User Manual Part 1

ManualsBrandsEMS Technologies Canada ManualsElectronicsKA Band Aviation Radio

Honeywell International Inc.

400 Maple Grove Road

Ottawa, Ontario

Canada K2V 1B8

CAGE: 38473

Telephone: (800) 601-3099 (Toll Free U.S.A./Canada)

Telephone: +1-(602) 365-3099 (International Direct)

Website: www.myaerospace.com

Page T-1

Publication Number D201401000049, Revision 1 Initial 16 Jan 2015

Revised 16 Sep 2015

23-15-29

This 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

JetWave™ System

System Description and Installation Manual

This guide provides procedures for installation, configuration, and operation of the equipment listed

below.

Model Part Number

JetWave™ System Class A Forced Air KRFU 90401028-001

JetWave™ System Class A Conduction Cooled KRFU, Version 1 90401028-002

JetWave™ System Class A Conduction Cooled KRFU, Version 2 90401028-003

JetWave™ System Class B Forced Air KRFU 90401027-001

JetWave™ System Class B Conduction Cooled KRFU, Version 1 90401027-002

JetWave™ System Class B Conduction Cooled KRFU, Version 2 90401027-003

JetWave™ System Class A Conduction Cooled KRFU, Version 2, FMA 90401027-004

JetWave™ System Class A Forced Air KRFU, Version 2, FMA 90401027-005

A791 Radome Package 90400017-XXX

Non-A791 Radome Package 90400016-XXX

Legal Notice

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Summary of content (120 pages)

