00134-0001VPN: TED Mfg. 5-30-102-1 8.0PN: 024-00051-0060VPN: RG400/U PN: 030-00134-0000VPN: TED Mfg. 5-10-30 PN: 030-00134-0001VPN: TED Mfg. 5-30-102-1 8.00 to 80 feet (0 to 24.4 meters) PN: 024-00072-0000VPN: ECS 311601 PN: 030-00108-0002VPN: TED Mfg. 5-10-307 PN: 030-00108-0002VPN: TED Mfg. 5-10-307 8.00 to 100 feet (0 to 30.5 meters) PN: 024-00071-0000VPN: ECS 311201 PN: 030-00108-0003VPN: TED Mfg. 5-10-306 PN: 030-00108-0003VPN: TED Mfg. 5-10-306 8.0100 to 165 feet (30.5 to 50.3 meters) Contact TED, ECS or PIC for complete cable/connector assemblyTable 2-25. Cable Vendor Contact InformationTED Manufacturing Corp.11415 Johnson DriveShawnee Mission, Kansas 66203Tel: (913) 631-6211http://www.tedmanufacturing.comElectronic Cable Specialists (now part of CarlisleIT)5300 W. Franklin DriveFranklin, Wisconsin 53132Tel: 800 327-9473 or (414) 421-5300http://www.ecsdirect.com/http://www.carlisleit.com/PIC Wire and CableN53 W24747 South Corporate CircleSussex, WI 53089-0330Tel: (800) 742-3191 or (262) 246-0500http://www.picwire.com/sales@picwire.comNOTE: Manufacturer contact information is provided as convenience only and may change any time.Draft as of 10/15/2012
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DraftPage 2-496 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.2.4.2 COM and NAV Antenna Installation Considerations2.4.2.1 COM Antenna LocationThe VHF COM antenna must be mounted as far away as possible (8.0 feet [244 cm] minimum) from other similar antennas and the vertical stabilizer. Mounting the COM antenna as far away as possible from the navigation antenna will help reduce COM to NAV interference. The COM antenna must also be mounted as far away as possible from an ELT antenna to prevent distortion of the radiated pattern and to prevent radiated broadband noise from affecting the ELT when excited by the COM transmissions. Radiated broadband noise from an ELT is a common cause of COM-to-COM and COM-to-NAV interference. Mounting one antenna on top of the fuselage at the highest location to ensure a good radiation pattern and the other on the bottom of the fuselage offers good separation with a minimum of interaction.It is recommended that one COM transceiver be connected to the top antenna for good GND communication and that the other COM transceiver be connected to the bottom antenna to provide good airborne communications. If mounting antennas on the same side of the aircraft is unavoidable, maintain the minimum allowable separation (8.0 feet [244 cm]).The antenna must be mounted on a section of the aircraft that is horizontal during cruise flight. The base of the antenna must be well bonded to the metal aircraft skin. Remove any paint from around the mounting holes to ensure a good connection between the antenna and the skin. The metal aircraft skin at the base of the antenna must extend a minimum of 24.0 inches (610 mm) in every direction. This provides the GND plane required for the antenna. Any less metallized area will result in reduced communication range at some bearings around the aircraft and may increase interference to and from other systems.The COM transceiver performance depends heavily on the integrity of the electrical bonding to the airframe and also the electrical integrity of the aircraft structure. If the electrical resistance between an antenna and the aircraft or between adjacent skin panels changed intermittently, noisy communications may result.Connect the antenna to the COM unit with 50-ohm coaxial cable, keeping the cable length to a minimum and avoiding sharp bends in the cable. Keep the COM antenna cable as far away from other antenna cables as possible and do not bundle several antenna cables together. Prepare the cable to the BNC connector as shown in Figure 2-6.Use Dow-Corning DC-4, or equivalent, on both inside and outside of the connector and its mate as an effective barrier against moisture and to prevent corrosion.2.4.2.2 NAV Antenna LocationThe NAV antenna must be well removed from other antennas, projections, engines or propellers. It must have a clear line of sight area if possible. The antenna must be mounted symmetrically with the center line of the aircraft. Avoid running other coaxial cables and wires near the NAV antenna cable.The VOR/LOC antenna with Glideslope is a two piece dipole with one part mounted on each side of the vertical stabilizer. It must be installed on the upper section of the vertical stabilizer of single finned aircraft and be at least 28.0 inches (711 mm) (measured vertically) from the horizontal stabilizer.Draft as of 10/15/2012
DraftPage 2-506 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.On dual VOR/ILS installations, it is recommended that a splitter be used to divide signals from a single VOR/LOC antenna into two or more receivers. Use double shielded cables to reduce interference to the receivers.Prepare the cable to the BNC connector as shown in Figure 2-6.2.5 Optional Accessory Installation2.5.1 External AnnunciatorsThe recommended external annunciator for the KSN 7xx is the Mid Continent MD41-TBD (refer to the Mid Continent installation manual for installation instructions).2.5.2 External SwitchesExternal switches may be added for functions such as external increment and decrement of channel frequencies. Unless otherwise noted, these are signal level inputs and may be activated using MS 25089-1C Normally Open switches or equivalent necessary for system operation.2.6 Magnetic Compass RecalibrationAfter the KSN 7xx has been installed and is operational, be sure to recalibrate the magnetic compass.Draft as of 10/15/2012Section 2.5.1 We do not want to be tied down to only one Brand and Model of External Annunciators. Is the MD 41 the only option? Section 2.5.2 Same comment for External switches as 2.5.1.
DraftPage 3-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.SECTION III - SYSTEM INTERCONNECT3.1 IntroductionSection III contains information relative to KSN 7xx Safety Navigator interconnection diagrams, options available to the system planner, and specific electrical characteristics of the various interfaces where applicable. Each paragraph in this section contains the installation wiring diagrams for that section.For information regarding the compatibility of equipment not listed in this manual, the installing agency must contact Bendix/King customer service at www.BendixKing.com.Section III is divided into major sections by interface type or major topic. Each major section describes in detail the specifications for particular types of interfaces connecting to the KSN 7xx.3.2 Standard Interface DefinitionsUnless otherwise stated, the following interface definitions will apply.3.2.1 Discrete InputRefer to Table 3-1 for the discrete input states.3.2.2 Discrete OutputUnless otherwise stated, the following interface definitions will apply. Unless otherwise stated, all outputs may be used as high current discrete outputs.3.2.2.1 High CurrentRefer to Table 3-2 for the high current discrete output states.Table 3-1. Discrete Input StatesState Voltage Upper Limit Voltage Lower Limit CommentOpen/High N/A 14 VDC for aircraft power24.8 VDC7.0 VCD for aircraft power12.4 voltsImpedance is >230 kilohms to GNDLow 3.0 VDC 0 VDC Impedance is <95ohms to GNDTable 3-2. High Current Discrete Output StatesState Voltage Upper Limit Sinking Current CommentActive 2.0 VDC 0 to 250 mA DC -Inactive N/A N/A Open collectorDraft as of 10/15/2012
DraftPage 3-26 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.2.2.2 SuperflagRefer to Table 3-3 for the superflag output states.3.2.3 EIA Standard Serial Interfaces3.2.3.1 RS-232Electrical characteristics are per ANSI TIA/EIA-232-F. Each RS-232 port will be configurable on the maintenance pages for the following:• Buad Rate• Data Bits• Parity Bit• Stop Bits.3.2.3.2 RS-422Electrical characteristics are per ANSI TIA/EIA-422-A.3.2.4 ARINC 429 Standard Serial InterfacesElectrical characteristics are per ARINC 429.3.2.5 ARINC 453 InterfaceThis bus format is 1600 bit Manchester bi-phase per ARINC 708A. The data rate on this bus is 1 Mbit/s.Table 3-3. Superflag Output StatesState Voltage Upper Limit Voltage Lower Limit CommentActive N/A 18 VDC When the normal AC power is 24.8 VDC and the output is sourcing up to 250 mA.N/A 10 VDC When the normal AC power is 12.4 VDC and the output is sourcing up to 250 mA.Inactive 3.5 VDC 0 VDCDraft as of 10/15/2012
DraftPage 3-36 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.3 Power System Interface3.3.1 GeneralThe KSN 7xx power system interface contains information relative to both the aircraft power bus and the lighting bus.The KSN 7xx is compatible with 14 VDC, 28 VDC aircraft. The 16 watts VHF COM option provided with the KSN 7xx requires a 28 VDC power source.The KSN 7xx will accept 5 VAC, 5 VDC, 14 VDC, or 28 VDC for panel lighting control. Panel lighting on the KSN 7xx is adjusted based on the aircraft lighting bus.3.3.2 Electrical CharacteristicsRefer to Table 3-4 for the TBD.The KSN 7xx will draw 4.5 AMP maximum current at 28 VDC input voltage with panel lighting at maximum brightness and all superflags active and loaded.Total power consumption is no more than:Unit power: 150 watts receive, 350 watts transmit.Panel lighting at maximum brightness: 100 mA maximum.Superflag power: Up to 0.25 AMP per active superflag (lateral, vertical, steering, and serial superflags).Refer to Table 3-5 for the TBD.Table 3-4. TBDKSN 7xx Version Pins Description NotesKSN 765 J3-A3 MAIN POWER IN (11 to 33 VDC) Main power for unit.KSN 77010W COM J3-A3 MAIN POWER IN (11 to 33 VDC)J3-A2 MAIN POWER IN (11 to 33 VDC) Main power for unit.Power for NAV/COMKSN 77016W COM J3-A3 MAIN POWER IN (11 to 33 VDC)J3-A2 MAIN POWER IN (11 to 33 VDC) Main power for unit.Power for NAV/COM 16 watts COM must have +28 VDC.NOTE: These pin connects to the aircraft power with 16 AWG wire minimum.Draft as of 10/15/2012
DraftPage 3-46 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.3.3 Panel Lighting InputsJ4-17 REMOTE DIMMING HIJ4-38 REMOTE DIMMING LOThese pins connect to airframe GND with 22 AWG wire minimum.The KSN 7xx is compatible with 28 VDC, 14 VDC, 5 VDC, and 5 VAC for panel lighting voltages.These inputs do not supply power to the KSN 7xx panel lighting; rather, the KSN 7xx senses the level on this input and drives the panel lighting lamps using the 14 to 28 VDC MAIN POWER IN input.The KSN 7xx must be configured for the correct lighting voltage on the Maintenance pages for proper operation. No damage will occur to the KSN 7xx if the lighting is configured improperly. If configured for too low a voltage, the lamps will be full brightness for most of the panel lighting rheostat range. If configured for too high a voltage, the lamps will only be adjustable between dim and OFF.3.3.4 Interconnect DiagramRefer to Figure 3-1 for the power system interface interconnect diagram.Table 3-5. TBDKSN 7xx Version Pins Description NotesKSN 765 J3-A4 GND Main power return for unit.KSN 77010W COM J3-A4 GNDJ3-A1 GND Main power return for unit.Power return for NAV/COMKSN 77016W COM J3-A4 GNDJ3-A1 GND Main power return for unit.Power return for NAV/COM 16 watts COM must have +28 VDC.NOTE: These pins connect to the airframe GND with 16 AWG wire minimum.Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-56 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-1. Power System Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-76 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.4 Position Interface3.4.1 Applicable Part NumbersAll part numbers and software revisions perform all position interface functions.3.4.2 FunctionThe position interface outputs allow moving map products (such as the EFIS 40/50, Aspen EFD, and ARGUS 3000/5000/7000 series of products) and ELT products to use KSN 7xx position data. Position is output as both RS-232 data and ARINC 429 data.3.4.3 Requirements and LimitationsThe position interface must be left open if there are no using units are connected to the KSN 7xx.3.4.4 Electrical CharacteristicsJ1-62 GPS FLIGHT PLAN 232 TXJ1-42 GPS/AIRDATA/FUEL 232 GNDThis serial data bus conforms to EIA RS-232 electrical characteristics. This bus outputs position information, which also includes (but may not be limited to) distance to go, groundspeed, time to go, and flight plan waypoint data.J1-71 GPS GAMA 429 TX AJ1-51 GPS GAMA 429 TX BThis serial data bus conforms to ARINC 429 electrical characteristics, and is configured for low operating speed.J1-63 LEGACY PXPRESS 232 TXJ1-43 LEGACY PXPRESS 232 GNDThis serial data bus conforms to EIA RS-232 electrical characteristics, and may be configured for speed on the maintenance pages.3.4.5 Interconnect DiagramRefer to Figure 3-2 for the position interface interconnect diagram.