FCC ID: K6KSMALLSATCOM Small UAV Satcom

Honeywell International Inc. 400 Maple Grove Road Ottawa, Ontario K2V 1B8 Canada CAGE: 38473 Telephone: 800-601-3099 (Toll Free U.S.A./Canada) Telephone: 602-365-3099 (International Direct) Website: https://aerospace.honeywell.com System Description, Installation, and Maintenance Manual Small SATCOM Part Number 90410350 Export Control Model Small SATCOM Kit Legal Notice These items are controlled by the U.S. government and authorized for export only to the country of ultimate destination for use by the ultimate consignee or end-user(s) herein identified They may not be resold, transferred, or otherwise disposed of, to any other country or to any person other than the authorized ultimate consignee or end-user(s), either in their original form or after being incorporated into other items, without firs obtaining approval from the U.S. government or as otherwise authorized by U.S. law and regulations. ECCN: 7E994. Publication Number D202006001015, Revision 2 Honeywell International Inc. Do not copy without express permission of Honeywell. Page T-1 Initial 30 Oct 2020 Revised 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Proprietary Information Honeywell - Confidential COPYRIGHT BY HONEYWELL INTERNATIONAL INC. (HONEYWELL). ALL RIGHTS RESERVED. THIS DOCUMENT AND ALL INFORMATION CONTAINED HEREIN ARE THE CONFIDENTIAL AND PROPRIETARY INFORMATION OF HONEYWELL AND CONTAIN HONEYWELL TRADE SECRETS. NEITHER THIS DOCUMENT NOR THE INFORMATION CONTAINED HEREIN MAY, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OF HONEYWELL. PLEASE REVIEW THE TERMS OF THIS AGREEMENT CAREFULLY BEFORE USING THIS DOCUMENT, AS BY USING IT, YOU ACKNOWLEDGE THAT YOU HAVE REVIEWED THIS AGREEMENT AND AGREE TO BE BOUND BY ITS TERMS AND CONDITIONS. Honeywell Materials License Agreement This document and the information contained herein (the Materials) are the proprietary data of Honeywell. These Materials are provided for the exclusive use of Honeywell-authorized Service Centers;

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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 Advisory WARNING: 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. Honeywell International Inc. Do not copy without express permission of Honeywell. Page T-4 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Copyright - Notice Copyright 2020, 2021 Honeywell International Inc. All rights reserved. Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies. THIS IS THE CMM FOSI - DATE: 20171123 Honeywell International Inc. Do not copy without express permission of Honeywell. Page T-5 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Blank Page Honeywell International Inc. Do not copy without express permission of Honeywell. Page T-6 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM TRANSMITTAL INFORMATION REVISION NUMBER 2 DATED 18 FEB 2021 TO HOLDERS OF SMALL SATCOM SDIM, PUB NO. D202006001015 AND IS ISSUED FOR USE IN SUPPORT OF THE FOLLOWING:

Table TI-1 shows the applicable components. Table TI-1. Applicable Components Component Part Number 90600511 89000015-009 90600596 90600551 90100090 Revision History Revision Number 0 1 2 Nomenclature Indoor Unit Low Gain Antenna Coaxial Cable Assembly Harness Assembly SIM Card SBB Revision Date 30 Oct 2020 30 Nov 2020 18 Feb 2021 Table TI-2 shows the revision history of this SDIM. Table TI-2. Revision History This revision is a full replacement. All changed pages have a new date, as identified in the List of Effective Pages. Revision bars identify the changed data. See Transmittal information for history of revisions to this SDIM. 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. The table of highlights tells users what has changed as a result of the revision. The table of highlights tells users what has changed as a result of the revision. The table consists of three columns. 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. The block of information often includes the MTOSS code. 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. The Effectivity column tells the user the part number(s) to which the block of information applies. The default value for this column is "All." "All" means that the block applies to all parts. Table of Highlights Task/Page Description of Change Effectivity Honeywell International Inc. Do not copy without express permission of Honeywell. Page TI-1 18 Feb 2021 Task/Page Description of Change Effectivity SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table of Highlights (Cont) Paragraph 1.A.6 Updated procedural step. Paragraph 2.A.5 Updated procedural step. Paragraph 2.A.7 Added procedural step. Paragraph 2.A.8 Added procedural step. Paragraph 2.A.11 Updated procedural step. All Paragraph 2.A.12 Updated procedural step and added list items. Paragraph 2.A.13 Changed the data from list items to procedural step. Paragraph 4.B.2 Added figure reference. Page11 Page11 Page12 Page12 Page12 Page12 Page12 Page24 Page26 Added figure. Page28 Paragraph 2.B.1 Added note. Page33 Added graphic sheet. Page41 Paragraph 2.A.1 Updated table. All All All All All All All All All All All Honeywell International Inc. Do not copy without express permission of Honeywell. Page TI-2 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Blank Page Honeywell International Inc. Do not copy without express permission of Honeywell. Page TI-3 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM RECORD OF TEMPORARY REVISIONS Instructions on each page of a temporary revision tell you where to put the pages in your manual. Remove the 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: A TR may be active, incorporated, or deleted. Active is entered by the holder of the manual. Incorporated means a TR has been incorporated into the manual and includes the revision number of the manual when the TR was incorporated. Deleted means a TR has been replaced by another TR, a TR number will not be issued, or a TR has been deleted. Temporary Revision Number Status Page Number Date Put in Manual Issue Date Date Removed from Manual By By Honeywell International Inc. Do not copy without express permission of Honeywell. Page RTR-1 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Blank Page Honeywell International Inc. Do not copy without express permission of Honeywell. Page RTR-2 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM SERVICE BULLETIN LIST Service Bulletin /

Revision Number Title Modification Manual Date Put in Honeywell International Inc. Do not copy without express permission of Honeywell. Page SBL-1 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Blank Page Honeywell International Inc. Do not copy without express permission of Honeywell. Page SBL-2 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM LIST OF EFFECTIVE PAGES Subheading and Page Date Subheading and Page Date Title T-1 T-2 T-3 T-4 T-5 T-6 TI-1 TI-2 TI-3 Transmittal Information Record of Temporary Revisions Service Bulletin List List of Effective Pages RTR-1 RTR-2 SBL-1 SBL-2 LEP-1 LEP-2 Table of Contents TC-1 TC-2 TC-3 TC-4 TC-5 TC-6 Introduction INTRO-1 INTRO-2 INTRO-3 INTRO-4 INTRO-5 INTRO-6 1 2 3 4 System Description 18 18 18 18 18 18 Feb 2021 Feb 2021 Feb 2021 Feb 2021 Feb 2021 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 indicates pages changed or added data

F indicates a right foldout LF indicates a left foldout 5 6 7 8 9 10

* 28 29 30 31 32

* 33 34 35 36 37 38 39 40 Installation

* 11

* 12

* 13 F F 14/15 16 17 18/19 20 21 22 23

* 24 25

* 26 27 System Operation Maintenance Practices Troubleshooting

* 41 42 43 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 Page LEP-1 18 Feb 2021 Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM LIST OF EFFECTIVE PAGES (Cont) Subheading and Page Date Subheading and Page Date Appendix A Appendix B 44 45 46 47 48 49 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 18 Feb 2021 indicates pages changed or added data