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Honeywell International Inc. 400 Maple Grove Road Ottawa, Ontario Canada K2V 1B8 CAGE: 38473 Telephone: (800) 601-3099 (Toll Free U.S.A./Canada) Telephone: +1-(602) 365-3099 (International Direct) Website: www.myaerospace.com JetWave™ System System Description and Installation Manual This guide provides procedures for installation, configuration, and operation of the equipment listed below.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Proprietary Information Honeywell – Confidential THIS 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.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 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.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Copyright - Notice Copyright 2015 Honeywell International Inc. All rights reserved. Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies. JetWave™ System, System Description, Installation, and Maintenance Manual Document Number: D201401000049, Revision 1 16 Sep 2015 Our products are under continuous research and development.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System TRANSMITTAL INFORMATION TO THE HOLDERS OF JETWAVE™ SYSTEM SDIM, ATA NO. 23-15-29 (PUB. NO. D201401000049), ISSUED FOR USE IN SUPPORT OF THE FOLLOWING: Table TI-1 shows the applicable components. Table TI-1.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The Task/Page column identifies the blocks of changed information, such as a task, subtask, graphic, or parts list, and the page on which that block starts. Revision marks, when provided, identify the location of the change within the block. The Description of Change column tells about the change or changes within each block. The description of change is often preceded by a paragraph or figure reference that applies to the block of information.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System RECORD OF REVISIONS When revisions are received, insert revised pages, record the date, and initial. Revision Number Issue Date Date Inserted Inserted by (initial) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System RECORD OF TEMPORARY REVISIONS Instructions on each page of a temporary revision tell you where to put the pages in your manual. Remove temporary revision pages only when discard instructions are given. For each temporary revision, put the applicable data in the record columns on this page. Definition of Status column: TR may be active, incorporated, or deleted. “Active” is entered by the holder of manual.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SERVICE BULLETIN LIST Service Bulletin Number Subject Manual Rev. Number 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell. Manual Rev.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page Date Title T-1 T-2 T-3 T-4 Transmittal Information TI-1 TI-2 TI-3 TI-4 TI-5 TI-6 TI-7 TI-8 TI-9 TI-10 Record of Revisions RR-1 RR-2 Record of Temporary Revisions RTR-1 RTR-2 Service Bulletin List SBL-1 SBL-2 List of Effective Pages LEP-1 LEP-2 LEP-3 LEP-4 LEP-5 LEP-6 Table of Contents TC-1 TC-2 TC-3 TC-4 TC-5 TC-6 TC-7 TC-8 TC-9 TC-10 Introduction INTRO-1 *16 Sep 2015 16 Sep 2015 16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F Date 2-25 2-26 2-27 2-28 2-29 2-30 2-31 2-32 2-33 2-34 2-35 2-36 2-37 2-38 2-39 2-40 2-41 2-42 2-43 2-44 2-45 2-46 2-47 2-48 2-49 2-50 2-51 2-52 2-53 2-54 2-55 2-56 2-57 2-58 2-59 2-60 2-61 2-62 2-63 2-64 2-65 2-66 2-67 2-68 2-69 2-70 2-71 2-72 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *1
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F F Date 2-121 2-122 2-123 2-124 2-125 2-126 2-127 2-128 2-129 2-130 2-131 2-132 2-133 2-134 2-135 2-136 2-137 2-138 2-139 2-140 2-141 2-142 2-143 2-144 2-145 2-146 2-147 2-148 2-149 2-150 2-151 2-152 2-153 2-154 2-155 2-156 2-157 2-158 2-159 2-160 2-161 2-162 2-163 2-164 2-165 2-166 2-167 *16 Sep 2015 16 Sep 2015 *16 Sep 2015 16 Sep 201
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page 3-6 3-7 3-8 3-9 3-10 3-11 3-12 3-13 3-14 3-15 3-16 3-17 3-18 3-19 3-20 3-21 3-22 3-23 3-24 3-25 3-26 3-27 3-28 3-29 3-30 3-31 3-32 3-33 3-34 3-35 3-36 3-37 3-38 3-39 3-40 3-41 3-42 3-43 3-44 3-45 3-46 3-47 3-48 3-49 3-50 3-51 3-52 3-53 * F Date Subheading and Page Date *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *16 Sep 2015 *1
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page Date Subheading and Page Date A-10 *16 Sep 2015 A-11 *16 Sep 2015 A-12 16 Sep 2015 Appendix B: MIB / SNMP B-1 *16 Sep 2015 B-2 *16 Sep 2015 B-3 *16 Sep 2015 B-4 *16 Sep 2015 B-5 *16 Sep 2015 B-6 *16 Sep 2015 B-7 *16 Sep 2015 B-8 *16 Sep 2015 B-9 *16 Sep 2015 B-10 *16 Sep 2015 B-11 *16 Sep 2015 B-12 *16 Sep 2015 B-13 *16 Sep 2015 B-14 *16 Sep 2015 Appendix C: Installation Information Sheet C-1 *16 Sep 2015 C-2 *16 Sep 2015 Ap
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System TABLE OF CONTENTS Title Page INTRODUCTION 1. How to Use This Manual ..................................................................................................INTRO-1 A. General .......................................................................................................................INTRO-1 B. Observance of Manual Instructions ............................................................................INTRO-1 C. Symbols ......