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-96 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-2. Position Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-116 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.5 WX RDR Interface3.5.1 Applicable Part NumbersThis function is only available when the optional KSN 7xx WX RDR/EGPWS option board is installed and the associated product feature key is installed.When the WX RDR is not connected to the KSN 7xx, the pins must be left open.3.5.2 FunctionRadar is a method for locating thunderstorms using radio waves. The radar transmitter generates microwave energy in the form of pulses which are then transferred to the antenna where they are focused into a beam by the antenna and radiated. When the beam intercepts a target, the energy is reflected as an echo back to the antenna. It is then transferred to the receiver and processing circuits in the receiver/transmitter unit. These echoes are displayed on the KSN 7xx.3.5.3 Requirements and LimitationsThe KSN 7xx must be configured for the radar installed for proper operation. The following radar types are supported. Configuration of each type is covered in Section 4.Refer to Table 3-6 for the WX RDR requirements and limitations.3.5.4 Electrical CharacteristicsA. WX RDR Control (ARINC 429)J14-2 WX RDR CTL 429 TX AJ14-14 WX RDR CTL 429 TX BThis serial data bus conforms to ARINC 429 electrical characteristics, and may be configured for operating speed on the maintenance pages.B. Power ON/OFFJ14-15 WX RDR POWER ON/OFFThis pin controls the power emissions of the WX RDR, and is active low, so that when the output is pulled low, the WX RDR turns ON.C. WX RDR Data (ARINC 708A)J14-5 WX RDR 708A 453 RX AJ14-17 WX RDR 708A 453 RX BThis serial data bus conforms to ARINC 708A electrical characteristics.3.5.5 Interconnect DiagramRefer to Figure 3-3 for the WX RDR interface interconnect diagram.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-136 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06 Table 3-6. WX RDR Requirements and LimitationsRDR Type(Note 9) Horizontal Scan AngleVertical Profile Enable Vertical ScanAngleAuto Tilt WX Manual Gain Sector Scan WX/ARL Mode 5,320 nm Ranges Auto StandbyRDR 2000 100 (90) Enabled 60 N/A N/A N/A N/A N/A EnabledRDR 2100 120 (100) Enabled 60 Enabled Disabled Disabled Enabled Enabled EnabledRDS 8190 N/AN/AN/AN/AN/AN/AN/AEnabledRDS 8290 N/AN/AN/AN/AN/AN/AN/AEnabledRDS 82VP 90 Enabled 50 N/A N/A N/A N/A N/A EnabledRDS 84 120 N/A N/A N/A N/A N/A N/A Enabled EnabledRDS 84VP 120 Enabled 60 N/A N/A N/A N/A Enabled EnabledRDS 86 120 N/A N/A Enabled N/A N/A Enabled Enabled EnabledRDS 86VP 120 Enabled 60 Enabled N/A N/A Enabled Enabled EnabledOther 120 (90) (100) Disabled 60 (50) Disabled Disabled Disabled Disabled Enabled EnabledDraft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-156 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-3. WX RDR Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-176 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.6 EGPWS Interface3.6.1 Applicable Part NumbersA. Internal EGPWS (Growth)All part numbers and software versions perform all published internal EGPWS functions.B. External EGPWSThis function is only available when the optional KSN 7xx WX RDR/EGPWS option board is installed and the associated product feature key is installed. Contact Bendix/King Product Support for the feature key.When the EGPWS is not connected to the KSN 7xx, the pins must be left open.The following are part number families of the external EGPWS units that will interface with the KSN 7xx. The minimum EGPWS software versions (the last six digits) required for compatibility with KSN 7xx installations is as follows:• 965-0976-XXX-212-212 Mark V EGPWC• 965-0976-XXX-212-212 Mark V EGPWC• 965-0976-XXX-212-212 Mark V EGPWC• 965-1076-XXX-212-212 Mark VII EGPWC• 965-1076-XXX-212-212 Mark VII EGPWC• 965-1076-XXX-212-212 Mark VII EGPWC• 965-1176-005 Mark VI EGPWC• 965-1186-005 Mark VI EGPWC• 965-1206-005 Mark VIII EGPWC• 965-1216-005 Mark VIII EGPWC• 965-1227-0XX Mark XXI EGPWC• 965-1590-006 Mark XXII EGPWC• All versions of the KGP 560 EGPWS• All versions of the KMH 880 EGPWS.Draft as of 10/15/2012 and KGP 860 and KMH 980
DraftPage 3-186 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.6.2 FunctionEGPWS is a terrain awareness and alerting system. It uses aircraft inputs including geographic position, attitude, airspeed, and glideslope combined with internal terrain, obstacle, and airport databases to predict a potential conflict between an aircraft’s flight path and terrain or an obstacle. The KSN 7xx has both an internal and an external EGPWS option which are defined below.In a later certification, the KSN 7xx will offer an internal/integrated EGPWS function.3.6.2.1 Internal EGPWS Function (Growth)The internal EGPWS function uses GPS position along with altitude from a blind encoder or air data computer to verify obstacle clearance.3.6.2.2 External EGPWS FunctionThe external EGPWS function allows the KSN 7xx to interface to a variety of external EGPWS units providing ground proximity warnings to pilots.3.6.3 Requirements and LimitationsA. Internal EGPWS (Growth)The KSN 7xx needs an external altitude reference for the internal EGPWS to work correctly. Refer to Paragraph 3.9 Altitude/Airdata/Fuel Interface for sources of altitude that may be used.B. External EGPWSThe external EGPWS unit will need a set of inputs described in its own installation manual. The KSN 7xx can supply the GPS position needed by the EGPWS boxes.3.6.4 Electrical CharacteristicsThe EGPWS will also output audio alerts. Refer to Paragraph 3.15 Audio Interface for connections to the audio system.A. Internal EGPWS (Growth)(1) Terrain InhibitJ2-74 TERRAIN INHIBITNormal Operation: OpenEGPWS Inhibited: GNDThis input inhibits the operation of the internal EGPWS.(2) EGPWS Self Test (Growth)J2-75 EGPWS SELF TESTDraft as of 10/15/2012
DraftPage 3-196 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Normal Operation: OpenStart Self Test: Momentary GNDThis input starts the EGPWS Self Test.(3) Landing Gear (Growth)J2-34 LANDING GEARGear Down: GNDGear Up: OpenThis input signals the state of the landing gear.(4) Flaps or Tactical Select (Growth)J2-15 SHARED-FLAPS OR TACTICAL SELECT (LOW ALTITUDE MODE)For fixed wing aircraft, this indicates the position of the flaps as follows:Flaps Retracted: OpenFlaps Extended: GNDFor Rotorcraft, this input indicates normal or low altitude mode:Normal Operation: OpenLow Altitude Operation: GND(5) Annunciations (Growth)J2-24 TERRAIN CAUTION ANNUNCIATEJ2-4 TERRAIN WARN ANNUNCIATEJ2-3 TERRAIN FAILURE ANNUNCIATEJ2-23 SHARED-AUDIO OR LOW ALTUTIDE MODE ANNUCIATEThese annunciations are active when grounded.B. External EGPWS(1) EGPWS ControlJ14-13 EGPWS CTRL 429 TX AJ14-12 EGPWS CTRL 429 TX BThis serial data bus conforms to ARINC 429 electrical characteristics, and is configured for high operating speed.Label 017 (discretes data) is provided on this output of the KSN 7xx to implement the EGPWS control functions.Draft as of 10/15/2012
DraftPage 3-206 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Currently, the KGP 560, MK XXI and KMH-880 EGPWS units will accept label 017 from the KSN 7xx starting with the 003 version of the EGPWS software.Refer to Table 3-7 for the ARINC 429 Label 017 control function availability in EGPWS units.(2) Audio InhibitJ14-24 EXTERNAL AUDIO INHIBIT (LOW TO INHIBIT, OPEN TO ALLOW).This is an input from the external EGPWS system telling the KSN 7xx to stop EGPWS audio annunciations.(3) Terrain DataJ14-9 KCPB RX AJ14-22 KCPB RX BThis serial data bus conforms to ARINC 429 electrical characteristics, and is configured for high operating speed. This allows the KSN 7xx to receive terrain warning information from the external EGPWS.Table 3-7. ARINC 429 Label 017 Control Function Availability in EGPWS UnitsEGPWS UnitMinimum EGPWS Software Revision Level Required to Support ARINC 429 ControlTest Inhibit LO ALT G/S Cancel Steep Approach Flap OverrideKGP-560 003 003 N/A N/A N/A N/AKMH-880 003 003 N/A N/A N/A N/AMK-IVN/AN/AN/AN/AN/AN/AMK-VN/AN/AN/AN/AN/AN/AMK-VIN/AN/AN/AN/AN/AN/AMK-VIIN/AN/AN/AN/AN/AN/AMK-VIII N/A N/A N/A N/A N/A N/AMK-XXI 003 003 003 N/A N/A N/AMK-XXIIN/AN/AN/AN/AN/AN/ANOTE: Currently, no EGWPS unit supports control of G/S cancel, steep approach or flap override through ARINC 429.Draft as of 10/15/2012 include KGP 860Bendix King products don't use hyphens
DraftPage 3-216 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.(4) Position DataJ14-43 LEGACY PXPRESS 232 GNDJ14-63 LEGACY PXPRESS 232 TXThis serial data bus conforms to EIA RS-232 electrical characteristics. This allows the KSN 7xx to transmit position information to the external EGPWS, if required.3.6.5 Interconnect DiagramRefer to Figure 3-4 for the EGPWS interface - internal (growth) interconnect diagram.Refer to Figure 3-5 for the EGPWS interface - external interconnect diagram.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-236 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-4. EGPWS Interface - Internal (Growth) Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-256 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-5. EGPWS Interface - External Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012Figure 3-5 does not call out all of the EGPWS options, like KMH 980 and KGP 860
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DraftPage 3-276 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.7 Traffic Interface3.7.1 Applicable Part NumbersA. TISAll part numbers and software versions perform all published TIS functions.When the TIS is not connected to the KSN 7xx, the pins must be left open.B. TCAS/TASThis function is only available when the optional KSN 7xx WX RDR/EGPWS option board is installed and the associated product feature key is installed. Contact Bendix/King Product Support for the feature key.When the TCAS/TAS is not connected to the KSN 7xx, the pins must be left open.3.7.2 FunctionA. TISTIS is a data link service that provides information similar to VFR RDR traffic advisories received over voice radio. The data is received from the terminal Mode S radar system through the Mode S transponder to the KSN 7xx once per radar scan (approximately every 5 seconds).TIS provides the relative position, relative altitude, altitude trend, and estimated ground track angle for as many as eight intruders that are within 7 nm horizontally and +3500/3000 feet (+1067 to 914 meters) vertically of the aircraft receiving TIS. This function is only available when optional KSN 7xx software is installed.B. TCAS/TASTCAS and TAS are airborne systems used to detect and track aircraft in the vicinity of a particular aircraft through the interrogation of their transponders. Aircraft detected, tracked, and displayed by the TCAS/TAS systems are referred to as intruders.The system then analyzes the transponder replies to determine range, bearing, and relative altitude. If the TCAS/TAS processor determines that a possible collision hazard exists, it issues visual and aural warnings.This function is only available when optional KSN 7xx software is installed.3.7.3 Requirements and LimitationsThe KSN 7xx must be configured for the traffic equipment installed for proper operation. Configuration of each type is covered in Section 4.Draft as of 10/15/2012
DraftPage 3-286 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.7.4 Electrical CharacteristicsA. Traffic ControlJ14-73 TRAFFIC CTRL TX AJ14-53 TRAFFIC CTRL TX BThis serial data bus conforms to ARINC 429 electrical characteristics, and is configured for high operating speed. This is the bus that controls the traffic LRUs.B. Traffic DisplayJ14-69 TRAFFIC DISPLAY 429 RX AJ14-49 TRAFFIC DISPLAY 429 RX BThis serial data bus conforms to ARINC 429 electrical characteristics, and is configured for high operating speed. This is the bus that supplies the KSN 7xx with traffic information to display.C. Traffic Alert Aural AnnunciationJ14-22 TA AURAL ACTIVEAural ON: LowAural OFF: HighThis is a normally open discrete input to the KSN 7xx. This input signals to the KSN 7xx when the traffic alert aural for traffic is active, for audio priority management within the KSN 7xx.D. Traffic Discretes(1) TPU-66A, TPU-67A, KTA 810/910, KMH 820/920J14-2 TRAFFIC DISC 1 OUT (TRAFFIC DISPLAY VALID)Active: LowInactive: HighThese are high current discrete outputs. This output is set up for proper operation on the maintenance pages.For TPU-66A, TPU-67A, KTA 810/910, and KMH 820/920, TRAFFIC DISC 1 OUT is active whenever the KSN 7xx is displaying traffic data. TRAFFIC DISC 2 OUT is not used in these systems, and must remain unconnected.Draft as of 10/15/2012