F indicates a right foldout LF indicates a left foldout Honeywell International Inc. Do not copy without express permission of Honeywell. Page LEP-2 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM TABLE OF CONTENTS LIST OF SECTIONS Title INTRODUCTION 1. How to Use This Manual ............................................................................................ A. General ............................................................................................................... B. Observance of Manual Instructions .................................................................... C. Units of Measure ............................................................................................... D. Illustration .......................................................................................................... E. Scope ................................................................................................................. F. Hardware Part Numbers .................................................................................... G. Organization ...................................................................................................... 2. Customer Support ...................................................................................................... A. Honeywell Aerospace Online Technical Publications Website ........................... INTRO-2 B. Honeywell Aerospace Contact Team .................................................................. C. References .......................................................................................................... 3. Acronyms and Abbreviations ...................................................................................... A. General .............................................................................................................. SECTION 1 SYSTEM DESCRIPTION 1. General Information .................................................................................................... A. General ............................................................................................................... B. Hardware Part Numbers ..................................................................................... 2. Indoor Unit ................................................................................................................... A. Indoor Unit Description ....................................................................................... 3. Antenna ....................................................................................................................... A. Antenna Description ........................................................................................... 4. Inmarsat Network ........................................................................................................ A. Scope .................................................................................................................. B. Honeywell SwiftBroadband System Overview .................................................... C. Expected Data Rate ........................................................................................... SECTION 2 INSTALLATION 1. General ....................................................................................................................... Honeywell International Inc. Do not copy without express permission of Honeywell. Page INTRO-1 INTRO-1 INTRO-1 INTRO-1 INTRO-1 INTRO-1 INTRO-1 INTRO-1 INTRO-2 INTRO-2 INTRO-3 INTRO-3 INTRO-3 1 1 3 3 3 4 4 5 5 5 6 11 Page TC-1 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title Page A. Prior to Installation ................................................................................................ 2. Mechanical Installation ................................................................................................... A. Antenna Mounting ................................................................................................... B. Indoor Unit Mounting .............................................................................................. C. Cable Routing ......................................................................................................... D. Miscellaneous .......................................................................................................... E. Engineering Drawings ............................................................................................. 3. Electrical Installation ....................................................................................................... A. General .................................................................................................................... B. Indoor Unit Installation ........................................................................................... 4. Physical Connectors ...................................................................................................... A. RF Cable ................................................................................................................. B. Harness Assembly ................................................................................................ 5. Final Validation .............................................................................................................. A. Installation validation should be by the following steps .......................................... B. Mission Safety Checks ........................................................................................... SECTION 3 - SYSTEM OPERATION 1. General ........................................................................................................................... A. System Overview ..................................................................................................... 2. Modes of Operations ....................................................................................................... A. System Interfaces .................................................................................................. B. WebUI ...................................................................................................................... C. PPPoE .................................................................................................................... D. RESTful ................................................................................................................... 3. Example Use Case (VPN) ............................................................................................... A. General ................................................................................................................... 4. INMARSAT Operational ................................................................................................. A. General .................................................................................................................. 5. USIM .............................................................................................................................. 11 11 11 16 20 20 22 24 24 24 24 24 24 27 27 27 28 28 28 28 28 34 34 35 35 37 37 37 Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC-2 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title Page A. General ............................................................................................................... 6. LED Indicator .............................................................................................................. A. Indications are as listed below: ......................................................................... 7. Temperature Profile .................................................................................................... A. Antenna .............................................................................................................. B. Indoor Unit ........................................................................................................ SECTION 4 MAINTENANCE PRACTICES 1. Maintenance ............................................................................................................... A. General ............................................................................................................. B. Cleaning ............................................................................................................. C. Inspection ......................................................................................................... D. Servicing ............................................................................................................ SECTION 5 - TROUBLESHOOTING 1. Installation Issues ...................................................................................................... A. General ................................................................................................................ 2. Operation Issues ......................................................................................................... A. General ............................................................................................................... APPENDIX A - CERTIFICATION AND REFERENCE DOCUMENTS 1. General ...................................................................................................................... A. Reference Documents ....................................................................................... B. Regulatory .......................................................................................................... 2. Radio Transmission Licensing .................................................................................... A. FCC and IC ....................................................................................................... B. European Technical Standards Institute (ETSI) ................................................ APPENDIX B - EXAMPLE USE CASE (VPN) SETUP DETAILS 1. VPN Server (Ground Side) ......................................................................................... A. Install OpenWRT on the router ......................................................................... B. Configure the router ........................................................................................... 2. VPN Client (Air Side) ................................................................................................... A. Install OpenWRT on the router ......................................................................... 37 37 37 37 37 37 39 39 39 39 39 41 41 41 41 44 44 44 44 44 45 46 46 46 48 48 Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC-3 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM TABLE OF CONTENTS (Cont) LIST OF SECTIONS (Cont) Title B. Configure the router ............................................................................................ Page 48 Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC-4 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM TABLE OF CONTENTS (Cont) LIST OF FIGURES Figure Description Page 1 2 3 4 5 6 7 8 9 10 11 Indoor Unit Assembly ............................................................................................. Forward and Return to UAV ................................................................................. Effect of Banking on Data Rate ............................................................................. BGAN Coverage Map ............................................................................................ Antenna Dimensions .............................................................................................. Indoor Unit Dimensions .......................................................................................... Safety Information Warning and Caution ............................................................... Terminal Outline and Installation ........................................................................... LEMO Termination ................................................................................................. 26 WebUI Configuration and Status Information ........................................................ Example Use Case (VPN) ..................................................................................... 2 7 9 10 14 18 21 23 29 36 Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC-5 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM TABLE OF CONTENTS (Cont) LIST OF TABLES Table Description INTRO-1 List of Acronyms and Abbreviations ..................................................... 1 2 3 4 5 6 7 8 Small SATCOM Kit Part Numbers ...................................................... Indoor Unit Component Specification .................................................. Antenna Component Specification ..................................................... Equipment Class and Subclass Identification .......................................... Antenna Cable Properties .. ............................................................ Termination Table . .. .. ............................................................... Ground Level Thermal Capabilities ..................................................... Fault Possible Causes . .. ............................................................. Page INTRO-3 3 4 5 5 24 25 38 41 Honeywell International Inc. Do not copy without express permission of Honeywell. Page TC-6 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM INTRODUCTION 1. How to Use This Manual A. General

(1) This manual provides information about the installation of the Small SATCOM UAV System.

(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

(5) Warnings and cautions go before the applicable paragraph or step. Notes follow the applicable

(1) All personnel must 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 instruction. paragraph or step. B. Observance of Manual Instructions and obey the safety precautions. C. 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.

(1) Supplemental illustrations use a suffix number to the basic figure number. For example, if Figure 501-5 is used, it signifies that it is an illustration of the item identified by index number 5 in Figure 501. Illustrations with no specific designation are applicable to all units. D. Illustration

(2) E. Scope

(1) This manual provides detailed information for avionics technicians about the wiring, installation, and setup of every component of the Small Satcom. This manual includes information for end users about how to operate the Small SATCOM. The Small SATCOM connects to the Inmarsat satellite network and is intended for use on UAVs for command, control and streaming back of live video and other mission data.

(1) The SATCOM products are identified by the hardware part numbers indicated in Table 1. A change to form fit or function will be reflected in a new base part number. F. Hardware Part Numbers

(2) Where:

G. Organization

(1) This manual Includes the following sections:

Honeywell International Inc. Do not copy without express permission of Honeywell. Page INTRO-1 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM SECTION 1 - SYSTEM DESCRIPTION SECTION 2 - INSTALLATION SECTION 3 - SYSTEM OPERATION SECTION 4 - MAINTENANCE PRACTICES SECTION 5 - TROUBLESHOOTING APPENDIX A APPENDIX B 2. Customer Support A. Honeywell Aerospace Online Technical Publications Website

(1) Go to the Honeywell Online Technical Publications Website at (https:/

/aerospace.honeywell.com). To download or see publications online. To order a publication. To tell Honeywell of a possible data error in a publication. B. Honeywell Aerospace Contact Team

(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 Contact Team 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). Honeywell International Inc. Do not copy without express permission of Honeywell. Page INTRO-2 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM C. References

(1) Honeywell/Vendor Publications Not applicable.

(b) Other Publications:

(a) Related Honeywell publications in this manual are shown in the list that follows:

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 Y14.38, Abbreviations for Use on Drawings and Related Documents (available from the American National Standards Institute at http://www.ansi. org) ASME Y14.5, Dimensioning and Tolerancing (available from the American National Standards Institute at http://www.ansi.org) ANSI/IEEE Std 91, Graphic Symbols for Logic Functions (available from the American National Standards Institute at http://www.ansi.org) CAGE codes and manufacturers addresses are available at https://cage.dla. mil IEEE 315/ANSI Y32.2, Graphic Symbols for Electrical and Electronics Diagrams

(available from the American National Standards Institute at http://www.ansi.org). 3. Acronyms and Abbreviations A. General

(1) The abbreviations are used in agreement with ASME Y14.38.

(2) Acronyms and non-standard abbreviations used in this publication are listed in Table INTRO-1 Table INTRO-1. List of Acronyms and Abbreviations FULL TERM Aeronautical Administrative Communication Aircraft Communications Addressing and Reporting System TERM AAC ACARS ACD AES AMSS ANSI AOC APC ARINC ASME ATA ATC ATE Aircraft Control Domain Aircraft Earth Station Aeronautical Mobile Satellite Services American National Standards Institute Aeronautical Operational Control Aeronautical Passenger Communications Aeronautical Radio, Incorporated American Society of Mechanical Engineers Air Transport Association Air Traffic Control Automated Test Equipment Honeywell International Inc. Do not copy without express permission of Honeywell. Page INTRO-3 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table INTRO-1. List of Acronyms and Abbreviations (Cont) Aeronautical Telecommunications Network FULL TERM Air Traffic Services American Wire Gage Broadband Global Area Network Celsius Commercial And Government Entity Code of Federal Regulation Cyclic Redundancy Check Circuit Switched Design Approval Holder Design Assurance Level Digital Signal Processor Electro-Magnetic Interference EMS Technologies Electrostatic Discharge Sensitive Fahrenheit Federal Communications Commission Government Printing Office Ground Earth Station Global Navigation Satellite System Global Positioning System Graphical User Interface High Power Amplifier HyperText Transfer Protocol Inches Interface Control Document Internet Protocol EASA EEPROM European Aviation Safety Agency Electrically Erasable Programmable Read-Only Memory TERM ATN ATS AWG BGAN C CAGE CFR CRC CS DAH DAL DSP EMI EMS ESDS F FCC GPO GES GNSS GPS GUI HPA HTTP in. ICD IP ISEDC ISO IEC IEEE Innovation, Science and Economic Development Canada International Standards Organization International Electro-technical Commission Institute of Electrical and Electronics Engineers Honeywell International Inc. Do not copy without express permission of Honeywell. Page INTRO-4 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table INTRO-1. List of Acronyms and Abbreviations (Cont) FULL TERM Illustrated Parts Catalog Light Emitting Diode Low Gain Antenna Micro Controller Unit Millimeter Minimum Operational Performance Standards Minimum Performance Standards Not Applicable Next Generation Satellite Services Operational Program Software Part Number Publication Printed Board Assembly Packet Data Protocol Point-to-Point Protocol over Ethernet Radio Frequency Radio Technical Commission for Aeronautics Society of Automotive Engineers Satellite Communications Swift Broad Band System Description and Installation Manual Satellite Data Unit Subscriber Identity Module International System of Units Transport Canada Civil Aviation Transport Layer Security Unmanned Aeronautical Vehicle United States Measurement System Universal Mobile Telecommunications Service UMTS Subscriber Identity Module Value Added Manufacturer Voice over IP Socit Internationale de Tlcommunications Aronautiques TERM IPC LED LGA MCU mm MOPS MPS NA NGSS OPS PN Pub. PBA PDP SBB SDIM SDU SIM SITA SI TCCA TLS UAV USMS UMTS USIM VAM VoIP PPPoE RF RTCA SAE SATCOM Honeywell International Inc. Do not copy without express permission of Honeywell. Page INTRO-5 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Blank Page Honeywell International Inc. Do not copy without express permission of Honeywell. Page INTRO-6 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM SECTION 1 SYSTEM DESCRIPTION 1. General Information A. General

(1) The Small SATCOM system is a very small and lightweight SATCOM terminal for use in UAVs for command, control and the streaming back of live video and other mission data. Refer to Figure 1.

(2) The Small SATCOM is an Inmarsat SwiftBroadband single channel low gain system providing an internet data connect with rates up to 200 kbps.

(3) The terminal comprises of an indoor unit and an external active antenna connected by a single cable.