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. System Initialization Mode ................................................................................................ 1-11 C. Normal Operating Mode .................................................................................................... 1-11 D. Critical Fault Mode ............................................................................................................ 1-12 E. Data Load Mode ..................................
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 1. Provisioning of User Services....................................................................................................3-1 2. About Installation and Registration............................................................................................3-2 3. Product Support Services..........................................................................................................3-2 A. Customer Support Overview ................
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System D. General Instructions for Inspection ................................................................................... 3-30 E. Electrical and Mechanical Inspection and Check .............................................................. 3-30 F. Scheduled Maintenance and Inspections .......................................................................... 3-30 G. Unscheduled Maintenance ..........................................................
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System APPENDIX C 1. Aircraft Information Sheet......................................................................................................... C-1 2. JetWave™ AES Subsystem Components................................................................................ C-1 A. JetWave™ AES OAE - FMA/TMA Installation Information Sheet ...................................... C-1 B. JetWave™ AES KANDU Installation Information Sheet ........................
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System LIST OF FIGURES Figure Description Page Figure INTRO-1. Symbols ....................................................................................................INTRO-1 Figure 1-1.Ka-Band System.............................................................................................................1-1 Figure 1-2. JetWave™ System Block Diagram ....................................................................1-8 Figure 2-1.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-32.Fuselage Mount Radome Outline and Installation Drawing (Sheet 1 of 6) 2-109 Figure 2-33.JetWave™ System Interconnect Diagram - TMA (Sheet 1 of 10) 2-121 Figure 2-34.JetWave™ System Interconnect Diagram - FMA (KRFU Inside Aircraft Fuselage) (Sheet 1 of 8) 2-141 Figure 2-35.JetWave™ System Interconnect Diagram - Boeing Specific FMA (External KRFU) (Sheet 1 of 8) 2-157 Figure 2-36.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System LIST OF TABLES Table Description Page Table 1-1.JetWave™ System LRUs ...............................................................................................1-1 Table 1-2.Modman Leading Particulars ..........................................................................................1-2 Table 1-3.APM Leading Particulars ................................................................................................1-3 Table 1-4.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table B-8.Mute Reason Enumeration Type ...................................................................................B-4 Table B-9.Satellite Handover Enumeration Type ...........................................................................B-5 Table B-10.Transmission State on Ground Enumeration Type ......................................................B-5 Table B-11.Port Link Status Enumeration Types ........................................
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System INTRODUCTION 1. How to Use This Manual A. General (1) This manual provides information about the installation of the AES Systems. (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.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System D. Units of Measure (1) E. 2. 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. Illustration (1) Supplemental illustrations use a suffix number to the basic figure number.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • APPENDIX B - JetWave™ system network performance data (MIB objects and SNMP traps) • APPENDIX C - Installation information sheets • APPENDIX D - Installation checklist • APPENDIX E - Airframe specific information required for configuration. 5. Customer Support A. Honeywell Aerospace Online Technical Publications Website (1) Go to the Honeywell Online Technical Publications Website at http://www.myaerospace.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • ANSI/IEEE Std 91, Graphic Symbols for Logic Functions (available from the American National Standards Institute at http://www.ansi.org) • H4/H8 CAGE Codes (available from DLA Logistics Information Services at http://www.logisticsinformationservice.dla.mil) • IEEE 315/ANSI Y32.2, Graphic Symbols for Electrical and Electronics Diagrams (available from the American National Standards InstituteInstitute at http://www.ansi.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations Term Full Term AC alternating current ACM aeronautical core module AES aircraft earth station AISD airline information services domain AIM aircraft interface mount AIT Avionics Interface Technologies AMIP open antenna to modem interface protocol ANSI American National Standards Institute APM aeronautical personality module ARINC Aeronautical Radio, Incorporated ASC antenna subsystem controll
