KV6-TFS-SDU82155ATopflight SATCOM Satellite data unit

Issue 2 TopFlight Satcom SDU & SCM Installation and Maintenance Manual Ref: TFS062/J-03/003 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. They cannot be reproduced, disclosed or utilized without the company’s prior written approval. 1 Installation and Maintenance Manual TopFlight Satcom SDU – 82155A Series SCM – 82158A Series Issue 2 TopFlight Satcom SDU & SCM Installation and Maintenance Manual Ref: TFS062/J-03/003 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. They cannot be reproduced, disclosed or utilized without the company’s prior written approval. 2 Page intentionally left blank Issue 2 TopFlight Satcom SDU & SCM Installation and Maintenance Manual Ref: TFS062/J-03/003 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. They cannot be reproduced, disclosed or utilized without the company’s prior written approval. 3 RECORD OF REVISIONS REV. NO. REVISION DATE DATE INSERTED BY REV. NO. REVISION DATE DATE INSTERTED BY 2 October 2007 Issue 2 TopFlight Satcom SDU & SCM Installation and Maintenance Manual Ref: TFS062/J-03/003 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. They cannot be reproduced, disclosed or utilized without the company’s prior written approval. 4 CONTENTS 1. INTRODUCTION....................................................................................6 1.1. Purpose of Manual............................................................................6 1.2. Scope.................................................................................................7 1.3. References ........................................................................................7 1.4. Compliance to Regulations .............................................................7 1.5. List of Abbreviations ........................................................................8 2. DESCRIPTION.....................................................................................10 2.1. TFS Satellite Communication System Domain ...........................10 2.2. TFS System Overview ....................................................................10 2.3. SDU General Description ...............................................................11 2.4. Interfaces.........................................................................................20 2.5. Configuration Straps ......................................................................21 2.6. SDU Interconnections....................................................................22 2.7. SCM General Description...............................................................30 3. INSTALLATION GUIDELINES..........................................................36 3.1. Introduction.....................................................................................36 3.2. Interchangeability ...........................................................................36 3.3. SDU / SCM Location and Accessibility Guidelines......................36 3.4. Mounting Tray .................................................................................37 3.5. Cooling ............................................................................................37 3.6. Power Requirements ......................................................................37 3.7. SDU RF Connections......................................................................38 3.8. Bonding Requirements ..................................................................39 Issue 2 TopFlight Satcom SDU & SCM Installation and Maintenance Manual Ref: TFS062/J-03/003 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. They cannot be reproduced, disclosed or utilized without the company’s prior written approval. 5 3.9. SDU Fitting Instructions.................................................................39 3.10. SDU Removal Instructions .........................................................40 3.11. SCM Fitting Instructions.............................................................40 3.12. SCM Removal Instructions.........................................................41 4. INSPECTION AND SYSTEM CHECKOUT......................................42 4.1. Inspection/Check procedure .........................................................42 4.2. System Checkout............................................................................42 5. MAINTENANCE...................................................................................44 5.1. Introduction.....................................................................................44 5.2. Cleaning of Mechanical Parts ........................................................44 5.3. Periodic Checks..............................................................................44 5.4. Cabling and Connections ..............................................................44 6. TESTING AND FAULT ISOLATION.................................................45 6.1. BITE Function .................................................................................45 6.2. Test Functions ................................................................................46 6.3. Fault Isolation .................................................................................48 7. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS......................54 Issue 2 TopFlight Satcom SDU & SCM Installation and Maintenance Manual Ref: TFS062/J-03/003 © THALES AVIONICS Ltd. This document and any information included are the property of Thales Avionics. They cannot be reproduced, disclosed or utilized without the company’s prior written approval. 6 1. INTRODUCTION 1.1. Purpose of Manual This manual sets forth installation and maintenance guidelines for the THALES TopFlight Satcom (TFS) Satellite Data Unit (S…

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Exhibit 2 - Attestation Statement.doc TFS062/SAT-001/STE- 012/002 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics Limited Page 1 of 2 COMMERCIAL IN CONFIDENCE THALES ‘TOP FLIGHT’ SATELLITE DATA UNIT (SDU) EXHIBIT 2 – ATTESTATION STATEMENT Any enquiries concerning this document should be addressed to: Satcom Product Group Manager Thales Avionics Limited 88 Bushey Road London SW20 0JW The copyright of this document is vested in Thales Avionics Limited, and the recipient should use it only for the purpose for which it was issued. The recipient shall not use the document in any manner that is competitive with or detrimental to the commercial interests of Thales Avionics Limited. Nor shall the recipient publish this document or make it available to any third party or in any other way divulge the contents or any technical expertise evident therein without Thales Avionics Limited prior written approval. © Thales Avionics Limited 2007 Exhibit 2 - Attestation Statement.doc TFS062/SAT-001/STE- 012/002 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics Limited Page 2 of 2 COMMERCIAL IN CONFIDENCE Extract from Exhibit 6a To whom It May Concern The Thales Avionics Ltd Satellite Data Unit Type Number 82155A ( FCC ID: KV6-TFS- SDU82155A) has been tested in accordance with the requirements contained in the appropriate Commission regulations. To the best of my knowledge these tests were performed using measurement procedures consistent with industry or Commission standards and demonstrate that the Satellite Data Unit Type Number 82155A complies with the appropriate standards. Each unit manufactured, imported or marketed, as defined in the Commission’s regulations, will conform to the samples within the variations that can be expected due to quantity production and testing on a statistical basis. I hereby certify that the tests described in this report were performed at my direction and under my supervision, and that the results and test data contained in this report truly and accurately show the performance of the Satellite Data Unit Type Number 82155A. I further certify that the ancillary information contained herein accurately reflects the design, installation requirements, alignment procedures and operational instructions of and for this equipment. ..................................................... Colin Appleyard Technical Consultant

Stan Lyles, FCC Equipment Authorization Branch, Applicant: Thales Avionics Limited FCC ID: KV6-TFS-SDU82155A Form 731 Confirmation Number: EA485291 Correspondence Reference Number: 34549 25 February 2008, Re: your original e-mail 19 December 2007 Stan, Thanks for you e-mail please see the replies below. 1) Form 731 has 4.0 watts, test report has 3.14 watts. Also page 10 of test report shows 27.78 (dMm) = 3.748 watts, should be 0.599 watts. Please explain this discrepancy. The report had a typo on page 10, and it should have read 35.78 dBm= 3.748 W. A new version of the report, produced by TUV, is attached named Exhibit 6b RO615497-01 Issue 4. The figure of 4.0 W in form 731 was an approximate figure. 2) Does this device have 16 QAM modulation? If yes, submit a waiver request to the FCC Wireless Telecommunications Bureau (WTB). No QAM, only QPSK – see page 7 of same report. 3) The waiver submitted in the letter exhibit must be submitted to the FCC Wireless Telecommunications Bureau (WTB). Upload the waiver once it is approved by the FCC Wireless Telecommunications Bureau (WTB). As you are aware we have had problems with this process, but we have now submitted the waiver and paid for this service and are expecting a response soon. Yours sincerely, Jennifer Livingstone.