(4) The indoor unit is typically mounted inside the fuselage.

(5) The antenna is typically mounted externally.

(6) Power and Ethernet are connected to the indoor unit and a single RF cable connects the indoor unit to the antenna. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 1 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 1. (Sheet 1 of 1) Indoor Unit Assembly Honeywell International Inc. Do not copy without express permission of Honeywell. Page 2 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM B. Hardware Part Numbers

(1) At the time of writing of this document, the SATCOM Products were identified by the hardware part numbers indicated in Table 1. SATCOM PRODUCT HARDWARE PART NUMBER Table 1. Small SATCOM Kit Part Numbers Indoor Unit Low Gain Antenna Harness Assembly Coaxial Cable Assembly SIM Card SBB

(2) Where:

90600511 89000015-009 90600551 90600596 90100090 A change to form fit or function will be reflected in a new base part number.

(3) The terminal is designed but not certified to DO-254 design assurance level (DAL) E Hardware functions whose failure or anomalous behavior, as shown by the hardware safety assessment, would cause a failure of system function with no effect on UAV operational capability or UAV flight operator workload. No guidance from DO-254 applies. 2. Indoor Unit A. Indoor Unit Description

(1) The Indoor unit contains the modem, digital and RF circuitry.

(2) The Indoor unit requires a combined power input and Ethernet cable which will be provided. The DC power input powers the whole system.

(3) The satellite data transfer, command, monitoring and debug are via Ethernet.

(4) A SIM card must be inserted into the indoor unit for it to operate.

(5) Table 2 provides the specifications or the Small SATCOMs Indoor Unit. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 3 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table 2. Indoor Unit Component Specifications COMPONENT Indoor Unit CHARACTERISTIC SPECIFICATION Part Number 90600511 Mounting Information Mounted inside the fuselage Length Width Height Weight Power Consumption 5.5 in. (140 mm) maximum 2.95 in. (75 mm) maximum 2 in. (50.8 mm) maximum 1.1 Lbs (0.5 kg) maximum 50 W for high use 65 W maximum 20 W in standby Operating Voltage 27-30V DC Cooling Refer to Section 3, Paragraph 7.B. Storage Temperature

-55 to 85C (-67 to 185F) Operational Temperature Refer to Section 3, Paragraph 7.B.

(6) The Indoor Unit has all the connectors on one side. This simplifies the installation of the Indoor Unit in a crowded avionics bay, as the box can be pushed into a corner or small gap between other equipment.

(7) An LED on the Indoor Unit provides an indication of its status. More detailed information can be accessed over the Ethernet connection. 3. Antenna A. Antenna Description

(1) The antenna will typically be mounted externally.

(2) A single RF cable connects the indoor unit to the antenna.

(3) Table 3 provides the specifications for the antenna. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 4 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table 3. Antenna Component Specifications COMPONENT Antenna CHARACTERISTIC SPECIFICATION Part Number 89000015-009 Length Width Height Weight Cooling Maintenance EIRP TX Operating Frequency 5.6 in. (142.24 mm) maximum 4.4 in. (111.76 mm) maximum 2 in. (50.8 mm) maximum 1.06 Lbs (0.482 Kg) maximum Passive Cooling No scheduled maintenance required 11.4 dBW nominal 1626.5-1660.5 MHz and 1668-1675 MHz (XLB) RX Operating Frequency 1518.0-1559.0 MHz Modulation G1D, G1E, G1W Emission Designation 1K69G1D, 1K69G1E, 1K69G1W Antenna Connector Type TNC (Female) Storage Temperature

-55 to 85C (-67 to 185F) Operational Temperature

-40 to 55C (-40 to 131F) RF Exposure Limits 3.517 ft (1.07 m) 4. Inmarsat Network A. Scope

(1) Please note all processes described in this manual apply to BGAN class 15.

(2) This class is detailed in the Table 4 Equipment Class Identification:

Table 4. Equipment Class and Subclass Identification EQUIPMENT CLASS IDENTIFIER DESCRIPTION AES Class 15 Aircraft Earth Station A 15 transceiver is defined as a transceiver unit capable of operating within an AES15 system, which uses a LGA. It includes the Indoor Unit and Antenna B. Honeywell SwiftBroadband System Overview

(1) The SATCOM Avionics Suite consists of a L-Band SATCOM system. The SATCOM system identified will operate on the Inmarsat network.

(2) Inmarsat supports the SwiftBroadband aeronautical service, also known as BGAN, which is supported through Inmarsat-4 satellites. Services offered in a given Ocean Region will operate from a single Inmarsat satellite at any one time.

(3) The Inmarsat L-Band SwiftBroadband Satellite Communications Network consists of:

Honeywell International Inc. Do not copy without express permission of Honeywell. Page 5 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Aircraft Earth Stations (AESs). Space segment formed by three Inmarsat-4 and an Inmarsat-4A geostationary satellites that provides global coverage, except for the polar regions. This will be supplemented by Inmarsat-6 satellites, which are scheduled for launch in 2020. A terrestrial ground infrastructure formed by the Satellite Access Stations (SASs). Terrestrial interconnect networks. Network Control Centre and a Business Support System.

(4) The user links are in L-band 1518-1559 MHz for satellite to AES, 1626.5-1660.5 MHz and 1668-1675 MHz for AES to satellite. C. Expected Data Rate

(1) The data rate through the Small Satcom terminal is dependent upon many factors such as size of ground plane, network congestion, satellite selection, multipath fading, satellite elevation, UAV banking etc. In general, the satellite with the highest elevation will work best and severe banking away from the satellite should be avoided.

(2) Forward refers to data being passed from the ground and return refers to data being passed from the UAV as seen in Figure 2. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 6 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 2. (Sheet 1 of 1) Forward and Return to UAV Honeywell International Inc. Do not copy without express permission of Honeywell. Page 7 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM

(3) The following charts provide an indication of how maximum data rates can be affected by banking towards the satellite (positive) or away from the satellite (negative), depending on satellite elevation, when T4.5 bearers are being used. Satellite elevation can be obtained via the webUI or by using a satellite pointer app. Refer to Figure 3 for effect of banking on data rate and Figure 4 for elevation. In Figure 3, if the signal is synced, the connection is maintained. If it is below the threshold, the connection will be lost. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 8 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 3. (Sheet 1 of 1) Effect of Banking on Data Rate Honeywell International Inc. Do not copy without express permission of Honeywell. Page 9 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 4. (Sheet 1 of 1) BGAN Coverage Map Honeywell International Inc. Do not copy without express permission of Honeywell. Page 10 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM SECTION 2 INSTALLATION 1. General A. Prior to Installation

(1) Upon receipt of the terminal, the components should be confirmed present against the enclosed parts list and inspected for any damage.

(2) The UAV satcom systems environmental parameters should be reviewed to ensure that the intended usage is within its envelope.

(3) An acceptable antenna mounting point should be identified and any UAV specific mounting parts procured or fabricated.

(4) A weight distribution analysis should be performed to demonstrate safe operation of the UAV subject to the mounting constraints outlined in the following sections.

(5) An electrical load analysis should be performed to ensure that the UAV can safely carry the additional electrical load. This is a maximum of 65 W.

(6) The terminal should be powered from a fused distribution board with voltage of 28V DC (27 to 30V DC). The fuse protecting the terminal supply circuit should be a 4A Fast Acting type, with a minimum interruption rating of 1000A. A recommended model is Littelfuse 0297004.WXNV which can be used in conjunction with the associated in-line holder Littelfuse 0FHM0001ZXJ.

(7) There should be a power isolation switch that can be operated without approaching within 3.517 ft (1.07 m) of the antenna.

(8) Safety precautions should be observed during installation and UAV maintenance.

(9) Integration with the avionic systems should be such that failure of terminals function should have no effect on the UAVs operational capability, safety or flying operators workload.

(1) The safety distance between operator and antenna is 3.517 ft (1.07 m).

(2) The antenna should be mounted so that it is in a horizontal plane when the UAV is flying straight and level. Refer to Figure 5 for antenna dimensions.

(3) The antenna should be positioned on the upper surface of the fuselage, near the centre-line of the UAV so that it has an unobstructed view of elevations above 5 for all azimuths. The connective performance for elevations below 20 will be degraded.

(4) The antenna should not adversely affect the control surfaces of the UAV.

(5) Separation resulting in greater than 42 dB isolation should be provided between the antenna and any other GPS antennas on the UAV at 1559 to 1605 MHz and 1626.5 to 1675.0 MHz

(Satcom band), 32 inch is typically required. If GLONASS is being used, the separation between the antenna and the GLONASS antenna should be sufficient to provide 50 dB isolation between them at 1559 to 1610 MHz and 1626.5 to 1675.0 MHz (Satcom band), 83 inch is typically required.

(6) GNSS antennas on the UAV should be compliant on DO-229D or later. 2. Mechanical Installation A. Antenna Mounting Honeywell International Inc. Do not copy without express permission of Honeywell. Page 11 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM

(7) The antenna mounting should be capable of dissipating at least 60W of heat from the antenna when in use. The heat load is primarily through the bottom metal surface of the antenna. Ensure that the mounting either conducts the heat away from the antenna or that there is sufficient airflow over the bottom of the antenna to take the heat out.

(8) The antenna should be mounted on, and electrically bonded to, a ground plane. The ground plane affects the antenna gain pattern. The larger the ground plane is the more reliable the satellite signal will be, particularly for lower satellite elevations. The minimum ground plane size should be 18cm in width by 30cm in length. The ground plane should be a conductive surface, level with the bottom surface of the antenna. The ground plane should have a resistivity of 6/cm or better. Where the ground plane leaves the plane of the bottom of the antenna, for example following the curve of a fuselage, its efficiency will drop.

(9) The antenna has a provision for mounting on the top surface of a UAV fuselage The hole for the RF connector should be 0.63 in. (16 mm) diameter.

(10) The O-ring for sealing the fuselage against water ingress should be fitted on the antenna.

