Draft as of 31 May 2017 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.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Proprietary Information Honeywell – Confidential COPYRIGHT BY HONEYWELL LIMITED. (“HONEYWELL”). ALL RIGHTS RESERVED. THIS DOCUMENT AND ALL INFORMATION CONTAINED HEREIN ARE THE CONFIDENTIAL AND PROPRIETARY INFORMATION OF HONEYWELL AND CONTAIN HONEYWELL TRADE SECRETS.
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Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 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.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Copyright - Notice Copyright 2015, 2017 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 4 3 Mar 2017 Our products are under continuous research and development.
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Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System TRANSMITTAL INFORMATION TO 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.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Remove and discard all pages of the manual and replace them with the attached pages. Write the revision number, revision date, and replacement date on the Record of Revisions page. Revision bars mark the technical data that changed in this revision; those changes are described in the Table of Highlights. Editorial changes are not marked with a revision bar.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 2-1 Paragraph 2.1, revised the title from “Overall Jetwave System Architecture” to “Jetwave System Overview”. All 2-2 Table 2-1, revised the PN for TMA from 904000013-0001 to 904000013-0001. All 2-3 Table 2-4, revised the operating temperature range and deleted APM in Interfaces.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 3-1 Table 3-1, removed the Primary/Secondary concept. Grouped Combined the rows for Labels 254, 255, 261, 132, 175 and Labels 112, 110, 111, 76 and 314. Removed rows for Labels 331, 332 and 333. All 3-2 Table 3-1, removed the Acceptable Replacement to Primary Labels 361 and 312 and added Labels 125. All 3-3 Paragraph 3.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 4-8 Paragraph 4.3(1), added reference to Figure 4-26 and updated Step (1)(g). All 4-9 Paragraph 4.3, Moved the existing Step (2)(a) to (1)(g). Added Steps (2)(a), (2)(b) and (2)(c) for KANDU receptacle A3J, KANDU receptacle A3J2 and KANDU receptacle A3J3. All 4-14 Paragraph 4.6, revised the title as “KRFU”. All 4-15 Added Paragraph 4.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 4-41 Paragraph 4-11, revised “Variant 1” as “Variant 2” in the step referring to Figure 4-26. All 4-41 Paragraph 4-11, added reference to new Figure 4-24. All 4-43 Paragraph 4.11, added note stating that the Fuselage Mount Radome is offered as a standard part with varying skirts to the step referring to Figure 4-32.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 6-2 Paragraph 6.1, revised “maximum spot beam capacity” to “defined Maximum Information Rate” and “or Minimum” as “for 95% of the time”. All Revised to state that the updates do not adversely affect system safety, operational capabilities and does not impact flight crew workload. Revised to remove "On the next power up" 6-3 Paragraph 6.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 6-13 Paragraph 6.5A, revised to add “or replacement” condition. All 6-13 Paragraph 6.5A, Step (2), revised the physical installation procedure. All 6-14 Paragraph 6.6A., Step (3) revised the requirement for antenna alignment. All 6-14 Paragraph 6.6A, Step (5), replaced “open the link index.html” with “enter 172.29.55.1 in the address bar”.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 7-7 Paragraph 7.2F, Step (2), added a note to refer to Saint Gobain SRM for FMA radome. 7-14 Table 7-1, added L1 code 0x23 with description “Modman input discretes from LRU”. All 7-16 Table 7-3, added “Modman input discretes from KANDU (23)” under L1 column with 0x 00 under L2 Code and “Unknown” under L2 Description column.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity 7-41 thru 7-43 Table 7-6, revised L2 code Software runtime (FE) completely. All 7-43 Table 7-6, moved L3 code 0x 0022 and its L3 description and repair action entries under L2 Unknown (00). All 7-44 Table 7-6, moved L2 code ASC (01) to KANDU (06). Deleted entry ASC (05).
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table of Highlights (Continued) Page Description of Change Effectivity C-3 Paragraph 1.A, in the table, revised the item description for the parameter “Electrical wiring - APM to Modman”. All C-5 Revised the figure reference from 4-21 to Figures 4-30. All C-7 Revised the figure reference as Figures 4-21 and 4-22. All Paragraph 1.
