K6KHSD-MK2Satcom Transeiver

23-15-30TITLE PAGE T-1 3 JUN 10 eNfusion ® HSD-440 Mark 2 Terminal System Description, Installation, and Maintenance Manual MN-1252-33412, Revision 001 This document provides procedures for the equipment listed below. ModelPart Number eNfusion ® HSD-440 Mark 2 Terminal 115 V ac or 28 V dc 1252-A-3820-01 23-15-30TITLE PAGE T-2 3 JUN 10 PROPRIETARY STATEMENT This document contains information which is proprietary and 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. HSD-440 Mark 2 Terminal System Description, Installation, and Maintenance Manual Document Number: MN-1252-33412, Revision 001 Revision Table RevisionECRDescription 001N/ADraft release for review. Cabin Network Xcelerator® and CNX® are registered trade marks of EMS Technologies, Ltd. 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 deve lopment. 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, Ontario, 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 3 JUN 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-1252-33412 Publication title:HSD-440 Mark 2 TerminalSystem Description, Installation, and Maintenance Manual Latest issue date:June 3, 2010 Document revision:001 Customer information: Name: Company: Tel: Fax: Email: Comments and suggestions: Date: Comments: 23-15-30CR-2 3 JUN 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL eNfusion® HSD-440 Mark 2 Terminal 23-15-30RR-1 3 JUN 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 eNfusion® HSD-440 Mark 2 Terminal 23-15-30RR-2 3 JUN 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL eNfusion® HSD-440 Mark 2 Terminal 23-15-30SBL-1 3 JUN 10 SERVICE BULLETIN LIST Service Bulletin Number Subject Manual Rev. Number Manual Rev. Da te N/AN/AN/AN/A SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL eNfusion® HSD-440 Mark 2 Terminal 23-15-30SBL-2 3 JUN 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL eNfusion® HSD-440 Mark 2 Terminal 23-15-30LEP-1 3 JUN 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 eNfusion® HSD-440 Mark 2 Terminal 23-15-30LEP-2 3 JUN 10 Blank Page SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL eNfusion® HSD-440 Mark 2 Terminal 23-15-30TC-1 3 JUN 10 TABLE OF CONTENTS 1. Illustration of Equipment .............................................................................INTRO-2 2. Product Terms and Conditions ...................................................................INTRO-2 3. Acronyms and Abbreviations......................................................................INTRO-2 4. Safety Advisories .........................................................................................INTRO-6 1. Inmarsat System Overview................................................................................... 1-1 2. Equipment Overview ............................................................................................. 1-3 3. Equipment Specifications..................................................................................... 1-5 4. System Interfaces................................................................................................ 1-10 A. Central Maintenance Computer (CMC) .......................................................................... 1-10 B. Source Destination Identification (SDI) .......................................................................... 1-11 C. FWD IDs, ICAO IDs, and IMSI ....................................................................................... 1-11 D. Weight-On-Wheel (WOW) Pin Wiring ............................................................................ 1-11 E. IRS ARINC 429 Interface ............................................................................................... 1-12 F. Antenna Interface .................................................................................…

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R Avrnr¡oru I'i\lS Iee lrrrologics Carrr.lrr I t,l [.N.15 .\r'itrtir.rr¡ - (]ur¡s a 4(){l \lal'lc' (iror c lìrr¿d ()tt¡rr a. O\r Kl \1 I ßij (. arì¡.Iiì [cl. :l l, l_ì.ieI 9()6-[ [:¡r. I ti l.ì 591 9l 20 \\ \\ \,, .i\t)ìSil\ iltti()ìì.e()rìì Date: May 7,2010 Federal Communication Commission EQU IPMENT APPROVAL SERVICES P.O. Box 358315 Pittsburgh, PA 1 5251-531 5 Request for Confidentiality Subject: Confidentiality Request for: FCC lD: K6KHSD-MK2 Pursuant to FCC 47 CRF 0.457(d) and 0.459 and lC RSP-100, Section 10, the appl¡cant requests that a part of the subject FCC application be held confidential. Type of Confidentiality Requested Exhibit I Short Term n Short Term E Snort Term E Sfrort Term f]Short Term E Short Term E Short term E Short Term D Short Term I Permanent I Permanent E] Permanent E Permanent I Permanent Block Diagrams ExternalPhotos lnternalPhotos Operation Description/Theory of Operation Parts List & PlacemenUBOM Tune-Up Procedure Schematics Test Setup Photos User's Manual EMS Aviation has spent substantial effort in developing this product and it is one of the first of its kind in industry. Having the subject information easily available to "competition" would negate the advantage they have achieved by developing this product. Not protecting the details of the design will result in financial hardship. Permanent Confidentiality: The applicant requests the exhibits listed above as permanently confidential be permanently withheld from public review due to materials that contain trade secrets and proprietary information not customarily released to the public. Short-Term Confidentiality : The applicant requests the exhibits selected above as short term confidential be withheld from public view for a period of days from the date of the Grant of Equipment Authorization and prior to marketing. This is to avoid premature release of sensitive information prior to marketing or release of the product to the public. Applicant is also aware that they are responsible to notify Compliance Testing in the event information regarding the product or the product is made available to the public. Compliance Testing will then release the documents listed above for public disclosure pursuant to FCC Public Notice DA 04-1705. Sincerely, W Director, Business Process lmprovement and Quality EMS Aviation - Ottawa