(11) On metal skinned UAVs the thermal and ground plane requirements may be met if the antenna is thermally and electrically bonded to the surface of the aircraft. If the surface requires preparation to achieve electrical bond, refer to SAE AR 1870 Section 5. The electrical bond between the antenna and local structure must be less than or equal to 3 milliohm direct current (DC) resistance. Compliance should be verified using a calibrated milliohm meter. Any paint removed from the UAV skin to meet the bonding requirement should have a corrosion resistance protective coating applied that meets MIL-DTL-5541 TY II CL3 or MIL-C-5541 CL3, commonly known as Alodine. A doubler plate fabricated by the installer is normally used.

(12) On composite UAVs, additional structure may need to be added to meet the antenna thermal and ground plane requirements. The electrical bond between the antenna and ground plane must be less than or equal to 3 milliohm direct current (DC) resistance. Compliance should be verified using a calibrated milliohm meter. 2000 series aluminium or copper is recommended to meet the ground plane conductivity requirements. Normally, carbon fibre structures have too high a thermal and electrical resistance to meet the thermal and ground plane requirements.

(13) The antenna should be secured to the airframe using the 4 mounting screws supplied

(MS24693-C279: 10-32 UNF-2A X 1.50 long cross recessed flat head 100, SST). Honeywell International Inc. Do not copy without express permission of Honeywell. Page 12 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM The antenna mounting screws should be torqued to 2.37 to 2.60 N.m (21.0 to 23.0 in-lbs). If sealing of the antenna holes is needed, then RTV is recommended to be applied around the edge of each hole between both the UAV skin and ground plane and the ground plane and antenna. Ensure that the antenna remains in electrical contact with the ground plane. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 13 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 5. (Sheet 1 of 1) Antenna Dimensions Honeywell International Inc. Do not copy without express permission of Honeywell. Pages 14/15 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM B. Indoor Unit Mounting

(1) The indoor unit should be mounted in the avionics bay of the UAV.

(2) The indoor unit may be mounted in any orientation The label is on the back, exterior face of the Indoor Unit.

(3) The indoor units environment should be maintained within its environmental parameters. Anti-vibration mounts (not supplied) can be used to reduce the severity of the vibration.

(4) The indoor unit should be bolted to the floor of the avionics bay or on the external fuselage with 4 M4 bolts and torqued to 2.0 to 2.4 N.m. NOTE:

Mounting Hardware not included. Hardware to be supplied by customer based on installation.

(5) The SIM card should be fully inserted into the SIM card slot on the front face of the indoor unit.

(6) To ensure that the indoor unit can dissipate heat, refer to Paragraph 7.B.

(7) Refer to Figure 6 for Indoor Unit dimensions. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 16 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Blank Page Honeywell International Inc. Do not copy without express permission of Honeywell. Page 17 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 6. (Sheet 1 of 1) Indoor Unit Dimensions Honeywell International Inc. Do not copy without express permission of Honeywell. Pages 18/19 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM C. Cable Routing

(1) The installer should connect the Indoor Unit and Antenna with supplied RF cable. The RF cable has a fixed loss requirement and should not be substituted or shortened, or the terminal will not function properly.

(2) The RF connector torque settings depend on the connector and the recommendations are given in Table 5.

(3) The antenna mounting, indoor unit mounting and cable routing should be such to avoid sharp bends in the RF cable. The bending radius of each cable type that should be respected is given in Table 5.

(4) The RF cable should be routed below the ground plane level.

(5) The RF cable should not be in tension.

(6) The cables should not be routed near high voltage sources or flammable fluid

(7) The cables should be maintained within the terminals environment parameters.

(8) The supplied power/Ethernet cable shall have a minimum bending radius of 6.6 cm.

(9) Power should be maintained in the range 27 to 30V DC when up to 65 W is drawn.

(10) The Ethernet connection will be to a 10/100 Base-T network.

(11) The power/Ethernet connector should be inserted into the socket on the indoor unit.

(12) The Indoor Unit provides a female SMA connector for the antenna coax cable. D. Miscellaneous

(1) Below are the list of warnings and cautions necessary while performing installation tasks. Refer to Figure 7 for safety information. Safety Information Regarding Exposure to RF Signals. Safety Information for Hot Surfaces. Safety information for Electrostatic Discharge. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 20 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 7. (Sheet 1 of 1) Safety Information Warning and Caution Honeywell International Inc. Do not copy without express permission of Honeywell. Page 21 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM E. Engineering Drawings

(1) For Terminal Outline and Installation, refer to Figure 8. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 22 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 8. (Sheet 1 of 1) Terminal Outline and Installation Honeywell International Inc. Do not copy without express permission of Honeywell. Page 23 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM

(1) If there is a common UAV ground, the Indoor Unit should be electrically cross bonded with less than or equal to 3.0 milliohms direct current (DC) resistance.

(2) Only 2 cables are required for operation. One to connect the boxes and the other to connect to 3. Electrical Installation A. General the UAV. B. Indoor Unit Installation

(1) General 4. Physical Connectors A. RF Cable The terminal does not require any calibration by the user/installer.

(1) The Honeywell part number 90600596 will be supplied with the terminal.

(2) The coax cable is able to handle temperatures between -40C to 55C (-40F to 131F).

(3) The cable has a fixed loss requirement and should not be substituted or shortened, or the terminal will not function properly. Part Number Coax Type Length Weight (g) Bending

(cm) SMA Torque

(N.m) TNC Torque

(N.m) Table 5. Antenna Cable Properties Radius In-

stallation

(cm) Bending Radius Repeated

(cm) 90600596 50 36 0.7 2.5 0.8-1.13 0.46-0.69 LMR-

100A-FR

(4) The coax cable connector is a male TNC (to the antenna) and male SMA to the indoor unit. B. Harness Assembly

(1) Length and weight of harness assembly is 150 cm and 120 g, respectively.

(2) Cable has an 8-pin circular, latching male connector at the Indoor Unit end, namely FGG-1B-308-CLAD76Z (LEMO 1B range, 8-pin plug with collet for max 7.6 mm diameter cable), with screening braid and drain wire clamped. Refer to Table 6 and Figure 9. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 24 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table 6. Termination Table From Connector FIND NO. REF DES PIN SIGNAL SIGNAL TYPE WIRE TYPE To Connector WIRE GROUP FIND NO. REF DES WIRE FIND NO. V_IN POWER STP AWG 22 1 P1 SDU GND GND 1 2 6 7 3 8 4 5 RX_N RX_P TX_N TX_P 3 PWR

+28VDC PWR GND SPADE TON-

GUE SPADE TON-

GUE PIN SIGNAL V_IN GND RX_N RX_P TX_N TX_P 6 3 2 1 4 5 1 2 1 2 3 3 4 4 ETHER-

NET STP AWG 26 2 COMM Honeywell International Inc. Do not copy without express permission of Honeywell. Page 25 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 9. (Sheet 1 of 1) LEMO Termination Honeywell International Inc. Do not copy without express permission of Honeywell. Page 26 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM 5. Final Validation A. Installation validation should be by the following steps

(1) Check that the LED lights up green.

(2) If the SIM card supplied with the terminal is being used, then activate the airtime.

(3) When the terminal is powered up and the antenna is not connected or if there is a fault, the status LED is red.

(4) Observe safety distances to the antenna detail above throughout.

(5) Ensure that the UAV is outdoors and has good line of sight to the satellite.

(6) Connect a laptop to the terminals Ethernet connection and check that no errors are reported by the WebUI. Refer to Section 3.1.A.2.

(7) Verify that there is no adverse interaction with other avionics when the terminal is powered up.

(8) Check that the GPS has a fix and that the position is correct.

(9) The safety distance between operator and antenna is 3.517 ft (1.07 m).

(10) Manually set up a data connection using the WebUI and check that signal quality is the good

(11) Verify there is no interference with GNSS or other systems when the terminal transmits data. or excellent ranges. B. Mission Safety Checks

(1) Safety of flight should be tested through ground tests before each mission.

(2) Bring up all the normal drone electronics systems (all C2 links, autopilot, motors and ESCs) and determine the performance of the GPS receiver, e.g. number of received satellites, blocking level.

(3) Add the Satcom terminal and verify that the GPS performance has not been degraded. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 27 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM SECTION 3 - SYSTEM OPERATION 1. General A. System Overview 2. Modes of Operations A. System Interfaces

(1) The Small SATCOM UAV system is part of the Aircraft Earth Station (AES) that facilitates airborne satellite communications using Swift Broadband (SBB) services over the Inmarsat L-Band satellite communications network.

(2) Set your laptop to obtain an IP address automatically or set a static IP address in the 192.168.1.2-255 or using satcom.honeywell.com

(1) This section describes the external hardware interfaces provided by the indoor unit. The presence of hardware interfaces in this section does not mean that these interfaces are supported by software or that they are functional in every mode of operation.

(2) Over Ethernet, the following logical control interfaces are available:

Storage Temperature/JSON interface is the primary command interface. WebUI interface is a web page to control and monitor the terminal. PPPoE connections are supported. B. WebUI

(1) Is accessed by typing 192.168.1.1 or satcom.honeywell.com into the address bar of any browser. NOTE: When accessing the WebUI an expired/not valid SSL certificate warning might be shown. This is expected behaviour and the warning can be bypassed. Depending on the web browser used, a button such as "Continue anyway" or "I understand the risk" might have to be clicked in order to bypass the message and access the WebUI.

(2) Figure 10 displays the WebUI configuration and status information. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 28 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 10. (Sheet 1 of 5) WebUI Configuration and Status Information Honeywell International Inc. Do not copy without express permission of Honeywell. Page 29 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 10. (Sheet 2 of 5) WebUI Configuration and Status Information Honeywell International Inc. Do not copy without express permission of Honeywell. Page 30 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 10. (Sheet 3 of 5) WebUI Configuration and Status Information Honeywell International Inc. Do not copy without express permission of Honeywell. Page 31 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 10. (Sheet 4 of 5) WebUI Configuration and Status Information Honeywell International Inc. Do not copy without express permission of Honeywell. Page 32 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 10. (Sheet 5 of 5) WebUI Configuration and Status Information Honeywell International Inc. Do not copy without express permission of Honeywell. Page 33 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM

(3) It enables the setting up of a single background data connection, which is the most common use case.

