Acceptance Test Procedure

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ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Aviation Communication and Surveillance Systems CAGE Code Initial Release Date Revision Date Document Number Revision 1WYD3 01-JUNE-05 01-FEB-06 8002217-001 D Proprietary Notice This document and the information disclosed herein are proprietary data of Aviation Communication & Surveillance Systems, LLC. Neither this document nor the information contained herein shall be reproduced, used, or disclosed to others without the written authorization of Aviation Communication & Surveillance Systems, LLC. Notice Freedom of Information Act (5 USC 552) and Disclosure of Confidential Information Generally (18 USC 1905) This document is being furnished in confidence by Aviation Communication & Surveillance Systems, LLC. The information disclosed herein falls within exemption (b) (4) of 5 USC 552 and the prohibitions of 18 USC 1905. Copyright 2005 Aviation Communication & Surveillance Systems, LLC. All Rights Reserved.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D Record of Revisions Rev Date Authorization Description of Change - 6/01/05 ECR008688 Initial Release. A 9/15/05 ECR008943 Added Tests B 10/14/05 ECR009052 Added Tests C 12/15/05 ECR009153 Added Tests D 2/01/06 ECR009305 New RF FPGA ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 2 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D Table of Contents 1 INTRODUCTION ............................................................................................................................ 4 1.1 Purpose ................................................................................................................................... 4 1.2 Scope ...................................................................................................................................... 4 1.3 References .............................................................................................................................. 4 1.4 Definitions ............................................................................................................................... 4 1.4.1 Acronyms and Abbreviations ............................................................................................ 4 2 SYSTEM OVERVIEW .................................................................................................................... 5 3 GENERAL INFORMATION............................................................................................................. 5 3.1 General Requirements............................................................................................................. 5 3.2 General RF Test Requirements ............................................................................................... 5 3.3 Power Requirements ............................................................................................................... 5 4 TEST EQUIPMENT REQUIREMENTS........................................................................................... 6 4.1 Test Equipment Hardware ....................................................................................................... 6 4.2 Test Equipment Software......................................................................................................... 6 4.3 Test Equipment / UUT Interconnect ......................................................................................... 6 5 MTS END ITEM TEST.................................................................................................................... 8 5.1 ATP / MTS Test Software Synchronization .............................................................................. 8 5.2 UUT Alignment / Calibration .................................................................................................... 8 5.3 Loading of Embedded Test Software ....................................................................................... 8 5.3.1 Emulator Loading.............................................................................................................. 8 5.4 MTS End Item Test Initialization .............................................................................................. 8 5.4.1 Test Setup ........................................................................................................................ 8 5.4.2 Compact Flash Loading Of HTS ....................................................................................... 9 5.5 MTS End Item Test Execution ................................................................................................. 9 6 BITE LOG FAULT CLEARING...................................................................................................... 