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations (Cont) Term Full Term DP distribution partner EMEA Europe, the Middle East, and Africa ESDS electrostatic discharge sensitive EST Eastern Standard Time F Fahrenheit FAA Federal Aviation Administration FAR Federal Aviation Regulations FMA fuselage mount antenna FTP file transfer protocol FXS foreign exchange subscriber GHz gigahertz GPO Government Printing Office GPS global positioning sys
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations (Cont) Term Full Term Ka part of the radio frequency spectrum: 26.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations (Cont) Term Full Term PN part number PODD passenger owned devices domain POTS plain old telephone system POST power-on self test PSI pound per square inch RF radio frequency RFM radio frequency module RMA return material authorization RSSI receive signal strength indicator RX receive SAS satellite access station SATCOM satellite communication SDIM system description, and installation manu
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations (Cont) Term Full Term WOW weight on wheels 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System DESCRIPTION AND OPERATION 1. Overall JetWave™ System Architecture The JetWave™ SATCOM system supplies a broadband communication link that can be used to supply data, video, and voice communications for passengers communications and entertainment. The AES communicates to the SAS through a satellite as shown in Figure 1-1. Figure 1-1. Ka-Band System A Modman is provided within the AES to enable two-way communications.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 1-1. JetWave™ System LRUs (Cont) B. LRU PN APM 90401121 KANDU 90401566 KRFU CC1 90401203 KRFU CC2 90402346 KRFU 90401202 FMA 90000380-1 TMA 904000013-0001 A791 FM radome 90400017 Non-A791 FM radome 90400016 JetWave™ System LRU Leading Particulars (1) Refer to Table 1-2 for the Modman leading particulars. (2) Refer to Table 1-3 for the APM leading particulars. (3) Refer to Table 1-4 for the KANDU leading particulars.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 1-2. Modman Leading Particulars (Cont) Characteristic Specification Cooling 48.5 lb/hr (22 kg/hr) at 104°F (40°C) Operating temperature 5°F (-15°C) to 131°F (55°C) Mounting information 4-MCU, forced-air, ARINC 600 series tray Maintenance No scheduled maintenance required Interfaces J1A - PODD, PIESD, and AISD J1B - APM, Aircraft, APM, PODD, PIESD, AISD, and KANDU J1C - IF to/from KRFU and aircraft power Table 1-3.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 1-4. KANDU Leading Particulars (Cont) Characteristic Specification Power dissipation 50 watts Class A maximum average power 42 watts Class B maximum average power Cooling Cooling clearance is 2.0 inches (5.1 cm) above and 1 inch (2.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 1-5. KRFU Leading Particulars(Cont) Characteristic Specification Length 16.55 inches (42.0 cm) maximum Width 9.01 inches (22.9 cm) maximum Height 2.08 inches (7.1 cm) maximum Weight 11.30 pounds (5.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 1-5. KRFU Leading Particulars(Cont) Characteristic Specification Interfaces J1 - Aircraft power input J2 - Control interface from KANDU J3 - RF TX to OAE J4 - RF RX from OAE J5 - IF TX from Modman J6 - IF RX to Modman Table 1-6. TMA Leading Particulars Characteristic Specification Length 13.38 inches (339.9 mm) maximum Width 12.00 inches (304.8 mm), maximum reflector sweep volume Height 13.57 inches (344.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 1-7. FMA Leading Particulars Characteristic Specification Cooling Natural convection and radiation only Maintenance No scheduled maintenance required Interfaces P1 - Power from KANDU P2 - Control interface from KANDU P3 - IMU power and control from KANDU J4 - RF RX to KRFU J5 - RF TX from KRFU Table 1-8. B757 FMA Radome Leading Particulars Characteristic Specification Length 95.472 inches (585 mm) maximum Width 43.881 inches (907.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 1-2. JetWave™ System Block Diagram The JetWave™ system LRUs are as follows: A. Outside Antenna Equipment • The OAE is made up of a mechanically steered antenna: • Either fuselage mount or tail mount • Radome package. • The antenna includes an aperture. • The OAE is powered by the KANDU. 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Contains an LNA for amplification of signals in the receive path. • Includes the mechanical pointing system, positioner, motors and sensors, and an INU to detect movement of the platform. • The TMA or FMA accepts the transmit Ka-band signal from the KRFU for the antenna. • The antenna K-band receive path is amplified by the LNA and sent to the KRFU by the TMA or FMA. • The TMA or FMA receives power from the KANDU.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • It supplies the user interfaces to the aircraft and passengers as follows: • The PODD interfaces provide service to the passengers through the use of Ethernet (10/100/1000 Base T). • The PIESD interfaces provide services to passenger entertainment devices installed on the aircraft (in flight entertainment systems). This system uses Ethernet (10/100/1000 Base T).
