K6KIPLDAircraft Earth Station

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: www.myaerospace.com Page T-1 Publication Number MN-0000042, Revision F6 May 2011 Revised 28 Feb 2018 © Honeywell International Inc. Do not copy without express permission of Honeywell. 23-15-45 Legal Notice Export Control 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 first obtaining approval from the U.S. government or as otherwise authorized by U.S. law and regulations. ECCN: 7E994. ASPIRE-200 System Description, Installation, and Maintenance Manual This guide provides procedures for installation, configuration, and operation of the equipment listed below. ModelPart Number Low Gain Antenna System1541-K-1015-01 AMT-3500 Intermediate Gain Antenna System1541-K-1007-01 AMT-700 High Gain Antenna System1541-K-1006-01 AMT-3800 High Gain Antenna System1541-K-1006-02 AMT-1800 Intermediate Gain Antenna System1541-K-1007-42 AMT-1800 Intermediate Gain Antenna System with CCU-2001541-K-1007-02 AMT-1800 Intermediate Gain Antenna System with CNX-2501541-K-1007-32 AMT-3500 Intermediate Gain Antenna System with CNX-2001541-K-1007-11 AMT-1800 Intermediate Gain Antenna System with CNX-2001541-K-1007-12 Page T-2 28 Feb 2018 23-15-45 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 © Honeywell International Inc. Do not copy without express permission of Honeywell. ModelPart Number AMT-1800 Intermediate Gain Antenna with CNX-9001541-K-1007-52 AMT-700 High Gain Antenna with CNX-2001541-K-1006-11 AMT-700 High Gain Antenna with CNX-2501541-K-1006-31 AMT-700 High Gain Antenna with CNX-9001541-K-1006-51 AMT-3800 High Gain Antenna with CNX-2001541-K-1006-12 AMT-3800 High Gain Antenna with CNX-2501541-K-1006-32 AMT-3800 High Gain Antenna with CNX-9001541-K-1006-52 Page T-3 28 Feb 2018 23-15-45 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL Aspire-200 © 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. 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; Honeywell-authorized repair facilities; owners of a Honeywell aerospace product that is the subject of these Materials (“Honeywell Product”) that have entered into a written agreement with Honeywell relating to the repair or maintenance of Honeywell Product; and direct recipients of Materials from Honeywell via https://myaerospace.honeywell.com/wps/portal/ that own a Honeywell Product. The terms and conditions of this Honeywell Materials License Agreement (“License Agreement”) govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the maintenance or repair of a Honeywell Product and that is the subject of the Materials conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. However, this License Agreement will govern in the event of a conflict between these terms and conditions and those of a purchase order or acknowledgement. Your access or use of the Materials represents your acceptance of the terms of this License Agreement. 1. License Grant - If you are a party to an applicable written agreement with Honeywell relating to the repair or maintenance of the subject Honeywell Product, subject to your compliance with the terms and conditions of this License Agreement, Honeywell hereby grants you, and you accept, a limited, personal, non-transferrable, non-exclusive license to use these Materials only in accordance with that agreement. If you are a direct recipient of these Materials from Honeywell’s MyAerospace Technical Publication website and are not a party to an agreement related to the maintenance or repair of the subject Honeywell Product, subject to your compliance with the terms and conditions of this License Agreement, Honeywell hereby grants you, and you accept, a limited, personal, non-transferrable, non-exclusive license to use a single copy of these Materials to maintain or repair only the subject Honeywell Product installed or intended to be installed on the aircraft you own and/or operate and only at the facility to which these Materials have been shipped (“the Licensed Facility”). Transfer of the Materials to another facility owned by you is permitted only if the original Licensed Facility retains no copies of the Materials, the transferee accepts all of your obligations and liabilities under this License Agreement, and you provide prior written notice to Honeywell with the name and address of the transferee. You agree not to use these Materials for commercial purposes. 2. Restrictions on Use - You may not sell, ren…

Text truncated - open the document above for the full version.