(4) It enables the setting up of 8 kbps, 16 kbps and 32 kbps streaming connections.

(5) HTTP runs over Transport Layer Security (TLS), i.e., HTTPS, providing communication security over the Internet. The usage of TLS requires that the client must support an X.509 certificate to communicate with the terminal web server. The web server uses the standard port number assigned to TLS connection: 443. The terminal will use the default self-assigned HTTPS certificate stored in the terminals non-volatile memory. The default certificate has a validity period of 10 years. The terminal will be configured with a user account with an initial password (that can be changed by the user) that is unique for each terminal. The initial username and password will be communicated by the label on the indoor unit. To restore the username and password to its initial values:

Log into the reset account and select the option in the WebUI or by sending the appropriate Connect using PPPoE with the following parameters:

RESTful message. C. PPPoE Username: void Password: <blank>

Service Name - @Background. D. RESTful

(1) RESTful/JSON interface is the primary machine to machine command interface.

(2) The communication protocol for RESTful is HTTP/HTTPS.

(3) Websocket interface handles asynchronous messages from the terminal. There are 3 types of web sockets messages. Responses to network commands. Periodic information updates. Unsolicited/Alerts messages.

(4) Example python scripts for controlling the terminal via the RESTful interface are available for download via the terminal's web page. The Key resources available via the RESTful interface are:

Secid Connectionprofileid Location Temp GNSS Lowpower Signalstrength Honeywell International Inc. Do not copy without express permission of Honeywell. Page 34 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Reboot Config terminal's web page. 3. Example Use Case (VPN) A. General

(5) See the ICD for more details about this interface, which is available for download from the

(1) A common use of Satcom is to allow equipment based on the ground to interrogate equipment on the UAV, for example to pull position data from the flight controller, refer to Figure 11. One way of achieving this is to create a Virtual Private Network (VPN) from the UAV to the ground equipment. Some advantages of this approach are:

When set up correctly, the VPN can appear as a transparent wire allowing seamless connections between the ground and air. If the VPN client is setup on the air side, the Satcom terminal does not need a static IP address, Dynamic DNS or similar. The VPN provides end-to-end encryption under your control. The air side router can be configured to automatically establish the Satcom connection on power up. Depending on the choice of router, it can remove the need for a separate Ethernet switch.

(2) To provide an easy starting point, the following system has been designed by Honeywell with configuration instructions in Appendix B. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 35 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Figure 11. (Sheet 1 of 1) Example Use Case (VPN) Honeywell International Inc. Do not copy without express permission of Honeywell. Page 36 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM 4. INMARSAT Operational A. General

(1) Class 15 Services. Standard IP Streaming IP BGAN IP Voice Combinations of the above. 5. USIM A. General 6. LED Indicator A. Indications are as listed below:

(1) No Power Off

(2) OK Green

(3) Error - Red 7. Temperature Profile A. Antenna to 131F). B. Indoor Unit

(2) Background, streaming and subscription traffic classes are supported.

(3) User is able to set up 1 primary and up to 9 PDP contexts on a connection. Primary and secondary connections can be set up via the RESTful interface The WebUI can only set up a primary connection

(1) When a user inserts or removes a SIM card, the indoor unit will reset.

(2) The terminal works with an Inmarsat class 15 USIM Aeronautical provided by the Honeywell service provider and the Honeywell distribution partner.

(1) The antenna will survive through a temperature range of -55 to 85C (-67 to 185F).

(2) The antenna will operate through an environmental temperature range of -40 to 55C (-40

(1) The indoor unit will survive through a temperature range of -55 to 85C (-67 to 185F).

(2) The Indoor Unit will operate through an environmental temperature range of -40 to 55C

(-40 to 131F).

(3) Refer to Table 7 for ground level thermal capabilities. To ensure that the unit can dissipate heat at an altitude of more than 15000 ft and less than 55000 ft, a minimum of 2 SCFM is required. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 37 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table 7. Ground Level Thermal Capabilities Mounting Mounting Description Minimum Air Flow Required to Operate at 55C (131F) Standard On Controlled Plate 123 CFM No Airflo Indoor Unit is mounted or bolted directly to insulating surface. For instance, onto a composite surface. Indoor Unit is mounted or bolted directly to a thermally conductive surface. For instance, actively controlled cooling plate. Indoor Unit is mounted or bolted with a gap to an insulating surface. For instance, vibration mounts. The gap allows airflow underneath the Indoor Unit. On Standoff 27.43 CFM Honeywell International Inc. Do not copy without express permission of Honeywell. Page 38 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM SECTION 4 MAINTENANCE PRACTICES 1. Maintenance A. General B. Cleaning

(1) The Indoor Unit should be isolated from the UAV power network prior to any maintenance to avoid any possibility of personnel being irradiated.

(1) The Indoor Unit and antenna can both be cleaned with a microfibre or soft cotton cloth dampened with clean water.

(2) Chemical cleaning agents should not be used. C. Inspection

(1) The Indoor Unit and antenna should be inspected every year for general condition and integrity of the mounting and connectors.

(2) The cables should be inspected every year for general condition, chafing kinking and routing.

(3) The electrical cross-bonding between the indoor unit and the antenna should be tested ever 2 years. D. Servicing

(1) There are no adjustments, lubrication or scheduled servicing tasks needed for the satcom terminal while installed on the UAV.

(2) The satcom terminal is not field repairable. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 39 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Blank Page Honeywell International Inc. Do not copy without express permission of Honeywell. Page 40 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM SECTION 5 - TROUBLESHOOTING

(1) Most common installation issues include breaks/disconnection in the antenna cable and 1. Installation Issues A. General power supply. 2. Operation Issues A. General

(1) The fault possible causes and its troubleshooting solutions are listed in below Table 8. PROBLEM POSSIBLE CAUSE SOLUTION Table 8. Fault Possible Causes Satcom doesnt come on LED off Power supply Check that 28V DC is being supplied Terminal works with some power supplies and not others - check that the terminal inrush current is not causing the supply voltage to drop below 27v Indoor Unit failure Contact support Water in Indoor Unit Dry out Satcom error LED red Antenna not connected Connect antenna Error condition Check using WebUI Satcom works for a while then stops Antenna overheating Check that the antenna mounting can dissipate the heat from the antenna base plate MCU error on WebUI Code 0x0C MCU error on WebUI 0x02 to 0x0B, 0x0D Modem temperature

>85C (185F), or MCU temperature

>85C (185F) Unresponsive for more than 30s Antenna not connected Connect Antenna RF cable damaged Antenna failure Swap RF cable Contact support Corrupt configuration Contact support Indoor Unit failure Contact support Indoor Unit overheating Several Check SIM status and position Increase airflow over the Indoor Unit, mount Indoor Unit on stand-offs, or increase conductive cooling Check that 28V DC is being supplied Power cycle terminal Honeywell International Inc. Do not copy without express permission of Honeywell. Page 41 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM Table 8. Fault Possible Causes (Cont) PROBLEM POSSIBLE CAUSE SOLUTION SIM status not ready SIM card not fitted Insert SIM card in slot SIM card invalid Use supplied class 15 SIM Contact Service Provider Position undetermined Insufficient GPS satellites visible Ensure antenna is outside with an unobstructed view of the sky Fails to connect to network Satellite blockage Interference Interference Prevent interference in the GNSS band Ensure antenna is outside with an unobstructed view of the sky Prevent interference in Satcom receive band Loose connectors Correctly torque RF connectors Damaged RF cable Replace RF cable Low data rate to terminal Component failure Low signal quality Contact Support See below background Low rate streaming connection Disconnect and reconnect to Low signal quality Satellite partial blockage Network contention Wait for the network should adapt Connected to satellite with low elevation Interference Ensure antenna is outside with an unobstructed view of the sky Disconnect and reconnect Prevent interference in Satcom receive band Loose connectors Correctly torque RF connectors Damaged RF cable Replace RF cable Power supply Check that 28V is being supplied Component failure Contact Support Honeywell International Inc. Do not copy without express permission of Honeywell. Page 42 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM PROBLEM POSSIBLE CAUSE SOLUTION Table 8. Fault Possible Causes (Cont) Low data rate from terminal Satellite partial blockage Ensure antenna is outside with an unobstructed view of the sky Disconnect and reconnect Connected to satellite with low elevation Loose connectors Correctly torque RF connectors Damaged RF cable Replace RF cable Component failure Contact Support Low rate streaming connection Disconnect and reconnect to background Network contention Wait for the network should adapt Poor latency Background connection Switch to a streaming connection UAVs GPS fails to lock Interference from Satcom emissions Increase isolation between Satcom antenna and GPS antennas Honeywell International Inc. Do not copy without express permission of Honeywell. Page 43 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM APPENDIX A - CERTIFICATION AND REFERENCE DOCUMENTS 1. General A. Reference Documents

(1) SP-90600571 - Small Satcom External ICD.

(2) SP-90600570 - Small Satcom System Requirements Document. B. Regulatory

(1) 47 CFR, US FCC Title 47 CFR: Part 87 for Aeronautical classes (section 87.139 Emissions Limitations).

(2) European Regulation (EC) No. 1907/2006 concerning the Registration, Evaluation, Authorization and Restriction of Chemicals (REACH). 2. Radio Transmission Licensing A. FCC and IC

(1) This product has been certified with the following license Ids:

FCC-ID: K6KSMALLSATCOM. IC-ID: 1275B-SMALLSATCOM. the aircraft or fleet

(2) The radio transmission is licensed in accordance to 47 CFR part 87 [RD7] by the operator of

(3) As per 47 CFR part 87.39 the acceptability of the equipment for licensing is achieved by obtaining FCC certification, as per 47 CFR [RD7] part 2 Subpart J Section 2.1033. The FCC ID received is marked on the physical nameplate of all non-prototype certified equipment.

