K6KJETWAVE3Jetwave

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 JetWave™ MCS-8562 Terminal Part NumberModel 90400012-0001 or 90400012-0002 Modman 90401121APM 90002609-001FMA 90404518KANDU 90003227-003BUC-HPA Legal Notice Export Control This document contains technical data and is subject to Canadian and U.S. export regulations. If these commodities, technology, or software were exported from Canada, no export permit is required. If these commodities, technology, or software were exported from the United States, they must be exported in accordance with the Export Administration Regulations Diversion contrary to Canadian or U.S. Law or regulations is prohibited. Canadian ECL: C-NEPR ECCN: EAR99 23-15-84 Publication Number D202009001302, Revision 0 Page T-1 Initial 11 Nov 2020 Revised 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. 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. 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You agree that Materials shall only be used for the purpose of the rights granted herein. The Material furnished hereunder may be subject to U.S. export regulations. You will adhere to all U.S. export regulations as published and released from time to time by the U.S. Government. You may not design or manufacture a Honeywell part or detail of a Honeywell part, to create a repair for a Honeywell part, design or manufacture any part that is similar or identical Page T-2 23-15-84 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal to a Honeywell part, compare a Honeywell part or design of a Honeywell part to another part design, or apply for FAA PMA or other domestic or foreign governmental approval to manufac…

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Figure 3-11. (Sheet 5 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-69/3-70 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 6 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-71/3-72 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 7 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-73/3-74 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 8 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-75/3-76 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 9 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-77/3-78 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 10 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-79/3-80 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 11 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-81/3-82 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 12 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-83/3-84 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 13 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-85/3-86 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-11. (Sheet 14 of 14) FMA Outline and Installation Drawing (90002609-001) Page 3-87/3-88 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 1 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-89/3-90 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 2 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-91/3-92 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 3 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-93/3-94 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 4 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-95/3-96 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 5 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-97/3-98 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 6 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-99/3-100 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 7 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-101/3-102 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 8 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-103/3-104 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Figure 3-12. (Sheet 9 of 9) JetWave™ MCS-8562 Terminal Interconnect Diagram - (90410870) Page 3-105/3-106 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal SECTION 4 – SOFTWARE CONFIGURATION 1.ARINC 615A Software Data Load Process A.Introduction As a minimum, APM system configuration files need to be loaded onto the JetWave™ MCS-8562 Terminal. The Jet…