SATCOM 400 Maple Grove Road Ottawa, ON K2V 1B8 www.honeywell.com Honeywell Internal May 12, 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, EMS Technologies Canada, Ltd., a wholly owned subsidiary of Honeywell International Inc., hereby authorize Compliance Testing, LLC 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 Teske Sr. Director Engineering Honeywell International Inc.

SATCOM 400 Maple Grove Road Ottawa, ON K2V 1B8 www.honeywell.com Honeywell Internal May 12, 2020 Federal Communications Commission Authorization & Evaluation Division 7345 Oakland Mills Road Columbia, Maryland 21046 RE: Long-Term Confidentiality Request for IPLD MODEL # 1541-A-2000, FCC ID: K6KIPLD 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, EMS Technologies Canada, Ltd., a wholly owned subsidiary of Honeywell International Inc., 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 Teske Sr Director Engineering Honeywell Interational Inc.

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. Page 1 Figure 1: IPLD Front View 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. Page 2 Figure 2: IPLD Isometric View 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. Page 3 Figure 3: IPLD Side View 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. Page 4 Figure 4: HDU Bottom View 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. Page 5 Figure 5: IPLD Back View

APPDCHKBYDATEDESCRIPTIONCHG ORGREV THIS DOCUMENT CONTAINS INFORMATION WHICH IS PROPRIETARY AND CONFIDENTIAL TO EMS TECHNOLOGIES. THIS INFORMATION MAY NOT BE USED, DISCLOSED OR COPIED, IN WHOLE OR IN PART, WITHOUT THE PRIOR WRITTEN PERMISSION OF EMS TECHNOLOGIES. CONTRACT/PROJECT APPROVALS DRAWN SIGNDATE CHECKED MECH. ELECT. MFG ENG PASIZEFSCM NO.DWG. NO.REV CMO PGM MGRSCALE TITLE LIBRARYSHEETOF © EMS TECHNOLOGIES. ALL RIGHTS RESERVED. 400 MAPLE GROVE ROAD OTTAWA, ONTARIO K2V 1B8 IPLD, FCC ID LABEL IPLD A38473 54000-D-1180 54000-D-1180_REVC 11NTS M. BOYLE 13JAN2011 C NOTE: 1. USE BLANK LABEL STOCK (ITEM 10) WITH ARTWORK 54000-G-1180 (ITEM 30) TO PERMANENTLY MARK IDENTIFICATION LABEL FOR: - FCC ID. - FCC Statement 2. THE BORDERS OF THE LABEL ARE SHOWN FOR ORIENTATION PURPOSES ONLY. 3. PROTECT COMPLETED LABEL BY APPLYING OVERLAMINATE (ITEM 20). 4. IF REQUIRED, CUT THE LABEL TO THE SIZE SHOWN. 0.75” 2.25” This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) This device may not cause harmful interference, and (2) This device must accept any interference received, including interference that may cause undesired operation. FCC ID: K6KIPLD CAGE CODE CREVISED PER ECN-8002033 13JUN20 NB I. MILANOVIC 14JAN2011 A. BLACKADDER I. MILANOVIC M. TADIELLO S. MULDER S. BRAZEAU N/A SEE ECN B A REMOVE “-FCC ID.” FROM NOTE INITIAL RELEASE N/A 110535 11OCT11 13JAN11 MB MB SBMT N/A N/A 27APR2011 14JAN2011 27APR2011 27APR2011 02FEB2011 SEE SEPARATE PARTS LIST PRODUCTION - Released - 24 Jun 2020 15:50:05 UTC REF: ECN-8002033

