GB8HS-720High Speed Data Unit for the MCS-7200 SATCOM System

SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS-4200/7200 TEMPORARY REVISION NO. 23-1 23-20-35 Page 1 of 53 28 Sep 2009 Publication Number A15-5111-010 © Honeywell International Inc. Do not copy without express permission of Honeywell. TO HOLDERS OF MULTI-CHANNEL SATCOM SYSTEM, SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL WITH ILLUSTRATED PARTS LIST 23-20-35, REVISION 0, DATED 15 JUL 2006. INSERT THIS PAGE AS THE FIRST PAGE OF THE MANUAL. Temporary Revision Number Applicable Page Number 23-1 TC-9 INTRO-5 INTRO-6 INTRO-7 INTRO-8 1-1 1-3 1-4 1-5 1-6 1-7/1-8 1-9 1-10 1-11 1-12 1-13 1-14 1-15 1-17 1-18 1-21 1-22 1-23 1-24 1-25 1-45 2-1 2-3 2-8 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS-4200/7200 TEMPORARY REVISION NO. 23-1 23-20-35 Page 2 of 53 28 Sep 2009 © Honeywell International Inc. Do not copy without express permission of Honeywell. 2-9 2-13 2-14 2-15 2-19 2-20 3-1 5-41/5-42 5-57 5-64 6-96 6-100 6-108 6-116 C-15 C-16 D-11 F-21 Copyright - Notice Copyright 2009 Honeywell International Inc. All rights reserved. Honeywell is a registered trademark of Honeywell International Inc. All other marks are owned by their respective companies. Honeywell – Confidential THIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF HONEYWELL INTERNATIONAL 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 HONEYWELL INTERNATIONAL INC. ALL RIGHTS RESERVED. This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. Honeywell International Inc. 21111 N. 19th Ave. Phoenix, AZ 85027-2708 U.S.A. (CAGE 55939) Publication Number A15--5111--010, Revision 000 23--20--35 Page T--1 15 Jul 2006 Honeywell International Inc. Do not copy without express permission of Honeywell. Telephone: (800) 601--3099 (U.S.A.) Telephone: (602) 365--3099 (International) System Description, Installation, and Maintenance Manual with illustrated parts list Multi--Channel SATCOM System SystemDesignationType MCS--42004--Channel MCS--72007--Channel SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006 Honeywell International Inc. Do not copy without express permission of Honeywell. Page T--2 Honeywell--Confidential THIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF HONEYWELL INTERNATIONAL 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 HONEYWELL INTERNATIONAL INC. ALL RIGHTS RESERVED. Honeywell Materials License Agreement The documents and information contained herein (“the Materials”) are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc (collectively “Honeywell”). These Materials are provided for the exclusive use of Honeywell Service Centers; Honeywell--authorized repair facilities; operators of Honeywell aerospace products subject to an applicable product support agreement, their wholly owned--subsidiaries or a formally designated third party service provider thereunder; and direct recipients of Materials from Honeywell’s Aerospace Technical Publication Distribution. 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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006 Honeywell International Inc. Do not copy without express permission of Honeywell. Page 5--1 SECTION 5 ELECTRICAL INSTALLATION 1. Overview A. General (1) This section supplies electrical installation procedures, power distribution, and interconnect diagrams for each component of the MCS system. 