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- For each unique L1-L3 code, maintained across reset/power down, it records the number of occurrences and the time of the last occurrence. - For every link the LRU has, it records the status: UNKNOWN (default after power on), DISABLED, INACTIVE, NO_LAYER_1 (when applicable), HIGH_PACKET_LOSS, ACTIVE (normal). It also records if the link is causing a mute of the system. - For every ARINC 429 label the LRU understands, it records the status: DISABLED, UNKNOWN (default after power on), ACTIVE, SSMERROR, MISSING. It also records if the label is causing a mute of the system. - For every input discrete the LRU possesses, it records the status: ASSERTED, DEASSERTED. - The LRU maintains in memory the reason, if any, for muting. (2)LRU Codes BITE event information is encoded by the LRUs in three values. The values are named L1 thru L3: L1 denotes the LRU or interface (generated by an LRU on its behalf) which is generating the event - - L2 denotes the Shop Replaceable Module within an LRU for a event relating to an LRU, or for interfaces it denotes a particular part of the interface which is generating the event. - L3 further defines the unique event that occurred. Each fault or event also has an additional text field which can carry additional information helpful to understand the fault or event that happened. The combination of L1 thru L3 alone uniquely identifies a BITE event in the system. (3)L1 Codes (a)The event L1 code uses two hexadecimal digits to identify a LRU or an interface within an AES LRU. NOTE:All other codes not explicitly stated are spare. (4)L2 Codes (a)The event L2 code uses two hexadecimal digits to identify a shop-replaceable module within an AES LRU: (b)The event L2 code further identifies specific inter LRU interfaces. (c)The event L2 code further identifies ARINC 429 and ARINC 791 discrete interfaces, coded. (d)The event L2 code further identifies user interfaces. Page 6-12 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal (5)L3 Codes (a)The L3 code is four hexadecimal digits, used to uniquely identify the fault or event against an L1, L2 code pair. (b)Each LRU defines their own L3 codes. These are given in the fault table, refer to Table 6-1. Table 6-1. L1, L2 and L3 Codes Repair actionLog type L3L2L1 DescriptionCode Descrip- tion Code Descrip- tion Code Status Message OAE Not pointed correctly 1Unknown0System0 look for the contributing critical fault entries Critical Faults critical fault mode entry 0Mode1System0 Status Message dataload mode entry 1Mode1System0 Status Message Commanded mode entry 2Mode1System0 Status Message Normal mode entry 3Mode1System0 configure tail number on the GUI, ensure APM is installed Critical Faults Tail number Missing 0 Configura- tion 3System0 Dataload APM configuration files Critical Faults Configuration File Missing 1 Configura- tion 3System0 Datload the incompatible LRU. Note: could happen on the power up after dataload and that is normal. Critical Faults Inter-LRU SW Incompatibility 2 Configura- tion 3System0 Normal for first boot upStatus Message Geographical map missing 3 Configura- tion 3System0 Dataload APM configuration filesCritical Faults Configuration File in APM missing 4 Configura- tion 3System0 enter the proper mission configurationsWarning ACTIVE MISSION FILE MISSING 7 Configura- tion 3System0 Page 6-13 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Table 6-1. L1, L2 and L3 Codes (Cont) Repair actionLog type L3L2L1 DescriptionCode Descrip- tion Code Descrip- tion Code Check discrete installation and APM configuration parameters Warning DISCRETE I/O PIN MAP DUPLICATION 8 Configura- tion 3System0 Status Message Log clearance AES Operational Historical Log 21 SNMP Engineering 5System0 Status Message Log clearance AES Fault Historical Log 22 SNMP Engineering 5System0 Status Message Log clearance AES Usage Historical Log 23 SNMP Engineering 5System0 Normal for lost connection Status Message Regulatory Log Upload Failure 0 Regulatory Log 7System0 format the drive using EUI tool. If problem reappears, contact service provider Critical FaultsReg Log Full1 Regulatory Log 7System0 Status Message User Service Enabled 0 Information Events 8System0 Status Message User Service Disabled 1 Information Events 8System0 Status Message Geographic Map Stored 2 Information Events 8System0 Normal for first boot up Status Message Geographic Map download failed 3 Information Events 8System0 Status Message Aircraft On Ground 4 Information Events 8System0 Status Message Aircraft In Air5 Information Events 8System0 Status Message AES in Network6 Information Events 8System0 Status Message AES Out of Network 7 Information Events 8System0 Status Message AES Network Operating Parameters 8 Information Events 8System0 Page 6-14 23-15-84 EFFECTIVITY ALL 11 Nov 2020 © Honeywell International Inc. Do not copy without express permission of Honeywell. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL JetWave™ MCS-8562 Terminal Table 6-1. L1, L2 and L3 Codes (Cont) Repair actionLog type L3L2L1 DescriptionCode Descrip- tion Code Descrip- tion Code Status Message JetWave SW Stored 9 Information Events 8System0 Status Message JetWave SW Download Failed A Information Events 8System0 Status Message JetWave SW Download Initiated B Information Events 8System0 Status Message TemperatureC Information Events 8System0 Status Message AES LOG UPLOAD FAILED D Information Events 8System0 Status Message INTERNAL MODEM MODE 1 MODEM MODE CHANGE 9System0 Status Message EXTERNAL MODEM MODE 2 MODEM MODE CHANGE 9System0 Status Message SUCCESSFUL FILE TRANSFER 1 MISSION CONFIG FILE UPLOAD DASystem0 Status Message FAILED FILE TRANSFER 2 MISSION CONFIG FILE UPLOAD DASyste…

