K6KA781A781 Satcom Transceiver

23-15-30TITLE PAGE T-1 16 APR 10 ARINC 781 SDU, SCM, and FMPA System Description, Installation, and Maintenance Manual MN-1394-10078, Revision 001 This document provides procedures for the equipment listed below. ModelPart Number ARINC 781 Satellite Data Unit1394-A-1100 ARINC 781 Flange Mounted High Power Amplifier1394-A-1200 ARINC 781 SDU Configuration Module1394-A-1300 23-15-30TITLE PAGE T-2 16 APR 10 PROPRIETARY STATEMENT This document contains information which is proprietary a nd confidential to EMS Aviation (EMS Technologies Canada, Ltd., Formation Inc., Sky Connect LLC). Neither this document nor the information contained within may be used for any purpose other than the purpose for which it was prepared. Neither this document nor the information contained within may be disclosed or copied without the prior written permission of EMS Aviation. © 2010 EMS Technologies Canada, Ltd., Formation Inc., Sky Connect LLC. All Rights Reserved. ARINC 781 SDU, SCM, and FMPA System Descriptio n, Installation, and Maintenance Manual Document Number: MN-1394-10078, Revision 001 Revision Table RevisionECRDescription 001N/AFirst release. Windows® is a registered trademark of Microsoft Corporation in the United States and other countries. Other product, brand, service, and company names herein are the trademarks of their respective owners. Our products are under continuous research and devel opment. Any information may therefore be changed without prior notice. EMS Aviation reserves the right to make improvements or changes in the product described in this manual at any time without notice. While reasonable efforts have been made in the preparation of this document to assure its accuracy, EMS Aviation assumes no liability resulting from any errors or omissions in this document, or from the use of the information contained herein. Printed in Canada. EMS Aviation 400 Maple Grove Road, Ottawa, Ont ario, K2V 1B8, CANADA EMS Aviation Reception:(613) 591-9064 EMS Aviation Product Support:(888) 300-7415 (calls are routed to an on-call Product Support specialist after regular business hours) +44 1684 290 020 (UK) (613) 591-3086 (outside North America) EMS Aviation E-mail Help:[email protected] EMS Aviation Web site:www.emsaviation.com EMS Aviation Sales and Marketing:800-600-9759 23-15-30CR-1 16 APR 10 CUSTOMER RESPONSE FORM To help us improve the quality of our product documentation, EMS Aviation would appreciate your comments and suggestions on this publication. Please complete the following customer survey and send to EMS Aviation at: EMS Aviation 400 Maple Grove Road Ottawa, ON K2C 0P9 E-mail: [email protected] Publication information: Publication number:MN-1394-10078 Publication title:ARINC 781 SDU, SCM, and FMPA System Description, Installation, and Ma intenance Manual Latest issue date:16 APR 10 Document revision:001 Customer information: Name: Company: Tel: Fax: Email: Comments and suggestions: Date: Comments: 23-15-30CR-2 16 APR 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ARINC 781 SDU, SCM, and FMPA 23-15-30RR-1 16 APR 10 RECORD OF REVISIONS When revisions are received, insert revised pages, record the date, and initial. Revision Number Issue Date Date Inserted Inserted b y (initial) Revision Number Issue Date Date Inserted Inserted by (initial) SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ARINC 781 SDU, SCM, and FMPA 23-15-30RR-2 16 APR 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ARINC 781 SDU, SCM, and FMPA 23-15-30SBL-1 16 APR 10 SERVICE BULLETIN LIST Service Bulletin Number Subject Manual Rev. Number Manual Rev. Da te SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ARINC 781 SDU, SCM, and FMPA 23-15-30SBL-2 16 APR 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ARINC 781 SDU, SCM, and FMPA 23-15-30LEP-1 16 APR 10 LIST OF EFFECTIVE PAGES * An asterisk indicates pages changed, added, or deleted by the current revision. F ind icates a right foldout page with a blank back. SectionPageDate SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ARINC 781 SDU, SCM, and FMPA 23-15-30LEP-2 16 APR 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL ARINC 781 SDU, SCM, and FMPA 23-15-30TC-1 16 APR 10 TABLE OF CONTENTS INTRODUCTION 1. Illustration of Equipment .............................................................................INTRO-1 2. Acronyms and Abbreviations......................................................................INTRO-2 3. Safety Advisories .........................................................................................INTRO-4 SYSTEM DESCRIPTION 1. Inmarsat System Overview................................................................................... 1-1 2. Equipment Overview ............................................................................................. 