DraftPage 3-296 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.(2) Skywatch 497J14-2 TRAFFIC DISC 1 OUT (TEST command signal)Normal: HighTest Command: LowJ14-21 TRAFFIC DISC 2 OUT (OPERATE / STANDBY)Operate: LowStandby: HighFor L3 Skywatch 497, TRAFFIC DISC 1 OUT is the test command signal and TRAFFIC DISC 2 OUT is the operate/standby command. This output is set up for proper operation on the maintenance pages.3.7.5 Interconnect DiagramRefer to Figure 3-6 for the traffic interface interconnect diagram.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-316 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-6. Traffic Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-336 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.8 Heading/AHRS Interface3.8.1 Applicable Part NumbersAll part numbers and software revisions perform all Heading/AHRS functions.3.8.2 FunctionConnecting a heading input to the KSN 7xx is optional, but highly recommended. However, the KSN 7xx uses its heading input to orient its map and to compute wind speed, wind direction and drift angle. In addition, the KSN 7xx requires heading to compute both analog and ARINC 429 roll steering, and for moving map overlays of data from heading referenced sensors.A. All part numbers of the following AHRS systems are compatible with the KSN 7xx:• Bendix/King KAH 460• Rockwell Collins AHC 85• Bendix/King KFD-840• Bendix/King KSG-7200• Bendix/King KFD 840• Aspen EFD 1000.B. All part numbers of the following compass systems are compatible with the KSN 7xx:• Aeronetics 9100’s with remote bootstrap synchros• Bendix/King KCS 55A (only with KI 525As with compass bootstrap synchros)• Bendix/King KCS 305, Bendix/King KI 825• Rockwell Collins MCS 65 (only with DGS 65’s with compass bootstrap synchros)• Rockwell Collins PN 101 (only with 331A-3G or 331A-6P indicators with bootstrap synchros)• Rockwell Collins MC 102• Rockwell Collins MC 103• Honeywell Sperry C14.Draft as of 10/15/2012
DraftPage 3-346 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.8.3 Requirements and LimitationsAlthough only one heading source is necessary for computations involving heading, the KSN 7xx will operate properly with any combination of XYZ, RS 232, ARINC 429, and ARINC 429 EFIS heading inputs connected simultaneously. In this case, the KSN 7xx will first look for ARINC 429 true heading (EFIS, IRU or INS label 314) and the internally derived magnetic variation to create magnetic heading; if not available, ARINC 429 magnetic heading (EFIS, AHRS, IRU or INS label 320) is used; if not available XYZ heading is used ( XYZ heading is always assumed to be magnetic). If no other sources of heading are available, RS232 heading is used.If the XYZ heading output of an IRU or INS may be switched between magnetic and true, it must not be connected to the KSN 7xx; use only the ARINC 429 heading for this installation.The KSN 7xx INDICATOR 26 VAC input is used as the reference for detecting the XYZ heading input; both must be the same phase. The KSN 7xx will accept either a superflag format heading valid or a “ground-for-valid” format heading valid. The Maintenance page is used to select the correct format. No damage to the KSN 7xx will occur if configured incorrectly; however the heading data will always be flagged.3.8.4 Electrical CharacteristicsA. AHRS HeadingJ1-66 AHRS 429 RX AJ1-46 AHRS 429 RX BThe AHRS input is for high speed ARINC 429. Low speed ARINC 429 must not be connected to this input.All serial data must conform to ARINC 429, ARINC 704 and ARINC 705 for electrical characteristics, content and transmission interval (high speed bus). The KSN 7xx is configured to know whether an AHRS is connected or not. A system may have many more labels than those listed below. Label 314, true heading, is used if it is available, and combined with the KSN 7xx computed magnetic variation to determine magnetic heading. If true heading is not available from the AHRS, then the input magnetic heading is used.Refer to Table 3-8 for the AHRS labels.Table 3-8. AHRS LabelsLabel Parameter314 True heading320 Magnetic headingDraft as of 10/15/2012
DraftPage 3-356 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.B. XYZ HeadingJ1-21 HEADING VALIDThis pin is configurable on the Maintenance page for either valid high or valid low. An open HEADING VALID pin always indicates invalid.J1-77 HEADING XJ1-58 HEADING YJ1-59 HEADING ZThree-wire XYZ format with Z grounded. Input impedance is no less than 10 kilohms. Maximum lead-to-lead voltage is 11.8 Vrms.NOTE: To accept this input HEADINGVALID (J1-21) must be valid. The 26 VAC used to excite the heading source synchro must be of the same phase as the KSN 7xx 26 VAC reference input.J1-6 HDG REF HIThis is the indicator 26 VAC reference. Input impedance no less than 10 kilohms.J1-7 HDG REF LOThis pin serves as the 26 VAC return. Impedance to AC GND less than 0.1 ohm.3.8.5 Interconnect DiagramRefer to Figure 3-7 for the heading interface - XYZ interconnect diagram.Refer to Figure 3-8 for the AHRS interface interconnect diagram.HI: No less than 18.5 VDC (or two-thirds the voltage applied to the 18-33 VDC AC POWER).Load Resistance: No more than 3.5 VDC. Input impedance no less than 10 kilohms.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-376 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-7. Heading Interface - XYZ Interconnect Diagram (Sheet 1 of 2)Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-386 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-396 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-7. Heading Interface - XYZ Interconnect Diagram (Sheet 2 of 2)Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-406 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-416 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-8. AHRS Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-436 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.9 Altitude/Airdata/Fuel Interface3.9.1 Applicable Part NumbersAll part numbers and software revisions perform all Altitude/Airdata/Fuel functions.3.9.2 FunctionsA. AltitudeAll part numbers of the Bendix/King KEA 346-08 or above, with MOD 3 incorporated, are compatible as a DC precision baro-corrected altitude or baro-setting source with the KSN 7xx through the Analog BARO CORRECTION HI interface.All part numbers of the Bendix/King KEA 130A (not including KEA 130) are compatible as a baro setting source with the KSN 7xx through the analog BARO CORRECTION HI interface.Kollsman-IDC model 519-28702-906 and Smiths model WL 1407/AM/MS 5 or 6 are compatible as a baro setting source with the KSN 7xx through the Analog BARO CORRECTION HI interface.Kollsman-IDC models PD 44929-935, 28704-495, and 28704-XXX are compatible as a baro setting source with the KSN 7xx through the Analog BARO CORRECTION HI interface.The KSN 7xx is capable of receiving barometric altitude data from multiple sources. These include (in order of priority):• ARINC 429/419 digital air data computers (highest priority)• RS-232 digital air data computers• Gillham altitude data (lowest priority). Certain altimeters provide an internal potentiometer that is driven by a baro setting mechanism. The baro setting mechanism can be linear with inches of mercury (kPa) or linear with feet of baro correction. Inches of mercury (kPa) represent the sea level baro metric pressure. The altitude value in feet represents the difference between pressure altitude (gray code altitude) and the baro corrected altitude. The potentiometer must be excited by an external voltage. If two or more devices are monitoring this potentiometer output then only one of them can excite the potentiometer and the other(s) must only monitor the reference input. In some aircraft installations the KSN 7xx will be the only user of the baro setting potentiometer and it will need to supply the excitation. In others, it will share the potentiometer with the flight control system. Some flight control systems must always supply their own excitation. For these systems the KSN 7xx must not supply the excitation but must monitor what the supplied excitation is so that it can divide its value into the value from the potentiometer to determine the potentiometer value.The DC baro setting reference is configurable as input or output based on whether KSN 7xx is going to provide the excitation voltage or monitor the externally supplied excitation voltage.Refer to the maintenance pages on how to set the parameters in the configuration module. There are two major types of DC baro setting outputs on encoding altimeters: Baro set linear and altitude correction linear.Draft as of 10/15/2012
DraftPage 3-446 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.(1) Altitude Function - Baro Set LinearBaro set linear encoding altimeters have a DC output voltage that is linear to the barometric pressure setting (inches of mercury). Encoding altimeter models which use this type of baro correction output include:519-44929-935 (Kollsman-IDC, used on Cessna 525s)519-28704-495 (Kollsman-IDC)(2) Altitude Function - Altitude Correction LinearAltitude correction linear encoding altimeters have a DC output voltage that is linear to the correction from pressure altitude to indicated altitude. Encoding altimeter models which use this type of baro correction output include:KEA 346 (Bendix/King)KEA 130A (Bendix/King)519-28704-5XX (Kollsman-IDC)B. AirdataThe -0200 and -0300 part numbers of the B&D 2600 transmit data too slowly to be compatible with the KSN 7xx. These units may be converted to -0600 and -0700 part numbers respectively, which are compatible with the KSN 7xx. All other part numbers of the B&D 2600 are compatible with the KSN 7xx.All part numbers of the B&D 2601, B&D 2800, and BENDIX/KING KDC -481 are compatible with the KSN 7xx through the ARINC serial airdata interface using ARINC 429.All part numbers of the Rockwell Collins ADC 81A and ADC 82 are compatible with the KSN 7xx through the ARINC serial airdata interface using ARINC 575-3.The following models of the Rockwell Collins ADC 80 are compatible with the KSN 7xx through the ARINC serial airdata interface using ARINC 575-3, and transmit all airdata labels:The following models of the Rockwell Collins ADC 80 are compatible with the KSN 7xx through the ARINC serial airdata interface using ARINC 419 (575-3); however, they only transmit label 210, TRUE AIRSPEED.ABCDE -G- I JKLM- - -Q-----F-H------N--Draft as of 10/15/2012
DraftPage 3-456 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.The KSN 7xx can be configured to receive RS-232 serial air data in one of two different formats:• Format C-Fuel and Airdata• Format D-Fuel and Barometric Airdata.The format of the RS-232 data can be configured in the Maintenance pages.Barometric altitude information is used for aiding the GPS receiver in acquiring and tracking its position, ensuring the accuracy of RAIM calculations (outside of SBAS coverage),for altitude alerting functions, and for advisory VNAV calculations.True airspeed is used to compute winds aloft.C. Fuel FlowThe KSN 7xx may be interfaced to fuel flow systems with a separate fuel flow indicator for enhanced flight planning.3.9.3 Requirements and LimitationsA. Altitude/AirdataA source of true airspeed is optional. With an airspeed input, an automatic winds aloft calculation is provided. True airspeed may be entered manually when it is not provided electrically.A source of barometric altitude is required for GPS installations certified for IFR.The KSN 7xx accepts analog altitude inputs which utilize DC excitation only. Certain aircraft are wired to excite altimeters with 400 Hz AC, and the KSN 7xx is not compatible with these installations.The KSN 7xx DC altitude resolution is such that you may see as much as 200 feet (61 meters) of error between the altimeter and the altitude displayed on the KSN 7xx. This performance is acceptable for aiding the GPS receiver, but is marginal if VNAV or altitude alerting are to be used.Some Airdata computers require up to ten minutes warm-up time. This can result in an ALTITUDE FAIL message on the KSN 7xx during the Airdata warm-up period. Connecting to a gray code altitude source that does not require warm-up will prevent this message as the KSN 7xx will revert to the gray code source until the airdata becomes valid.B. Fuel FlowThe KSN 7xx receives fuel flow information from external equipment over the AIRDATA/FUEL/HDG 232 RX bus. It can receive one fuel flow from each of up to two engines.Draft as of 10/15/2012