p16c0010_FCC_Part 87_Rev 1.0 Page 1 of 27 Test Report Prepared for: EMS technologies Canada Lts. Model: IPLD Description: Aircraft earth station Serial Number: N/A FCC ID: K6KIPLD To FCC Part 87 Date of Issue: April 12, 2020 On the behalf of the applicant: EMS Technologies Canada Ltd. 400 Maple Grove Road Ottawa, ON K2V 1B8 Canada Attention of: Hicham El-Zibawi Phone: (613)595-7631 Email: [email protected] Prepared by Compliance Testing, LLC 1724 S. Nevada Way Mesa, AZ 85204 (480) 926-3100 phone / (480) 926-3598 fax www.compliancetesting.com Project No: p16c0010 Poona Saber Project Test Engineer This report may not be reproduced, except in full, without written permission from Compliance Testing. All results of this test report relate only to the item(s) that were tested. p16c0010_FCC_Part 87_Rev 1.0 Page 2 of 27 Test Report Revision History Revision Date Revised By Reason for Revision 1.0 April 12 th ,2020 Poona Saber Original Document p16c0010_FCC_Part 87_Rev 1.0 Page 3 of 27 Table of Contents Description Page Standard Test Conditions Engineering Practices .................................................................................................................... 5 Test Results Summary ............................................................................................................................................................. 9 Occupied Bandwidth ............................................................................................................................................................. 10 Carrier Output Power (Conducted) ....................................................................................................................................... 11 Conducted Spurious Emissions ............................................................................................................................................. 14 Field Strength of Spurious Radiation .................................................................................................................................... 17 Emission Masks ..................................................................................................................................................................... 18 Frequency Stability (Temperature Variation) ....................................................................................................................... 19 Frequency Stability (Voltage Variation) ................................................................................................................................ 20 Necessary Bandwidth and Emission Bandwidth ................................................................................................................... 21 Measurement Uncertainty .................................................................................................................................................... 23 Test Equipment Utilized ........................................................................................................................................................ 24 Test Setup Pictures................................................................................................................................................................ 25 p16c0010_FCC_Part 87_Rev 1.0 Page 4 of 27 ILAC / A2LA Compliance Testing, LLC, has been accredited in accordance with the recognized International Standard ISO/IEC 17025:2005. This accreditation demonstrates technical competence for a defined scope and the operation of a laboratory quality management system (refer joint ISO-ILAC-IAF Communiqué dated January 2009). The tests results contained within this test report all fall within our scope of accreditation, unless noted in the table below Please refer to http://www.compliancetesting.com/labscope.html for current scope of accreditation. Testing Certificate Number: 2152.01 FCC Site Reg. #349717 IC Site Reg. #2044A-2 Non-accredited tests contained in this report: N/A p16c0010_FCC_Part 87_Rev 1.0 Page 5 of 27 Standard Test Conditions Engineering Practices Except as noted herein, the following conditions and procedures were observed during the testing: All tests and measurement data shown were performed in accordance with FCC Rules and Regulations, Volume II; Part 2, Sub-part J, Sections 2.947, 2.1033(c), 2.1041, 2.1046, 2.1047, 2.1051, 2.1053, 2.1055, 2.1057 and the following individual Parts: FCC Part 87. Measurement results, unless otherwise noted, are worst-case measurements. Environmental Conditions Temperature (ºC) Humidity (%) Pressure (mbar) 24-25.3 24.1-32.2 956-962 EUT Description: Model: IPLD Description: aircraft earth station Part number: 1524-A-2000 Additional Information: The aircraft user terminal functions also known as the SATCOM Avionics is an integral part of the complete L- band Inmarsat Satellite communications system and comprises of the following components: • SDU or HDU-200 Transceiver • SDU Configuration Module (SCM) • The IPLD integrates the HPA function, the RF diplexer and a Low Noise Rx Amplifier (.i.e. a DLNA) • Antenna - Intermediate Gain (IGA) or High Gain (HGA) • Satellite network Services The IPLD works in conjunction with a Satcom Transceiver unit. An HDU-200 (FCC ID K6K HSDXi) is used as a source generator. DC Power and Control signaling is used to connect the HDU-200 Transceiver to the IPLD. The High Power Amplifier (HPA), Diplexer and Low-Noise Amplifier functions are integrated into the IPLD. The testing included in this report exclusively exercizes the compliance of the IPLD. Software Configuration Software configuration is defined by the software LI document as follows: • Platform 1541-A-3000-01 is LI-90406994 (HDU-200) • Platform 1542-A-2000 is LI-1541-10000 (IPLD). Hardware Configuration Hardware configuration is defined by the respective platforms as follows: • 1541-A-3000-01 – HDU-200 Transceiver • 1542-A-2000 – IPLD DC Powered p16c0010_FCC_Part 87_Rev …