1-2 A. SDU ................................................................................................................................. 1-3 B. SCM ................................................................................................................................. 1-3 C. FMPA ............................................................................................................................... 1-4 3. Equipment Specifications..................................................................................... 1-4 4. System Interfaces.................................................................................................. 1-7 A. SDU ................................................................................................................................. 1-8 B. SCM ................................................................................................................................. 1-9 C. FMPA ............................................................................................................................... 1-9…

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Fn'S_. [:\l\ le'cllnt,lLryr.:( ¡n¡'ia [.td -f ¡1. ll tjl] i9l1)()6-[ [-\l! \t irrtiu¡i - (,)tt¿ir,.u I ¡11. f l ôli iql (/l](.) -l{lt) \llrIl¡ ('irrrr.. [ìr)irtl \\\\\\ itììsir\iiriìrì!1.(\)¡rl ( )ltiì\\:r- ()N l<l\ I llfÌ C.lìttlrl:: Avrnnorv 4 May 2010 Federal Aviation Administration Office of Spectrum Policy and Management ASR-1 800 lndependence Avenue, SW Washington D.C.20591 Reference: FAA Notification of FCC Equipment under FCC Part 87 4781,4781-MK2, and A78l-MK3, Aeronautical Earth Station Satellite Gommunications Transceive¡s FCG l.D.'s K6K4781, KOKA781-MK2, and K6KA781-MK3 Dear Sir, ln accordance with Federal Communications Commission (FCC) Rules and Regulations, Part 87.147(d), EMS Technologies Canada, Ltd. (EMS) hereby notifies the Federal Aviation Administration of its filing with the FCC of an application for certification of the 4781 Aeronautical Earth Station Satellite Communications Transceiver models referenced above. Please find below the information required pursuant to Part 87.147(d)(1). f ) Description of Equipment The EMS 4781 Aeronautical Earth Station (AES) satellite communication transceiver supports the lnmarsat Classic-Aero H+, Swift64, and SwiftBroadband aeronautical satellite communications services. The A781 meets the applicable requirements of ARINC Characteristic 781 "Mark 3 Aviation Satellite Communication Systems" and RTCA/DO-210D "Minimum Operational Performance Standards for Geosynchronous Orbit Aeronautical Mobile Satellite Services (AMSS) Avionics". The 4781 transceiver system consists of an 4781 Satellite Data Unit (SDU), an SDU Configuration Module (SCM), and an optional Flange Mount Power Amplifier (FMPA). The SDU is packaged in a six Modular Concept Unit (6-MCU) enclosure as defined in ARINC Specification 600. The SDU contains 2 channel card circuit card assemblies (CCA), an RF power amplifier, a voice and data processor CCA, a control processor CCA, a multi-voltage output power supply, and interconnection wiring. The channel cards provide the interface between the user voice or data and the lnmarsat L-band satellite signal. Multiple L-band signals are produced on each channel card. The various models of the A78l (4781, A781-Ml<2, and 4781-MK3) differ in the type and capability of channel card used. The voice and data processor CCA provides the interface between user data and voice circuits and the channel cards. The control processor CCA provides the interface to the aircraft and controls the overall operation of the SDU. The power amplifier combines the RF signals from the channel cards and provides signal gain. The amount of gain depends upon whether or not the SDU is configured to operate with the external the Flange Mount Power Amplifier (FMPA). The FMPA provides additional RF gain with a nominal maximum output power of 32 watts. The SDU Configuration Module provides configuration information forthe SDU, and the Universal Subscriber ldentity Module (USIM) cards necessary for SwiftBroadband operation. The interconnection between the A78l transceiver and the other sub-systems of the Aeronautical Earth Station is illustrated in Figure 1 and Figure 2 for operation with and withoutthe FMPA respectively. Avnnoru EñlS Tc'chnologies Canada Ltcl. ENIS Ar iation - Ouasa 40() tr,laple Grr¡ve Ro¿rd Ottana, ON KzV lB8 Canada Tel. +l 613 591 9061 [ax. +l ó13 591 9120 rl u'u . emsaviation.c'oln Pmr + Pmr Pffi t Figure 1: ATS1 Transceiver with External Power Amplifier Poüü t PoüarPor + Figure 2: 4781 Transceiver without FMPA Power Amplifier 2l Manufacturer's ldentification The EMS model identification and the FCC ldentifier for the 4781 equipment are presented in Table 1. For reference, the supported Inmarsat services are included. 8Dl' iFïx Pmt t RF TI DLI{A Alll{G r.r q Alll{C r.r tñldm 3td.il ,*^ll (Em'¡omHPA| I lultlcmùoD ^Rl¡C a2t lBllE lm Aî!.nn.l 3l¡nrl¡ng 8Ct eou RFRT DLI{A IF ¡.