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Refer to JetWave™ AES system Configuration, AES Configuration Data for the details of ARINC 429 labels required for the JetWave™ System. 4. JetWave™ System Modes of Operation The JetWave™ system supports the following modes of operation: A. • Power On • System Initialization • Normal Operation • Critical Fault • Data-Load • Commanded. Power On Mode Each LRU enters Power On Mode when power is applied.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System traffic can be started once the antenna is pointed correctly to the satellite and the terminal locks on to the satellite for providing the connectivity. The system enables all the supported services like continuous BITE, SNMP, Access system, user services, etc. in this mode. The system enters the Normal Operating Mode approximately 5 minutes after continuous power is applied to the last LRU. D.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System INSTALLATION 1. Overview A. JetWave™ System Components The JetWave™ system includes five LRUs: • Modman • APM • KANDU • KRFU • OAE - either a TMA or FMA. NOTE: OAE equipment must be installed within an approved radome. B. Installation Procedure Overview for the JetWave™ System The overview of the installation procedure for the JetWave™ system is as follows: 2. (1) Install adapter plate for the FMA.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System A. Testing and Commissioning Process with Restrictions (1) The JetWave™ system under normal operating conditions mutes and disables the modem when the Air/Ground status in "On Ground". (2) The Air/Ground status will be set to "On Ground" when one of the conditions that follow are met: • Weight on wheels discrete is enabled in the system configuration and is indicating "Weight on Wheels”. • The ground speed is less than 50 knots.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (9) 4. (c) At the time of manufacturing of Modman, the serial numbers of the Modman and associated DIDs of the ACM are communicated to the Inmarsat service provider as part of pre-provisioning. (d) The Modman and associated DIDs of the ACM also allocated a specific SSPP. This SSPP is required to verify the terminal connectivity to the NMS.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Install the Modman in a standard 4-MCU tray. The customer is responsible for providing the mounting tray, the mating ARINC 600 connector, contacts, as well as all the cabling for the installaton. Refer to Figure 2-24 for outline and installation information, and Figure 2-33 thru Figure 2-36 for the applicable interconnect diagram. There are no special tools, fixtures, and equipment required for the Modman installation.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System for Ethernet interfaces terminating on Quadrax receptacles. Refer to the applicable interconnection diagrams for the indicator that the connector rotation of the wire is in a clockwise direction. (3) The Modman bonding is as follows: The Modman must be electrically bonded to the airframe. Make sure that the mating surfaces are free from contaminants such as paints or other non-conductive elements.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The APM must be electrically bonded to the airframe through contact with the base of the unit or through a bonding cable attached to M3 earth stud. The APM bonding resistance must be less than or equal to 2.5 mΩ. D. KANDU Refer to Figure 2-26 for outline and installation information. Refer to Figure 2-33 thru Figure 2-36 for the applicable interconnect diagram.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (b) KANDU receptacle A3J2 is MIL-DTL-38999/20FC4SN, series Ill, flange mount receptacle, insert 13-4, normal keying, with four socket-type contacts of size 16 AWG. Mates with D38999/26FC4PN for power output. (c) KANDU receptacle A3J3 is MIL-DTL-38999/20FG35PN, series III, flange mount receptacle, insert 21-35, normal keying, with 79 pin-type contacts of size 22 AWG. Mates with D38999/26FG35SN for control interface.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The KANDU bonding resistance measured from the measuring point and the surface the unit is mounted must be less than 2.5 mΩ. E. KRFU A waveguide is used for the KRFU to OAE RF TX connection. The waveguide run must include a short length of seamless flexible waveguide along the routing to accommodate tolerances. The waveguide must have mounting points to interface to the attachment points provided.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The KRFU must be electrically bonded to the airframe through contact with the base of the unit as follows: • At least one of the four mechanical attachment points must be used for electrical bonding. • Make sure that the mating surfaces are free from contaminants such as paints or other non-conductive elements. • A circular or elongated conductive area must be provided around the mounting hole of the equipment base plate.