(4) Pursuant to section 1.925 of 47 CFR of the Commissions rules, Honeywell International Inc. has been granted waivers of Sections 87.131, 87.133, 87.137, 87.139(i)(1) and 87.141(j) of the FCC rules. The waivers of these sections permit the FCC certification of the Small SATCOM transceiver to support the Inmarsat SwiftBroadband aircraft communications services. The waivers of these sections have been granted uncondtionally. This device has been tested and found to comply with the remaining sections of Part 87 of the FCC rules, thefore the conditions of the waiver are met at all times.

(5) As per Canadian Radio Communication Regulations SOR/96-484 [RD15], 21(1) Innovation, Science and Economic Development Canada (ISEDC) Technical Acceptance Certification is required. The ISEDC ID received is marked on the physical nameplate of all non-prototype certified equipment.

(6) The FCC and ISEDC complies with DO-262D section 2.1.3 Note 1.

(7) NOTE: This equipment has been tested and found to comply with the limits for a Class A digital device, pursuant to Part 15 of the FCC Rules. These limits are designed to provide reasonable protection against harmful interference when the equipment is operated in a commercial environment. This equipment generates, uses, and can radiate radio frequency energy and, if not installed and used in accordance with the instruction manual, may cause harmful interference to radio communications. Operation of this equipment in a residential area is likely to cause harmful interference in which case the user will be required to correct the interference at his own expense. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 44 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM

(8) NOTICE: Changes or modifications made to this equipment not expressly approved by EMS Technologies Canada, Ltd., a wholly owned subsidiary of Honeywell International Inc. may void the FCC authorization to operate this equipment.

(9) NOTICE: This device complies with Part 15 of the FCC Rules [and with Industry Canada licence-exempt RSS standard(s)]. Operation is subject to the following two conditions: this device may not cause harmful interference, and this device must accept any interference received, including interference that may cause undesired operation (Le prsent appareil est conforme aux CNR d'Industrie Canada applicables aux appareils radio exempts de licence. L'exploitation est autorise aux deux conditions suivantes: l'appareil ne doit pas produire de brouillage, et l'appareil doit accepter tout brouillage radiolectrique subi, mme si le brouillage est susceptible d'en compromettre le fonctionnement).

(10) Radio frequency radiation exposure Information: This equipment complies with FCC and IC radiation exposure limits set forth for an uncontrolled environment. This equipment should be installed and operated with minimum distance of 107 cm between the radiator and your body. This transmitter must not be co-located or operating in conjunction with any other antenna or transmitter. B. European Technical Standards Institute (ETSI)

(1) Satellite Earth Stations and Systems (SES); Harmonised Standard for Aircraft Earth Stations

(AES), providing Aeronautical Mobile Satellite Service (AMSS)/Mobile Satellite Service (MSS) and/or the Aeronautical Mobile Satellite on Route Service (AMS(R)S)/Mobile Satellite Service

(MSS), operating in the frequency band below 3 GHz covering the essential requirements of article 3.2 of the Directive 2014/53/EU, ETSI EN 301 473 V2.1.2 (2016-11). Honeywell International Inc. Do not copy without express permission of Honeywell. Page 45 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM APPENDIX B - EXAMPLE USE CASE (VPN) SETUP DETAILS 1. VPN Server (Ground Side) A. Install OpenWRT on the router

(1) Download OpenWRT 19.07.4 from the below link: http://downloads.openwrt.org/releases

/19.07.4/targets/ar71xx/generic/openwrt-19.07.4-ar71xx-generic-gl-ar750s-squashfs-

sysupgrade.bin

(2) Perform upgrade 192.168.1.1 Connect your computer to any of the LAN ports on the router. Set the IP address of the computer to 192.168.1.2, mask 255.255.255.0, gateway Hold RESET button on the router and plug in the power supply. Keep holding until the WiFi LED flashes 5 times, then release the button. Navigate to 192.168.1.1 and upload the OpenWRT image. The router will reboot automatically. B. Configure the router

(1) Set the router LAN IP to 192.168.1.1 if it isnt already. Set the DHCP server start address to 80 and limit to 40.

(2) Temporarily connect the router to the internet (via WAN port or use a mobile hotspot on the mobile phone) and open an SSH session.

(3) Execute the following commands to install required packages:

# opkg update

# opkg install kmod-usb-core kmod-usb2 usb-modeswitch libusb-1.0 kmod-usb-net-cdc-ether openvpn-openssl openvpn-easy-rsa luci-app-openvpn luci-app-ddns

(4) Set the WAN IP address to 192.168.8.100, netmask 255.255.255.0, gateway 192.168.8.1. Use custom DNS 8.8.8.8.

(5) Connect the USB modem and reboot router. list. Save & Apply.

(7) Delete WAN6 interface from Network -> Interfaces.

(6) Open WAN interface settings, go to Physical Settings and elect eth1 from the drop-down

(8) Navigate to 192.168.8.1 and enable DMZ on the 192.168.8.100 IP address. Ensure the modem has established connection to the internet.

(9) Configure Dynamic DNS settings according to your selected provider. You might need to install additional packages for some providers. Verify the IP address is updated in your user panel.

(10) Execute the following commands on the router (this will take a while to generate):

# cd /etc/easy-rsa/

# easyrsa gen-dh

# easyrsa build-ca nopass (enter smallsatcom as CA when prompted)

# easyrsa build-server-full server nopass

# easyrsa build-client-full smallsatcom nopass Honeywell International Inc. Do not copy without express permission of Honeywell. Page 46 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM

# cp /etc/easy-rsa/pki/ca.crt /etc/openvpn/

# cp /etc/easy-rsa/pki/dh.pem /etc/openvpn/

# cp /etc/easy-rsa/pki/issued/server.crt /etc/openvpn/

# cp /etc/easy-rsa/pki/private/server.key /etc/openvpn/

/etc/easy-rsa/pki/ca.crt

/etc/easy-rsa/pki/issued/smallsatcom.crt

/etc/easy-rsa/pki/private/smallsatcom.key

(11) Copy the following files to your machine: (These will be required by the client)

(12) Open port 1194 in the firewal by going to Network -> Firewall. Then Traffi Rules tab and click Add on the bottom. Enter the following configuration Name: openvpn-udp Protocol: UDP Source zone: wan Destination zone: Device (input) Destination port: 1194 Action: Accept

(13) Using the LUCI WebUI Select VPN -> OpenVPN. Then enter smallsatcom_tap in the instance name below Template Based Configuration Select Server configuration for an ethernet bridge VPN from the template list and click Add. Click Edit next to the newly added interface.

(14) (Some fields might be missing; these can be added by going to the bottom of the page and selecting it from the Additional-field drop-down menu.) Enter the following configuration server_bridge: 192.168.1.1 255.255.255.0 192.168.1.128 192.168.1.254 ca: [click on File not accessible and select ca.crt]

dh: [click on File not accessible and select dh.pem]

cert: [click on File not accessible and select server.crt]

key: [click on File not accessible and select server.key]

verb: 3 port: 1194 dev_type: tap comp_lzo: yes keepalive: 10 60 proto: udp VPN Server.

(15) Click Save & Apply, then Back to Overview.

(16) Tick the Enabled box next to the smallsatcom_tap line. Save & Apply and then Start the

(17) Open LAN interface settings, go to Physical Settings tab and add tap0 to the interfaces from drop-down list. Save, then Save & Apply.

(18) Reboot the router to Apply all changes.

(19) Server configuration is complete. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 47 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM 2. VPN Client (Air Side) A. Install OpenWRT on the router Follow the same directions as for the server to install OpenWRT. B. Configure the router

(1) Set the router LAN IP to 192.168.1.2. Disable the DHCP server.

(2) Delete WAN6 interface from Network -> Interfaces. mobile phone) and open an SSH session.

(4) Execute the following commands to install required packages:

# opkg update

# opkg install openvpn-openssl luci-app-openvpn

(3) Temporarily connect the router to the internet (via WAN port or use a mobile hotspot on the

(5) Using the LUCI WebUI Select VPN -> OpenVPN. Then enter smallsatcom_tap in the instance name below Template Based Configuration Select Client configuration for an ethernet bridge VPN from the template list and click Add. Click Edit next to the newly added interface.

(6)

(Some fields might be missing; these can be added by going to the bottom of the page and selecting it from the Additional-field" drop-down menu.) Enter the following configuration verb: 3 port: 1194 dev_type: tap nobind: [tick]

comp_lzo: yes client: [tick]

proto: udp VPN Server. remote: [Public ip address or ddns address of the VPN Server]

ca: [click to upload and select ca.crt downloaded from server]

dh: [do not select any file cert: [click to upload and select smallsatcom.crt downloaded from server]

key: [click to upload and select smallsatcom.key downloaded from server]

(7) Click Save & Apply, then Back to Overview.

(8) Tick the Enabled box next to the smallsatcom_tap line. Save & Apply and then Start the

(9) Open LAN interface settings, go to Physical Settings tab and add tap0 to the interfaces from drop-down list. Save, then Save & Apply.

(10) Reboot the router to Apply all changes.

(11) If the server is running, the client should now establish a VPN connection. This can be confirmed by inspecting the System Log and the VPN Server router should reply to ping.