- lllllG ¡r q Allllc r.r Altaon! ¡'¡Ln nF& ARINC ¡l20llt*codrolt âill{C lze |lllEfunAilÍn ) 8f¡.fù 8C¡tl EJIS.-_ Av¡nnoru t:\lS'l iclrn,rltrr:i.: C¡n¡.la [.i,1. -l rl.- I rili 591 ()tì(r-l f-.\iS \rirri,rri - ()rra$il Iar.'il trll -i9l tl:l{) -li){t\írrltli:(rtrrr'¡fìrttr.l \\\\\\\'ilriir\iilti\ìtl.c{ìllt t )ti.rll. ()N I.,l\ Illlì Clnrl.lu Table 1: Equipment ldentification Equ ipment ldentification lnmarsat Services EMS ModelFCC ID Classic Aero Swift64 SwiftBroadband 4781 K6KA781 PRT Data 1 SCPC voice 64kbps MPDS 64kbps ISDN voice (optional) 64kbps CS data (optional) ABME 4.Bkbps voice (optional) PS Background Class PS Streaming Class 64kbps CS data AMBE 4kbps voice A7B1-MK2 K6KA781-MK2 PRT Data 2 SCPC voice 64kbps MPDS 64kbps ISDN voice (optional) 64kbps CS data (optional) ABME 4.8kbps voice (optional) PS Background Class PS Streaming Class 64kbps CS data AMBE 4kbps voice 4781-MK3 K6lG781-MK3 PRT Data 1 SCPC voice 64kbps MPDS 64kbps ISDN voice (optional) 64kbps CS data (optional) ABME 4.8kbps voice (optional) 2 of the following: PS Background Class PS Streaming Class 64kbps CS data AMBE 4kbos voice 3) Antenna Characteristics The 4781 equipment is designed to operate with lnmarsat approved Satcom aeronautical antenna systems. These antennas meet the requirements of ARINC CharacteristicT4l andlor ARINC Characteristic 781, and RTCA/DO-210. 4l Rated Output Power 32 watts 5) Emission Types and Characteristics The 4781 equipment emission types and characteristics are summarized in Table 2. Avrnnoru l:\l\'lcclrrli'ìr'.-r.'.(.lrrll,lir{t,l'l¡1.I I rilli9l (){X)I f:\i\ \riirli(-)tì - ()ìta\\ir ll\. il lìl.i j!)l 9l:10 -la)l) \lirl)lù (i¡o\'c fìrtirtl \\ \\\\.('lììsiì\iirtiL,ll.r(,il1 ( )rtrrrr r. ()N lll\ ¡ IJS Crrnail¡ 6) 7l Table 2: Emission Types and Characteristics Frequencies of Operat¡on 1626.5 to 1660.5 MHz transmitting 1525 to 1559 MHz receiving Receiver Characteristics The receiving characteristics of the 4781 equipment meet the applicable requirements of the lnmarsat System Definition Manuals (SDMs) and RTCA/DC,-210. lf this information meets with your approval, EMS herei…

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CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transm ittal of this work for any purpose, in any form, or by any m eans 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. Figure 1: SDU Front View Page 1 CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transm ittal of this work for any purpose, in any form, or by any m eans 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. Figure 2: SDU Isometric View Page 2 CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transm ittal of this work for any purpose, in any form, or by any m eans 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. Figure 3: SDU Side View Page 3 CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transm ittal of this work for any purpose, in any form, or by any m eans 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. Figure 4: SDU Back View Page 4 CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transm ittal of this work for any purpose, in any form, or by any m eans 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. Figure 5: SDU Bottom View Page 5

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 A781 SDU, FCC ID LABEL 781 A38473 1394-D-1324 1394D1324RevA00 11NTS Mark Boyle14APR2010 A NOTE: 1. USE BLANK LABEL STOCK (ITEM 10) WITH ARTWORK 1394-G-1324 (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 . 7 5 ” 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: K6KA781

0 . 7 5 ” 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: K6KA781

CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transm ittal of this work for any purpose, in any form, or by any m eans 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. L IST OF F IGURES F IGURE 1: 1394 ‐ A ‐ 1103 C ONTROL P ROCESSOR T OP .................................................................................................................................................................................................................. 2 F IGURE 2: 1394 ‐ A ‐ 1103 C ONTROL P ROCESSOR B OTTOM ............................................................................................................................................................................................................ 3 F IGURE 3: 1210 ‐ A ‐ 0010 ‐ 02 BGAN 2 C HANNEL C ARD T OP ........................................................................................................................................................................................................ 4 F IGURE 4: 1210 ‐ A ‐ 0010 ‐ 02 BGAN 2 C HANNEL C ARD B OTTOM .................................................................................................................................................................................................. 