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (d) Apply tacky side of thermal pad to the bottom side of unit as shown in Figure 2-1. 1 Making sure to keep a setback dimension of 0.032 to 0.125 inch (0.79 to 3.18 mm) around the edges of the installed thermal pad. (e) Remove the clear protective backing to expose the tacky side of thermal pad PN MPW0000122. (f) Apply the pad flush to the interior edge of the thermal pad PN MPW0000118, in order to maintain consistent setback dimension of 0.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (1) Introduction The TMA assembly is to be installed on the top of the tail empennage of the aircraft. For the JetWave™ system to correctly point the antenna, the installation offsets should not exceed more than 1 degree off heading, pitch or roll with respect to principle axis of aircraft.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The installer must select the appropriate gauge of wire as specified in the TMA interconnection diagram in Figure 2-33 for power and control connections. Interconnect cables must be routed away from sources of potential electromagnetic interference. (3) Advisories The JetWave™ TMA and the KRFU subsystems include components that radiate RF and microwave emissions in the band between 29.0 and 30.0 GHz.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-5. TMA Installation Kits PN Description SCD-90402677 WR42 to 2.92 mm coax adapter CAUTION: (6) THE TAIL MOUNT OAE ASSEMBLY IS ELECTROSTATIC-SENSITIVE. STANDARD ELECTROSTATIC-SENSITIVE HANDLING PROCEDURES MUST BE OBSERVED.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (9) TMA Interface Mount Brackets (if Required) Depending on the airframe, there may be a need to install a TMA to airframe interface mount brackets, which adapts to the tail empennage of the aircraft and in turn supplies a firm flat base for the TMA assembly. This is not detailed in this document as the requirement of antenna interface mount is air frame specific.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The KRFU can be installed either on front or rear of tail mount antenna assembly horizontally or vertically depending on space availability. The KRFU is conduction cooled through the base plate with thermal pad. Mount the Honeywell recommended thermal pad (refer to KRFU Thermal Pad Kit installation in section 3.F.) while installing KRFU LRU.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Connecting the waveguide, RF coax interface to the TMA. • Positioning and installation of the TMA assembly onto tail empennage antenna slot/antenna interface mount, installation of bonding straps. • Installation of the KRFU and bonding straps. • Installation of the waveguide and coax between the TMA and KRFU. • Connecting the TMA interface, KRFU power, and control interfaces. • Position and installation of the radome.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (b) Before proceeding with the KRFU installation, connect the WR42 waveguide to 2.92 mm coaxial connector adapter to KRFU J4 RF RX. 1 The adapter allows connection between a WR-42 waveguide cover flange UG595/U per MIL-DTL-3922/54 (modified with threaded mounting holes) and a 2.92 mm coaxial connector. 2 The WR42 waveguide side of the adapter has a mechanical flange interface with four 0.117 inch (2.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-7. KRFU Bonding Strap Arrangement (4) Installation of the Waveguide and Coaxial Cable Interconnect Between the TMA and KRFU (a) Loosely attach the waveguide and coax support brackets to antenna interface mount or the tail empennage structure. The flexible wave guide and coax cable assembly kit and its routing is aircraft specific. (b) Remove the protective covers from the TMA J3 RF TX.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-8. View of H Plane and E Plane Bends (5) Connecting the TMA interface, KRFU Power, and Control Interface Power and control signals for the TMA assembly is supplied from the KANDU and is connected to TMA J2 receptacle. Install location of KANDU is airframe specific. KANDU could be installed in unpressurized area near the tail empennage of the aircraft or inside pressurized area of the aircraft.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (d) 3 Make sure that the over braid of the cable assembly is terminated to connectors at both KRFU and Modman or the bulkhead interface feed through ends. 4 The over braid can be terminated to connector shield/housing or directly to housing. Make sure that all cable assembly routing are firmly held with wire clamps in accordance with the airframe specific wiring diagram and there are no obstruction to the free movement of tail mount antenna.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Technology; Bulletin Number 65, Edition 97-01: Evaluating compliance with FCC Guidelines for human exposure to Radio Frequency Electromagnetic fields. M. (2) The areas which the risk exists are based upon the location of the antenna. This means personnel operating on the apron, transient personnel, and the general population in the controlled exposure category will not be exposed to levels in excess of the limits.