Text truncated - open the document above for the full version.

p16c0010_FCC_Part 1.1310_Rev 1.0 Page 1 of 7 Test Report Prepared for: EMS technologies Canada Lts. Model: IPLD Description: Aircraft earth station Serial Number: N/A FCC ID: K6KIPLD To FCC Part 1.1310 Date of Issue: August 12, 2020 On the behalf of the applicant: EMS Technologies Canada Ltd. 400 Maple Grove Road Ottawa, ON K2V 1B8 Canada Attention of: Hicham El-Zibawi Phone: (613)595-7631 Email: [email protected] Prepared By Compliance Testing, LLC 1724 S. Nevada Way Mesa, AZ 85204 (480) 926-3100 phone / (480) 926-3598 fax www.compliancetesting.com Project No: p16c0010 Poona Saber Project Test Engineer This report may not be reproduced, except in full, without written permission from Compliance Testing All results contained herein relate only to the sample tested p16c0010_FCC_Part 1.1310_Rev 1.0 Page 2 of 7 Test Report Revision History Revision Date Revised By Reason for Revision 1.0 August 12, 2020 Poona Saber Original Document p16c0010_FCC_Part 1.1310_Rev 1.0 Page 3 of 7 ILAC / A2LA Compliance Testing, LLC, has been accredited in accordance with the recognized International Standard ISO/IEC 17025:2005. This accreditation demonstrates technical competence for a defined scope and the operation of a laboratory quality management system (refer joint ISO-ILAC-IAF Communiqué dated January 2009) The tests results contained within this test report all fall within our scope of accreditation, unless below Please refer to http://www.compliancetesting.com/labscope.html for current scope of accreditation. Testing Certificate Number: 2152.01 FCC Site Reg. #349717 IC Site Reg. #2044A-2 Non-accredited tests contained in this report: N/A EUT Description: Model: IPLD Description: aircraft earth station Part number: 1524-A-2000 Additional Information: The aircraft user terminal functions also known as the SATCOM Avionics is an integral part of the complete L-band Inmarsat Satellite communications system and comprises of the following components: • SDU or HDU-200 Transceiver • SDU Configuration Module (SCM) • The IPLD integrates the HPA function, the RF diplexer and a Low Noise Rx Amplifier (.i.e. a DLNA) • Antenna - Intermediate Gain (IGA) or High Gain (HGA) • Satellite network Services The IPLD works in conjunction with a Satcom Transceiver unit. An HDU-200 (FCC ID K6K HSDXi) is used as a source generator. p16c0010_FCC_Part 1.1310_Rev 1.0 Page 4 of 7 DC Power and Control signaling is used to connect the HDU-200 Transceiver to the IPLD. The High Power Amplifier (HPA), Diplexer and Low-Noise Amplifier functions are integrated into the IPLD. The testing included in this report exclusively exercises the compliance of the IPLD. Antennas: The IPLD as part a SATCOM systems has been configured and tested with the following antenna Types: - HGA (AMT-3800, AMT-700) - IGA (AMT-1800) - LGA (Omnidirectional Blade antenna) Below are some details on the antennas. - HGA = AMT-3800 (P/N = 1242-A-0010) [Manufacturer = EMS Aviation] – Maximum Antenna Gain = 17 dBi - HGA = AMT-700 (P/N = 1428-A-0010) [Manufacturer = EMS Aviation] – Maximum Antenna Gain = 17 dBi - IGA = AMT-1800 (P/N: 1242-A-7010) [Manufacturer = EMS Aviation] – Maximum Antenna Gain = 12 dBi - LGA = SATCOM Antenna (Omni-directional Blade Antenna, P/N = S65-8282-101) [Manufacturer = Sensor Systems, Inc.] p16c0010_FCC_Part 1.1310_Rev 1.0 Page 5 of 7 MPE Evaluation This is a mobile device used in Uncontrolled Exposure environment. Limits Uncontrolled Exposure 47 CFR 1.1310 Table 1, (B) 0.3-1.234 MHz: Limit [mW/cm²] = 100 1.34-30 MHz: Limit [mW/cm²] = (180/f²) 30-300 MHz: Limit [mW/cm²] = 0.2 300-1500 MHz: Limit [mW/cm²] = f/1500 1500-100,000 MHz Limit [mW/cm²] = 1.0 Test Data Test Frequency, MHz 1643.5 Power, Conducted, mW (P) 14825.1 Antenna Gain Isotropic 17 dBi Antenna Gain Numeric (G) 50.11 Antenna Type HGA Distance (R) 20 cm 푆푆= 푃푃∗퐺퐺 4휋휋푟푟 2 Power Density (S) mw/cm 2 Power Density (S) = 147.8 Limit = (from above table) = 1.096 p16c0010_FCC_Part 1.1310_Rev 1.0 Page 6 of 7 Minimum Safe Distance Evaluation This is a mobile device used in Uncontrolled Exposure environment. Limits Uncontrolled Exposure 47 CFR 1.1310 Table 1, (B) 0.3-1.234 MHz: Limit [mW/cm²] = 100 1.34-30 MHz: Limit [mW/cm²] = (180/f²) 30-300 MHz: Limit [mW/cm²] = 0.2 300-1500 MHz: Limit [mW/cm²] = f/1500 1500-100,000 MHz Limit [mW/cm²] = 1.0 Test Data Test Frequency, MHz 1643.5 Power, Conducted, mW (P) 14825.1 Antenna Gain Isotropic 17 dBi Antenna Gain Numeric (G) 50.11 Antenna Type HGA Limit (L) 1.096 R=√(PG/4πL) Distance (R) cm Power mW (P) Numeric Gain (G) Limit (L) 232.3062639 14825.1 50.11 1.096 The minimum safe distance for installation is 232.306 centimeters. END OF TEST REPORT