2. Equipment and Materials A. General (1) None. 3. Electrical Installation Procedure A. Connector Layout and Contact Arrangement (1) Each front panel connector of the SDU, HSU, and HPA complies with ARINC characteristic 615, and is used to interface the LRU with an ARINC 615 portable data loader for software uploads. Pin callouts are specified in Table 5-1. See the MECHANICAL INSTALLATION section for specifics regarding connector part numbers for the ARINC 615 connector for each LRU and the corresponding mating connector. (2) Table 5-2 lists the pin arrangements for the RJ--45 jack for the Ethernet Port 1. When a user terminal is connected to this jack, the rear connectors are disconnected so only the Ethernet Port 1 communications are available from this interface. (3) The rear connectors of the SDU, HPA, RFUIA, and HSU comply with ARINC characteristic 600 as specified in Table 5-3. The ARINC 600 connector layouts and contact arrangement for the various connector plugs for each LRU of the MCS system are shown in Figure 5-1 thru Figure 5-11. (4) Table 5-4 and Table 5-5 list the contact arrangements for the top and middle inserts for the SDU ARINC 600 connector. Table 5-6 lists the ICAO Block Strapping. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006 Honeywell International Inc. Do not copy without express permission of Honeywell. Page 5--2 Table 5-1. ARINC 615 Connector Pin Callouts PinSDU Signal NameHSU Signal NameHPA Signal Name 1PDL 429 A INPDL 429 A INPDL TO HPA 429 A 2PDL 429 B INPDL 429 B INPDL TO HPA 429 B 5SHIELD GNDSHIELD GNDSHIELD GND 8PDL 429 A OUTPDL 429 A OUTHPA TO PDL 429 A 9PDL 429 B OUTPDL 429 B OUTHPA TO PDL 429 B 16SHIELD GNDSHIELD GNDSHIELD GND 18PDL LINK APDL LINK APDL LINK A 19GND (PDL LINK B)GND (PDL LINK B)GND (PDL LINK B) 20115 VAC HOT115 VAC HOT115 VAC HOT 21CHASSIS GNDCHASSIS GNDCHASSIS GND 22115 VAC GND115 VAC GND115 VAC GND 37-- --28 V DC OUTPUT28 V DC OUTPUT 38-- --28 V DC RETURN28 V DC RETURN 40RS232 A RX--DLT-- ---- -- 41RS232 A TX--DLT-- ---- -- 42RS232 B RX--CMTRS232 TO HSURS232 TO HPA 43RS232 B TX--CMTRS232 TO DEBUGRS232 TO DEBUG 48LOGIC COMMON GNDLOGIC COMMON GNDLOGIC COMMON GND 49LOGIC COMMON GNDLOGIC COMMON GNDLOGIC COMMON GND Table 5-2. HSU Front Panel RJ--45 Pin Arrangements RJ--45 Connector PinPin NameSignal Name 1TX +RJ--45 from User (+) 2TX --RJ--45 from User (--) 3RX +RJ--45 to User (+) 6RX --RJ--45 to User (--) SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006 Honeywell International Inc. Do not copy without express permission of Honeywell. Page 5--3 Table 5-3. ARINC 600 Connector Requirements LRUConnector Description LRU Rear Connector Part No. Rack Mounting Connector Part No. Outline Diagram SDUARINC 600 -- Size 6 MCU No. 2 Shell •Type 02 Top Insert •Type 02 Middle Insert •Type 04 Bottom Insert •Index Pin Code 04 620--600--022 (Radiall) NSXN2P201X0004 (Radiall) Figure 4-2, Figure 5-1, Figure 5-2, Table 5-4, and Table 5-5 HPA (60 W) ARINC 600 -- Size 8 MCU No. 2 Shell •Type 08 Top Insert •Type 05 Middle Insert •Type 04 Bottom Insert •Index Pin Code 08 620--600--076 (Radiall) NSXN2P221X0008 (Radiall) Figure 4-3 Figure 5-3 thru Figure 5-6 RFUIAARINC 600 -- Size 4 MCU No. 2 Shell •Type 08 Top Insert •Type 05 Middle Insert •Type 04 Bottom Insert •Index Pin Code 03 NSXNR221X0103 (Radiall) NSXNP221S0103 (Radiall) Figure 4--4 Figure 5-11 HSUARINC 