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Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System RECORD OF REVISIONS For each revision, write the revision number, revision date, date put in the manual, and your initials in the applicable column. NOTE: Refer to the Revision History in the TRANSMITTAL INFORMATION section for revision data. Revision Number Issue Date Date Inserted Inserted by (initial) 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 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.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SERVICE BULLETIN LIST Service Bulletin Number Manual Rev. Number Subject Manual Rev. Date JETWAVE-23-0001, COMMUNICATIONS - JETWAVE™ SYSTEM Rev.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page Date Title T-1 T-2 T-3 T-4 T-5 T-6 * * * * * * 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 Transmittal Information TI-1 TI-2 TI-3 TI-4 TI-5 TI-6 TI-7 TI-8 TI-9 T-10 T-11 T-12 * * * * * * * * * * * * 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 Record of Revisions 1 2 3 Mar 2017 3 Mar 2017
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page F F F F F F F Date 4-4 4-5 4-6 4-7 4-8 4-9 4-10 4-11 4-12 4-13 4-14 4-15 4-16 4-17 4-18 4-19 4-20 4-21 4-22 4-23 4-24 4-25 4-26 4-27 4-28 4-29 4-30 4-31 4-32 4-33 4-34 4-35 4-36 4-37 4-38 4-39 4-40 4-41 4-42 4-43 4-44 4-45 4-46 4-51 4-52 4-53 4-54 4-55 * * * * * * * * * * * * * * * * * * F 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2
Draft as of 31 May 2017 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 Date 4-104 4-105 4-106 4-107 4-108 4-109 4-110 4-111 4-112 4-113 4-114 4-115 4-116 4-117 4-118 4-119 4-120 4-121 4-122 4-123 4-124 4-125 4-126 4-127 4-128 4-129 4-130 4-131 4-132 4-133 4-134 4-135 4-136 4-137 4-138 4-139 4-140 4-141 4-142 4-143 4-144 * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page Date 7-8 7-9 7-10 7-11 7-12 7-13 7-14 7-15 7-16 7-17 7-18 7-19 7-20 7-21 7-22 7-23 7-24 7-25 7-26 7-27 7-28 7-29 7-30 7-31 7-32 7-33 7-34 7-35 7-36 7-37 7-38 7-39 7-40 7-41 7-42 7-43 7-44 7-45 7-46 7-47 7-48 7-49 7-50 7-51 7-52 7-53 7-54 7-55 * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * F 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Subheading and Page Date 8-4 8-5 8-6 * * * Appendix A: Specifications A-1 A-2 A-3 A-4 A-5 A-6 A-7 A-8 A-9 A-10 A-11 A-12 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 3 Mar 2017 Appendix B: Installation Information Sheet B-1 3 Mar 2017 B-2 3 Mar 2017 Appendix C: Installation Checklist C-1 * 3 Mar 2017 * F Subh
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Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System TABLE OF CONTENTS Title Page SECTION 1 - INTRODUCTION 1.1 How to Use This Manual .................................................................................................................... 1-1 A. General ......................................................................................................................................... 1-1 B. Observance of Manual Instructions .................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 2.5 About Inmarsat Services ................................................................................................................. 2-14 SECTION 3 - SYSTEM PRE-CONFIGURATION 3.1 AES Configuration Data .................................................................................................................... 3-1 A. B. C. AES System Configurations ..........................................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System E. F. G. H. I. J. K. L. 4.9 TMA Installation Kit Details ..................................................................................................... 4-36 TMA Airframe Structural Modifications ................................................................................... 4-37 TMA Mounting Guidelines.......................................................................................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 7 -TROUBLESHOOTING 7.1 Post-installation Troubleshooting ....................................................................................................... 7-1 7.2 Accessing the Maintenance Interface ................................................................................................ 7-1 A. B. C. D. E. F. G. H. Checking Status Information............................................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. D. E. JetWave™ AES KRFU Installation Information Sheet..............................................................B-1 JetWave™ AES Modman Installation Information Sheet..........................................................B-2 JetWave™ AES APM Installation Information Sheet................................................................B-2 APPENDIX C 1. Installation Checklist........................................