5 F IGURE 5:1210 ‐ A ‐ 0010 ‐ 01 BGAN 1 C HANNEL C ARD T OP ......................................................................................................................................................................................................... 6 F IGURE 6: 1210 ‐ A ‐ 0010 ‐ 01 BGAN 1 C HANNEL C ARD B OTTOM .................................................................................................................................................................................................. 7 F IGURE 7: 1210 ‐ A ‐ 0002 ‐ 01 HSD D IGITAL M ODULE T OP (P ART OF THE BGAN 1 AND BGAN 2 C HANNEL C ARDS ) ............................................................................................................................... 8 F IGURE 8: 1210 ‐ A ‐ 0002 ‐ 01 HSD D IGITAL M ODULE B OTTOM (P ART OF THE BGAN 1 AND BGAN 2 C HANNEL C ARDS )......................................................................................................................... 9 F IGURE 9: 1210 ‐ A ‐ 0003 RF M ODULE T OP (P ART OF THE BGAN 1 AND BGAN 2 C HANNEL C ARDS ) ................................................................................................................................................ 10 F IGURE 10: 1210 ‐ A ‐ 0003 RF M ODULE B OTTOM (P ART OF THE BGAN 1 AND BGAN 2 C HANNEL C ARDS ) ........................................................................................................................................ 10 F IGURE 12: 1394 ‐ F ‐ 1117 OXCO T OP ................................................................................................................................................................................................................................... 11 F IGURE 13: 1394 ‐ F ‐ 1117 OXCO B OTTOM ............................................................................................................................................................................................................................ 12 F IGURE 14: 1394 ‐ F ‐ 1117 OXCO I NSTALLED .......................................................................................................................................................................................................................... 13 F IGURE 15: 1394 ‐ F ‐ 1141 SDU P OWER S UPPLY T OP ................................................................................................................................................................................................................ 14 F IGURE 16: 1394 ‐ F ‐ 1141 SDU P OWER S UPPLY B OTTOM ......................................................................................................................................................................................................... 15 F IGURE 17: 1394 ‐ F ‐ 1140 SDU P OWER A MPLIFIER T OP ........................................................................................................................................................................................................... 16 F IGURE 18: 1394 ‐ F ‐ 1140 SDU P OWER A MPLIFIER B OTTOM ..................................................................................................................................................................................................... 17 F IGURE 19: I NTERCONNECTIONS ............................................................................................................................................................................................................................................. 18 Page 1 CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATION”). USE AND DISTRIBUTION LIMITED SOLELY TO AUTHORIZED PERSONNEL The use, disclosure, reproduction, modification, transfer or transm ittal of this work for any purpose, in any form, or by any m eans 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. Figure 1: 1394-A-1103 Control Processor Top Page 2 CONFIDENTIAL, UNPUBLISHED PROPERTY OF ONE OR MORE OF THE FOLLOWING - EMS TECHNOLOGIES CANADA, LTD., FORMATION INC., SKY CONNECT LLC (COLLECTIVELY “E MS AVIATIO…

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Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030015, d1040030 Rev 2.0 Date: April 14, 2010 Applicant: EMS Technologies Canada, Ltd 400 Maple Grove Rd Ottawa, ON K2V 1B8 Canada Attention of: Ron Halka - Director, Business Process Improvement & Quality Ph: (613) 591-9064 Ext. 3244 Fax: (613) 591-9107 E-mail: [email protected] Equipment: A781 FCC ID: K6KA781 FCC Rules: Part 87 Gentlemen: Enclosed please find your copy of the Engineering Test Report for which you are subject to the restrictions as listed on the attached summary. Once a Telecommunication Certification Body (TCB) issues a Grant the Federal Communication Commission (FCC) has 30 days to review the application and request added information. It is your decision whether or not to market the equipment subject to a possible recall before the end of the 30 days. If your equipment is still retained by us, it will be returned to you 30 days after approval is achieved. Our invoice for services has been directed to your Accounts Payable Department. For any additional information please contact us. Thank you. Sincerely yours, John Erhard: Engineering Manager Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030015, d1040030 Rev 2.0 Summary of Restrictions 1. All submissions to the FCC are subject to their Examiner's interpretation. 