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • FMA LRU • KRFU LRU (if installed outside aircraft) • Radome assembly • A791 based AIM or the LAIM • Radome skirt fairing. The exact install location of the A791 based AIM or LAIM and KRFU is airframe specific. The KRFU can be installed on the inside or outside the fuselage of the aircraft. Honeywell recommends to install the KRFU on the A791 based AIM or LAIM outside the fuselage of the aircraft.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System WARNING: THIS EQUIPMENT RADIATES HIGH FREQUENCY RADIATION AND POSES A RADIATION HAZARD. CONSIDERING THE WORST CASE CONDITION OF 100 PERCENT REFLECTION FOR THE FUSELAGE MOUNT ANTENNA, HONEYWELL DEEMS IT NECESSARY TO ASSURE OEM FUSELAGE ATTENUATION EXCEEDS 21.03 dB FOR FUSELAGE MOUNTED ANTENNAS SYSTEM INSTALLATION.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-7. FMA installation Kits(Cont) (6) PN Description 90404243 RF component kit (KRFU to FMA waveguide and RX coax cable FMA to KRFU) Airframe Structural Modifications For the installation of OAE-FMA, structural modifications to the airframe may be required in the region where the OAE-FMA is to be mounted to accommodate the additional mass of the antenna assembly and resulting aerodynamic loads.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-9. FMA Install Location The fuselage antenna assembly and KRFU (if installed outside the aircraft) will be mounted on the antenna interface mount and it suplies a means to secure all equipment and wiring mounted on it. Depending on the airframe, the A791 based AIM or LAIM is installed to provide a firm flat base for installation of the FMA and KRFU. These are detailed in the next sections.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-10. Typical Ground Strap Arrangement for A791 Compliant Fittings The aircraft coordinate system orientation and fitting layout are shown in Figure 2-11. Figure 2-11. Aircraft Coordinate System Orientation and Fitting Layout (a) Position and install the A791 based AIM fittings onto aircraft fittings for fittings #1, #2, #5, #6, and #7.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System that they will pass through the openings in the adapter plate as AIM assembly is lowered onto aircraft. Refer to Figure 2-12. (e) Refer to the airframe specific kits and assembly for fastener specifications to install A791 complaint AIM fittings to aircraft fittings. NOTE: Consult airframe manufacturer for choosing the correct torque values.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Install the LAIM to the Aircraft Fuselage (a) Make sure that all the fittings are oriented vertically with the alignment tools, to help when you lower the LAIM onto aircraft fittings. (b) Put the LAIM assembly onto aircraft install location. Refer to Figure 2-13 for a generic LAIM installation on airframe structure. Figure 2-13. LAIM Assembly (c) The LAIM gets attached to aircraft structure at six machined fitting locations.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-14. Radome Skirt Fairing and LAIM Assembly Position on Aircraft (10) FMA Bonding The bonding straps are installed before proceeding with installation of FMA assembly on the A791 based AIM or LAIM. The FMA assembly and KRFU must be bonded to the airframe. Consult the airframe manufacturer for the correct torque values. N.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (a) Align the FMA assembly above adapter plate with an aircraft service hoist. Attach hoist to the FMA lifting fixture at two locations on each side of fixture. Refer to Figure 2-15. Figure 2-15. FMA Assembly (b) Put the FMA onto the FMA mounting holes with alignment pins and make sure that the waveguide flange is pointed to the rear of the AIM. Make sure that the pigtails do not interfere to avoid damage. (c) Remove the FMA lifting fixture.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-16. FMA Assembly Lifting Fixture Removal (2) (3) (4) (d) The orientation of the FMA assembly is defined with respect to the principal axes of the aircraft. (e) Attach the FMA to the AIM with screws and flat washers. The AIM is provisioned with captive nuts. Refer to the airframe specific kits and assembly for fastener specifications and required torque.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (f) (5) It is recommended to use flexible waveguide / Coax RF interface with interconnect losses not to exceed 1.5 dB on the transmit path and 2.9 dB on the receive path between the KRFU and FMA assembly. Honeywell has developed a RF component kit (90404243) containing a suitable waveguide and coaxial cable. KRFU Installation Refer to Section 4.K.(3). KRFU Installation procedure.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The IF TX and IF RX signals to KRFU are supplied from the Modman. These are routed through bulkhead interface. Refer to the appropriate FMA interconnection diagram Figure 2-34, Figure 2-35, or Figure 2-36 for details. (a) (b) (c) (d) Remove the protective covers from the FMA P2 and KANDU J2 receptacles. Visually examine the connectors and make sure that the pins are straight and undamaged.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-18. A791 Based AIM Assembly with FMA and KRFU Placement on Aircraft Figure 2-19. LAIM Assembly with FMA and KRFU Placement on Aircraft On completion of the LRU interconnection and applying power to the FMA, the FMA will stay in its current position until it is told to move by the KANDU. (8) AIM/LAIM Radome Installation The radome installation is aircraft specific. See aircraft specific SDIM for details.