l:\I\'l ¡cllrrt.,l,¡.gi;s (- iìrl¡rla I [. \ l\ '\r iirtior¡ - (-)ttarr li 'l{l{) \ lirl-rli (.¡rtrr t' fùr¡rtl ( )ttrtrr rr. ()N l(l\ I liS C.¡rra.l¡ rd -l'rl. 'r I (; I I 591 q(io-l I rr... .r I ri l'ì 591 9l]o \,.',\ \\ \'lìt.iit \ itrl irrit.Lolll AvrRr¡oru 4May 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 HSD-MK2, and HSD-MK3, Aeronautical Earth Station Satellite Commu nications Transceiverc FCC ID's K6KHSD.MK2 and K6KHSD.MK3 Dear Sir, ln accordance with Federal Communications Commission (FCC) Rules and Regulations, Part 87.'t47(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 HSD-MK2 and HSD-MK3 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 HSD-MK2 and HSD-MK3 Aeronautical Earth Station (AES) satellite communication transceivers support the lnmarsat Classic-Aero H+, Swift64, and SwiftBroadband aeronautical satellite communications services. These transceivers meet the applicable requirements of RTCA/DO-210D "Minimum Operational Performance Standards for Geosynchronous Orbit Aeronautical Mobile Satellite Services (AMSS) Avionics". Both the HSD-MK2 and the HSD-MK3 are product derivatives of the FCC authorized and FAA Technical Standard Order (TSO C-132) authorized HSD440. The HSD-MK2 transceiver replaces one of the HSD-440 channel cards with a version that provides two lnmarsat Aero H+ voice channels versus one. The HSD-MK3 transceiver replaces the other HSD-440 channelcard with a version that provides multiple lnmarsat services on the same circuit card assembly. The following provides a brief description of the HSD-MK2 and HSD-MK3 transceivers. When used, the abbreviation HSD refers to either model of transceiver. Where distinction is necessary, the appropriate model name is used. The EMS HSD is the transceiver of an Aeronautical Earth Station (AES) which incorporates the satellite data unit and the high power amplifier functions of the AES. The SDU is packaged in an eight Modular Concept Unit (8-MCU) enclosure as defined in ARINC Specification 600. The SDU contains 2 channel card circuit card assemblies (CCA), a data inpuVoutput CCA, a control processor CCA, an RF inpuVoutput module, an RF power amplifier, a multi-voltage output power supply, and interconnection wiring. The channel cards provide the interfaces between the user voice or data and the lnmarsat L-band satellite signal. Multiple L-band signals are produced on each channel card. The HSD-MK2 and HSD-MK3 ditfer in the type and capability of channel card used. The data inpuUoutput 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 AES. The RF inpuUoutput module combines the L-band signals from the channel cards and distributes the receive signal from the AES diplexer/low noíse amplifier. The power amplifier provides the high power RF signal gain with a nominal maximum output power of 60 watts. F|l|S*_ AvlRnoru MCDU (x2) or WSCI (x2) { \l\-1.r.:l¡1,'!,,.:i¡. ( ¡rr¡,lli f t'l l.