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Coverletter: EMS Technologies Honeywell Satcom wants to get FCC-Certification for the following product: KRFU Ka Band Radio Frequency Unit (Block Up Convertor – High Power Amplifier) The unit will get the following FCC-ID: K6KJETWAVE3 List of documents: Exhibit Thema File Exhibit 01 Label and placement 90004031_-.pdf Label-Location-3516775.pdf Exhibit 02 Not needed -------------------- + Exhibit 03 External Photos extern_FG20-225.pdf * Exhibit 04 Block Diagrams MCS-8562_terminal_block_diagram.pdf * Exhibit 05 Schematic Diagrams SCH-APC0000148_D (PCB Assy, Gate Regulator, Ka, E-Probe ).pdf SCH-APC0000177_A (PCB Assy, RF, Ka Deck,E- Probe,Microstrip ).pdf SCH-APC0000360_A ( PCB Assy, IF, Ka, WB, Airborne ).pdf SCH-APC0000361_A (PCB Assy, BUC, Ka Airborne, WB ).pdf Exhibit 06 Testreport FG20-225_part1.pdf FG20-225_part2.pdf FG20-225_part3.pdf FG20-225_part4.pdf Exhibit 07 Test Set-up Photos setup_FG20-225.pdf + Exhibit 08 User Manual View_D202009001302_R00_part1.pdf View_D202009001302_R00_part2.pdf View_D202009001302_R00_part3.pdf + Exhibit 09 Internal Photos intern_FG20-225.pdf Exhibit 10 Informations 23-15-56.pdf Tune-Up Procedure_taken_from_Theory_of _operation.pdf Exhibit 11 RF exposure RF exposure statement taken from SYSTEM DESCRIPTION_INSTALLATION_AND MAINTENANCE MANUAL.pdf * Exhibit 12 Operational Description TN-90411170_MCS-8562_Theory_of_operation.pdf Exhibit 13 Cover letter Agent Authorization Request for confidentiality This file FCC Agent Authorization.pdf FCC Long-Term Confidentiality Request Letter (BUC- PA).pdf FCC Short-Term Confidentiality Request Letter (BUC- PA).pdf For the Exhibits marked with ‘*’ EMS Technologies Honeywell Satcom requested Confidentiality according to 47 CFR 0.457 and 0.459 of the FCC rules because these are sensitive parts owned by this company and include much of Know-How or sensitive data, it will not be provided to the public. For the Exhibits marked with ‘ + ’ EMS Technologies Honeywell Satcom requested short term confidentiality. The grantee will not market or distribute product during the Short-Term Confidentiality period requested. When the device is ready to be marketed the grantee will inform the TCB to release the Short-Term Confidentiality. The labelling on some photos may be not the actual status. The correct labelling is shown on the label photo in Exhibit 1.

HONEYWELL CONNECTED ENTERPRISE S AT C O M 400 Maple Grove Road Ottawa, K2V 1B8, Ontario www.honeywell.com December 2, 2020 Federal Communications Commission Authorization & Evaluation Division 7345 Oakland Mills Road Columbia, Maryland 21046 RE: LETTER OF AGENT AUTHORIZATION To Whom It May Concern: We, the undersigned, hereby authorize TÜV Austria to act on our behalf in all matters relating to application for equipment authorization, including the signing of all documents relating to these matters. We also hereby certify that no party to the application authorized hereunder is subject to the denial of benefits, including FCC benefits, pursuant to Section 5301 of the Anti-Drug Abuse Act of 1988, 21 U.S.C.853(a). Sincerely, Dennis F. Teske Sr. Engineering Director

HONEYWELL CONNECTED ENTERPRISE S AT C O M 400 Maple Grove Road Ottawa, K2V 1B8, Ontario www.honeywell.com December 2, 2020 Federal Communications Commission Authorization & Evaluation Division 7345 Oakland Mills Road Columbia, Maryland 21046 Subject: Long-Term Confidentiality Request for K6KJETWAVE3 To Whom It May Concern: This letter serves as an official request for confidentiality under § 0.457(d) and § 0.459 of CFR 47. We have requested that the following documents required to be submitted with this application be permanently withheld from public review. • Block Diagram • Schematics • Theory of Operation • Parts List/BOM These documents contain detailed system and equipment descriptions and related information about the product, which manufacturer/applicant considers to be proprietary, confidential, and a custom design and otherwise, would not release to the general public. Since this design is a basis from which future technological products will evolve, manufacturer/applicant feels that this information would be of benefit to its competitors, and that the disclosure of the information in these documents would give our competitors an unfair advantage in the market. Please contact me if there is any information you may need. Sincerely, Dennis F. Teske Sr. Engineering Director

HONEYWELL CONNECTED ENTERPRISE S AT C O M 400 Maple Grove Road Ottawa, K2V 1B8, Ontario www.honeywell.com December 2, 2020 Federal Communications Commission Authorization & Evaluation Division 7345 Oakland Mills Road Columbia, Maryland 21046 Subject: Short-Term Confidentiality Request for K6KJETWAVE3 To Whom It May Concern: In accordance with sections 0.457 and 0.459 of CFR 47, EMS Technologies Canada LTD. requests Short-Term Confidentiality for the following exhibits of this application for a period of 180 days after grant is issued: • External photos • Internal photos • User’s manual These documents contain detailed system and equipment descriptions and related information about the product, which manufacturer/applicant considers to be proprietary, confidential, and a custom design and otherwise, would not release to the general public. Since this design is a basis from which future technological products will evolve, manufacturer/applicant feels that this information would be of benefit to its competitors, and that the disclosure of the information in these documents would give our competitors an unfair advantage in the market. Grantee will not market or distribute product during the Short-Term Confidentiality period requested. When the device is ready to be marketed the grantee will inform the TCB to release the Short-Term Confidentiality. Please contact me if there is any information you may need. Sincerely, Dennis F. Teske Sr. Engineering Director

www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU (JW-2 BUC HPA V3) external view #1 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 1 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU external view #2 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 2 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU external view #3 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 3 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU external view #4 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 4 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU external view #5 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 5 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU external view #6 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 6 of 42 Date: 21.12.2020