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Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System LIST OF TABLES Table Description Page Table 2-1 JetWave™ System LRUs ...............................................................................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table D-6 Table D-7 Table D-8 Table D-9 Table D-11 Table D-12 Table D-13 Table D-14 Weight on Wheels ..........................................................................................................D-4 ARINC Tx Mute and Tail Sector Mute Switch ................................................................D-4 ARINC791 Equipped .........................................................................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System LIST OF FIGURES Figure Description Figure 1-1 Symbols ......................................................................................................................... 1-2 Figure 2-1 Ka-Band System ............................................................................................................ 2-1 Figure 2-2 JetWave™ System Block Diagram ..............................................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-31 Figure 4-32 Figure 4-33 Figure 4-34 Figure 4-35 Figure 4-36 Figure 4-37 (Sheet 1 of 14) FMA Outline and Installation Drawing (90000380ICD, REV L) ........... 4-82 (Sheet 1 of 6) Fuselage Mount Radome Outline and Installation Drawing (90401395, REV D) .........................................................................................................................
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 1 INTRODUCTION 1.1 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.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 1-1. Symbols D. Units of Measure (1) E. 1.2 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.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • 90401027-005 - JetWave™ System MCS 8000 Class A Forced Air KRFU, Version 2, FMA • 90400017-XXX - A791 Radome Package • 90400016-XXX - Non-A791 Radome Package. 1.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. Other Publications (1) These publications are standard references. Check for the latest version of the publication. • The United States GPO Style Manual (available at http://www.gpo.gov/fdsys/pkg/GPO-STYLEMANUAL-2008/content-detail.html) • IEEE Std 260.1, Standard Letter Symbols for Units of Measurement (available from the American National Standards Institute at http://www.ansi.org) • ASME Y14.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System CAUTION: 1.8 THIS EQUIPMENT INCLUDES ITEMS THAT ARE ELECTROSTATIC DISCHARGE SENSITIVE DEVICES. ELECTROSTATIC DISCHARGE SENSITIVE DEVICES ARE SUBJECT TO DAMAGE BY EXCESSIVE LEVELS OF VOLTAGE AND/OR CURRENT. THE LOW-ENERGY SOURCE THAT MOST COMMONLY DESTROYS ESDS DEVICES IS THE HUMAN BODY, WHICH, IN CONJUNCTION WITH NONCONDUCTIVE GARMENTS AND FLOOR COVERINGS, GENERATES AND RETAINS STATIC ELECTRICITY.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations (Continued) Term Full Term CAT commercial air transport CBIT continuous built-in test CIR committed information rate cm centimeter dB decibel DER designated engineering representative DHCP dynamic host configuration protocol DID data item description DNS domain name system DP distribution partner EMEA Europe, the Middle East, and Africa ESDS electrostatic discharge s
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations (Continued) Term Full Term IRU inertial reference unit ISDN integrated services digital network ISP Inmarsat service provider or internet service provider Ka part of the radio frequency spectrum: 26.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System List of Acronyms and Abbreviations (Continued) 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 descr
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 2 DESCRIPTION 2.1 JetWave™ System Overview 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 2-1. Figure 2-1. Ka-Band System A Modman is provided within the AES to enable two-way communications.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-1. JetWave™ System LRUs LRU PN Modman 90400012-0001 Modman Variant 2 90400012-0002 APM 90401121 KANDU 90401566 KANDU Variant 2 90404518 KRFU Conduction Cooled Variant 1 90401203 KRFU Conduction Cooled Variant 2 90402346 KRFU Forced Air Cooled 90401202 FMA 90000380-1 TMA 90400013-0001 A791 FM radome 90400017-XXX Non-A791 FM radome 90400016-XXX Table 2-2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-3. Non A791 Style Radome Package Variant Aircraft Non A791 Style Radome Package Variant A319/A320/A321 90400016-01 A330/A340 90400016-02 A350 90400016-03 A380 90400016-04 B737/B757 90400016-05 B747 90400016-06 B777 90400016-08 B787 90400016-09 B767 90400016-10 B. JetWave™ System LRU Leading Particulars (1) Refer to Table 2-4 for the Modman leading particulars.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-4. Modman Leading Particulars (Continued) Characteristic Specification Mounting information 4-MCU, forced-air, ARINC 600 series tray Maintenance No scheduled maintenance required Interfaces J1A - PODD, PIESD, and AISD J1B - APM, Aircraft, PODD, PIESD, AISD, and KANDU J1C - IF to/from KRFU and aircraft power Table 2-5. APM Leading Particulars Characteristic Specification Length 4.515 inches (114.