\l'¡ \i i;1rì,ri¡ - ()tr;t,,,'r ,illf r \ i t,)i . (¡r'rrr'.. fìr)llrl ( )ititi\ r. t )N hl\ i llfì L..rrr;rrlu '1.l. I tiI1 i()| i){rl)i I i1\. .i.l lr I 1 !a | '/ l.l{) \\,,\ \\ i'tììjit\..i:rli0it , (ìlìt The relationship between the HSD transceiver and the other subsystems of the Aeronautical Earth Station is illustrated in Figure 1. C€nùal Llåhtenoæ Swilr6{ Soryl@s Cwputo, (CMC) loll Oul'ty Vdæ (6,4 kÞs) 3.1 kHz audþ ,: 55. 64 kbps ciart-swilcfBd data 64 lbps pactelsktchod data SwlttE.ddb¡nd Sed¡cerl Toll Qu¿l'ly Vdæ (ü kbps) AMBE|2 Voke 3.1 kHz ôudp 56, 64 kbps ord¡t.sw'tcùed data Up to 432 kbps paclofsetched dåta Aô.o.H.,H+ Sôry14 4.8 kb0s úæ Syslm C0fi9 Str¿ps D¡$roto L/O Figure 1: Aeronautical Earth Station 2l Manufacturer's ldentification The EMS model identification and the FCC ldentifier for the HSD equipment are presented in Table 1. For reference, the supported lnmarsat services are included. Table 1: Equipment ldentification Anten na Characteristics The HSD 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. Rated Output Power 60 watts lI! - AcARs/ æ cMU <--------J (x2) I + 3) 4l Equipment ldentification lnmarsat Services EMS ModelFCC ID Classic Aero Swift64SwiftBroadband HSD-MK2 K6KHSD-MK2 PRT Data 2 SCPC voice 64kbps MPDS 64kbps ISDN voice (optional) 64kbps CS data (optional) PS Background Class PS Streaming Class 64kbps CS data AMBE 4kbps voice HSD-MK3 K6KHSD-MK3 PRT Data 1 SCPC voice 64kbps MPDS 64kbps ISDN voice (optional) 64kbps CS data (optional) 2 of the following: PS Background Class PS Streaming Class 64kbps CS data AMBE 4kbps voice Avlnno¡v [;\l\.1 ..clrrrrrlt',:i¡s(_trta,i?l Lt,l. -l cl.-: I r, l] igl ()lr(r,[ i:\lS \ri¡¡¡i¡¡¡¡ - ()¡¡¿ri¡ [¡r. t l r¡1" \ql 9l-](-) -lt-ttl\llrlrlc(rt(¡\('fì()i!(l \\\\\\.!'tììsir\i.lii(rtl.(\ìilr ()triì\\ir. ()N l(l\ llJS Clll;ril¡ 6) 7l 5) Emission Types and Characteristics The HSD equipment emission types and character¡stics are summarized in Table 2. Table 2: Emission Types and Characteristics Frequencies of Operation 1626.5 to 1660.5 MHz transmitting 1525 to 1559 MHz receiving Receiver Characteristics The receiving characteristics of the HSD equipment meet the applicable requirement of the lnmarsat System Definition Manuals (SDMs) and RTCA/D0-210. lf this information meets with your approval, EMS herein requests that your office notify the FCC's Office of Engineering and Technology Labor…