DraftPage 3-466 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.9.4 Electrical CharacteristicsA. Gillham AltitudeGillham Altitude InputJ2-13 D4J2-34 A1J2-35 A2J2-49 A4J2-17 B1J2-54 B2J2-53 B4J2-45 C1J2-18 C2J2-31 C4These inputs are active low, and conform to the requirements of ARINC 575-3, Attachment 5.NOTE: Some receivers of the altitude encoder do not have internal isolation diodes to prevent the unit from pulling the encoder lines to GND when the unit is OFF. The KSN 7xx has diodes internal to the unit. However, some transponders and other devices do not have the internal diodes. These units require a diode to be added to the installation harness for every encoder line. The diodes are inserted at the connection to the unit that does not have internal diodes. The anode is on the receiving unit’s side and the cathode is on the encoder side. A set of diodes is required for each unit without internal diodes.B. Analog Baro CorrectionJ2-8 BARO CORRECTION HIJ2-28 BARO CORRECTION LOThese pins are configured on the maintenance pages for input of either DC altitude or DC barometric correction. This is an altimeter potentiometer voltage. The most positive lead of the potentiometer must be connected to BARO CORRECTION HI (i.e. if the potentiometer is excited with a negative voltage, the lead with the negative voltage must be connected to BARO CORRECTION LO).If the BARO CORRECTION inputs are used for baro correction, the maintenance page must be configured properly. Some altimeters output a baro correction voltage that is linear with inches of mercury barometric pressure. Others output a voltage that is linear with the altitude correction between pressure altitude and indicated altitude. Refer the installation manual for the piece of equipment being connected for more information.HI: A voltage of not less than 10.0 volts relative to AC GND or a resistance to AC GND of not less than 100 kilohms.LO: A voltage of not more than 1.9 volts relative to AC GND or a resistance to AC GND of not more than 375 ohms.Draft as of 10/15/2012
DraftPage 3-476 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Maximum differential input voltage: 21 voltsMaximum voltage to GND (each side): 13.5 voltsInput impedance: 420 kilohmsJ2-48 AIRDATA REFERENCE HIJ2-67 AIRDATA REFERENCE LOThese pins always read the voltage used to excite an altimeter’s potentiometer. If no other source in the aircraft is exciting the potentiometer, the KSN 7xx may be configured to excite the potentiometer through these pins. If this is the case, the following apply:AIRDATA REFERENCE HI is +9.0 volts referenced to AIRDATA REFERENCE LO.Maximum differential input voltage: 21 voltsMaximum voltage to GND (each side): 13.5 voltsInput impedance: 420 kilohmsMinimum output load impedance: 2 kilohmsNOTE: Although current limiting is provided internal to the KSN 7xx, damage could occur if the KSN 7xx is configured to excite the potentiometer at the same time another source is exciting it. In addition, the analog airdata interface will not function properly in this case.C. ARINC Serial Airdata InputJ2-46 BARO ALT 429 AJ2-65 BARO ALT 429 BThis input is for high speed ARINC 429. Low speed ARINC 429 must not be connected to this input.If the airdata source broadcasts a label used by the KSN 7xx with the SSM set to failure warning, then the ARINC 429 AIRDATA FAIL message will appear. An example of this is when the BENDIX/KING KDC 481 airdata computer broadcasts TAS with the SSM set to failure warning upon its determination that the temperature probe is not connected.A system may have many more labels than those listed. Selection of ARINC 429 or ARINC 419 is done in the maintenance pages.All versions of the KSN 7xx accept the following ARINC 429 serial airdata labels as shown in Table 3-9.Table 3-9. ARINC 429 Serial Airdata Labels429 Label Parameter203 Altitude (1013.25 mB)204 Barometer corrected altitude #1205 MACH (reserved for growth)206 Computed airspeed210 True airspeedDraft as of 10/15/2012
DraftPage 3-486 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.All versions of the KSN 7xx accept the following ARINC 419 (575-3) serial airdata labels shown in Table 3-10.D. RS 232 Serial Airdata InputJ1-61 AIRDATA/FUEL/HDG 232 RXThis signal is referenced to AC GND. It is an EIA RS-232 format serial bus. All versions of the KSN 7xx will receive RS 232 Airdata in either "Format C" or "Format D".When PRESSURE ALTITUDE, BAROMETRIC SETTING, and BARO-CORRECTED ALTITUDE are all available, pressure altitude and baro-corrected altitude are used to calculate the baro setting displayed on the KSN 7xx (rather than the KSN 7xx displaying the RS 232 BAROMETRIC SETTING).211 Total air temperature212 Altitude rate213 Static air temperatureTable 3-10. ARINC 429 Serial Airdata Labels429 Label Parameter203 Altitude (1013.25 mB)204 Barometer corrected altitude #1205 MACH210 True airspeed211 Total air temperature213 Static air temperatureTable 3-9. ARINC 429 Serial Airdata Labels429 Label ParameterDraft as of 10/15/2012
DraftPage 3-496 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.E. Outside Air Temperature (OAT) Input (Growth)J2-69 OAT+J2-68 OATThe OAT probe is used to correct internal TAWS altitude.The KSN 7xx is capable of interfacing directly to a standard 500-ohm temperature probe for aircraft operated in cold environments. Very cold air temperatures cause an increase in the density of the air mass and can result in barometric altimeter errors, both in sensitive altimeters/encoders and blind encoders. Aircraft normally operated in very cold climates can benefit from the addition of an OAT probe interfaced to the KSN 7xxThe Bendix/King OAT temp probe Kit is PN 050-03610-0002.3.9.5 Interconnect DiagramsA. Altitude InterfaceRefer to Figure 3-9 for the altitude interface interconnect diagram.B. Airdata/OAT InterfaceRefer to Figure 3-10 for the airdata/OAT interface interconnect diagram.C. Fuel Flow/Airdata InterfaceRefer to Figure 3-11 for the fuel flow/airdata interface interconnect diagram.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-516 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-9. Altitude Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-536 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-10. Airdata/OAT Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-556 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-11. Fuel Flow/Airdata Interface Interconnect Diagram (Sheet 1 of 2)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-576 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-11. Fuel Flow/Airdata Interface Interconnect Diagram (Sheet 2 of 2)Draft as of 10/15/2012
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DraftPage 3-596 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.10 Flight Control Interface3.10.1 Applicable Part NumbersAll part numbers and software revisions perform all flight control functions.3.10.2 FunctionA. GPSThree different interface methods exist to couple the KSN 7xx GPS function to an automatic flight control system. For lateral guidance, roll composite steering is provided which conforms to the ARINC 561 format for enroute/terminal use and has increased authority for approach arm and approach active modes. It is provide in ARINC 429, and an analog AC or DC command. If roll steering is not supported with the autopilot, analog course datum and D-bar signals may be used with or obtained from an HSI or NAV indicator connected to the KSN 7xx. For SBAS approaches ILS type vertical and lateral commands are generated in both analog deviations and ARINC 429 formats.B. VHF NAV (KSN 7x0 Only)For VHF NAV guidance based operation, LOC/VOR/GS outputs are provided in analog deviation/OBS resolver, an analog composite NAV output, and a dedicated ARINC 429 bus. A built in VHF NAV/GPS switching function for the analog deviations (lateral and vertical) outputs is incorporated internally, so that external switching is not required in the aircraft between GPS and VHF NAV sources.An ARINC 429 interface facilitates connection with numerous flight control systems.3.10.3 Requirements and LimitationsA. ARINC 429All part numbers of the Bendix/King KFC 400 are compatible with the KSN 7xx.The following part numbers of the KFC 275 and KFC 325 are compatible with the KSN 7xx ARINC 429 roll steering through the Bendix/King EFIS 40/50 when the KSN 7xx is installed for IFR non-precision approaches:KCP 220 065-0064-The following part numbers of the Bendix/King KFC 275 and KFC 325 flight control systems are compatible with the KSN 7xx ARINC 429 roll steering through the Bendix/King EFIS 40/50 when the KSN 7xx is not installed for IFR non-precision approaches:01 05 06 07 0815 --Draft as of 10/15/2012
DraftPage 3-606 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.KCP 220 065-0064-B. Roll Composite SteeringAll part numbers of the Rockwell Collins APS 65, and Bendix/King KFC 275 and KFC 325 are compatible with the KSN 7xx.The following part numbers of the Bendix/King KFC 275 and KFC 325 flight control systems are compatible with the KSN 7xx roll composite steering when the KSN 7xx is installed for IFR non-precision approaches:KCP 220 065-0064-The following part numbers of the Bendix/King KFC 275 and KFC 325 flight control systems are compatible with the KSN 7xx roll composite steering when the KSN 7xx is not installed for IFR non-precision approaches:KCP 220 065-0064-KSN 7xx interface to a flight control system is optional.If the KSN 7xx installation is to be certified for GPS/SBAS approaches and the aircraft’s flight control system uses course datum and analog deviation signals from the KSN 7xx, then use of the FCS LOCALIZER ENGAGE signal is strongly recommended. This KSN 7xx output is active when the KSN 7xx is in approach active mode and when the pilot manually sets the CDI scale to 0.3 nm, and is equivalent in function to an ILS energize signal in that it indicates approach autopilot gain scheduling is required.01 05 06 07 0815 162001 05 06 07 0815 --01 05 06 07 0815 1620Draft as of 10/15/2012
DraftPage 3-616 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.For enroute/terminal operations, roll composite steering is the preferred method of coupling to a flight control system. If flight control coupling is made using course datum and D-bar and the KSN 7xx cannot drive the course selector and the pilot will need to make manual course adjustments encountered in the flight plan. For the roll steering to function on the KSN 7xx a heading source must be connected to the KSN 7xx.The pilot must be made aware of the problems that can occur if the course selector is not manually updated as with simple course deviation indicators and HSIs without remote course select. The flight control system will be able to remain on course (CDI centered) if the combination of both the selected course error and the current cross-wind correction does not exceed the autopilot’s cross-wind correction authority which is typically 30 degrees. Once the cross-wind correction authority limit of the autopilot has been reached the autopilot will begin to fly the CDI with a constant offset.The size of the offset is proportional to the degree which the authority limit has been exceeded.Any bank angle limiting of less than 25 degrees within the flight control system will cause overshooting of the waypoint due to the KSN 7xx turn anticipation algorithm assuming a 25 degrees bank angle turn.FCS LOCALIZER ENGAGE is used to make an interfaced flight control system track more appropriately when the KSN 7xx is in approach active mode. Hookup is required if autopilot-coupled GPS approaches will be flown using course datum and D-bar from the KSN 7xx.For the roll steering to function on the KSN 7xx an ARINC 429 or XYZ heading source must be connected to the KSN 7xx.NOTE: In the cases of the following ports, unused pins must be configured as “NONE” or “N” on the maintenance pages for proper operation. Open pins configured as being used will flag data and may generate failure messages:3.10.4 Electrical CharacteristicsA. ARINC OutputJ1-71 GPS GAMA 429 TX AJ1-51 GPS GAMA 429 TX BThis output is shared with the ARINC position interface. Refer to Paragraph 3.4.4 Electrical Characteristics for details.Flight computer information is broadcast on this bus. The roll steering output is groundspeed scheduled. If there is no GPS groundspeed, 0 degree will be commanded by label 121, roll steering command. Post-installation checkout is facilitated by data output during self-test.While the self-test page is displayed on the KSN 7xx, label 121 goes through the following cycle continuously:NOTE: The output is 0 degree for 6 seconds, then ramps up to 5 degrees at 1 degree/sec. The output is then stable at 5 degrees for 6 seconds. The output then ramps down to 0 degree at 1 degree/sec.Draft as of 10/15/2012