1 A 234 B C D 1234 A B C D ()1.00 ()2.00 SHEET 1 OF 1WT: .16 LB CALCSCALE:1/1 REV - DWG NO 90004031 CAGE CODE 5VWN5 SIZE C FCC LABEL MCS-8562 EMS DEFENSE TECHNOLOGIES INC. Norcross, GA USA CONTRACT NUMBER NA ELECTRONIC APPROVALS INITIAL RELEASE: ECN-XXXXXX ALL APPROVALS CONTROLLED BY THE PRODUCT DATA MANAGEMENT SYSTEM ANALYST QUALITY PROJECT CHECKER DESIGN 12-16-2020DRAWING START THIRD ANGLE PROJECTION SALES ORDER NUMBER NA MA WORK ORD/EWO/NETWORK ACTIVITY NO NA PROGRAM NA SIMILAR PART NO NA INITIAL APPLICATION USED ONNEXT ASSY EMS DTI-CONFIDENTIAL: THIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF EMS DEFENSE TECHNOLOGIES, INC, CONTAIN TRADE SECRETS AND MAY NOT, IN WHOLE OR IN PART, BE USED, DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OF EMS DEFENSE TECHNOLOGIES, INC. ALL RIGHTS RESERVED. EMS DATA RIGHTS HONEYWELL STANDARD PROPRIETARY US GOVERNMENT DATA RIGHTS NONE CAD MAINTAINED. CHANGES SHALL BE INCORPORATED BY THE CURRENT DESIGN ACTIVITY REVISION HISTORY - ALL SHEETS ARE THE SAME REVISION APPROVEDDATEDESCRIPTIONREVZONE SEE PDMSEE PDMSEE INITIAL RELEASE ECN-6093262- TITLE AP-1302 20100517PRO/ENGINEER NOTES: 1. MATERIAL: .002 THICK POLYMIDE BACKED WITH PRESSURE SENSITIVE ADHESIVE. 2. FINISH: BLACK LETTERING ON WHITE BACKGROUND 3. PRINT LABEL AS NOTED USING ITEMS 1 AND 2 USING MINIMUM .125 HIGH CHARACTERS. ISO VIEW SCALE 1/1 SCALE 2/1 3 1 2 NOT RELEASED FOR REFERENCE ONLY VERSION:6

CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “EMS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transmittal of this work for any purpose, in any form, or by any means without the prior written permission of EMS Aviation is strictly prohibited. This document does not contain technical data as defined in the International Traffic and Arms Regulations (ITAR) 22 CFR 120-130. Date: 1 February 2017 Federal Communication Commission EQUIPMENT APPROVAL SERVICES P.O. Box 358315 Pittsburgh, PA 15251-5315 ATTN: Authorization and Evaluation Division PER: Label Placement RE: K6KJetWave2 JETWAVE LABEL PLACEMENT Enclosed in this document are drawings showing the FCC label placement for the JetWave™ Aircraft Earth Station which supports Inmarsat Global Xpress Aviation data services. EMS Technologies Canada Ltd. CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “EMS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transmittal of this work for any purpose, in any form, or by any means without the prior written permission of EMS Aviation is strictly prohibited. This document does not contain technical data as defined in the International Traffic and Arms Regulations (ITAR) 22 CFR 120- 130. KRFU Note: The FCC label location of all KRFU variants is identical.

www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU internal view Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 7 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU internal detail view #1 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 8 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU internal detail view #2 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 9 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU internal detail view #3 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 10 of 42 Date: 21.12.2020 www.tuv.at | [email protected] | TÜV ® DN- FM-INE-EMV-ALL-Anl2_en Rev00 Appendix 2 Photodocumentation Description: KRFU internal detail view #4 Division: Industry & Energy Department: FG Test report reference: INE-AT/FG-20/225 Page: 11 of 42 Date: 21.12.2020

Figure 3-5. LAIM Assembly with FMA and BUC-HPA Placement on Aircraft (Typical Installation) (e)On completion of the LRU interconnection and applying power to the FMA, the FMA will stay in its current position until it is told to move by the KANDU. 6.Inspection of Waveguide A.FMA Human Expos…

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