Exhibit 3 – External PhotosTFS062/SAT-001/STE-012/003 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 1 of 7 COMMERCIAL IN CONFIDENCE THALES ‘TOP FLIGHT’ SATELLITE DATA UNIT (SDU) EXHIBIT 3 - EXTERNAL PHOTOS Any enquiries concerning this document should be addressed to: Satcom Product Group Manager Thales Avionics Limited 88 Bushey Road London SW20 0JW The copyright of this document is vested in Thales Avionics Limited, and the recipient should use it only for the purpose for which it was issued. The recipient shall not use the document in any manner that is competitive with or detrimental to the commercial interests of Thales Avionics Limited. Nor shall the recipient publish this document or make it available to any third party or in any other way divulge the contents or any technical expertise evident therein without Thales Avionics Limited prior written approval. © Thales Avionics Limited 2007 Exhibit 3 – External PhotosTFS062/SAT-001/STE-012/003 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 2 of 7 COMMERCIAL IN CONFIDENCE Figure 1: SDU Top Exhibit 3 – External PhotosTFS062/SAT-001/STE-012/003 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 3 of 7 COMMERCIAL IN CONFIDENCE Figure 2: SDU Bottom Exhibit 3 – External PhotosTFS062/SAT-001/STE-012/003 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 4 of 7 COMMERCIAL IN CONFIDENCE Figure 3: SDU Front Exhibit 3 – External PhotosTFS062/SAT-001/STE-012/003 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 5 of 7 COMMERCIAL IN CONFIDENCE Figure 4: SDU Left Exhibit 3 – External PhotosTFS062/SAT-001/STE-012/003 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 6 of 7 COMMERCIAL IN CONFIDENCE Figure 5: SDU Rear Exhibit 3 – External PhotosTFS062/SAT-001/STE-012/003 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 7 of 7 COMMERCIAL IN CONFIDENCE Figure 6: SDU Right Figure 7: SDU with Antenna Radome

Exhibit 1 - Label TFS062//SAT-001/STE-012/001 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics Limited Page 1 of 10 COMMERCIAL IN CONFIDENCE THALES ‘TOP FLIGHT’ SATELLITE DATA UNIT (SDU) EXHIBIT 1 - LABEL Any enquiries concerning this document should be addressed to: Satcom Product Group Manager Thales Avionics Limited 88 Bushey Road London SW20 0JW The copyright of this document is vested in Thales Avionics Limited, and the recipient should use it only for the purpose for which it was issued. The recipient shall not use the document in any manner that is competitive with or detrimental to the commercial interests of Thales Avionics Limited. Nor shall the recipient publish this document or make it available to any third party or in any other way divulge the contents or any technical expertise evident therein without Thales Avionics Limited prior written approval. © Thales Avionics Limited 2007 Exhibit 1 - Label TFS062//SAT-001/STE-012/001 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics Limited Page 2 of 10 COMMERCIAL IN CONFIDENCE Figure 1: Placement of Part Label on SDU Front Panel Figure 1 shows the placement of the part label on the SDU. The artwork shown in Figures 2 and 3 details the main and secondary labels for the current production version. The FCC ID is not an Airbus requirement and so not shown on Figure 3. However, there is an engineering change reference, EC07/58, to get the FCC ID KV6-TFS-SDU82155A added to the secondary label. See Appendix for details of engineering changes. Note that the following statement is included in the User Manual but cannot be found on the label: “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.” Exhibit 1 - Label TFS062//SAT-001/STE-012/001 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics Limited Page 3 of 10 COMMERCIAL IN CONFIDENCE Figure 2: SDU Front Panel Main Label Figure 3: SDU Front Panel Secondary Label Exhibit 1 - Label TFS062//SAT-001/STE-012/001 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics Limited