P16c0019_Annex A_Rev 1.0 Page 1 of 21 Annex A Occupied Bandwidth P16c0019_Annex A_Rev 1.0 Page 2 of 21 FR80T25X16 OBW HI FR80T25X16 OBW LO P16c0019_Annex A_Rev 1.0 Page 3 of 21 FR80T25X16 OBW MD FR80T25X32 OBW HI P16c0019_Annex A_Rev 1.0 Page 4 of 21 FR80T25X32 OBW LO FR80T25X32 OBW MD P16c0019_Annex A_Rev 1.0 Page 5 of 21 FR80T25X64 OBW HI FR80T25X64 OBW LO P16c0019_Annex A_Rev 1.0 Page 6 of 21 FR80T25X64 OBW MD FR80T5X16 OBW HI P16c0019_Annex A_Rev 1.0 Page 7 of 21 FR80T5X16 OBW LO FR80T5X16 OBW MD P16c0019_Annex A_Rev 1.0 Page 8 of 21 FR80T5X32 OBW HI FR80T5X32 OBW LO P16c0019_Annex A_Rev 1.0 Page 9 of 21 FR80T5X32 OBW MD FR80T5X64 OBW HI P16c0019_Annex A_Rev 1.0 Page 10 of 21 FR80T5X64 OBW LO FR80T5X64 OBW MD P16c0019_Annex A_Rev 1.0 Page 11 of 21 R20T05QD OBW HI R20T05QD OBW LO P16c0019_Annex A_Rev 1.0 Page 12 of 21 R20T05QD OBW MD R20T1QD OBW HI P16c0019_Annex A_Rev 1.0 Page 13 of 21 R20T1QD OBW LO R20T1QD OBW MD P16c0019_Annex A_Rev 1.0 Page 14 of 21 R5T1XD OBW HI R5T1XD OBW LO P16c0019_Annex A_Rev 1.0 Page 15 of 21 R5T1XD OBW MD R5T2QD OBW HI P16c0019_Annex A_Rev 1.0 Page 16 of 21 R5T2QD OBW LO R5T2QD OBW MD P16c0019_Annex A_Rev 1.0 Page 17 of 21 R5T2XD OBW HI R5T2XD OBW LO P16c0019_Annex A_Rev 1.0 Page 18 of 21 R5T2XD OBW MD R5T45QD OBW HI P16c0019_Annex A_Rev 1.0 Page 19 of 21 R5T45QD OBW LO R5T45QD OBW MD P16c0019_Annex A_Rev 1.0 Page 20 of 21 R5T45XD OBW HI R5T45XD OBW LO P16c0019_Annex A_Rev 1.0 Page 21 of 21 R5T45XD OBW MD