10 7 SIMPAN END ITEM TEST............................................................................................................ 11 APPENDIX A....................................................................................................................................... 12 SOFTWARE / FIRMWARE CONFIGURATION ................................................................................... 12 1 INTRODUCTION .......................................................................................................................... 13 1.1 Purpose ................................................................................................................................. 13 2 SOFTWARE / FIRMWARE CONFIGURATION AND VERIFICATION .......................................... 13 2.1 Initial Test Configuration Software Loading............................................................................ 13 2.2 Final Configuration Software Loading And Verification........................................................... 14 2.3 Synchronization Between ATP / Test Software ...................................................................... 15 APPENDIX B....................................................................................................................................... 17 TEST REPORT / TRD CROSS REFERENCE ..................................................................................... 17 ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 3 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D 1 INTRODUCTION This document is the Acceptance Test Procedure for the TCAS 3000 Computer Unit. 1.1 Purpose  To provide instruction on the loading of embedded Hardware Test Software (HTS).  To provide instruction on the execution of a TCAS 3000 Final Acceptance Test utilizing automated test equipment with embedded test software (HTS).  To provide instruction on the loading of Operational Flight Software and testing after Operational Flight Software has been loaded.  To provide instruction on the downloading and clearing of the Maintenance (BITE) Fault Log. 1.2 Scope This Acceptance Test Procedure specification (ATP) establishes the manufacturing and operational requirements that the TCAS 3000 Computer Unit, Part Numbers 9003000-55001, 9003000-65001, and 9003000-10001 must meet to ensure that the unit is in proper operating condition. 1.3 References Document No. Description Revision 8002216-001 TCAS 3000 Test Requirements Document C (or subsequent) EB7517947 Using JCAIR TCAS Simulation Panel F (or subsequent) 8005745-001 W ebEDDIT Tool User Guide - (or subsequent) 1.4 Definitions 1.4.1 Acronyms and Abbreviations Acronym Definition ACSS Aviation Communication and Surveillance Systems AIU Aircraft Interface Unit CCP Common Computing Platform FPGA Field Programmable Gate Array HTS Hardware Test Software LRU Line Replaceable Unit MTS Manufacturing Test Station RFIU RF Interface Unit SDRAM Synchronous Dynamic Random Access Memory TCAS Traffic Collision Avoidance System TRD Test Requirements Document UUT Unit Under Test ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 4 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D 2 SYSTEM OVERVIEW The TCAS 3000 Acceptance Test is a fully automated end item test that is performed using the ACSS TCAS MTS (Part No. T336255). At the MTS level of testing, there are two primary types of software utilized. The first type of software is the HTS program which is loaded into the FLASH memory of the UUT and then executes within the UUT’s SDRAM. The second type of software is the MTS program that executes on the MTS PC. The HTS program receives high level commands from the MTS program via an RS232 interface. It executes commands and returns a response. The responses returned from HTS may range from acknowledgement of receipt of a command to returning data and/or status of a test that was performed by the embedded software. The MTS program is comprised of a Test Executive, Instrument Drivers, and Test Functions. The Test Executive, which provides an operator interface, directs test sequencing, determines pass/fail status and enables test report generation. The Instrument Drivers communicate with and control the MTS test equipment via an IEEE488 interface and PCI bus for the PC based instruments. The Test Functions perform the individual tests that comprise a TCAS 3000 Acceptance Test and are described in the TCAS 3000 Test Requirements Document (TRD). 3 GENERAL INFORMATION 3.1 General Requirements The following conditions are recommended for performance of a TCAS 3000 Acceptance Test:  Temperature = 25 ± 5 ºC  Relative humidity = 95% maximum  Pressure = between 20 and 32 in Hg  Power to the UUT should be removed before attaching or removing any interconnecting systems. 3.2 General RF Test Requirements  All antenna ports must be terminated in 50 ohms while power is applied to the UUT.  