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-6. KANDU Leading Particulars (Continued) Characteristic Specification Operating temperature -67°F (-55°C) to 158°F (70°C) Maintenance No scheduled maintenance required Interfaces J1 - Aircraft and Modman J2 - Power to OAE and IMU (38.5 and 24 VDC) J3 - KRFU, OAE, and maintenance J4 - Ethernet (quadrax) Table 2-7.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-7. KRFU Leading Particulars (Continued) Characteristic Specification Conduction-cooled 2 configuration: Length 16.55 inches (420.4 mm) maximum Width 9.01 inches (228.8. mm) maximum Height 2.08 inches (52.8 mm) maximum Weight 11.30 pounds (5.1 kg) maximum Operating voltage 115 VAC, 400 Hz Power consumption 300 watts maximum at transmit amplifier saturation.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-7. KRFU Leading Particulars (Continued) Characteristic Specification Power dissipation 260 watts maximum at transmit amplifier saturation. 200 watts maximum at maximum nominal system transmit power. 167 watts typical at maximum nominal system transmit power. Cooling Forced air, 169.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 2-9. FMA Leading Particulars Characteristic Specification Weight 83 pounds (37.6 kg) maximum NOTE: The lifting fixture is 5.5 pounds (2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 2-2. JetWave™ System Block Diagram The JetWave™ system LRUs are as follows: A. Outside Antenna Equipment • The OAE can include the following components: • Mechanically steered antenna - either fuselage mount or tail mount. • Radome package - fuselage mount configuration only (tail mount individual radomes are available per aircraft type). • KRFU 23-15-29 © Honeywell International Inc.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • RF component kit - fuselage mount configuration only. (tail platforms installation kits containing RF interconnects are available depending on aircraft type). • OAE installation kit (optional, for ARINC 791 style configuration only). • The antenna includes an aperture. • The OAE is powered by the KANDU. • Contains an LNA for amplification of signals in the receive path.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. D. KANDU • Receives commands from the Modman through an Ethernet interface to configure the antenna/KRFU and reports status over this Ethernet interface. • Contains the positioning algorithm to allow the pointing of the antenna with inputs from the IRU, information from the RSSI detector in the Modman, and the IMU from the antenna. • Provides power and control to the antenna.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 2.3 Honeywell Implementation The Honeywell implementation varies from the ARINC 791 configuration as follows: • No ARINC 629 support is provided (optional in ARINC 791). • No EN1 Ethernet functionality between the KRFU and KANDU is provided (the provisioned standard inter-wiring is not utilized).
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. System Initialization Mode In the System Initialization Mode, the Modman starts additional POST and BITE, system access, and SNMP services. The Modman attempts to establish communication with KANDU and OAE. The RF transmission is disabled in this mode. While in System Initialization Mode, the RS422, discrete signal and the Ethernet interfaces are available and active on all the JetWave™ LRUs which are powered up.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System F. Commanded Mode The system also provides a Commanded Mode of operation which may be initiated through the GUI when the aircraft is on ground. This mode provides access to user initiated tests for system testing, initiating automatic antenna alignment, transmit cable calibration, manual antenna pointing to defined location, etc. The system will come out of the commanded mode by a System reset. 2.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 3 SYSTEM PRE-CONFIGURATION 3.1 AES Configuration Data NOTE: Any tools for preparing the config files for the terminal must be licensed from Honeywell. The AES configuration data is a set of configuration files, stored on the APM. Each configuration file contains a set of airplane-unique parameters.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 3-1. ARINC 429 Label List 255 /111 Yes 261 /76 132 /314 324 Yes Hybrid /GNSS 160 /1000 100 /20 0.000172° 65 /1000 110 40 /20 50 0.125 ft Pitch Angle Hybrid /GNSS Hybrid /INS INS 50 20 0.0055° /0.4° 0.011° 325 Yes Roll Angle INS 50 20 0.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System B. Regulatory Log Configuration Parameters The regulatory log configuration parameters file (APM file - reglog.cfg) contains details of the remote server to use to transfer the regulatory log data. C. Aircraft Service Configuration There are a number of functions that an Ethernet port can support namely, data traffic, data loading, GUI, AES logs extraction (maintenance function) and status/control (through the SNMP).