DraftPage 3-626 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.B. 26 VAC Reference InputJ2-30 ROLL STEER REF HI (26 VAC REFERENCE)J2-29 ROLL STEER REF LOThe KSN 7xx ROLL STEER REF HI input is a 26 VAC signal and is used to provide a phase reference for the KSN 7xx steering output. This signal is independent of the 26 VAC phasing signal used for the indicator interface.Input impedance is no less than 10 kilohms.C. Roll Steering Command OutputJ2-10 ROLL STEER+J2-9 ROLL STEERBased on the configuration module, the KSN 7xx will output either a commanded bank angle or a commanded turn rate. This output is groundspeed scheduled. If there is no GPS groundspeed, 0 degree will be commanded.(1) Commanded Bank Angle (DC)(2) Commanded Turn Rate (DC)Scale: 550 mV/degree (of bank).Accuracy: Less than the greater of 0.3 degree or 5% of the commanded bank angle.Voltage Range: 13.75 VDCResolution: 0.125 degree or moreUpdate Rate: 10 Hz or greaterPolarity: Angles between 0 and 180 degrees (commanding a right turn) are positive angles between 180 and 360 degrees (commanding a left turn) are negative.Scale: 2V/degree per second (positive right turn) Accuracy: No worse than 5% of the full scale: 0.3 dps, or 600 mVVoltage Range: 13.75 VDCResolution: 0.05 degree per second, or 92 mVUpdate Rate: 10 Hz or greaterPolarity: Angles between 0 and 180 degrees (commanding a right turn) are positive angles between 180 and 360 degrees (commanding a left turn) are negative.Draft as of 10/15/2012
DraftPage 3-636 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.D. Steering Superflag OutputJ2-59 ROLL STEER VALIDE. GPS/LOC Approach OutputJ2-22 GPS/LOC APPROACHThis is an open collector output. When active, the output device is turned on and conducting which provides a GND path for a load such as a lamp or relay which is pulled up to a maximum voltage of +38 VDC.Connection of this output is not required when roll steering is used. No localizer output from any unit must be connected directly to the flight control system. The GPS/NAV relay, or other relays, must insure that only the navigation source that is driving the flight control system is driving the localizer energize input. In addition, the KSN 7xx GPS/LOC APPROACH logic must not drive the localizer energize input on an RMI or HSI as this could park the RMI pointer or remove the TO/FROM indicator when the KSN 7xx is in approach active mode.F. Remote Go Around InputJ2-72 REMOTE GO AROUND (Growth)This input is normally OPEN and is activated with a momentary LOW.G. GPS Steering Select OutputJ2-77 GPS STEERING SELECTThis is a high current discrete output. This output may be used by a flight control system to activate the flying of roll steering commands during the enroute portion of the flight.Valid: HI (18.0 VDC when 18 to 33 volts AC POWER 24.8 volts.10 VDC when 18 to 33 volts AC POWER 12.4 volts); maximum current 250 mA.Invalid: LO (No more than +3.5 VDC)Draft as of 10/15/2012
DraftPage 3-646 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.10.5 Interconnect DiagramA. Roll Composite SteeringRefer to Figure 3-12 for the flight control interface - roll composite steering interconnect diagram. B. Deviation/Course DatumRefer to Figure 3-13 for the flight control interface - deviation/course datum interconnect diagram.C. DCRefer to Figure 3-14 for the flight control interface - DC interconnect diagram.D. ARINC 429Refer to Figure 3-15 for the flight control interface - ARINC 429 interconnect diagram.Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-656 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-12. Flight Control Interface - Roll Composite Steering Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-676 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-13. Flight Control Interface - Deviation/Course Datum Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-696 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-14. Flight Control Interface - DC Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-716 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-15. Flight Control Interface - ARINC 429 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-736 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.11 DME Interface3.11.1 Applicable Part NumbersThe KSN 7x0 are DME.All part numbers and software revisions perform all DME functions.3.11.2 FunctionThe SERIAL CLOCK, DATA, SYNC bus may be used to drive distance, groundspeed, and time-to-go indicators. This is a King Serial DME bus only.King Serial DME allows display of the KSN 7xx distance, groundspeed, and time-to-go on Bendix/King KDI-572 and KDI-574 DME indicators.The ARINC TRANSMITIER (ARINC 429) bus may be configured for high-speed or low-speed on the Maintenance pages, and contains a large variety of labels that may be used by many different receivers. Transmission of distance, groundspeed, and time-to-go is discussed in this chapter.3.11.3 Requirements and LimitationsFor proper functioning of the King Serial DME indicator interface, a DME receiver (in addition to the KSN 7xx and the indicator) must be connected to the SERIAL CLOCK and SERIAL DATA lines.When the KSN 7xx is mounted in the aircraft pedestal, some certification agencies (including the FAA) require a distance display in the pilot's scan area for IFR certification. Consult your approval agency for additional information.The KSN 7xx may display distance, groundspeed and time-to-station on the KPI-553A, KDI-572, KDI-573 and KDI-574 DME distance displays. The DME in the aircraft continues to supply power to these displays while the KSN 7xx information is displayed. A NAV/GPS annunciator switch and relays can switch the DME display between displaying DME and GPS information (refer to the DME installation documentation for details).3.11.4 Electrical CharacteristicsA. ARINC 429 TransmitterJ1-72 VOR/ILS TX AJ1-52 VOR/ILS TX BThis serial data bus conforms to ARINC 429 electrical characteristics, and may be configured for low-speed on the Maintenance pages. Many ARINC 429 labels are output on the ARINC TRANSMITTER bus. ARINC 429 labels relating to the distance indicator interface are shown in Table 3-11.Draft as of 10/15/2012
DraftPage 3-746 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.B. King Serial DME BusJ1-75 SERIAL CLOCKJ1-57 SERIAL DATAJ1-76 DME CHANNEL REQUESTJ1-56 DME COMMONThese connections transmit Bendix/King format serial DME information.In the King Serial DME configuration, SERIAL SYNC is an input. When the KSN 7xx receives an active-high pulse on SERIAL SYNC, it transmits pulses on the SERIAL CLOCK and SERIAL DATA lines.3.11.5 Interconnect DiagramRefer to Figure 3-16 for the DME interface - remote interconnect diagram.Refer to Figure 3-17 for the DME interface - panel mount interconnect diagram.Refer to Figure 3-18 for the DME interface - ARINC 429 interconnect diagram.Table 3-11. ARINC 429 LabelLabel Parameter Type001 Distance to go BCD002 Time to go BCD012 Groundspeed BCD251 Distance to go Binary252 Time to go Binary312 Groundspeed BinaryDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-756 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-16. DME Interface - Remote Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012Figure 3-16 & 17 The DME interface cannot work as drawn. It has the RNAV/Channel Request and DME Channel Request confused and shown incorrectly. There is no DME Channel request. There is an RNAV/Channel Request and a DME Request and they are different functions.
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-766 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-776 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-17. DME Interface - Panel Mount Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012Figure 3-16 & 17 The DME interface cannot work as drawn. It has the RNAV/Channel Request and DME Channel Request confused and shown incorrectly. There is no DME Channel request. There is an RNAV/Channel Request and a DME Request and they are different functions.
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-786 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-796 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-18. DME Interface - ARINC 429 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012Figure 3-18 cannot work. This is mixture of King Serial and ARINC 429.
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DraftPage 3-816 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.12 NAV Indicator Interface3.12.1 Applicable Part NumbersAll part numbers and software revisions perform all NAV indicator functions. The comosite indicator interface is only available in KSN 7x0 models.3.12.2 FunctionThe NAV indicator displays the lateral deviation from selected course, TO/FROM indications, and NAV flag (both meter level and superflag). In addition, the KSN 7xx includes outputs for vertical deviation, meter flag, and superflag.The KSN 7xx has the ability to read selected course from the NAV indicator. The selected course is used by the KSN 7xx in both the leg and OBS modes. In OBS mode, the NAV indicator selected course is input as the GPS selected course, eliminating the need for the pilot to select the course on both the indicator and the KSN 7xx. In Leg mode, the KSN 7xx notifies the pilot when there is a discrepancy of 5 degrees or more between the KSN 7xx magnetic desired track and the NAV indicator selected course.An input called GPS DISPLAYED tells the KSN 7xx whether its navigation information is presently being displayed on the NAV indicator and consequently whether the NAV indicator selected course must be used by the KSN 7xx.The KSN 7xx provides selected course drive capability for EFIS. Slewable NAV indicators (XYZ or SIN/COS drive) may be driven by the KSN 7xx. When interfaced with nonslewable NAV indicators, the pilot is directed with messages to manually move the course selector to match the selected course displayed on the KSN 7xx.3.12.3 Requirements and LimitationsIFR certified installations of the KSN 7xx are required to have a NAV indicator installed, and it must be located in the pilot’s primary scan area. RS-232 receivers may not be used as the primary flight display for the KSN 7xx.Selected course may be input as OBS SIN/COS, RS 422, or ARINC 429. Only one of the three possible interfaces can be connected in the aircraft.GPS DISPLAYED must be connected if the selected course is input as OBS SIN/COS or RS 422.GPS DISPLAYED is not required if selected course is input as ARINC 429 into the EFIS RECEIVER. In addition, the Maintenance page must be configured for OBS RESOLVER: Y, for the OBS SIN/COS inputs to be used.KPI 552, KPI 553, and KPI 553A units which interface with Bendix/King KNR-665A or KNR-615 units do not have course selection knobs. Some certification agencies require entry of OBS selected course on the CDI/HSI.NOTE: In the cases of the following ports, unused pins must be configured as “None” or “N” on the Maintenance pages for proper operation. Open pins configured as being used will flag data and may generate failure messages:Draft as of 10/15/2012
DraftPage 3-826 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.12.4 Electrical CharacteristicsA. DeviationJ1-29 LATERAL DEVIATION RIGHTJ1-10 LATERAL DEVIATION LEFTJ1-31 VERTICAL DEVIATION UPJ1-12 VERTICAL DEVIATION DOWND-Bar sensitivity depends on the navigation mode and is indicated in Table 3-12.B. Meter Level FlagsJ1-28 LATERAL DEV FLAG+J1-9 LATERAL DEV FLAGJ1-30 VERTICAL DEV FLAGJ1-11 VERTICAL DEV FLAGRange: 300 mVDC.Load Resistance: 200 ohms in parallel with a capacitance of 0.01 F.Resolution: 1.5 mV.Accuracy: less than the greater of 4.5 mV or 5% of commanded deviation.Update Rate: 10 Hz or greater.Table 3-12. TBDMode D-Bar SensitivityEn Route 30.0 mVDC/NMApproach Arm (ARM) 150.0 mVDC/NMApproach Active (ACTV) 500.0 mVDC/NMValid: HI (voltage at FLAG+ is no less than +350 mV and no more than +900 mV with respect to FLAG).Invalid: LO (voltage at FLAG+ is within 50 mV of the voltage at FLAG). Flag current is 0 50 A.Load Resistance: 200 ohms in parallel with a capacitance of 3 nF.Update Rate: 10 Hz or greater.Draft as of 10/15/2012