Page 4 of 10 COMMERCIAL IN CONFIDENCE A PPENDIX : ENGINEERING CHANGE EC07/58 Figure 4: Labels Undergoing Engineering Changes Exhibit 1 - Label TFS062//SAT-001/STE-012/001 Thales Avionics Limited Page 5 of 10 COMMERCIAL IN CONFIDENCE Figure 5: Marked-Up Engineering Changes for SCM Label Exhibit 1 - Label TFS062//SAT-001/STE-012/001 Thales Avionics Limited Page 6 of 10 COMMERCIAL IN CONFIDENCE Figure 6: Marked-Up Engineering Changes for IGA Label Exhibit 1 - Label TFS062//SAT-001/STE-012/001 Thales Avionics Limited Page 7 of 10 COMMERCIAL IN CONFIDENCE Figure 7: Marked-Up Engineering Changes for DLNA Label Exhibit 1 - Label TFS062//SAT-001/STE-012/001 Thales Avionics Limited Page 8 of 10 COMMERCIAL IN CONFIDENCE Figure 8: Marked-Up Engineering Changes for Antenna Interface Mount Label Exhibit 1 - Label TFS062//SAT-001/STE-012/001 Thales Avionics Limited Page 9 of 10 COMMERCIAL IN CONFIDENCE Figure 9: Marked-Up Engineering Changes for SDU Front Panel (Primary) Label Exhibit 1 - Label TFS062//SAT-001/STE-012/001 Thales Avionics Limited Page 10 of 10 COMMERCIAL IN CONFIDENCE Figure 10: Marked-Up Engineering Changes for SDU Front Panel (Secondary) Label

Exhibit 9a – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 1 COMMERCIAL IN CONFIDENCE THALES ‘TOP FLIGHT’ SATELLITE DATA UNIT (SDU) EXHIBIT 9A - INTERNAL PHOTOS Any enquiries concerning this document should be addressed to: Satcom Product Group Manager Thales Avionics Limited 88 Bushey Road London SW20 0JW The copyright of this document is vested in Thales Avionics Limited, and the recipient should use it only for the purpose for which it was issued. The recipient shall not use the document in any manner that is competitive with or detrimental to the commercial interests of Thales Avionics Limited. Nor shall the recipient publish this document or make it available to any third party or in any other way divulge the contents or any technical expertise evident therein without Thales Avionics Limited prior written approval. © Thales Avionics Limited 2007 Exhibit 9a – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 2 COMMERCIAL IN CONFIDENCE Figure Index for Exhibit 9 – Internal Photos DocumentFigure Exhibit 9a – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Top Exhibit 9a – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Top. Showing Middle Section of Board with Heatsink Removed. Exhibit 9a – Internal PhotosFigure 3. SDU Avionics Processor Module (APM) Top. Showing Right Side of Board with Heatsink Removed. Exhibit 9b – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Bottom Exhibit 9b – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Bottom. Enlarged view of Left Side of Board. Exhibit 9b – Internal PhotosFigure 3: SDU Channel Card Module (CCM) Top Exhibit 9c – Internal PhotosFigure 1: SDU Channel Card Module (CCM) Bottom Exhibit 9c – Internal PhotosFigure 2: SDU Communication Processor Module (CPM) Top Exhibit 9c – Internal PhotosFigure 3: SDU Communication Processor Module (CPM) Bottom Exhibit 9d – Internal PhotosFigure 1: SDU Backplane Top Exhibit 9d – Internal PhotosFigure 2: SDU Backplane Bottom Exhibit 9d – Internal PhotosFigure 3: SDU Power Supply Module (PSM) Top Exhibit 9d – Internal PhotosFigure 4: SDU Power Supply Module (PSM) Bottom Exhibit 9d – Internal PhotosFigure 5: SDU Front Panel Board Assembly Top Exhibit 9d – Internal PhotosFigure 6: SDU Front Panel Board Assembly Bottom Exhibit 9d – Internal PhotosFigure 7: SDU Chassis With PCBs In Place Exhibit 9a – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 3 COMMERCIAL IN CONFIDENCE Figure 1: SDU Avionics Processor Module (APM) Top Figure 2: SDU Avionics Processor Module (APM) Top. Showing Middle Section of Board with Heatsink Removed. Exhibit 9a – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 4 COMMERCIAL IN CONFIDENCE Figure 3. SDU Avionics Processor Module (APM) Top. Showing Right Side of Board with Heatsink Removed.