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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 Arm s Regulations (ITAR) 22 CFR 120-130. Figure 1: H S D M K 2 F r o n t V i e w 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 Arm s Regulations (ITAR) 22 CFR 120-130. Figure 2: H S D M K 2 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 Arm s Regulations (ITAR) 22 CFR 120-130. Figure 3: H S D M K 2 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 Arm s Regulations (ITAR) 22 CFR 120-130. Figure 4: H S D M K 2 Back 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 Arm s Regulations (ITAR) 22 CFR 120-130. Figure 5: H S D MK2 Bottom View

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: K6KHSD-MK2 400 Maple Grove Road Ottawa, ON K2V 1B8 CANADA TEL: +1 613 591-9064 DESC REV NSN EMS P/N MFG DATE XXXXXXXXXXXX CA XXXX-X-XXXX XXXXXXXXXXXX EMS S/N 000 XXX SUPL CODE MMM, YYYY WT XX.X X.X LBS KG

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 HSD-MK2, FCC ID LABEL HSD A38473 1252-D-3851 1252D3851RevA00 11NTS Mark Boyle14APR2010 A NOTE: 1. USE BLANK LABEL STOCK (ITEM 10) WITH ARTWORK 1252-G-3851 (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: K6KHSD-MK2

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: 1252 ‐ K ‐ 3411 ‐ 01 C ONTROL P ROCESSOR T OP ............................................................................................................................................................................................................. 2 F IGURE 2: 1252 ‐ K ‐ 3411 ‐ 01 C ONTROL P ROCESSOR WITHOUT S HIELD ............................................................................................................................................................................................ 3 F IGURE 6: 1252 ‐ K ‐ 3411 ‐ 01 C ONTROL P ROCESSOR B OTTOM ....................................................................................................................................................................................................... 4 F IGURE 3: 1210 ‐ A ‐ 1510 HSD M ULTI C HANNEL C ARD T OP ......................................................................................................................................................................................................... 5 F IGURE 5: 1210 ‐ A ‐ 1510 HSD M ULTI C HANNEL C ARD WITHOUT S HIELD ........................................................................................................................................................................................ 6 F IGURE 4: 1210 ‐ A ‐ 1510 HSD M ULTI C HANNEL C ARD B OTTOM ................................................................................................................................................................................................... 7 F IGURE 7: 1210 ‐ A ‐ 0010 ‐ 02 BGAN 2 C HANNEL C ARD T OP ........................................................................................................................................................................................................ 8 F IGURE 8: 1210 ‐ A ‐ 0010 ‐ 02 BGAN 2 C HANNEL C ARD B OTTOM .................................................................................................................................................................................................. 9 F IGURE 9: 1210 ‐ A ‐ 0002 ‐ 01 HSD D IGITAL M ODULE T OP (P ART OF THE BGAN 2 C HANNEL C ARD ) .................................................................................................................................................. 10 F IGURE 10: 1210 ‐ A ‐ 0002 ‐ 01 HSD D IGITAL M ODULE B OTTOM (P ART OF THE BGAN 2 C HANNEL C ARD ) ......................................................................................................................................... 11 F IGURE 11: 1210 ‐ A ‐ 0003 RF M ODULE T OP (P ART OF THE BGAN 2 C HANNEL C ARD ) ................................................................................................................................................................... 12 F IGURE 12: 1210 ‐ A ‐ 0003 RF M ODULE B OTTOM (P ART OF THE BGAN 2 C HANNEL C ARD ) ............................................................................................................................................................. 12 F IGURE 13: 1110 ‐ F ‐ 0017 OXCO T OP ................................................................................................................................................................................................................................... 13 F IGURE 14: 1110 ‐ F ‐ 0017 OXCO B OTTOM ............................................................................................................................................................................................................................ 14 F IGURE 15: 1110 ‐ F ‐ 0017 OXCO I NSTALLED .......................................................................................................................................................................................................................... 15 F IGURE 16: 1252 ‐ F ‐ 3344 P OWER S UPPLY T OP ....................................................................................................................................................................................................................... 16 F IGURE 17: 1252 ‐ A ‐ 3344 P OWER S UPPLY B OTTOM ................................................................................................................................................................................................................ 17 F IGURE 18 1252 ‐ F ‐ 1120 HPA T OP ....................................................................................................................................................................................................................................... 18 F IGURE 19: 1252 ‐ F ‐ 1120 HPA B OTTOM ............................................................................................................................................................................................................................... 19 F IGURE 20: 1252 ‐ A ‐ 3439 RF C OMBINER T OP ........................................................................................................................................................................................................................ 20 F IGURE 21: 1252 ‐ A ‐ 3439 RF C OMBINER I NSIDE ........................................................................................................................................................................…

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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 p1030016, d1040038 Rev 1.0 Date: April 20, 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: HSD-MK2 FCC ID: K6KHSD-MK2 FCC Rules: Part 87 To Whom It May Concern: 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 p1030016, d1040038 Rev 1.0 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 Parts 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. (FCC 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 p1030016, d1040038 Rev 1.0 Date: April 20, 2010 Federal Communications Commission Via: Electronic Filing Attention: Authorization & Evaluation Division Applicant: EMS Technologies Canada, Ltd Equipment: HSD-MK2 FCC ID: K6KHSD-MK2 FCC Rules: Part 87 To Whom It May Concern: 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. If you should need any further information, kindly contact the writer who is your authorized 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 p1030016, d1040038 Rev 1.0 Test Report for FCC ID: K6KHSD-MK2 Model: HSD-MK2 to Federal Communications Commission Rule Part(s) 87 Date of report: April 20, 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 p1030016, d1040038 Rev 1.0 Test Report Revision History Revision Date Revised By Reason for revision 1.0 April 20, 2010 J. Erhard Original Document Compliance Testing 3356 N. San Marcos Place, Suite 107 Chandler, Arizona 85225-7176 (866) 311-3268 phone, (480) 926-3598 fax p1030016, d1040038 Rev 1.0 List of Exhibits (FCC Certification (Transmitters) - Revised 9/28/98) Applicant: EMS Technologies Canada, Ltd FCC ID: K6KHSD-MK2 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 p1030016, d1040038 Rev 1.0 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 Acc…

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