P16c0010_Annex B1_Rev 1.0 Page 1 of 9 Annex B1 Spurious Emissions Conducted Part 187.139 a) Low and Mid Channel P16c0010_Annex B1_Rev 1.0 Page 2 of 9 FR80T2.5X32 low Channel 1-18 GHz FR80T2.5X32 low Channel 30 MHz- 1GHz P16c0010_Annex B1_Rev 1.0 Page 3 of 9 FR80T2.5X32 Mid Channel 1-18 GHz FR80T2.5X32 Mid Channel 30 MHz- 1GHz P16c0010_Annex B1_Rev 1.0 Page 4 of 9 FR80T5X64 Low Channel 1-18 GHz FR80T5X64 Low Channel 30MHz-1GHz P16c0010_Annex B1_Rev 1.0 Page 5 of 9 FR80T5X64 Mid Channel 1-18 GHz FR80T5X64 Mid Channel 30MHz-1GHz P16c0010_Annex B1_Rev 1.0 Page 6 of 9 R20T0.5QD low Channel 1-18 GHz R20T0.5QD low Channel 30MHz- 1GHz P16c0010_Annex B1_Rev 1.0 Page 7 of 9 R20T0.5QD Mid Channel 1-18 GHz R20T0.5QD Mid Channel 30MHz- 1GHz P16c0010_Annex B1_Rev 1.0 Page 8 of 9 R5T1XD low Channel 1-18 GHz R5T1XD low Channel 30 MHz- 1 GHz P16c0010_Annex B1_Rev 1.0 Page 9 of 9 R5T1XD Mid Channel 1-18 GHz R5T1XD Mid Channel 30 MHz-1 GHz