(12) Disconnect the temporary internet connection and select edit next to the WAN interface under Network -> Interfaces. Change Protocol to PPPoE. Enter void in both username and passwords fields Enter @Background to Service Name field. Save, then Save & Apply. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 48 18 Feb 2021 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL SMALL SATCOM

(13) Connect the router to the Small Satcom IDU using the WAN port. The router should establish connection to the internet and open a VPN tunnel to the server automatically. Honeywell International Inc. Do not copy without express permission of Honeywell. Page 49 18 Feb 2021

NOTES:

1. USE .003 THICK POLYESTER LABEL, COLOR PANTONE 420 C OR EQUIVALENT, BACKED WITH PRESSURE SENSITIVE ADHESIVE 3M 966. 2. USE ARTWORK 90600622 FOR THE CREATION OF THE LABEL. A INITIAL RELEASE PER ECN-8203513 25SEP20 NB SEE PDM ECR 4.5"

I Small Satcom EMS Technologies Canada Ltd. DESCRIPTION SMALL SATCOM H/W P/N 90600511 REV S/N DATE WEIGHT 0.5 kg 1.1 lb CAGE CODE KF586 MADE IN CANADA User Account Username: user Password:

Reset Account Username: reset Password:

SMALL UAV SATCOM FCC ID: K6KSMALLSATCOM IC ID: 1275B-SMALLSATCOM

7

. 1 SEE PDM CorelDraw 19 Green Lane, Ashchurch Tewkesbury, Glos GL20 8HD UK SMALL SATCOM N BOWYER 25SEP20 J AZEVEDO 28JSEP20 SEE PDM N/A SEE PDM SEE PDM SEE PDM SEE PDM LABEL, ID, SW, FCC, SMALL SATCOM KF586 NTS 90600621 90600621_REVA.CDR A C T U 6 4

4 3

0 1 0 2 0 2 t c O 9 0

d e s a e e R l

I N O T C U D O R P REF: ECN-8203513

HONEYWELL AEROSPACE SERVICES AND CONNECTIVITY 400 Maple Grove Road Ottawa, K2V 1B8, Ontario www.honeywell.com Re: EMS Technologies Canada, Ltd. Applicability and Conditions for Waiver of Part 87 Rules to Allow Equipment Certification of Aeronautical Mobile Satellite Service Transceiver (Small UAV SATCOM, Pending FCC ID K6KSMALLSATCOM) Dear Mr. Tobias:

On the 20th November 2020, EMS Technologies Canada, Ltd. (EMS) a wholly owned subsidiary of Honeywell International Inc., pursuant to section 1.925 of the Commissions rules, requested a waiver of Sections 87.131, 87.133, 87.137, 87.139(i)(1) and 87.141(j) of the Commissions rules to permit certification of its next generation Aeronautical-Mobile Satellite Service (AMSS) transceiver, Small UAV SATCOM. The transceiver supports the SwiftBroadband aircraft communications service for use with, but not solely confined to, unmanned aircraft e.g. drones, UAVs. On the 7th May 2021, EMS received confirmation that the waiver request was accordingly GRANTED and sections 87.131, 87.133, 87.137, 87.139(i)(1) and 87.141(j) of the Commissions rules are WAIVED as requested. No additional conditions were stated, and EMS considers the waiver valid for the duration of the product lifetime of the transceiver with the FCC ID K6KSMALLSATCOM. The waiver is applicable to this product as it permits the certification of the companys transceivers to support the Inmarsat SwiftBroadband aircraft communications services. Current Part 87 rules do not allow for the wider bandwidth, higher transmission speeds and more efficient modulation techniques of newer AMSS systems. The Small SATCOM transceiver has been tested and found to meet the technical requirements of Part 87 AMSS rules with respect to output power, spurious emissions and intermodulation. With the grant of the above waiver, the conditions of both Part 87 of the Commissions Rules and the granted waiver will be met for the duration of the product lifetime of the Small UAV SATCOM transceiver. May 11th, 2021 Mr. Jeff Tobias, Chief, Mobility Division Wireless Telecommunications Bureau, Federal Communication Commission 445 12th St SW Washington, DC 20554 Sincerely, Dennis Teske, SR Director Engineering Honeywell Confidential

SATCOM 400 Maple Grove Road Ottawa, ON K2V 1B8 www.honeywell.com November 20, 2020 Federal Aviation Administration Spectrum Engineering Services Group, AJW-1C Room 715E 800 Independence Ave., SW Washington, DC 20591 Reference:

FAA Notification of FCC Equipment under FCC Part 87 Small SATCOM, Aeronautical Earth Station, Satellite Communications Transceiver FCC ID K6KSmallSATCOM To Whom It May Concern:

ln accordance with Federal Communications Commission (FCC) Rules and Regulations, Part 87.147(d), EMS Technologies Canada, Ltd. (EMS), a wholly owned subsidiary of Honeywell International Inc, hereby notifies the Federal Aviation Administration of its filing with the FCC of an application for certification of the Small SATCOM Aeronautical Earth Station Satellite Communications Transceiver model referenced above. Please find below the information required pursuant to Part 87.147(d)(1). 1) Description of Equipment The Small SATCOM Aeronautical Earth Station (AES) satellite communication transceiver supports the lnmarsat SwiftBroadband 200 aeronautical satellite communication service. It is intended for use on Unmanned Aeronautical Vehicles only, where size and weight are paramount. The following provides a brief description of the Small SATCOM terminal. The transceiver system comprises an indoor unit and an external active antenna connected by a single cable. The indoor unit requires a combined power input and ethernet cable. The Direct Current (DC) power input powers the whole system. A Universal Subscriber Identity Module (USIM) card needs to be inserted into the indoor unit for it to operate. The Indoor Unit contains a stack of Radio Frequency (RF) card, digital cards and BGAN Radio Module

(BRM). The USIM holder and power supply are mounted on the digital card. Coaxial cables provide the interconnection of the BRM with the RF board. Honeywell Internal The BRM includes low power RF hardware, physical layer data processing, Universal Subscriber Identity Module (USIM), GNSS receiver, and high-level application interfaces. An Ethernet interface supporting Network Address Translation (NAT) and Point-to-Point Protocol over Ethernet (PPPoE) protocols allows the Small SATCOM to be used in a wide range of network configurations. A secure RESTful command interface over Ethernet provides the command interface. The active antenna unit is revision C of the established AeroAntenna AT1595-13. The connector is a female TNC. 2) Emission Types and Characteristics The Small SATCOM emission types and characteristics are summarized below. FCC Designator Inmarsat Service Performance Factor (K) Modulation Type Data Rate

(kbps) 33.6 67.2 134.4 302.4 134.4 268.8 604.8 Symbol Rate ksym/s 16.8 33.6 67.2 151.2 33.6 67.2 151.2 QPSK QPSK QPSK QPSK 16 QAM 16 QAM 16 QAM Signal States

(S) 4 4 4 4 16 16 16 0.74 0.74 0.74 0.66 0.74 0.74 0.66 SwiftBroadband SwiftBroadband SwiftBroadband SwiftBroadband SwiftBroadband SwiftBroadband SwiftBroadband Necessary Bandwidth

(kHz) 25.0 50.0 100 200 50.0 100 200 Authorized Bandwidth

(kHz) 225 225 225 225 225 225 225 25K0G1W 50K0G1W 100KG1W 200KG1W 50K0D1W 100KD1W 200KD1W 3) Output Power The nominal EIRP is 11.4 dBW. 4) Frequencies of Operation The Small Satcom transceiver is capable of operation over the following frequency ranges:

Transmitting: 1626.5 to 1660.5 MHz and 1668.0 to 1675.0 MHz Receiving:

GNSS:

1518.0 - 1559.0 MHz 1559.0 to 1610 MHz The operational frequencies of transmission and reception are controlled by frequency channel assignments from the Inmarsat satellite system. The Small Satcom will not transmit unless assigned a valid transmit frequency by the satellite system. Note that 1668.0 to 1675.0 MHz frequency band will not be used in USA/Canada. 2 5) Receiver Characteristics The receiving characteristics of the Small SATCOM meet the applicable requirement of the lnmarsat System Definition Manuals (SDMs) for a class 15 terminal. If this information meets with your approval, Honeywell herein requests that your office notify the FCC's Office of Engineering and Technology Laboratory, Authorization and Evaluation Division, in order to indicate that, pursuant to Section 87.147(dX2) of the FCC's rules, the FAA does not have an objection to the certification of the equipment described in this letter. lf you have any questions on the above information, please feel free to contact me directly. Sincerely, Dennis Teske Sr. Director Engineering Honeywell International Inc. 3

800 Independence Ave., S. W. Washington, D. C. 20591 Federal Communications Commission 7435 Oakland Mills Road Columbia, MD 21046 Dear Mr. Corey Cahill:

The Federal Aviation Administration, Spectrum Engineering Services Group received the EMS Technologies Canada, Ltd. notification letter of its filing with the Federal Communications Commission (FCC). The application is for certification of the Small SATCOM, Aeronautical Earth Station, Satellite Communications Transceiver with FCC ID:

K6KSmallSATCOM. We have completed the review process of the information submitted by EMS Technologies Canada, Ltd. and concluded that we have no objection to the FCC granting certification for this equipment. If you require any additional information, please contact Mr. Jae Shin, Electronics Engineer, Spectrum Planning and International Group, at (202) 267-7365 or via e-mail jae.w.shin@faa.gov. Sincerely, James D. Linney Director Operations Support, AJW-1 January 12, 2021

SATCOM 400 Maple Grove Road Ottawa, ON K2V 1B8 www.honeywell.com October 9, 2020 Federal Communication Commission Equipment Authorization Division, Application Processing Branch 7435 Oakland Mills Road Columbia, MD 21048 Subject: CONFIDENTIALITY REQUEST for Certification Service in USA TO WHOM IT MAY CONCERN Pursuant to Paragraphs 0.457 and 0.459 of the Commissions Rules (47 C.F.R.) and Section 552(b)(4) of the Freedom of Information Act, we request confidentiality for the following products:

FCC ID K6KSMALLSATCOM For the product stated above, we request permanent confidentiality for exhibits which contain Operational Description, Block Diagram, Schematics, Parts Lists or Tune Up Information. The above exhibits contain our trade secrets and proprietary information that could be of benefit to our competitors. If you have any questions, please feel free to contact me at the address shown below. Sincerely, Model name Small SATCOM Assembly PN: 90600511 Name: Dennis Teske Company: EMS Technologies Canada Ltd. Address: 400 Maple Grove Road Ottawa, ON K2V 1B8 Canada Phone: +1 613 591 9064 Fax: +1 613 591 9120 Email: dennis.teske@honeywell.com Honeywell Confidential