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Blank Page 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System SECTION 4 INSTALLATION 4.1 Overview A. Installation Procedure Overview for the JetWave™ System This section includes information about installing the equipment in the core JetWave™ system. Contact VAR/DP/Honeywell about installation kits that include mating connectors and cables.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 4.2 (2) Install the OAE and JetWave™ components in accordance with the installation drawings provided. (3) Install wiring in accordance with the interconnection diagram. The cables and adapters are available as installation kits from various suppliers. (4) Do wiring and RF cable checks to make sure they are installed correctly and meet the installation requirements. (5) Apply power to the system.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 4-1.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 4-2. Modman Cable Loss Values Cable Loss @ 950 MHz < 6.5 dB > 6.5 dB, <11 dB > 11 dB Equalizer in TX path 10.5 dB Minicircuits, PN TAT-10R5DC1+ (10.5 dB equalizer) or equivalent 4.8 dB Minicircuits, PN TAT-4R8DC11+ (4.8 dB equalizer) or equivalent None Attenuator in RX path 10.5 dB Minicircuits, PN TAT-10R5-1+ (10.5 dB attenuator) or equivalent 4.8 dB Minicircuits, PN TAT-4R8-1+ (4.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Data link available (Modman MP13F) open/ ground output connected to a lamp.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 4-3.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Table 4-3.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System NOTE: The following ARINC 791 discretes are not supported: 4.3 • Cell Transmit Enable (ModMan J1-MP11B) • Remote Management Enable (ModMan J1-MP10A) • Cooling System Available (ModMan J1-MP11F). KANDU Refer to Figure 4-25 and Figure 4-26 for outline and installation information. Refer to Figure 4-34 thru Figure 4-37 for the applicable interconnect diagram.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (i) It is recommended that the bulkhead interface be installed such that receptacle pins are on the pressurized area and receptacle sockets are on the unpressurized side of the aircraft. (j) The bulkhead interface connectors must be electrically bonded to the aircraft.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (3) The KANDU must be electrically bonded to the airframe through contact with the base of the unit as follows: • At least one of the two provided mechanical attachment points for electrical bonding must be used for bonding the KANDU to the airframe. Make sure that the all mating surfaces in the bonding path are free from contaminants such as paints or other non-conductive elements. • One 0.65 inch (16.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The aircraft coordinate system orientation and fitting layout are shown in Figure 4-2. Figure 4-2. Aircraft Coordinate System Orientation and Fitting Layout (1) Position and install the A791 based AIM fittings onto aircraft fittings for fittings #1, #2, #5, #6, and #7. (2) Use the alignment tools to make sure that the fitting slip in X-direction is centered for fittings #2, #6, and #7.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-3. AIM Assembly Placement on Aircraft Figure 4-4. A791 Based AIM Assembly with FMA and KRFU Placement on Aircraft 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 4.5 Installation Guidelines for the LAIM (If applicable) NOTE: Please see Figure 4-33 LAIM outline and installation drawing, 90404861, for installation details. The installation sequence suggested for mounting the LAIM is as follows: A. B. • Install the LAIM and radome skirt fairing bonding straps. • Install the LAIM to the aircraft fuselage. • Install the radome skirt fairing.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (3) C. Refer to the airframe specific kits and assembly for fastener specifications to install LAIM to aircraft. Install the Radome Skirt Fairing (1) Put the radome skirt fairing assembly onto the aircraft. Refer to the airframe specific kits and assembly for fastener specifications to install radome skirt fairing assembly to aircraft. Figure 4-6 shows the radome skirt assembly along with LAIM.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (2) B. The TX path interconnect loss between the KRFU and the FMA must not exceed 1.5 dB. The loss is from KRFU flange to antenna flange. KRFU Thermal Pad Kit (1) The thermal pad kit, PN SCD-90402388, is intended to provide a conduction interface between the bottom surface of the KRFU conduction units of two configurations, PN 90401203 and PN 90402346, and airplane cold plate or mounting panel.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (b) Immediately before installing the KRFU into the aircraft, remove white opaque protective backing on both pads to expose the non-tacky side of the thermal pad. NOTE: If the KRFU unit is to be shipped or stored before installation, do NOT remove the white opaque backing on the thermal pads. NOTE: Honeywell does not recommend applying the thermal pad to the KRFU if the KRFU is to be shipped or stored.