P16c0019_Annex B2_Rev 1.0 Page 1 of 34 Annex B2 Spurious Emissions Conducted Part 87.139 i) High Channel P16c0019_Annex B2_Rev 1.0 Page 2 of 34 FR80T25X32 10 KHz-1525 MHz 12000-18000 MHz FR80T25X32 3 KHz P16c0019_Annex B2_Rev 1.0 Page 3 of 34 1525- 1559 Mhz FR80T25X32 1559- 1585 Mhz FR80T25X32 P16c0019_Annex B2_Rev 1.0 Page 4 of 34 1585- 1605 Mhz FR80T25X32 1605 -1610 Mhz FR80T25X32 P16c0019_Annex B2_Rev 1.0 Page 5 of 34 1610 -1610.6 Mhz FR80T25X32 1610.6-1613.8 Mhz FR80T25X32 P16c0019_Annex B2_Rev 1.0 Page 6 of 34 1613.8-1614 Mhz FR80T25X32 1614- 1626.5 MHz FR80T25X32 (With Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 7 of 34 1626.5- 1660 MHz FR80T25X32 3 KHz( Without Notch Filter) 1660- 1670 MHz FR80T25X32 20 KHz( Without Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 8 of 34 1670- 1735 MHz FR80T25X32 4 KHz( Without Notch Filter) 1735-12000 MHz FR80T25X32 4 KHz( With Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 9 of 34 FR80T25X64 10 KHz- 1525 MHz 10-300 KHz P16c0019_Annex B2_Rev 1.0 Page 10 of 34 12-18 GHz FR80T25X64 3 KHz 1525-1559 Mhz FR80T25X64 3 KHz P16c0019_Annex B2_Rev 1.0 Page 11 of 34 1559-1585 Mhz FR80T25X64 3 KHz 1585-1605 Mhz FR80T25X64 3 KHz P16c0019_Annex B2_Rev 1.0 Page 12 of 34 1605-1610 Mhz FR80T25X64 3 KHz 1610-1610.6 Mhz FR80T25X64 3 KHz P16c0019_Annex B2_Rev 1.0 Page 13 of 34 1610.6-1613.8 Mhz FR80T25X64 3 KHz 1613.8-1614 Mhz FR80T25X64 3 KHz P16c0019_Annex B2_Rev 1.0 Page 14 of 34 1614-1626.5 MHz FR80T25X64 3 KHz( With Notch Filter) 1626.5- 1660 MHz FR80T25X64 3 KHz( With Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 15 of 34 1626.5- 1660 MHz FR80T25X64 3 KHz( Without Notch Filter) 1660- 1670 MHz FR80T25X64 20 KHz( Without Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 16 of 34 1670- 1735 MHz FR80T25X64 3 KHz( With Notch Filter) 1670- 1735 MHz FR80T25X64 3 KHz( Without Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 17 of 34 1735-12000 MHz FR80T25X32 4 KHz( With Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 18 of 34 R5T1XD 12-18 GHz R5T1XD 3 KHz 1525-1559 Mhz R5T1XD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 19 of 34 1559-1585 Mhz R5T1XD 1 MHz 1559-1585 Mhz R5T1XD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 20 of 34 1585-1605 Mhz R5T1XD 1 MHz 1585-1605 Mhz R5T1XD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 21 of 34 1605-1610 Mhz R5T1XD 1 MHz 1605-1610 Mhz R5T1XD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 22 of 34 1610-1610.6 Mhz R5T1XD 1 MHz 1610-1610.6 Mhz R5T1XD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 23 of 34 1610.6 - 1613.8 Mhz R5T1XD 3 KHz 1613.8- 1614 Mhz R5T1XD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 24 of 34 1614-1626.5 MHz R5T1XD 3 KHz ( With Notch Filter) 1626.5-1660 Mhz R5T1XD 3 KHz ( With Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 25 of 34 1660- 1670 MHz R5T1XD 20 KHz( Without Notch Filter) 1670- 1735 MHz R5T1XD 4 KHz( Without Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 26 of 34 1735-12000 MHz R5T1XD 20 KHz( With Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 27 of 34 R20T05QD 12-18 GHz R20T0.5QD 3 KHz 1525-1559 Mhz R20T0.5QD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 28 of 34 1559-1585 Mhz R20T0.5QD 1 MHz 1559-1585 Mhz R20T0.5QD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 29 of 34 1585-1605 Mhz R20T0.5QD 1 MHz 1585-1605 Mhz R20T0.5QD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 30 of 34 1605-1610 Mhz R20T0.5QD 1 MHz 1605-1610 Mhz R20T0.5QD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 31 of 34 1610-1613.8 MHz R20T0.5QD 3 KHz( With Notch Filter) 1613.8-1614 Mhz R20T0.5QD 3 KHz P16c0019_Annex B2_Rev 1.0 Page 32 of 34 1614-1626.5 MHz R20T0.5QD 3 KHz( With Notch Filter) 1626.5-1660 Mhz R20T0.5QD 3 KHz ( With Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 33 of 34 1660- 1670 MHz R20T0.5QD 10 KHz( Without Notch Filter) 1660- 1670 MHz R20T0.5QD 20 KHz( Without Notch Filter) P16c0019_Annex B2_Rev 1.0 Page 34 of 34 1670- 1735 MHz R20T0.5QD 4 KHz( Without Notch Filter) 1735-12000 MHz R20T0.5QD 4 KHz( With Notch Filter)

P16c0019_Annex C_Rev 1.0 Page 1 of 4 Annex C Radiated Emissions Conducted P16c0019_Annex C_Rev 1.0 Page 2 of 4 High Channel 1-18 GHz High Channel 30 MHz-1GHz P16c0019_Annex C_Rev 1.0 Page 3 of 4 Low Channel 1-18 GHz Low Channel 30 MHz-1GHz P16c0019_Annex C…

Text truncated - open the document above for the full version.