600-- Size 4 MCU No. 2 shell •Type 08 Top Insert •Type 05 Middle Insert •Type 04 Bottom Insert •Index Pin Code 03 620--600--075 (Radiall) NSXN2P221X0003 (Radiall) Figure 4--5 Figure 5--7 thru Figure 5--10 SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006 Honeywell International Inc. Do not copy without express permission of Honeywell. Page 5--4 Figure 5-1. SDU ARINC 600 Connector Layout SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006 Honeywell International Inc. Do not copy without express permission of Honeywell. Page 5--5 Table 5-4. Contact Arrangements for Top Insert, SDU ARINC 600 Connector ABCDEFGHJK 1 WH--10 CABIN VOICE CHANNEL 1 HOOK-- SWITCH WH--10 CABIN VOICE CHANNEL 2 HOOK-- SWITCH WH10--1 STATUS A (RINGER) WH10--1 STATUS B (RINGER) WH10--2 STATUS A (RINGER) WH10--2 STATUS B (RINGER) AVIONICS SUB-- SYSTEM SATCOM FAIL WARNING (NON MCS FAIL) WH--10 CABIN VOICE CHANNEL 1 IN--USE SATELLITE LINK NOT READY WH--10 CABIN VOICE CHANNEL 2 IN--USE 2 ANALOG PBX CHANNEL 1 INPUT HI ANALOG PBX CHANNEL 1 INPUT LO ANALOG PBX CHANNEL 1 OUTPUT HI ANALOG PBX CHANNEL 1 OUTPUT LO ANALOG PBX CHANNEL 2 INPUT HI ANALOG PBX CHANNEL 2 INPUT LO ANALOG PBX CHANNEL 2 OUTPUT HI ANALOG PBX CHANNEL 2 OUTPUT LO OO 3 COCKPIT VOICE UN-- AVAILABLE CABIN VOICE UN-- AVAILABLE PACKET DATA UN-- AVAILABLE PACKET DATA LOW SPEED ONLY AVAILABLE (CD2--2) SATCOM IN-- OPERABLE (MCS FAIL) CEPT--E1 0V SHIELD (GND) CEPT--E1 to BRIDGED CTU (CM--250) 1A CEPT--E1 to BRIDGED CTU (CM--250) 1B CEPT--E1 to BRIDGED CTU (CM--250) 2A CEPT--E1 to BRIDGED CTU (CM--250) 2B 4RESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVED CEPT--E1 0V 5RESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVED 6RESERVEDRESERVED SPARE 429 OUTPUT A SPARE 429 OUTPUT B RESERVEDRESERVEDRESERVEDRESERVEDRESERVEDSPARE 7RESERVEDRESERVEDSPARERESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVEDRESERVED 8RESERVEDRESERVEDRESERVEDRESERVEDRES…

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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTE NANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell. Page A--5/A--6 Figure A--3. Dimensions for ECS Tray Assemblies SYSTEM DESCRIPTION, INSTALLATION, AND MAINTE NANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell. Page A--7/A--8 Table A--3. SD--720 (120--10141--1XX) Pressurized Hardware Kit 4 4 4 4 4 4 4 4 4 4 4 MS51957--29 6--32 X 7/16 IN. PAN HEAD 4 4 4 4 4 4 4 4 4 4 4 NAS1149DN616J WASHER, FLAT 1 1 1 1 1 1 1 1 1 1 1 NSXN2P201S01 SD--720 ARINC CONNECTOR W/PINS ANDSOCKETS (NOTE 1 AND 2) 1 -- -- -- -- -- -- -- -- -- -- 6028--101 6 MCU TRAY SHORT, RIGHT SIDE DC FAN -- 1 -- -- -- -- -- -- -- -- -- 6068--101 6 MCU TRAY, SHORT, LEFT SIDE DC FAN -- -- 1 -- -- -- -- -- -- -- -- 6413--101 6 MCU TRAY, LONG, REAR DC FAN -- -- -- 1 -- -- -- -- -- -- -- 6013--102 6 MCU TRAY, SHORT, BOTTOM DC FAN -- -- -- -- 1 -- -- -- -- -- -- 6218--101 6 MCU TRAY, LONG, RIGHT REAR AC FAN -- -- -- -- -- 1 -- -- -- -- -- 6217--101 6 MCU TRAY, LONG, LEFT REAR AC FAN -- -- -- -- -- -- 1 -- -- -- -- 6080--101 6 MCU TRAY, LONG, NO FAN -- -- -- -- -- -- -- 1 -- -- -- 6110--101 6 MCU TRAY, SHORT, RIGHT SIDE AC FAN -- -- -- -- -- -- -- -- 1 -- -- 6216--101 6 MCU TRAY, SHORT, LEFT SIDE AC FAN -- -- -- -- -- -- -- -- -- 1 6013--106 6 MCU TRAY, SHORT, BOTTOM AC FAN -- -- -- -- -- -- -- -- -- -- 1 6035--101 6MCUTRAY,SHORT,NOFAN QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D COMPONENTS P A R T N O N O M E N C L A T U R E --111 -- 11 0 --109 --108 --107 --106 --105 --104 --103 --102 --101 PART NO. O R N O M E N C L A T U R E OR D E S C R I P T I O N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N O R IDENTIFYING NO. DESCRIPTION NOTES:1. ALTERNATE P/N: AD2--313--3AA00, NIC66H21A00AA0.2. CONTACTS ARE: 22 AWG PINS, QTY OF 300; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS. QTY OF 3; 12 AWG SOCKETS, QTY OF 4. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTE NANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell. Page A--9/A--10 Table A--4. SD--720 (120--10142--1XX) Unpressurized Hardware Kit 4 4 4 4 4 4 4 4 4 4 4 MS51957--29 6--32 X 7/16 IN. PAN HEAD 4 4 4 4 4 4 4 4 4 4 4 NAS1149DN616J WASHER, FLAT 1 1 1 1 1 1 1 1 1 1 1 NSXN2P201S01 SD--720 ARINC CONNECTOR W/PINSAND SOCKETS (NOTE 1 AND 2) 1 -- -- -- -- -- -- -- -- -- -- 200--10276--101 6 MCU TRAY SHORT, RIGHT SIDE DC FAN(NOTE 3) -- 1 -- -- -- -- -- -- -- -- -- 200--85743--101 6 MCU TRAY, SHORT, LEFT SIDE DC FAN -- -- 1 -- -- -- -- -- -- -- -- 200--93955--101 6 MCU TRAY, LONG, REAR DC FAN -- -- -- 1 -- -- -- -- -- -- -- 200--93112--101 6 MCU TRAY, SHORT, BOTTOM DC FAN -- -- -- -- 1 -- -- -- -- -- -- 6281--101 6 MCU TRAY, LONG, RIGHT REAR AC FAN -- -- -- -- -- 1 -- -- -- -- -- 6045--109 6 MCU TRAY, LONG, LEFT REAR AC FAN -- -- -- -- -- -- 1 -- -- -- -- 6080--101 6 MCU TRAY, LONG, NO FAN -- -- -- -- -- -- -- 1 -- -- -- 6282--101 6 MCU TRAY, SHORT, RIGHT SIDE AC FAN -- -- -- -- -- -- -- -- 1 -- -- 6232--101 6 MCU TRAY, SHORT, LEFT SIDE AC FAN -- -- -- -- -- -- -- -- -- 1 -- 6283--101 6 MCU TRAY, SHORT, BOTTOM AC FAN -- -- -- -- -- -- -- -- -- -- 1 6035--101 6MCUTRAY,SHORT,NOFAN QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D COMPONENTS P A R T N O . N O M E N C L A T U R E --111 -- 11 0 --109 --108 --107 --106 --105 --104 --103 --102 --101 P A R T N O . OR I D E N T I F Y I N G N O M E N C L A T U R E OR D E S C R I P T I O N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N IDENTIFYING NO. DESCRIPTION NOTES:1. ALTERNATE P/N: AD2--313--3AA00, NIC66H21A00AA0.2. CONTACTS ARE: 22 AWG PINS, QTY OF 300; 20 AWG SOCKETS, QTY OF 4; 16 AWG SOCKETS, QTY OF 3; 12 AWG SOCKETS, QTY OF 4.3. 200--10276--101 TRAY NOT CURRENTLY DESIGNED. APPROVED FAN ASSEMBLIES ARE: S0085--125, --134, --135, --138, AND --142. SYSTEM DESCRIPTION, INSTALLATION, AND MAINTE NANCE MANUAL MCS--4200/7200 Multi--Channel SATCOM System 23--20--35 15 Jul 2006  Honeywell International Inc. Do not copy without express permission of Honeywell. Page A--11/A--12 Table A--5. HS--720 (120--10267--1XX) Pressurized Hardware Kit 4 4 4 4 4 4 4 4 4 4 4 MS51957--29 6--32 X 7/16 IN. PAN HEAD 4 4 4 4 4 4 4 4 4 4 4 NAS1149DN616J WASHER, FLAT 1 1 1 1 1 1 1 1 1 1 1 NSXN2P221S01 HS--720 ARINC CONNECTOR W/PINS ANDSOCKETS (NOTE 1 AND 2) 1 -- -- -- -- -- -- -- -- -- -- 200--10510--101 4 MCU TRAY SHORT, RIGHT SIDE DC FAN -- 1 -- -- -- -- -- -- -- -- -- 200--92609--101 4 MCU TRAY, SHORT, LEFT SIDE DC FAN -- -- 1 -- -- -- -- -- -- -- -- 200--92893--101 4 MCU TRAY, LONG, REAR DC FAN -- -- -- 1 -- -- -- -- -- -- -- 200--84977--101 4 MCU TRAY, SHORT, BOTTOM DC FAN -- -- -- -- 1 1 -- -- -- -- -- 6083--102 4 MCU TRAY, LONG, REAR AC FAN -- -- -- -- -- -- 1 -- -- -- -- 6026--101 4 MCU TRAY, LONG, NO FAN -- -- -- -- -- -- -- 1 -- -- -- 