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System NOTE: When the aircraft is on the ground and the AES is transmitting, and the ambient outside temperature is very hot, then the mounting plate temperature can be exceeded. The exact outside air temperature and operating conditions are installation dependent. Consult with your hardware supplier for further details.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System than 1° off heading, pitch or roll with respect to principle axis of aircraft. Depending on the airframe, as part of the OAE FMA, the LRUs and assemblies that follow will be installed outside aircraft: • FMA LRU • KRFU LRU (if installed outside aircraft) • Radome assembly • ARINC 791 based AIM or the LAIM • Radome skirt fairing.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System C. Advisories The JetWave™ FMA and the KRFU subsystems include components that radiate RF and microwave emissions in the band between 29.0 and 30.0 GHz. All service technicians and operators must be informed of the potential hazards of RF and microwave radiation. When installing and servicing equipment, exercise the safety precautions that follow.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System For the ARINC 791 configuration; the seven aircraft side fittings, internal structural modifications, internal wiring, and bulkhead connectors are the responsibility of the installer.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The FMA may be installed anywhere on the top of the aircraft, Honeywell recommends not installing the FMA at the mid fuselage station near the wing or slightly aft of the wing due to higher aero loads. . Figure 4-8.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System • Connecting Bulkhead Interface, KRFU power and control interfaces. • Position and installation of radome. (1) Installation of the FMA Assembly (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 4-9. Figure 4-9.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-10. FMA Assembly Lifting Fixture Removal (2) (3) (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.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Remove protective cap on FMA J4 (2.92 mm female coax) and FMA J3. Connect K-type disconnect plug to K-type disconnect receptacle J4 on the FMA and torque to 7 in-lb (0.79 Nm) or as specified by the cable manufacturer. Connect the WR34 waveguide assembly to the FMA receptacle J3.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System The 115 VAC power supply for the KRFU is supplied from the aircraft power and is connected to KRFU J1 receptacle. The IF TX and IF RX signals to KRFU are supplied from the Modman. These signals are routed through the bulkhead interface. Refer to the appropriate FMA interconnection diagram Figure 4-35, Figure 4-36 and Figure 4-37 for details.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System FUSELAGE ANTENNA MOUNT LOCAL ANTENNA INTERFACE MOUNT KRFU Figure 4-12. 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. (6) KRFU Installation Location with the TMA (if applicable) The KRFU install location at the top of aircraft tail empennage is airframe specific.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System It is recommended to use flexible waveguide/coax RF interface and with interconnect losses not exceeding 0.6 dB on the transmit path and stay within 0.5 to 2 dB on the receive path between the KRFU and the TMA assembly. The typical KRFU LRU and TMA assembly (swept volume model of antenna shown) interconnect arrangement is shown in Figure 4-13. Figure 4-13.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System 6 (c) Position and installation of the radome per Step (h). Waveguide and RF Coax interconnection to Tail Antenna assembly The waveguide and RF coax interconnect designs are aircraft specific. Consult aircraft specific SDIM for detailed installation instructions. NOTE: The waveguide and RF coax shall be connected to the TMA prior to installing the TMA to the aircraft.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System Figure 4-14. TMA RF TX J3 and RF RX J4 Interface Connector and Bonding Strap Locations 23-15-29 © Honeywell International Inc. Do not copy without express permission of Honeywell.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System (e) KRFU Installation 1 Make sure that the thermal pads are attached to the bottom of the KRFU. Refer to Section 4.6. KRFU. 2 Before proceeding with the KRFU installation, connect the WR42 waveguide to 2.92 mm coaxial connector adapter to KRFU J4 RF RX. a The adapter allows connection between the Rx WR-42 waveguide port on the KRFU and a 2.92mm coaxial connector.
Draft as of 31 May 2017 SYSTEM DESCRIPTION AND INSTALLATION MANUAL JetWave™ System selected. Apply torque to the fasteners in defined sequence for firmly mounting to the antenna interface mount or the tail structure of the aircraft. Do not use power tools to torque connection. 6 Install one end of the ground straps to the antenna interface mount or the tail structure plate at labeled ground points with screw and washers. Install bond connection joint sealant as required by installers standard procedures.