DraftPage 3-836 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.C. NAV SuperflagsJ1-13 LATERAL DEVIATION SUPERFLAGJ1-32 VERTICAL DEVIATION SUPERFLAGD. TO/FROM FlagJ1-27 CDI TOJ1-8 CDI FROMCDI TO and CDI FROM are within 5 mVDC when LATERAL DEVIATION FLAG is in the invalid state. CDI TO shall be 40 to 900 mV with respect to CDI FROM when the desired course is within 85 degrees of the bearing to active waypoint. CDI TO must be 100 to 900 mV with respect to CDI FROM when the desired course is 180 8.5 degrees with respect to the bearing to the active waypoint.Valid: HI (+18.0 VDC when aircraft power 24.8 VDC; (+10.0 VDC when aircraft power 12.4 VDC). Maximum current allowed is 250 mA.Invalid: LO (No more than +3.5 VDC).Update Rate: 10 Hz or greater.TO Flag: +TO is positive with respect to +FROMFROM Flag: +FROM is positive with respect to +TORange: +40 to +900 mV with respect to the CDI FROM output when in the TO state.40 to 900 mV with respect to the CDI FROM output when in the FROM stateLoad Resistance: 40 ohms in parallel with a capacitance of 3 nF.Accuracy: Within 5 mV of the CDI FROM output whenever the NAV FLAG is in the "not valid" (including "OFF state" for LOC) state.Update Rate: 10 Hz or greater.Draft as of 10/15/2012
DraftPage 3-846 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.E. SIN/COS OBS InputJ1-34 OBS F (SIN HI)J1-54 OBS D (COS HI)This is an AC SIN/COS OBS input, indexed at 300 degrees. Nominal input impedance 36.5 kilohmseach line. This interface is compatible with indicators that are EZ at 300 degrees and indicators that are ORZ at 300 degrees. This interface will operate properly with either "0.85 gain" or "0.41 gain" resolvers with no special programming requirements.Refer to the Maintenance pages for the indicator calibration procedure.F. OBS Excitation OutputJ1-14 OBS H (REF HI)J1-74 OBS C (REF LO)G. ARINC Selected Course InputJ1-68 EFIS CTRL 429 RX AJ1-48 EFIS CTRL 429 RX BAll serial data conforms to ARINC 429 for electrical characteristics, content and transmission interval.Input Impedance: 10 kilohmsResolution: 0.25 degree.Accuracy: 1 degree.Update Rate: 5 Hz.Amplitude: Unloaded peak amplitude of 5.8 volts 15%.Wave Form: 400 Hz 20% sin wave.Load Resistance: 10 ohms10%, or one Bendix/King 148-00043-0000 in parallel with 0.56 F (5%).Current Source: Minimum of 40 mA to a resistive load terminated at OBS_C.Draft as of 10/15/2012
DraftPage 3-856 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.All versions of the KSN 7xx accept the following ARINC 429 labels as shown in Table 3-13.H. NAV Composite Interface (KSN 7x0 models only)J1-60 VOR/LOC COMPOSITE OUTJ1-48 VOR/LOC COMPOSITE OUT REFThis is a standard localizer composite signal containing two tones whose nominal frequencies are 90 Hz and 150 Hz. 3.12.5 Interconnect DiagramA. Deviation and Flags InterfaceAll part numbers of the Bendix/King models KI 202, KI 206, KI 525A, KPI 552/B, KPI 553/A/B, and IN 863A, Rockwell Collins models HSI 84, 331A-6P and 331A-9G, and Honeywell Sperry models RD 550A and RD 650 are compatible with the KSN 7xx deviation and flags interface.Refer to Figure 3-21 for the NAV indicator interface - deviation and flag interconnect diagram.B. OBS Resolver InterfaceAll part numbers of the Bendix/King models KI 202, KI 206, KI 525A, KPI 552B and IN 863A, Rockwell Collins models HSI 84, 331A-6P and 331A-9G, and Honeywell Sperry models RD 550A and RD 650 are compatible with the KSN 7xx OBS resolver interface.The following part numbers of Bendix/King KPI 553 and 553B are compatible with the KSN 7xx OBS Resolver interface:Table 3-13. ARINC 429 LabelsLabel Parameter100 Selected course306 NAV/WPT/APT latitude307 NAV/WPT/APT longitude314 True heading320 Magnetic headingRange: 300 to 500 mVRMS. 350 mVRMS into a 47 kilohms load (factory setting).Accuracy: 9% of the set point.Update Rate: 10 Hz.Draft as of 10/15/2012
DraftPage 3-866 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.KPI 553 066-3027-KPI 553B 066--3069-The 30 Hz-only part numbers of Bendix/King KPI 552/B and KPI 553/A require a modified interconnection. This interconnection requires the use of a spare winding on the resolver.Some units may have been produced from the factory with the connections to this winding reversed. These units will not work correctly if connected as shown on the alternate interconnect for the 30 Hz only KPI 552/B and the KPI 553/A. The majority of the units will work properly when wired per the primary drawing, and this interface must be attempted first. No damage will occur to the units in either configuration however, the wrong configuration will result in the KSN 7xx OBS display incrementing when the OBS decrements, and vice versa. The following part numbers are compatible with the KSN 7xx OBS resolver interface:KPI 552 066-3024-KPI 553 066-3027-------1617------2425----00 - 02 03 - 05 08 -1011 - 13 17181920---- --- - ----10 12 13 - 15 - - 18 -2021-23- -26Draft as of 10/15/2012
DraftPage 3-876 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.KPI 553A 066-3045-Refer to Figure 3-19 for the NAV indicator interface - OBS 1 interconnect diagram.Refer to Figure 3-20 for the NAV indicator interface - OBS 2 interconnect diagram.C. ARINC 429 NAV Indicator InterfaceAll part numbers of the Bendix/King model KA 90 are compatible with the KSN 770 ARINC 429 NAV Indicator interface.The Bendix/King model KA 90, PN 071-01508-0202, with software MOD status 02/02, provides a warning through the KSN 770 if it loses the 400Hz power source.Bendix/King models SG 464 and SG 465 with software release 11 and above are compatible with the KSN 7xx ARINC 429 NAV Indicator interface when the KSN 7xx is to be used for non-precision approach operations. Symbol generators with software below release 11 will not correctly display the KSN 7xx variable deviation scale factors, but are compatible when the KSN 7xx is not configured for non-precision approach operations.If two KSN 7xx units are to be interfaced to a single EFIS symbol generator, the SG 464 or SG 465 must have software release 08 or above. The KSN 7xx uses the SDI bits in label 100 SELECTED COURSE to determine which KSN 7xx’s selected course must be changed by the EFIS. In addition, the #2 KSN 7xx’s SDI configuration must be set to “2” on the maintenance pages for proper EFIS receiver operation.Refer to Figure 3-22 for the NAV indicator interface - ARINC 429 interconnect diagram.D. Composite Indicator InterfaceRefer to Figure 3-23 for the NAV indicator interface - composite interconnect diagram (KSN 7x0 models only).10 - 12 13 - 15 18 -20 21 - 23 26---- ----Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-896 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-19. NAV Indicator Interface - OBS 1 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-916 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-20. NAV Indicator Interface - OBS 2 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-936 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-21. NAV Indicator Interface - Deviation and Flag Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-956 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-22. NAV Indicator Interface - ARINC 429 Interconnect Diagram (Sheet 1 of 2)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-976 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-22. NAV Indicator Interface - ARINC 429 Interconnect Diagram (Sheet 2 of 2)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-996 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-23. NAV Indicator Interface - Composite Interconnect Diagram (KSN 7x0 Models Only) (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1016 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.13 RMI/OBI Interface3.13.1 Applicable Part NumbersAC SIN/COS OBI and XYZ RMI information functions are only available when the KSN 7xx is interfaced to a Bendix/King KA 90 (PN 071-01508-02XX only) or a Bendix/King KDA 697.3.13.2 FunctionThe KSN 7xx provides bearing information TO the active waypoint in two ways:Serial OBI (OBI CLOCK, OBI DATA, OBI SYNC) and ARINC TRANSMITTER (A and B).The ARINC TRANSMITTER function and the SERIAL TRANSMITTER function are discussed in Paragraph 3.11 DME Interface.3.13.3 Requirements and LimitationsDisplay of KSN 7xx RMI/OBI information in the aircraft is optional. Annunciators, placards, or a supplement to the aircraft flight manual must clearly indicate the available sources and switching procedures for bearing pointers that are shared with other systems. An example of this would be a NAV/GPS relay switching a bearing pointer from the KSN 7xx bearing to the VOR bearing. It may not be possible to certify an installation that displays non-VOR bearing information on older RMIs or HSIs with selectors or flags labeled “VOR”.A Bendix/King KA 90 (PN 071-01508-02XX only) or a Bendix/King KDA 697 interface is required to provide bearing data in AC SIN/COS and XYZ RMI formats.3.13.4 Electrical CharacteristicsJ1-5 OBI DATAJ1-25 OBI CLOCKJ1-4 OBI SYNCThis is Bendix/King format serial OBI information.J1-4 OBI SELECT INThe KSN 7xx will output GPS OBI when this input is Open, and VOR OBI when the input is GND.3.13.5 Interconnect DiagramAll part numbers of the Bendix/King KNI 582 and KI 229 RMIs and the KDA 692 RMI adapter are compatible with this interface.Refer to Figure 3-24 for the RMI/OBI interface interconnect diagram.Draft as of 10/15/2012
DraftPage 3-1026 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1036 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-24. RMI/OBI Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1056 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.14 Dual System Interface (Cross-Fill)3.14.1 Applicable Part NumbersAll part numbers and software revisions perform all dual system interface functions.3.14.2 FunctionWhen two KSN 7xx’s are installed in an aircraft, they may be connected so they will cross-fill flight planning information between them.3.14.3 Requirements and LimitationsThe user data cross-fill function eliminates repetitive work such as creating flight plans and user waypoints on two individual KSN 7xx. The two units must both be KSN 7xx for the user data cross-fill to operate3.14.4 Electrical CharacteristicsJ4-6 KSN 7xx 422 TX AJ4-7 KSN 7xx 422 TX BJ4-24 KSN 7xx 422 RX AJ4-25 KSN 7xx 422 RX BThese are standard EIA-422 data busses.3.14.5 Interconnect DiagramRefer to Figure 3-25 for the dual system interface interconnect diagram.Draft as of 10/15/2012
DraftPage 3-1066 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1076 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-25. Dual System Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1096 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.15 Audio Interface3.15.1 Applicable Part NumbersAll part numbers and software revisions perform all audio interface functions.3.15.2 FunctionThe KSN 7xx provides audio information to the pilot for the alert audio.3.15.3 Requirements and LimitationsThe audio interface provides audio alerts based on EGPWS and internal SBAS terrain generated warnings.3.15.4 Electrical CharacteristicsJ4-16 AUDIO ALERT OUT HIJ4-35 AUDIO ALERT OUT LOThis is an analog output from the KSN 7xx with the following characteristics:3.15.5 Interconnect DiagramRefer to Figure 3-26 for the audio interface 1 interconnect diagram.Refer to Figure 3-27 for the audio interface 2 interconnect diagram.Impedance: 500 50 ohmsOutput Power: 10 mW RMS into 500 ohmsat 1 kHzFrequency Response: Less than 3 dB variation from 350 Hz to 2.5 kHz by 20 dB relative to a 1 kHz tone. Frequencies below 200 Hz and above 10 kHz are attenuated.Distortion: Less than 10% at rated audio and less than 3% at 10% of rated audio from 300 Hz to 2.5 kHz.Noise Level: Minimum of at least 50 dB below rated output.Protection: Electrically isolated by an audio transformer.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1116 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-26. Audio Interface 1 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012Figure 3-26 has the Audio Hi and Lo tied together. We cannot tie the Hi's and Lo's together.