6049--102 4 MCU TRAY, SHORT, RIGHT SIDE AC FAN -- -- -- -- -- -- -- -- 1 -- -- 6049--101 4 MCU TRAY, SHORT, LEFT SIDE AC FAN -- -- -- -- -- -- -- -- -- 1 -- 6050--101 4 MCU TRAY, SHORT, BOTTOM AC FAN -- -- -- -- -- -- -- -- -- -- 1 6034--101 4MCUTRAY,SHORT,NOFAN QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D QTY REQ’D COMPONENTS P A R T N O . N O M E N C L A T U R E --111 -- 11 0 --109 --108 --107 --106 --105 --104 --103 --102 --101 P A R T N O . OR I D E N T I F Y I N G N O M E N C L A T U R E OR D E S C R I P T I O N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSEMBLY P/N ASSE…

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Honeywell International Inc. Honeywell Aerospace 21111 N. 19 th Avenue Phoenix, AZ 85027 March 29, 2010 Federal Communications Commission Authorization & Evaluation Division 7345 Oakland Mills Road Columbia, Maryland 21046 Re: Agent Authorization To Whom It May Concern: This letter will authorize Compliance Testing LLC to act as our Agent in all FCC matters. This appointment is effective until otherwise notified by us. This is to advise that we are in full compliance with the Anti-Drug Abuse Act. The Applicant is not subject to a denial of federal benefits pursuant to Section 5301 of the Anti-Drug Abuse Act of 1988, 21 USC 862, and no party to the application is subject to a denial of federal benefits pursuant to that section. Sincerely, Honeywell International Inc. Charlie Dosdall HW Technical Manager-RF CoE/Radar and Satcom PMI

Honeywell International Inc. Honeywell Aerospace 2111 1 N. 19 th Avenue Phoenix, AZ 85027 March 29, 2010 Federal Communications Commission Authorization & Evaluation Division 7345 Oakland Mills Road Columbia, Maryland 21046 PER: 47 CFR 0.457 AND 0.459 RE: CONFIDENTIALITY REQUEST FOR FCC ID: GB8HS-720 Pursuant to FCC 47 CFR 0.457(d)(1)(ii) and 0.459 of the Commission’s Rules, the Applicant hereby requests confidential treatment of some of the information accompanying this Application as listed below, i.e. 1. Schematics 2. Block Diagrams 3. Parts Lists and Placement/BOM 4. Tune Up Procedure 5. System/Operational/Technical Descriptions These materials contain trade secrets and proprietary information not customarily released to the public and the public disclosure of these matters might be harmful to the Applicant and provide unjustified benefits to its competitors. The Applicant requests the exhibits listed above as permanently confidential to be permanently withheld from public review. The Applicant understands that pursuant to Rule 0.457(d)(1)(ii) disclosure of this Application and all accompanying documentation will not be made before the date of the Grant for this Application. Sincerely, Honeywell International Inc. Charlie Dosdall HW Technical Manager-RF CoE/Radar and Satcom PMI

HP-720 External Photos Front View Label View Rear View

7021570_CF.ZIP=50BFC486 DWG NO. 7021570 SH 1 FOR REVISION RECORD, SEE LAST SHEET FOR HONEYWELL REFERENCE DPA NO. A14738 PRODUCT LINE NO. 5111 AW/PS ANALYSIS EB 7516081 APPLICATION NEXT ASSY USED ON (SYS) 7516100 7516100 7516240 7516240 7516250 7516250 7517800 7517800 7516251 7516251 TYPED NAMES IN THE SIGNATURE BLOCKS AND CRC IN FORMAT MARGIN CONSTITUTE RELEASE. APPROVALS ON FILE. CF CF CF 120 119 118 CF CF CF CF CF CF CF CF CF CF CF CF CFREV SHEET 117 116 115 114 113 112 111 110 109 108 107 106 105SHEET INDEX