2. Please allow from 60 to 90 days before hearing from the FCC with regard to any submission. 3. The FCC can set aside any action or modify any action, within 30 days. (FCC Rule 1.108, 1.113). 4. Under Rule 2.803, if device is not type accepted/certificated then it must not be sold, leased, offered for sale, imported, shipped or distributed or advertised for sale. 5. FCC can revoke its certificates at any time if the equipment does not meet or continue to meet their Rules. (Rule Parts 2.927, 2.939). 6. FCC can request a sample at any time (2.936). Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030015, d1040030 Rev 2.0 Date: April 14, 2010 Federal Communications Commission Via: Electronic Filing Attention: Authorization & Evaluation Division Applicant: EMS Technologies Canada, Ltd Equipment: A781 FCC ID: K6KA781 FCC Rules: Part 87 Dear Gentleman: On behalf of the Applicant, enclosed please find Application Form 731, Engineering Test Report and all pertinent documentation, the whole for approval of the referenced equipment as shown. We trust the same is in order. Should you need any further information, kindly contact the writer who is authorized to act as agent. Best regards, John Erhard: Engineering Manager Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030015, d1040030 Rev 2.0 Test Report for FCC ID: K6KA781 Model: A781 to Federal Communications Commission Rule Part(s) 87 Date of report: April 14, 2010 On the Behalf of the Applicant: EMS Technologies Canada, Ltd At the Request of: EMS Technologies Canada, Ltd 400 Maple Grove Rd Ottawa, ON K2V 1B8 Canada Attention of: Ron Halka - Director, Business Process Improvement & Quality Ph: (613) 591-9064 Ext. 3244 Fax: (613) 591-9107 E-mail: [email protected] Reviewed by: John Erhard: Engineering Manager Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030015, d1040030 Rev 2.0 Test Report Revision History Revision Date Revised By Reason for revision 1.0 April 14, 2010 J. Erhard Original Document 2.0 May 28, 2010 K. Springer Corrected Last Calibration Date on asset i00331 Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030015, d1040030 Rev 2.0 List of Exhibits (FCC Certification (Transmitters) - Revised 9/28/98) Applicant: EMS Technologies Canada, Ltd FCC ID: K6KA781 By Applicant: 1. Letter of Authorization 2. Confidentiality Request: 0.457 And 0.459 3. Identification Drawings, 2.1033(c)(11) Label Location of Label Compliance Statement Location of Compliance Statement 4. Photographs, 2.1033(c)(12) 5. Documentation: 2.1033(c) (3) User Manual (9) Tune Up Info (10) Schematic Diagram (10) Circuit Description Block Diagram Parts List Active Devices By Compliance Testing: A. Testimonial & Statement of Certification Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030015, d1040030 Rev 2.0 The Applicant has been cautioned as to the following: 15.21 Information to the User. The user’s manual or instruction manual for an intentional radiator shall caution the user that changes or modifications not expressly approved by the party responsible for compliance could void the user's authority to operate the equipment. 15.27(a) Special Accessories. Equipment marketed to a consumer must be capable of complying with the necessary regulations in the configuration in which the equipment is marketed. Where special accessories, such as shielded cables and/or special connectors are required to enable an unintentional or intentional radiator to comply with the emission limits in this part, the equipment must be marketed with, i.e. shipped and sold with, those special accessories. However, in lieu of shipping or packaging the special accessories with the unintentional or intentional radiator, the responsible party may employ other methods of ensuring that the special accessories are provided to the consumer, without additional charge. Information detailing any alternative method used to supply the special accessories for a grant of equipment authorization or retained in the verification records, as appropriate. The party responsible for the equipment, as detailed in § 2.879 of this chapter, shall ensure that these special accessories are pro…

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Page 1 of 2 Test Setup Photos: EMS Technologies Canada, Ltd A781 Satcom Transceiver Conducted Conducted #2 Page 2 of 2 Radiated Radiated #2