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1136 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-27. Audio Interface 2 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1156 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.16 Annunciations - Suspend/Dead Reckoning/NAV Interface3.16.1 Applicable Part NumbersAll part numbers and software revisions perform all annunciatons - suspend/dead reckoning/NAV functions.3.16.2 FunctionA. SuspendWhen in the suspend mode, the KSN 7xx will suspend automatic sequencing of waypoints.SUSPEND ANNUNCIATE: When SUSPEND ANNUNCIATE is active, the KSN 7xx no longer automatically sequencing waypoints.SUSPEND IN: Signals to the KSN 7xx to stop automatic sequencing of waypoints.B. Dead ReckoningThe dead reckoning function indicates to the pilot when GPS is not available and the KSN 7xx is navigating by dead reckoning.DEAD RECKONING ANNUNCIATE: When DEAD RECKONING ANNUNCIATE is active, the KSN 7xx is navigating via dead reckoning.C. NAV(1) CDI Switching FunctionCDI SELECT IN: The CDI SELECT IN input pin is used to tell the KSN 7xx whether output GPS or VLOC information to the external indicator. The input is normally open, with a momentary GND applied when the switch is pressed. When the KSN 7xx sees this input go low, it toggles the navigation source on the primary CDI output between GPS and VLOC.(2) Annunciator FunctionsThe following outputs are provided to annunciate KSN 7xx conditions. They may be used to illuminate lamps, engage relays, or be sensed directly by other systems. The term “illuminated”, as used below, indicates the active low state of the annunciator output.LNAV APPROACH ACTIVE ANNUNCIATE: Will illuminate whenever the KSN 7xx is configured for LNAV IFR approaches and the unit is in the approach active mode.CDI GPS ANNUNCIATE: Will illuminate whenever the KSN 7xx is outputting GPS deviation signals to the NAV Indicator.LOSS OF INTEGRITY ANNUNCIATE: Will illuminate whenever the KSN 7xx integrity monitor indicates a loss of GPS integrity.Draft as of 10/15/2012
DraftPage 3-1166 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.MESSAGE ANNUNCIATE: Will illuminate whenever the message prompt on the KSN 7xx is ON.LP APPROACH ACTIVE ANNUNCIATE: Will illuminate whenever the KSN 7xx is configured for LP IFR approaches and the unit is in the approach active mode.CDI VLOC ANNUNCIATE: Will illuminate whenever the KSN 7xx is outputting VOR or LOCALIZER data.WAYPOINT ANNUNCIATE: Will illuminate indicating that the aircraft will soon arrive at the active waypoint. When in the leg navigation mode with turn anticipation enabled, the WPT annunciator will begin flashing 20 seconds before turn anticipation begins, then will go on solid when turn anticipation begins, through the conclusion of turn anticipation. When the KSN 7xx is in the OBS navigation mode or in the leg mode with turn anticipation disabled, the WPT annunciator will begin flashing 36 seconds prior to the estimated time of arrival at the active waypoint.LNAV/VNAV APPROACH ACTIVE ANNUNCIATE: Will illuminate whenever the KSN 7xx is configured for LNAV/VNAV IFR approaches and is outputting GPS information to the primary CDI.LPV APPROACH ACTIVE ANNUNCIATE: Will illuminate whenever the KSN 7xx is configured for LPV IFR approaches and is outputting GPS information to the primary CDI.3.16.3 Requirements and LimitationsA. SuspendN/AB. Dead ReckoningN/AC. NAVRequirements for remote switching and annunciation of the KSN 7xx navigation functions vary depending on the level of certification of the installation. The following requirements represent typical standards in the USA, but even so may vary regionally within the USA (refer to Table 3-14). If the switches/annunciators are required, it is required that the message and waypoint alert annunciators be in the pilot’s primary field of view area (refer to Paragraph 2.3.4.3 Field of View Considerations). Primary field of view location is highly recommended for the remainder of the annunciators, but not required. Many EFIS systems provide some amount of switching and annunciation. A typical EFIS system provides NAV/GPS switching/annunciation and message/waypoint alert annunciation.Draft as of 10/15/2012
DraftPage 3-1176 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.(1) VFR-Only InstallationsNo requirement for waypoint alert and message annunciator, or an OBS/Leg course mode annunciator. These are optional, and it may be desirable to include a waypoint alert/message annunciator in the primary instrument scan area for the pilots’ convenience. There is no need for approach mode switching or annunciation. A NAV/GPS navigation source switch is required if both NAV and GPS may be displayed on a single CDI or HSI.(2) IFR En Route and Terminal InstallationsWaypoint alert and message annunciators are required.Remote OBS/Leg course mode switch/annunciator is optional. There is no need for approach mode switching or annunciation. A NAV/GPS navigation source switch is required if both NAV and GPS may be displayed on a single CDI or HSI.(3) IFR En Route, Terminal, and Non-precision Approach InstallationsWaypoint alert and message annunciators are required. Remote OBS/Leg course mode switch/annunciator is optional.Table 3-14. NAV Annunciators by Installation TypeAnnunciationSuggested Legend and Color VFR OnlyIFREnroute/TerminalNon-Precision Approach LPV ApproachCDI GPS ANN GPS (Grn) May be Reqd May be Reqd May be Reqd May be ReqdCDI VLOC ANN NAV (Grn) May be Reqd May be Reqd May be Reqd May be ReqdWPT ANN WPT (Ambr) Optional Reqd Reqd ReqdMSG ANN MSG (Ambr) Optional Reqd Reqd ReqdLOSS OF INTEGRITY ANN LOI (Ambr) Optional Optional Optional OptionalOFFPATH ANN OFF PATH (Ambr) Optional Optional Optional OptionalLNAV APPROACH ACTIVE ANN LNAV (Grn) Of No Use Of No Use Reqd ReqdLNAV/VNAV APPROACH ACTIVE ANN L/VNAV (Grn) Of No Use Of No Use Reqd ReqdLP APPROACH ACTIVE ANN LP (Grn) Of No Use Of No Use Of No Use ReqdLPV APPROACH ACTIVE ANN LPV (Grn) Of No Use Of No Use Of No Use ReqdDraft as of 10/15/2012
DraftPage 3-1186 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Approach mode switching and annunciation are required. A NAV/GPS navigation source switch is required if both NAV and GPS may be displayed on a single CDI or HSI.(4) LPV Approach InstallationsWaypoint alert and message annunciators are required. Remote OBS/Leg course mode switch/annunciator is optional.Approach mode switching and annunciation are required. A NAV/GPS navigation source switch is required if both NAV and GPS may be displayed on a single CDI or HSI.3.16.4 Electrical CharacteristicsNOTE: Annunciators are to be DC voltage only with a maximum of +38 VDC. Annunciator dimming may be by photocell or day/night switch. Do not use panel lighting rheostat dimmed bus.These outputs are open collector outputs. When active, the output device is turned on and conducting which provides a GND path for a load such as a lamp or relay that is pulled up to a maximum voltage of +38 VDC.J1-3 CDI SELECT INJ1-16 LNAV APPROACH ACTIVE ANNUNCIATEJ1-18 CDI GPS ANNUNCIATEJ1-19 LOSS OF INTETRITY ANNUNCIATEJ1-20 MESSAGE ANNUNCIATEJ1-35 OFFPATH ANNUNCIATEJ1-37 LP APPROACH ACTIVE ANNUNCIATEJ1-38 CDI VLOC ANNUNCIATEJ1-39 WAYPOINT ANNUNCIATEJ2-38 LNAV/VNAV APPROACH ACTIVE ANNUNCIATEJ2-58 LPV APPROACH ACTIVE ANNUNCIATE3.16.5 Interconnect DiagramRefer to Figure 3-28 for the annunciations - suspend/dead reckoning interconnect diagram.Refer to Figure 3-29 for the annunciations - NAV interface interconnect diagram.Active: LO (1.0 VDC while sinking current up to 250 mA). Inactive: HI (50 kilohms to GND, and up to +38 VDC).Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1196 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-28. Annunciations - Suspend/Dead Reckoning Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1216 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-29. Annunciations - NAV Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1236 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.17 Miscellaneous Interface3.17.1 Applicable Part NumbersAll part numbers and software revisions perform all miscellaneous functions.3.17.2 Function3.17.2.1 CoolingTwo fans are used as the primary method of providing internal cooling to the KSN 7xx. Aircraft supply of forced air cooling is not required. Two externally mounted cooling fans (part of KSN 7xx equipment rack design) provide all required cooling for the KSN 7xx.3.17.2.2 Configuration ModuleThe configuration module is used to keep implementation specific setup information on board the aircraft. This facilitates configuration of the KSN 7xx in the event service is needed.3.17.2.3 WOW InputThe WOW input is configurable in the maintenance pages to be active either high or low, and must be configured correctly for proper operation.3.17.2.4 Spare, Reserved only PinsThis is a list of spare pins that are included in the KSN 7xx, but not used in installation, and is for reference only.3.17.3 Requirements and Limitations3.17.3.1 CoolingN/A3.17.3.2 Configuration ModuleN/A3.17.3.3 WOW InputN/A3.17.3.4 Spare PinsN/ADraft as of 10/15/2012
DraftPage 3-1246 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.17.4 Electrical Characteristics3.17.4.1 Cooling InterfaceJ2-20 KSN FANJ2-1 GND 3J2-39 MMDS FANJ2-19 FAN RETURNThese pins provide power and GND to the KSN 7xx cooling fans.3.17.4.2 Configuration Module InterfaceJ4-11 CONFIG MODULE POWERJ4-29 CONFIG MODULE GNDThese pins provide +5 VDC and GND to the Bendix/King KCM 200 configuration module.J4-30 CONFIG MODULE CLOCKJ4-12 CONFIG MODULE DATAThese pins provide the serial data interface to the configuration module. The wire length between the KSN 7xx and the KCM 200 must not exceed 72 inches (183 cm).If the KCM 200 configuration module is not present on unit power-up, the KSN 7xx’s internal configuration data is used. If there is an error detected in the KCM 200 configuration data and the internal KSN 7xx configuration data is good, the internal data will be used, but not copied to KCM 200. The message “CONFIGURATION MEM ERROR” is shown on the KSN 7xx screen. If errors are detected in both the KCM 200 and internal configuration data, the internal data shall change to the factory default values, and the KCM 200 data is not changed.3.17.4.3 WOWJ2-54 WOWThe WOW input is supplied by the aircraft. The input is normally open, and grounded when there is weight on the aircrafts wheels.3.17.4.4 Spare RS-232All pins identified as spare are reserved for future use.3.17.5 Interconnect DiagramRefer to Figure 3-30 for the miscellaneous interface 1 interconnect diagram.Refer to Figure 3-31 for the miscellaneous interface 2 interconnect diagram.Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1256 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-30. Miscellaneous Interface 1 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1276 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-31. Miscellaneous Interface 2 Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1296 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.18 XM Receiver Interface3.18.1 Applicable Part NumbersAll part numbers and software revisions perform all XM receiver functions.3.18.2 FunctionTBD3.18.3 Requirements and LimitationsTBD3.18.4 Electrical CharacteristicsJ4-26 DATALINK RECEIVER 422 #3 RX AJ4-27 DATALINK RECEIVER 422 #3 RX BThis is a standard EIA 422 data bus with the following characteristics: 3.18.5 Interconnect DiagramRefer to Figure 3-32 for the XM receiver interface interconnect diagram.BAUD: 57600Data Bits: 8Start Bits: NoneStop Bits: 2Parity: NoneHandshaking: NoneDraft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1316 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-32. XM Receiver Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1336 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.19 Maintenance Interface3.19.1 Applicable Part NumbersAll part numbers and software revisions perform all maintenance functions.3.19.2 FunctionAll pins and busses (with the exception of the front USB connector) are for shop maintenance only, and must not be included in the aircraft harness.A. Front USBInformation about navigational elements contained on thumb drives is transferred to the KSN 7xx data base memory the front USB port. Data base loading need only be performed upon the receipt of a new data (available every 28 days from Bendix/King).The KSN 7xx will not navigate during data loading, and therefore it is necessary to load the data base before flight. The thumb drive contains data for airports, VORs, NDBs, published Intersections, SID and STAR waypoints, non-precision approach waypoints, and other miscellaneous data. The procedure for updating the published data base is detailed in the KSN 7xx pilot’s guide.In addition to loading of the published data base, non-published data base items such as user-defined flight plans, waypoints, navaids and airports may be transferred between the KSN 7xx and a IBM-compatible personal computer via a thumb drive on the front USB port. The PC software kit for this function is available through Bendix King. User data such as user defined flight plans, waypoints, navaids, and airports may also be transferred between KSN 7xx systems in dual installations through use of the dual system interface. It is not possible to transfer the published data base from the KSN 7xx to a thumb drive or from one KSN 7xx to another over the dual system interface.B. Rear USBTBD3.19.3 Requirements and LimitationsAll pins and busses (with the exception of the front USB connector) are for shop maintenance only, and must not be included in the aircraft harness.Draft as of 10/15/2012