CACA CDBP CACE CECACF CA CA CA CAREV SHEET 104 103 102 101 10099 98 97 96 95 94 93 92 SHEET INDEX CACA CACA CCBD BCCACACA CA CA CAREV 91 90 89 88 87 86 85 84 83 82 81 80 79 SHEET SHEET INDEX CACA CACA CACA AT AT AT AT CA CA BL REV 78 77 76 75 74 73 72 71 70 69 68 67 66 SHEET SHEET INDEX BCBC CACA CACA CACACACA CA CA CAREV 7021569 OPERATIONAL NOTE SPECIFICATION CONTROL DRAWING 65 64 63 62 61 60 59 58 57 56 55 54 53 SHEET SHEET INDEX REF DWG CONTRACT AF AF CACA CACA CACACACA CA AF AF REV 52 51 50 49 48 47 46 45 44 43 42 41 40 SHEET SHEET INDEX ITEM CODE (PER EB699384) V CACA CACA CACA CACACACA CA CA CAREV DRAWN BY DATE 39 38 37 36 35 34 33 32 31 30 29 28 27 SHEET SHEET INDEX L. WHISLER 94-02-09 CACACACACACACAK CACA CA CA CAREV DESIGNED BY DATE 26 25 24 23 22 21 20 19 18 17 16 15 14 SHEET SHEET INDEX CA— — — — CACACACACA CA N CFREV INTERPRET DIMENSIONS AND TOLERANCES PER ANSI Y14.5M-1982. UNLESS OTHERWISE SPECIFIED, DIMENSIONS ARE IN INCHES; TOLERANCES: CHECKED BY DATE 13 12 11 10 9 8 7 6 5 4 3 2 1 SHEET SHEET INDEX G. BEILER 94-03-02 APPROVED FOR MFG DATE ANGLE ± 2 PL DEC ± 3 PL DEC ± ___ ___ ___ BUSINESS AND COMMUTER AVIATION SYSTEMS THIRD ANGLE PROJECTION APPROVED FOR QE DATE APPROVED FOR ENGRG DATE J. GHER 94-02-25 TITLE PLATE, IDENTIFICATION APPROVED FOR ENGRG DATE DWG CLASS A T. EUROPA 94-03-01 SIZE A CAGE CODE 55939 DRAWING NO. 7021570 REV CF FIRST USED ON APPROVED FOR PM&P DATE 7516100 SCALE NONE UNIT WT SHEET 1 OF 120 A5231-027 (BCAS_SCD97 R1.dot, rev 99/01/06) CREATING FIGURES: THE FIGURES IN THIS DOCUMENT NEED TO BE CREATED USING HELVETICA CONDENSED, EXCEPT FOR HONEYWELL INC. WHICH WILL BE HELVETICA BOLD. PRINTING INSTRUCTIONS: THE FIGURES IN THIS DOCUMENT NEED TO BE PRINTED OUT ON A HP LASERJET (POSTSCRIPT) (600 DPI OR HIGHER). A POSTSCRIPT FILE HAS BEEN GENERATED IN GRAYTECH USING THE POSTSCRIPT B SIZE, SCALE 1, KEY IN COORDINATES (0, 0), DWG NO. 7021570 SH 104 SIZE CAGE CODE DRAWING NO. REV A55939 7021570 CA SEE FIRST SHEET FOR CONTRACT NUMBER. USE OR DISCLOSURE OF INFORMATION ON THIS SHEET IS SUBJECT TO THE RESTRICTIONS ON THE FIRST SHEET OF THIS DOCUMENT. SCALE NONE UNIT WT SHEET 104 A5231-027 (BCAS_SCD97 R1.dot, rev 99/01/06) FIGURE 102 7021570-215

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 tran smittal of this work for any pur pose, 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 Inte rnational Traffic and Arms Regulations (ITAR) 22 CFR 120-130. List of Figures Figure 1: 1252-A-2001 Control Processor Top .......................................................................................................................................... 2 Figure 2: 1252-A-2001 Control Processor Bottom ..................................................................................................................................... 3 Figure 3: 1210-A-0010-02 BGAN Channel Card Top ............................................................................................................................... 4 Figure 4: 1210-A-0010-02 BGAN Channel Card Inside ............................................................................................................................ 5 Figure 5: 1210-A-0010-02 BGAN Channel Card Bottom .......................................................................................................................... 