Exhibit 9b – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 1 COMMERCIAL IN CONFIDENCE THALES ‘TOP FLIGHT’ SATELLITE DATA UNIT (SDU) EXHIBIT 9B - INTERNAL PHOTOS Any enquiries concerning this document should be addressed to: Satcom Product Group Manager Thales Avionics Limited 88 Bushey Road London SW20 0JW The copyright of this document is vested in Thales Avionics Limited, and the recipient should use it only for the purpose for which it was issued. The recipient shall not use the document in any manner that is competitive with or detrimental to the commercial interests of Thales Avionics Limited. Nor shall the recipient publish this document or make it available to any third party or in any other way divulge the contents or any technical expertise evident therein without Thales Avionics Limited prior written approval. © Thales Avionics Limited 2007 Exhibit 9b – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 2 COMMERCIAL IN CONFIDENCE Figure Index for Exhibit 9 – Internal Photos DocumentFigure Exhibit 9a – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Top Exhibit 9a – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Top. Showing Middle Section of Board with Heatsink Removed. Exhibit 9a – Internal PhotosFigure 3. SDU Avionics Processor Module (APM) Top. Showing Right Side of Board with Heatsink Removed. Exhibit 9b – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Bottom Exhibit 9b – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Bottom. Enlarged view of Left Side of Board. Exhibit 9b – Internal PhotosFigure 3: SDU Channel Card Module (CCM) Top Exhibit 9c – Internal PhotosFi gure 1: SDU Channel Card Module (CCM) Bottom Exhibit 9c – Internal PhotosFigure 2: SDU Communication Processor Module (CPM) Top Exhibit 9c – Internal PhotosFigure 3: SDU Communication Processor Module (CPM) Bottom Exhibit 9d – Internal PhotosFigure 1: SDU Backplane Top Exhibit 9d – Internal PhotosFigure 2: SDU Backplane Bottom Exhibit 9d – Internal PhotosFigure 3: SDU Power Supply Module (PSM) Top Exhibit 9d – Internal PhotosFigure 4: SDU Power Supply Module (PSM) Bottom Exhibit 9d – Internal PhotosFigure 5: SDU Front Panel Board Assembly Top Exhibit 9d – Internal PhotosFigure 6: SDU Front Panel Board Assembly Bottom Exhibit 9d – Internal PhotosFigure 7: SDU Chassis With PCBs In Place Exhibit 9b – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 3 COMMERCIAL IN CONFIDENCE Figure 1: SDU Avionics Processor Module (APM) Bottom Exhibit 9b – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 4 COMMERCIAL IN CONFIDENCE Figure 2: SDU Avionics Processor Module (APM) Bottom. Enlarged view of Left Side of Board. Exhibit 9b – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 5 COMMERCIAL IN CONFIDENCE Figure 3: SDU Channel Card Module (CCM) Top

Exhibit 9c – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 1 COMMERCIAL IN CONFIDENCE THALES ‘TOP FLIGHT’ SATELLITE DATA UNIT (SDU) EXHIBIT 9C - INTERNAL PHOTOS Any enquiries concerning this document should be addressed to: Satcom Product Group Manager Thales Avionics Limited 88 Bushey Road London SW20 0JW The copyright of this document is vested in Thales Avionics Limited, and the recipient should use it only for the purpose for which it was issued. The recipient shall not use the document in any manner that is competitive with or detrimental to the commercial interests of Thales Avionics Limited. Nor shall the recipient publish this document or make it available to any third party or in any other way divulge the contents or any technical expertise evident therein without Thales Avionics Limited prior written approval. © Thales Avionics Limited 2007 Exhibit 9c – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 2 COMMERCIAL IN CONFIDENCE Figure Index for Exhibit 9 – Internal Photos DocumentFigure Exhibit 9a – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Top Exhibit 9a – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Top. Showing Middle Section of Board with Heatsink Removed. Exhibit 9a – Internal PhotosFigure 3. SDU Avionics Processor Module (APM) Top. Showing Right Side of Board with Heatsink Removed. Exhibit 9b – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Bottom Exhibit 9b – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Bottom. Enlarged view of Left Side of Board. Exhibit 9b – Internal PhotosFigure 3: SDU Channel Card Module (CCM) Top Exhibit 9c – Internal PhotosFi gure 1: SDU Channel Card Module (CCM) Bottom Exhibit 9c – Internal PhotosFigure 2: SDU Communication Processor Module (CPM) Top Exhibit 9c – Internal PhotosFigure 3: SDU Communication Processor Module (CPM) Bottom Exhibit 9d – Internal PhotosFigure 1: SDU Backplane Top Exhibit 9d – Internal PhotosFigure 2: SDU Backplane Bottom Exhibit 9d – Internal PhotosFigure 3: SDU Power Supply Module (PSM) Top Exhibit 9d – Internal PhotosFigure 4: SDU Power Supply Module (PSM) Bottom Exhibit 9d – Internal PhotosFigure 5: SDU Front Panel Board Assembly Top Exhibit 9d – Internal PhotosFigure 6: SDU Front Panel Board Assembly Bottom Exhibit 9d – Internal PhotosFigure 7: SDU Chassis With PCBs In Place Exhibit 9c – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 3 COMMERCIAL IN CONFIDENCE Figure 1: SDU Channel Card Module (CCM) Bottom Figure 2: SDU Communication Processor Module (CPM) Top Exhibit 9c – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 4 COMMERCIAL IN CONFIDENCE Figure 3: SDU Communication Processor Module (CPM) Bottom

Exhibit 9d – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 1 COMMERCIAL IN CONFIDENCE THALES ‘TOP FLIGHT’ SATELLITE DATA UNIT (SDU) EXHIBIT 9D - INTERNAL PHOTOS Any enquiries concerning this document should be addressed to: Satcom Product Group Manager Thales Avionics Limited 88 Bushey Road London SW20 0JW The copyright of this document is vested in Thales Avionics Limited, and the recipient should use it only for the purpose for which it was issued. The recipient shall not use the document in any manner that is competitive with or detrimental to the commercial interests of Thales Avionics Limited. Nor shall the recipient publish this document or make it available to any third party or in any other way divulge the contents or any technical expertise evident therein without Thales Avionics Limited prior written approval. © Thales Avionics Limited 2007 Exhibit 9d – Internal PhotosTFS062/SAT-001/STE-012/009 __________________________________________________________________________________ ___________________________________________________________________________________ Thales Avionics LimitedPage 2 COMMERCIAL IN CONFIDENCE Figure Index for Exhibit 9 – Internal Photos DocumentFigure Exhibit 9a – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Top Exhibit 9a – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Top. Showing Middle Section of Board with Heatsink Removed. Exhibit 9a – Internal PhotosFigure 3. SDU Avionics Processor Module (APM) Top. Showing Right Side of Board with Heatsink Removed. Exhibit 9b – Internal PhotosFigure 1: SDU Avionics Processor Module (APM) Bottom Exhibit 9b – Internal PhotosFigure 2: SDU Avionics Processor Module (APM) Bottom. Enlarged view of Left Side of Board. Exhibit 9b – Internal PhotosFigure 3: SDU Channel Card Module (CCM) Top Exhibit 9c – Internal PhotosFi gure 1: SDU Channel Card Module (CCM) Bottom Exhibit 9c – Internal PhotosFigure 2: SDU Communication Processor Module (CPM) Top Exhibit 9c – Internal PhotosFigure 3: SDU Communication Processor Module (CPM) Bottom Exhibit 9d – Internal PhotosFigure 1: SDU Backplane Top Exhibit 9d – Internal PhotosFigure 2: SDU Backplane Bottom Exhibit 9d – Internal PhotosFigure 3: SDU Power Supply Module (PSM) Top Exhibit 9d – Internal PhotosFigure 4: SDU Power Supply Module (PSM) Bottom Exhibit 9d – Internal Photos…

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