El-Zibawi, Hicham Watson, Kevin (SATCOM) FW: [External] EMS Technologies Part 87 waiver request Freitag, 7. Mai 2021 14:37:04 Small SATCOM FCC Waiver Request.pdf Von:

An:

Betreff:

Datum:

Anlagen:

From:ThomasDerenge<Thomas.Derenge@fcc.gov>

Sent:Friday,May7,20217:32AM To:El-Zibawi,Hicham<Hicham.Zibawi@honeywell.com>

Cc:RogerNoel<Roger.Noel@fcc.gov>;JeffTobias<Jeff.Tobias@fcc.gov>;TimMaguire

<Tim.Maguire@fcc.gov>;ThomasDerenge<Thomas.Derenge@fcc.gov>

Subject:[External]EMSTechnologiesPart87waiverrequest CAUTION: Thisemailoriginatedfromoutsideoftheorganization.Donotclicklinksor openattachmentsunlessyourecognizethesenderandknowthecontentissafe. DearHichamEl-Zibawi, OnNovember30,2020,EMSTechnologiesCanada,Ltd.,awhollyownedsubsidiaryof HoneywellInternationalInc.,requestedwaiversofSections87.131,87.133,87.137,87.139(i)

(1)and87.141(j)oftheCommissionsrulestopermitcertificationofitsnextgeneration Aeronautical-MobileSatelliteService(AMSS)transceiver,SmallUAVSATCOM.The transceiversupportstheSwiftBroadbandaircraftcommunicationsserviceforusewith,but notsolelyconfinedto,unmannedaircrafte.g.drones,UAVs.Therequestwasfiledinthe CommissionsElectronicCommentFilingSystem(ECFS).See https://www.fcc.gov/ecfs/filing/1130152972206.Thewaiverswouldpermitthecertification ofthecompanystransceiverstosupportthenewInmarsatEnhancedSwiftBroadbandSafety ServicesandSwiftBroadbandaircraftcommunicationsservices.Wehavereviewedthe waiverrequest,andfindthatitsatisfiesthewaivercriteriainsection1.925ofthe Commissionsrulesforthereasonsstatedtherein.Thewaiverrequestisaccordingly GRANTED andsections87.131,87.133,87.137,87.139(i)(1)and87.141(j)ofthe CommissionsrulesareWAIVEDasrequested. QuestionsregardingthiswaivergrantshouldbeaddressedtoJeffTobias,at jeff.tobias@fcc.govor202.418.1617. Sincerely, ThomasDerenge DeputyChiefMobilityDivision,WTB,FCC

HONEYWELLCONNECTEDENTERPRISE SATCOM 400MapleGroveRoad Ottawa,K2V1B8,Ontario www.honeywell.com Nov 24th, 2020 Mr. Roger Noel, Chief, Mobility Division Wireless Telecommunications Bureau, Federal Communication Commission 445 12th St SW Washington, DC 20554 Re: WAVIER EXPEDITED ACTION REQUESTED EMS Technologies Canada, Ltd. Request for Waiver of Part 87 Rules to Allow Equipment Certification of Aeronautical Mobile Satellite Service Transceiver (Small UAV SATCOM, Pending FCC ID K6KSMALLSATCOM) Dear Mr. Noel:

EMS Technologies Canada, Ltd. (EMS) a wholly owned subsidiary of Honeywell International Inc., pursuant to section 1.925 of the Commissions rules, hereby requests waiver of Sections 87.131, 87.133, 87.137, 87.139(i)(1) and 87.141(j) of the Commissions rules to permit certification of its next generation Aeronautical-Mobile Satellite Service (AMSS) transceiver, Small UAV SATCOM. The transceiver supports the SwiftBroadband aircraft communications service for use with, but not solely confined to, unmanned aircraft e.g. drones, UAVs. Under Section 1.925, the FCC may grant a waiver if [t]he underlying purpose of the rule(s) would not be served or would be frustrated by application to the instant case, and that a grant of the waiver would be in the public interest or; [i]n view of unique or unusual factual circumstances of the instant case, application of the rule(s) would be inequitable, unduly burdensome or contrary to the public interest, or the applicant has no reasonable alternative.1 Similar waivers of Part 87 rules have been granted to EMS, Honeywell International, Inc, and Rockwell Collins Inc.2 Such equipment is intended for use on aircraft to provide high-speed Internet, voice and video conferencing capabilities in the cockpit, in the cabin and at the gate. A similar waiver of Part 87 rules has also been granted to Omnipless Manufacturing (PTY) Ltd. for UAV applications.3 These waivers have found that the waiver would be in the public interest because current Part 87 rules do not allow for the wider bandwidth, higher transmission speeds and more efficient modulation techniques of newer AMSS systems.4 A grant here would provide the same public interest benefits and allow EMSs next generation transceiver to deliver high-speed data in support of UAV applications. 1 47 C.F.R 1.925(b)(3) 2 See EMS equipment authorization for FCC ID K6KHSD-440, FCC ID K6KA781-MK4 Honeywell International Inc, equipment authorization for FCC ID G8BHD-128, and Rockwell Collins Inc equipment authorization for FCC ID AJK8222232 and AJK8222234. 3 See Omnipless Manufacturing (Pty) Ltd. authorization for FCC ID 2AS39-AVIATORUAV200 4 See Request of EMS for Waiver of Part 87 Emission Mask to Allow Certification and Use of Aeronautical Mobile Satellite Service Transceiver, 26 FCC Rcd 8824 (WTB 2011). Honeywell Confidential Description of the equipment The Small SATCOM transceiver supports Inmarsat SwiftBroadband signals using QPSK as well as 16-point Quadrature Amplitude Modulation (16-QAM). The Small SATCOM transceiver provides one communication channel capable of supporting full-duplex SwiftBroadband non-voice data functionality. The System functions in the 1525- 1559 MHz receive band and transmit bands of 1626.5-1660.5 and 1668-1675 MHz. The transmit band of 1668-1675 MHz is not supported in the USA or Canada. The Small SATCOM transceiver will meet the technical requirement of Part 87 AMSS rules with respect to output power, spurious emissions and intermodulation. As the FCC has acknowledged, Inmarsat's SwiftBroadband service offers higher data rates by utilizing more efficient modulation techniques.5 Grant of the instant waiver request would serve the public interest because the Part 87 rules have not yet been updated to reflect the Inmarsat SwiftBroadband emission types and bandwidths. Requested Waivers Part 87 87.131 Authorized Emissions Section 87.131 authorizes G1D, G1E and G1W for aircraft earth stations. The SwiftBroadband services, use 16 Point Quadrature Amplitude Modulation (16-QAM) and QPSK modulation schemes, with emission types G1W and D1W. Therefore, EMS requests a waiver of the authorized emissions in section 87.131 of the Commission's rules to employ D1W in addition to the G1W emission authorized under Section 87.131. 87.133 Frequency Stability Pursuant to Section 87.133(a), the frequency tolerance of an aircraft earth station operating in the 1626.5-

1660.5 MHz band is +/- 320 Hz. For purposes of bench testing for certification, a tolerance of +/- 160 Hz applies to the reference oscillator of the transmitter. The EMS transceiver contains a on board reference oscillator with an accuracy that has been shown in testing to have a worst-case error of 845Hz. Therefore, EMS requests a waiver of Section 87.133(a) of the Commissions rules for this reason. 87.137 Types of Emissions Section 87.137(a) of the Commissions rules authorizes for aircraft earth stations emissions designator 21K0G1D and the authorized bandwidth for aircraft earth station emissions above 50 MHz is 25 kHz. Lower values of necessary and authorized bandwidths are also permitted. SwiftBroadband service utilizes QPSK, and 16-QAM modulation schemes, with emissions class G1W and D1W. Due to the increased symbol rates for QPSK, 16-QAM a larger authorized bandwidth is necessary. An adequate bandwidth for SwiftBroadband is 225 kHz. Therefore, EMS seeks waiver of Section 87.137(a) of the Commissions rules to authorize the following emissions designators for the Small SATCOM transceiver:

Emissions Designator Modulation Type Necessary Bandwidth Authorized Bandwidth 25K0G1W 50K0G1W QPSK QPSK

(kHz) 25.0 50.0

(kHz) 225 225 5 EMS Stamp Grant, at 2 Honeywell Confidential 100KG1W 200KG1W 50K0D1W 100KD1W 200KD1W QPSK QPSK 16 QAM 16 QAM 16 QAM 100 200 50.0 100 200 225 225 225 225 225 87.139(i)(1), note 2 Emission Limitations Section 87.139(i)(1) of the Commissions rules provides the required attenuation for a modulated carrier and note 2 provides an absolute offset of +/-35 kHz. Under the required designs for the SwiftBroadband modulation techniques, 99 percent of the occupied bandwidth exceeds the +/-35 kHz offset in many cases. In short, the SwiftBroadband modulation schemes make meeting the offset impossible. Therefore, EMS requests waiver of Section 87.139(i)(1) note 2 to permit an absolute offset of +/-504 kHz due to the maximum SwiftBroadband symbol rate of 151.2 kSym/s. 87.141(j) Modulation Requirements Section 87.141(j) of the Commissions rules requires transmitters used as aircraft earth stations to employ BPSK for transmission rates up to and including 2400 bps, and QPSK for higher rates. Due to the requirements of the SwiftBroadband, the Small SATCOM transceiver uses an additional modulation scheme that does not meet this requirement, 16-QAM. EMS therefore requests waiver of Section 87.141(j) of the Commissions rules to permit the use of 16-QAM. EMS requests that the Commission waive the requirements of Part 87 described above to permit certification of its Inmarsat AMSS transceivers. The Commission has granted similar waivers to EMS, Rockwell Collins, Honeywell and others so that aircraft passengers and crew can receive high speed voice and data communications. In addition, a waiver has been granted to Omnipless for UAV applications. Such waiver will not cause harmful interference to other services and is in the public interest. EMS further requests expedited treatment of the instant waiver request. Conclusion Sincerely, Dennis Teske, Sr. Director Engineering Honeywell Confidential