6 Figure 6: 1210-A-0003 RF Modules Bottom ............................................................................................................................................. 7 Figure 7: 1110-F-0017 OXCO Top ............................................................................................................................................................ 8 Figure 8: 1110-F-0017 OXCO Bottom ....................................................................................................................................................... 9 Figure 9: 1252-F-0017 2 splitters and 10MHz OCXO Installed .............................................................................................................. 10 Figure 10: 1252-F-0124 Power Supply ..................................................................................................................................................... 11 Figure 11: 1252-A-2007 RF Combiner/Splitter Top ................................................................................................................................ 12 Figure 12: 1252-A-2007_1252-U-2008 TX Combiner CCA (Part of RF Combiner/Splitter) ................................................................. 13 Figure 13: 1252-A-2007 RF Combiner/Splitter Bottom ........................................................................................................................... 14 Figure 14: Interconnections ...................................................................................................................................................................... 15 Page 1 Figure 1: 1252-A-2001 Control Processor Top 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 tran smittal of this work for any pur pose, 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 Inte rnational Traffic and Arms Regulations (ITAR) 22 CFR 120-130. Page 2 Figure 2: 1252-A-2001 Control Processor Bottom 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 tran smittal of this work for any pur pose, 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 Inte rnational Traffic and Arms Regulations (ITAR) 22 CFR 120-130. Page 3 Figure 3: 1210-A-0010-02 BGAN Channel Card Top 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 tran smittal of this work for any pur pose, 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 Inte rnational Traffic and Arms Regulations (ITAR) 22 CFR 120-130. Page 4 Figure 4: 1210-A-0010-02 BGAN Channel Card Inside 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 tran smittal of this work for any pur pose, 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 Inte rnational Traffic and Arms Regulations (ITAR) 22 CFR 120-130. Page 5 Figure 5: 1210-A-0010-02 BGAN Channel Card Bottom 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 tran smittal of this work for any pur pose, in any form, or by any m …

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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 p09c0012, d1040043 Rev 3.0 Date: April 23, 2010 Applicant: Honeywell International Inc. 21111 N 19th Ave Phoenix, AZ 85027 Attention of: Charlie Dosdall, HW Technical Manager Ph: (602) 436-0684 Fax: (602) 822-7260 E-mail: [email protected] Equipment: HS-720 FCC ID: GB8HS-720 FCC Rules: Part 87 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…

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