DraftPage 3-1346 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.19.4 Electrical CharacteristicsA. GPS Dataload RS-232J4-13 GPS DATALOAD 232 TXJ4-32 GPS DATALOAD 232 RXJ4-31 GPS DATALOAD 232 GNDThis is a standard EIA-232 serial interface that is only used for shop testing, and must not be connected in the aircraft harness.B. Demo Mode SelectJ4-19 DEMO MODE SELECTThis pin is normally open, and when it is held low during power up, will take the KSN 7xx into demo mode. This pin is only used for shop testing, and must not be connected in the aircraft harness.C. Shop Mode SelectJ4-18 SHOP MODE SELECTThis pin is normally open, and when it is held low during power up, will take the KSN 7xx into shop mode. This pin is only used for shop testing, and must not be connected in the aircraft harness.D. Maintenance RS-422J4-22 MAINTENANCE 422 RX AJ4-23 MAINTENANCE 422 RX BJ4-4 MAINTENANCE 422 TX AJ4-5 MAINTENANCE 422 TX BThis is a standard EIA-422 data bus that is only used for shop testing, and must not be connected in the aircraft harness.E. IOP RS-422 AJ2-42 IOP 422 #4 RX AJ2-43 IOP 422 #4 RX BJ2-61 IOP 422 #4 TX AJ2-62 IOP 422 #4 TX BThis is a standard EIA-422 data bus that is only used for shop testing, and must not be connected in the aircraft harness.Draft as of 10/15/2012
DraftPage 3-1356 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.F. DiscretesJ3-1 33V Boost TestJ3-4 5V KSN TestJ3-5 5V7 Startup TestJ3-3 12V POS MMDS TestJ3-2 ON OFF Status NThese discretes are all used for shop testing, and must not be connected in the aircraft harness.G. Front USBFRONT-2 USB 1 D FRONT-3 USB 1 D +FRONT-4 USB 1 D GNDFRONT-8 USB 1 VBUSThis is a standard v2.0 USB bus that is used for data loading.H. Rear USBJ8-2 USB 2 D J8-3 USB 2 D +J8-5 USB 2 D GNDJ8-1 USB 2 D VBUSJ8-4 USB 2 IDThis is a standard v2.0 USB bus that is only used for shop testing.3.19.5 Interconnect DiagramRefer to Figure 3-33 for the maintenance interface interconnect diagram.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1376 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-33. Maintenance Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1396 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.20 Stormscope Interface (WX-500)3.20.1 Applicable Part NumbersAll part numbers and software revisions perform all stormscope interface functions.3.20.2 FunctionThe L3 WX-500 stormscope is a remote weather mapping sensor which detects and processes lightning strikes. It interfaces with the KSN 7xx in order to provide this lightning detection and avoidance information. WX-500 control and display information is communicated by a serial interface between the WX-500 and the KSN 7xx. Two modes of weather display are available: Strike Mode and Cell Mode. The KSN 7xx must be configured for a WX-500 on the maintenance pages for the WX-500 function to be displayed.3.20.3 Requirements and LimitationsThe WX-500 must be installed in accordance with its own installation manual in order to assure proper operation.3.20.4 Electrical CharacteristicsA. Stormscope ControlJ1-64 WX-500 422 #2 TX AJ1-65 WX-500 422 #2 TX BThis is a standard EIA-422 data bus.B. Stormscope DataJ1-44 WX-500 422 #2 RX AJ1-45 WX-500 422 #2 RX BThis is a standard EIA-422 data bus.3.20.5 Interconnect DiagramRefer to Figure 3-34 for the stormscope interface (WX-500) interconnect diagram.Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1416 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-34. Stormscope Interface (WX-500) Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftPage 3-1436 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.21 NAV/COM Interface (KSN 7x0 Only)3.21.1 Applicable Part NumbersAll KSN 7x0 navigators will be capable of all COM/NAV interface functions.3.21.2 FunctionThe NAV/COM function of the KSN 7x0 integrated navigators provides the following COM/NAV functions:A. Two way voice communications within the frequency range of 118.000 to 136.975 MHz (760 channels) in 25 KHz increments.B. Reception of navigation signals within the frequency range of 108.00 to 117.95 MHz in 50 kHz increments (200 channels).C. Reception of glide slope signals within the frequency range of 3.29.15 to 335.00 MHz in 150 kHz increments (40 channels).D. DME channeling to selected remote and panel mount DME equipment via the King Serial DME bus.3.21.3 Requirements and LimitationsA. COMA conventional 50-ohm vertically polarized COM antenna is required with the KSN 7x0. Vertically bent whip antennas are not recommended. Antennas must be installed per their manufacturer’s recommendations. Additional recommendations are as follows:(1) Mount the antenna on a flat metal surface or install a GND plane at least 18 inches (457 mm) square.(2) The antenna must be well removed from any projections, the engine(s), and the propeller(s).B. NAVA conventional 50-ohm horizontally polarized VOR/LOC/GS antenna is required with the KSN 7x0. Antennas must be installed per their manufacturer’s recommendations. Additional recommendations are as follows:(1) The location must be well removed from other antennas, projections, engine(s), and propeller(s). It must have a clear line of sight area if possible.(2) The antenna must be mounted symmetrically with the centerline of the aircraft.(3) Avoid running other coaxial cables and wires near the NAV antenna cable.Draft as of 10/15/2012
DraftPage 3-1446 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.C. DME ChannelingFor proper functioning of the King Serial DME indicator interface, a DME receiver (in addition to the KSN 7xx and the indicator) must be connected to the SERIAL CLOCK and SERIAL DATA lines.When the KSN 7xx is mounted in the aircraft pedestal, some certification agencies (including the FAA) require a distance display in the pilot's scan area for IFR certification. Consult your approval agency for additional information.The KSN 7xx may display distance, groundspeed and time-to-station on the KPI-553A, KDI-572, KDI-573 and KDI-574 DME distance displays. The DME in the aircraft continues to supply power to these displays while the KSN 7xx information is displayed. A NAV/GPS annunciator switch and relays can switch the DME display between displaying DME and GPS information (refer to the DME installation documentation for details).3.21.4 Electrical CharacteristicsJ2-33 EMERGENCY FREQUENCYThis input is normally open, and is active when pulled low. While pulled low, this discrete will force the COM transceiver to:A. Ignore all requests to change the COM channel until the input returns to open.B. Ignore all requests to change the COM volume until the input returns to open.C. Load the emergency frequency stored in NVM as the active frequency of the COM transceiver.D. Set the COM volume to the emergency volume Level as per the configuration module defined value (as set up in the maintenance pages).J2-52 COM REMOTE TRANSFERThis input is normally open, and is activated when pulled to GND. When this input is held low for longer than 2 seconds, the emergency frequency will be loaded into the standby channel. When a low to open transition is detected following a low signal of <2 seconds, the KSN 7xx will transfer the active COM frequency to standby and will transfer the standby COM frequency to active.J2-14 COM CHANNEL DECREMENTJ2-13 COM CHANNEL INCREMENTThese inputs are normally open and are activated by being momentarily pulled to GND. When the COM CHANNEL DECREMENT input is activated, the KSN 7xx will change the COM standby frequency to the previous channel in the user defined COM channel list. When the COM CHANNEL INCREMENT input is activated, the KSN 7xx will change the COM standby frequency to the next channel in the user defined COM channel list.Draft as of 10/15/2012
DraftPage 3-1456 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.J2-5 COM AUDIO OUT HIJ2-25 COM AUDIO OUT LOThis is an analog output from the KSN 7xx with the following characteristics:J2-6 COM MIC AUDIO IN HIJ2-26 COM MIC AUDIO IN LOThis is an analog input to the KSN 7xx with the following characteristics:J2-71 COM MIC KEYThis input is normally open, with a momentary GND applied when a switch is pressed. When the switch is open, the KSN 7xx disables the COM transmitter and sidetone; when grounded the COM transmitter and sidetone are enaled.J2-53 TRANSMIT INTERLOCKThis discrete input signal may be optionally activated from remote equipment that might interfere with the VHF COM. The input is normally open, and is activated momentarily as long as a GND is applied to it. When the input is open, the COM receiver operates normally with normal sensitivity and sidetone. When this input is held low, the COM receiver is desensitized. If held low for longer than 30 seconds continuously, the receiver reverts to the normal mode until the signal is released (open) and pulled low again.Impedance: 500 50 ohms from 350 to 2500 Hz when the KSN 7xx is powered, and450 ohms when the KSN 7xx is unpowered.Range: 15.0 Vrms from 350 to 2500 Hz with 10% THD into an open circuit.Rated Audio: 100 mW into 500 ohms.Squelch: 2 mVrms signal and noise into 500 ohmsMinimum State: 2 mVrms signal and noise into 500 ohmsImpedance: 485 49 ohmsfrom 350 to 2500 Hz.Bias Voltage: 9.0 1.0 VDC through an internal series resistance of 500 50 ohmsto a load which can range from 0 ohm to open.Range: 125 mVrms Signals 1.5 Vrms.Draft as of 10/15/2012
DraftPage 3-1466 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.J2-7 NAV AUDIO OUT HIJ2-27 NAV AUDIO OUT LOThis is an analog output from the KSN 7xx with the following characteristics:King Serial DME BusJ1-75 SERIAL CLOCKJ1-57 SERIAL DATAJ1-76 DME CHANNEL REQUESTJ1-56 DME COMMONThese connections transmit Bendix/King format serial DME information.In the King Serial DME configuration, SERIAL SYNC is an input. When the KSN 7xx receives an active-high pulse on SERIAL SYNC, it transmits pulses on the SERIAL CLOCK and SERIAL DATA lines.3.21.5 Interconnect DiagramRefer to Figure 3-35 for the COM interface interconnect diagram.Refer to Figure 3-36 for the NAV interface interconnect diagram.Refer to Figure 3-37 for the NAV interface - remote DME channeling interconnect diagram.Refer to Figure 3-38 for the NAV interface - panel mount DME channeling interconnect diagram.Impedance: 500 50 ohms from 350 to 2500 Hz when the KSN 7xx is powered, and 450 ohms when the KSN 7xx is unpowered.Range: 15.0 Vrms from 350 to 2500 Hz with 10% THD into an open circuit.Rated Audio: 100 mW into 500 ohms.Minimum State: 2 mVrms signal and noise into 500 ohmsDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1476 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-35. COM Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
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DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1496 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-36. NAV Interface Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1506 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1516 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-37. NAV Interface - Remote DME Channeling Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012Figure 3-37 & 3-38 seems to be a duplicate of Figure 3-16 & 3-17. They are wrong, because it has the RNAV/Channel Request and DME Channel Request confused and shown incorrectly. There is no DME Channel request. There is an RNAV/Channel Request and a DME Request and they are different functions.
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1526 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1536 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Figure 3-38. NAV Interface - Panel Mount DME Channeling Interconnect Diagram (Sheet 1 of 1)Draft as of 10/15/2012Figure 3-37 & 3-38 seems to be a duplicate of Figure 3-16 & 3-17. They are wrong, because it has the RNAV/Channel Request and DME Channel Request confused and shown incorrectly. There is no DME Channel request. There is an RNAV/Channel Request and a DME Request and they are different functions.
DraftSYSTEM INSTALLATION MANUAL066-01204 / 066-01213Page 3-1546 Dec 2012© Honeywell International Inc. Do not copy without express permission of Honeywell.34-70-06Blank PageDraft as of 10/15/2012
DraftPage 3-1556 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.3.22 Data Bus InformationTBD BY ENGINEERINGDraft as of 10/15/2012
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DraftPage 4-16 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.SECTION IVTBDDraft as of 10/15/2012
DraftPage 4-26 Dec 201234-70-06SYSTEM INSTALLATION MANUAL066-01204 / 066-01213© Honeywell International Inc. Do not copy without express permission of Honeywell.Blank PageDraft as of 10/15/2012

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