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System With the LAIM, the radome will be installed on the Radome skirt fairing assembly. Refer to the and Figure 2-20. Figure 2-20. Radome Assembly Mounted on Radome Skirt Fairing (LAIM) O. FMA Alignment On completion of physical installation of the FMA, the installed antenna system has to be aligned and calibrated for any possible installation offsets.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Q. (2) The areas which the risk exists are based upon the location of the antenna. This means personnel operating on the apron, transient personnel, and the general population in the controlled exposure category will not be exposed to levels in excess of the limits. Maintenance personnel working close to the tail must be protected by disabling the transmitter before they approach that area of the aircraft.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-21. GUI Login Page (b) Enter the username and password below to access the maintenance interface. • Username: "Maintenance" and Password: "Earthbound". (3) Positioning of Aircraft for Antenna Alignment (a) On the GUI Calibrate Antenna Alignment page, as shown in Figure 2-22, the current location of aircraft in terms of latitude and longitude is indicated along with the longitude of the servicing Geo stationary satellite.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-22. GUI Calibrate Antenna Alignment Page (b) For the automatic antenna alignment calibration, it is recommended to tow and put the aircraft in an open area away from aircraft hangers such that there is clear visibility to the open sky with the heading of the aircraft pointed in one of four recommended aircraft heading values displayed on the GUI antenna calibration page.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • RSSI as reported from the Modman. (a) The GUI page indicates the status of the aircraft. In order to proceed with the antenna calibration process, all LRUs of the JetWave™ system need to be powered up with aircraft IRS system functioning and providing valid inputs. The GUI page indicates the IRS status.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-8.
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E90400059-0001-1-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-24. Modman Outline and Installation Drawing (Sheet 1 of 4) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90400059-0001-2-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-24. Modman Outline and Installation Drawing (Sheet 2 of 4) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90400059-0001-3-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-24. Modman Outline and Installation Drawing (Sheet 3 of 4) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90400059-0001-4-C SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-24. Modman Outline and Installation Drawing (Sheet 4 of 4) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System E90401592-1-D DELETED Figure 2-25. APM Outline and Installation Drawing (Sheet 1 of 2) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401592-2-D SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-25. APM Outline and Installation Drawing (Sheet 2 of 2) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401567-1-B SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-26. KANDU Outline and Installation Drawing (Sheet 1 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401567-2-B SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-26. KANDU Outline and Installation Drawing (Sheet 2 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401567-3-B SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-26. KANDU Outline and Installation Drawing (Sheet 3 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401573-1-A PRODUCTION - Release - 15 Aug 2014 13:44:15 MST - Printed on 26 Aug 2014 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-27. KRFU, Conduction-Cooled 1, Outline and Installation Drawing (Sheet 1 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401573-2-A SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-27. KRFU, Conduction-Cooled 1, Outline and Installation Drawing (Sheet 2 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90401573-3-A SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-27. KRFU, Conduction-Cooled 1, Outline and Installation Drawing (Sheet 3 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90402347-1-B SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-28. KRFU, Conduction-Cooled 2, Outline and Installation Drawing (Sheet 1 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90402347-2-B SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-28. KRFU, Conduction-Cooled 2, Outline and Installation Drawing (Sheet 2 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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E90402347-3-B SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-28. KRFU, Conduction-Cooled 2, Outline and Installation Drawing (Sheet 3 of 3) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
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SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.