Any additional test equipment that may be connected to the antenna ports must have a voltage standing wave ratio (VSWR) of less than 1.5:1.  Any additional test equipment that may be connected to the antenna ports shall withstand peak power levels of at least 1000 W and average power levels of at least 2 W. 3.3 Power Requirements  115 Vac, 60 Hz, 20 A standard service power for test equipment operation. All power supplied to the UUT is provided by the test equipment via software controlled rack mounted power supplies. ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 5 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D 4 TEST EQUIPMENT REQUIREMENTS 4.1 Test Equipment Hardware The test equipment hardware that is required to perform a TCAS 3000 End Item Acceptance Test is as follows:  TCAS MTS, Part No. T336255 (Mod D or subsequent) T336255 contains the following assemblies which may be referenced in this document:  Aircraft interface unit (AIU) : Part No. T336253  RF interface unit (RIU) : Part No. T336254  PDL panel : Part No. T336259  Tray assembly : Part No. T336255-26 4.2 Test Equipment Software  TCAS 3000 PC Test Software - P/N 9000469-001. This program executes on the MTS test PC and automates the tests that are defined in the TCAS 3000 TRD.  Hardware Test Software (HTS) - This program executes within UUT memory and responds to commands sent by the TCAS 3000 PC Test Software. Refer to the “Initial Test Configuration Software Loading” section in Appendix A of this document for the Master Media Part Number. 4.3 Test Equipment / UUT Interconnect Figure 1 shows a general interconnect between the MTS test equipment and the UUT for performing an Acceptance test. Not shown in this figure are the Data Acquisition Unit DMM and switching matrices. Refer to drawing no. T336255 for detailed interconnections between the test equipment. Note: This setup shows power connections to a UUT that can accept both AC and DC input power. For a DC only UUT, only DC is provided. ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 6 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D Figure 1. General MTS / UUT Setup ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 7 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D 5 MTS END ITEM TEST At the MTS test phase, the TCAS 3000 Computer Unit shall be tested using product test software (HTS) that is specified in Appendix A of this document. 5.1 ATP / MTS Test Software Synchronization Note: If this is the first time that the current revision of this document is used at the MTS, the test software must be synchronized with this revision of ATP. Step 1. Refer to the “Synchronization Between ATP / Test Software” section in Appendix A of this document if needed. 5.2 UUT Alignment / Calibration Note: This does not apply to units that have been tested previously (unless new alignment or calibration is desired). Step 1. For units in initial manufacturing build and test only, perform the “TCAS 3000 Manual Alignment Procedure” described in Appendix B of the TCAS 3000 TRD (8002216-001). Step 2. Refer to the “Initial Test Configuration Software Loading” section in Appendix A of this document prior to performing an Auto Calibration on the MTS. Step 3. For units in initial manufacturing build and test only, perform the “TCAS 3000 Automatic Calibration Procedure” described in Appendix C of the TCAS 3000 TRD (8002216-001). 5.3 Loading of Embedded Test Software Note: This does not apply to units that have already been loaded with the correct test software prior to performing an Auto Calibration on the MTS. Loading of all images except for HTS must be performed using an emulator. Loading of HTS may be performed using an emulator or compact flash after all other images are present. 5.3.1 Emulator Loading Step 1. Refer to the “Initial Test Configuration Software Loading” section in Appendix A of this document if needed. 5.4 MTS End Item Test Initialization 5.4.1 Test Setup Step 1. Verify that the MTS test equipment is connected per Dwg No. T336255 and that it is calibrated. Step 2. Power up the ACSS TCAS MTS and allow it to warm up for at least 30 minutes. Verify that all IEEE488 test equipment has the correct addresses per Dwg No. T336255 and that all of the test equipment is functioning properly. Step 3. Insert the UUT into MTS UUT mount. Step 4. Connect the MTS W1 PDL cable (P/N T336259) to the UUT PDL front panel connector. ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 8 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D Step 5. Launch the Test Software by double clicking on the Desk-Top Icon labeled “9000469” Step 6. Log in with employee number and password. Step 7. Go to File, Select, Open. Step 8. Select one of the following sequence files: Sequence Description 9000469_Pre.squ Sequence that utilizes Pre Test Limits 9000469_Mfg.squ Sequence that utilizes Manufacturing Limits 9000469_Opr.squ Sequence that utilizes Operational Limits 5.4.2 Compact Flash Loading Of HTS Step 1. If HTS has already been loaded into the UUT, then proceed to the “MTS End Item Test Execution” section. Step 2. Refer to the “Initial Test Configuration Software Loading” section in Appendix A of this document to obtain the latest version of the HTS software on compact flash. Insert the HTS compact flash card into the UUT’s compact flash receiver. Step 3. Apply power to the UUT by clicking on the “DC Pwr” LED on the operator interface so that it illuminates. Step 4. The HTS program will automatically be loaded. This process should take approximately 1-3 minutes. The “XFER IN PROCESS” LED on the UUT front panel should begin flashing as data is being read from the compact flash card. Step 5. Wait until the “C/F LOAD STATUS” LED becomes illuminated a static (non-flashing) green. This is an indication that HTS has been successfully programmed into UUT flash. Step 6. Remove the HTS compact flash card from the UUT. Step 7. Remove power from the UUT by again clicking on the “DC Pwr” LED on the operator interface so that it is no longer illuminated. 5.5 MTS End Item Test Execution Note: If Operational Flight Software is to be loaded at the end of testing, refer to the “Final Configuration Software Loading And Verification” section of Appendix A of this document to obtain the correct Master Media copy. Step 1. From the test program’s operator interface, Click on one of the following: [Single Pass] : (Automatically power down after executing sequence) [Test UUT] : (Prompt operator for power down after executing sequence) Step 2. Enter all UUT information when prompted. Step 3. Select the UUT Part number from Menu selection. Step 4. Select one of the following Test Type: Pre Test or Final Test Step 5. Enter Employee number. Step 6. Upon Clicking on OK, automatic testing will commence. Step 7. Respond to all prompts and instructions that the test program may display during test execution. Step 8. At the completion of all tests, the operator will be asked if the UUT should be loaded with Operational Flight Software. If the Response is “YES”, the operator will be ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 9 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D prompted to insert the correct compact flash card and loading will commence. At the completion of loading, the Software part numbers and CRCs will automatically be verified with the information that appears in Appendix A of this document. Step 9. A test report text file will be generated at the end of test. The test report may be viewed and/or printed out at the end of the test sequence. Step 10. Verify that all tests have passed. Step 11. Remove the UUT from the MTS UUT mount after the UUT has been powered down. Note: For test methodology and pass/fail criteria, refer to Appendix B of this document for the cross reference between the Final Test Report and TRD (Doc. No. 8002216-001). 6 BITE LOG FAULT CLEARING This procedure describes the general steps required to dump and clear the UUT’s BITE Fault log from any accumulated errors. Note: The actual screen names and buttons that appear in the WebEDDIT application may not exactly match the text in the following procedure due to later revisions of the application. Therefore, this procedure is to be utilized as a guide in conjunction with the latest revision of the WebEDDIT Tool User Guide (8005745-001). Step 1. At this stage, the UUT should contain Operational Flight Software. If it does not contain Operational Flight Software, load all of the correct images before proceeding. Step 2. Attach the UUT to the SIMPAN (TCAS Simulation Panel) station holding fixture and connect the SIMPAN PDL cable to the UUT PDL connector for RS232 communications. Step 3. Refer to EB7517947 and setup the SIMPAN as described in the TCAS Simulation Front Panel Initial Setup section. Step 4. On the SIMPAN panel, set the ‘Gear’ switch to ‘down’ and the three ‘Air’ switches to ‘Gnd’. Step 5. Switch the MODE S control panel to ‘STBY’. Step 6. The required TCAS 3000 input power is +28 (±1 VDC), 10A. Perform the power up sequence per the Test Setup section in EB7517947. Step 7. From the PC Desk Top, launch the WebEDDIT application by double clicking on the WebEDDIT.exe icon. Step 8. When prompted to connect to CCP, select ‘YES’. The ‘active’ LED at the bottom of the screen will become illuminated when an RS232 connection has been established. Step 9. From the WebEDDIT GUI menu bar, select TargetCCP Maintenance Interface. This will bring up the ‘Common Computing Platform Maintenance Interface Function’ screen. Step 10. From the ‘Common Computing Platform Maintenance Interface Function’ screen, select ‘Fault Logs and Event Logs’. This will bring up the ‘CCP Logs’ screen. Step 11. From the ‘CCP Logs’ screen, select ‘Dump BITE FAULT LOG’ to dump all stored faults. Follow instructions when prompted and refer to the WebEDDIT Tool User Guide (8005745-001) for option details. Step 12. Open the ‘ccp_mifa_dump_fault_log_xxx.htm’ file (where xxx is variable that changes for each dump). Make note of any faults that may have been logged. ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 10 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D Step 13. After dumping the BITE Fault Log, return to the ‘CCP Logs’ screen and then select ‘Clear BITE FAULT LOG’. The UUT will be reset and RS232 communications will be disconnected when this occurs. Step 14. Allow the tool to automatically re-establish an RS232 connection or refer to WebEDDIT Tool User Guide if the tool is unable to re-connect. Step 15. When RS232 communication has been re-established, return to the ‘CCP Logs’ screen. Step 16. Select ‘Dump BITE FAULT LOG’ and verify that any stored faults that should have been cleared are no longer present. Note: Several faults may be logged due to known missing stimuli. Make note of any faults that should not be present. Step 17. Exit the WebEDDIT application and power off the UUT. Disconnect the PDL cable from the UUT 7 SIMPAN END ITEM TEST In this phase, the TCAS 3000 Computer Unit shall be tested at the SIMPAN (TCAS Simulation Panel) using Operational Flight Software that is specified in Appendix A of this document. The Operational Flight Software should have been loaded into the UUT at the completion of an MTS End Item Test prior to performing this test. Step 1. The BITE LOG FAULT CLEARING procedure (previous section) must be performed prior to performing a SIMPAN End Item Test. This will clear any faults that were logged at the MTS during loading and verification of Operational Flight Software. Step 2. Perform the procedure specified in Using JCAIR TCAS Simulation Panel Test Fixture (Doc. No. EB7517947). ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 11 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D APPENDIX A Software / Firmware Configuration ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 12 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D 1 INTRODUCTION This Appendix provides the TCAS 3000 Production End Item Test and Operational Software/Firmware Configuration Tables. 1.1 Purpose  To provide instruction on the loading of images prior to End Item Testing.  To provide instruction on the loading of Operational Flight Software prior to shipment of the product. 2 SOFTWARE / FIRMWARE CONFIGURATION AND VERIFICATION 2.1 Initial Test Configuration Software Loading Prior to performing an MTS Auto Calibration or an MTS End Item Test, the following images must be loaded into the UUT. Step 1. Obtain the Master Media (CD) for the images listed in the tables below. Step 2. Perform the emulator loading procedure described in Appendix A of the TCAS 3000 TRD (8002216-001). End Item Part Software Master Media Part Number Numbers TCAS 3000 Initial Configuration SW P/N 9300003-002D 9003000-55001 This Master Media Contains The Following Files 9003000-65001 9003000-10001 Description P/N File Name CRC Boot 9000356-001 T3000_FL_BP1.BIN B9E02DB2 Data Loader 9000355-001 T3000_FL_DL1.BIN 162CBA5E I/O FPGA 9003025-001 IO_001.BIN 65E4D78D RF FPGA 9003026-002 RF_002.BIN A2260964 HW Config 9000654-001 t3000_hardware_info.BIN 653FE076 Note: HTS may be compact flash loaded at the MTS after the other images have been loaded by the emulator. End Item Part Software Master Media Part Numbers Numbers 9003000-55001 9300002-002F 9003000-65001 Hardware Test Software (HTS) (If loading using Compact Flash at MTS) 9003000-10001 9300002-002D (If loading using emulator and CD) ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 13 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D 2.2 Final Configuration Software Loading And Verification Prior to shipping the End Item, the following images must be loaded into the UUT. Step 1. Obtain the Master Media for the images listed in the table below. Note: These images will be compact flash loaded at the MTS. End Item Part Software Master Media Part Number Numbers Master Media For OP Software P/N 9300001-002F 9003000-55001 This Master Media Contains The Following Files 9003000-65001 9003000-10001 Description P/N File Name CRC Application (OP SW) 9000354-001 T3000_FL.OP1 D233397C Data Loader 9000355-001 T3000_FL.DL1 162CBA5E I/O FPGA 9003025-001 IO_001.FGA 65E4D78D RF FPGA 9003026-002 RF_002.FGB A2260964 Config File N/A HEADER.CFG N/A ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 14 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D 2.3 Synchronization Between ATP / Test Software The loading and verification of operational software part numbers and CRC’s is an automated process. For this process to work correctly, TCAS 3000 PC Test Software - P/N 9000469-001 requires the presence of the configuration file 9000469Config.txt in order to select a UUT and for Loading/Verification of Operational Software. Step 1. If the PC Test Software (9000469) is currently executing, terminate execution. Step 2. Obtain the latest 9000469Config.txt file from the designated controlled source. Step 3. Place the file in the following path: D:\9000469\9000469Config.txt Note: Any changes or additions of UUT part numbers, software part numbers or CRC’s, or revision letter changes of this document must also be reflected in the 9000469Config.txt file. 9000469Config.txt Note: The current 9000469Config.txt file must contain the following information and format: [ATP] Dwg Number 8002217 Rev: D [9003000-55001] Application Software P/N: 9000354-001 Application Software CRC: 0xD233397C Boot Software P/N: 9000356-001 Boot Software CRC: 0xB9E02DB2 DataLoader Software Copy 1 P/N: 9000355-001 DataLoader Software Copy 1 CRC: 0x162CBA5E DataLoader Software Copy 2 P/N: 9000355-001 DataLoader Software Copy 2 CRC: 0x162CBA5E Hardware Config Software P/N: 9000654-001 I/O FPGA Copy 1 P/N: 9003025-001 I/O FPGA Copy 1 CRC: 0x65E4D78D I/O FPGA Copy 2 P/N: 9003025-001 I/O FPGA Copy 2 CRC: 0x65E4D78D RF FPGA P/N: 9003026-002 RF FPGA CRC: 0xA2260964 [9003000-65001] Application Software P/N: 9000354-001 Application Software CRC: 0xD233397C Boot Software P/N: 9000356-001 Boot Software CRC: 0xB9E02DB2 DataLoader Software Copy 1 P/N: 9000355-001 DataLoader Software Copy 1 CRC: 0x162CBA5E ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 15 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D DataLoader Software Copy 2 P/N: 9000355-001 DataLoader Software Copy 2 CRC: 0x162CBA5E Hardware Config Software P/N: 9000654-001 I/O FPGA Copy 1 P/N: 9003025-001 I/O FPGA Copy 1 CRC: 0x65E4D78D I/O FPGA Copy 2 P/N: 9003025-001 I/O FPGA Copy 2 CRC: 0x65E4D78D RF FPGA P/N: 9003026-002 RF FPGA CRC: 0xA2260964 [9003000-10001] Application Software P/N: 9000354-001 Application Software CRC: 0xD233397C Boot Software P/N: 9000356-001 Boot Software CRC: 0xB9E02DB2 DataLoader Software Copy 1 P/N: 9000355-001 DataLoader Software Copy 1 CRC: 0x162CBA5E DataLoader Software Copy 2 P/N: 9000355-001 DataLoader Software Copy 2 CRC: 0x162CBA5E Hardware Config Software P/N: 9000654-001 I/O FPGA Copy 1 P/N: 9003025-001 I/O FPGA Copy 1 CRC: 0x65E4D78D I/O FPGA Copy 2 P/N: 9003025-001 I/O FPGA Copy 2 CRC: 0x65E4D78D RF FPGA P/N: 9003026-002 RF FPGA CRC: 0xA2260964 ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 16 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D APPENDIX B Test Report / TRD Cross Reference ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 17 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D The following tables contain the cross reference between the tests executed during the Acceptance Test and the corresponding paragraph in the TRD that describes the test method and the PASS/FAIL criteria. Test 01_1A Through Test 09_13 Test TRD Test TRD Test TRD Test TRD Number Para. Number Para. Number Para. Number Para. 01_1A 4.1.1 05_03 4.6.3 07_34 4.9.5 08_02 4.10.1 01_2A 4.1.2 05_04 4.6.4 07_35 4.9.5 08_03 4.10.1 01_3A 4.1.3 06_01 4.7.1 07_36 4.9.6 08_04 4.10.1 01_4A 4.1.4 06_02 4.7.2 07_37 4.9.6 08_05 4.10.1 01_1D 4.2.1 06_03 4.8.1 07_38 4.9.6 08_06 4.10.1 01_2D 4.2.2 06_04 4.8.1 07_39 4.9.6 08_07 4.10.1 01_3D 4.2.3 06_05 4.8.2 07_40 4.9.6 08_08 4.10.1 01_4D 4.2.4 07_01 4.9.1 07_41 4.9.6 08_09 4.10.1 02_01 4.3.1 07_02 4.9.1 07_42 4.9.6 08_10 4.10.1 02_02 4.3.2 07_03 4.9.1 07_43 4.9.7 08_11 4.10.1 03_01 4.4.1 07_04 4.9.1 07_44 4.9.7 08_12 4.10.1 03_02 4.4.2 07_05 4.9.1 07_45 4.9.7 08_13 4.10.1 03_03 4.4.3 07_06 4.9.1 07_46 4.9.7 08_14 4.10.1 03_04 4.4.4 07_07 4.9.1 07_47 4.9.7 08_15 4.10.1 03_05 4.4.5 07_08 4.9.2 07_48 4.9.7 08_16 4.10.1 03_06 4.4.6 07_09 4.9.2 07_49 4.9.7 08_17 4.10.1 03_07 4.4.7 07_10 4.9.2 07_50 4.9.8 08_18 4.10.1 03_08 4.4.8 07_11 4.9.2 07_51 4.9.8 08_19 4.10.1 03_09 4.4.9 07_12 4.9.2 07_52 4.9.8 08_20 4.10.1 03_10 4.4.10 07_13 4.9.2 07_53 4.9.8 08_21 4.10.1 03_11 4.4.11 07_14 4.9.2 07_54 4.9.8 08_22 4.10.1 03_12 4.4.12 07_15 4.9.3 07_55 4.9.8 08_23 4.10.1 03_13 4.4.13 07_16 4.9.3 07_56 4.9.8 08_24 4.10.1 03_14 4.4.14 07_17 4.9.3 07_57 4.9.9 08_25 4.10.2 03_15 4.4.15 07_18 4.9.3 07_58 4.9.9 08_26 4.10.3 03_16 4.4.16 07_19 4.9.3 07_59 4.9.9 08_27 4.10.4 03_17 4.4.17 07_20 4.9.3 07_60 4.9.9 08_28 4.10.5 03_18 4.4.18 07_21 4.9.3 07_61 4.9.9 09_01 4.11.1 03_19 4.4.19 07_22 4.9.4 07_62 4.9.9 09_02 4.11.2 03_20 4.4.20 07_23 4.9.4 07_63 4.9.9 09_03 4.11.3 03_21 4.4.21 07_24 4.9.4 07_64 4.9.10 09_04 4.11.4 04_01 4.5.1 07_25 4.9.4 07_65 4.9.10 09_05 4.11.5 04_02 4.5.2 07_26 4.9.4 07_66 4.9.10 09_06 4.11.6 04_03 4.5.3 07_27 4.9.4 07_67 4.9.10 09_07 4.11.7 04_04 4.5.4 07_28 4.9.4 07_68 4.9.10 09_08 4.11.8 04_05 4.5.5 07_29 4.9.5 07_69 4.9.10 09_09 4.11.9 04_06 4.5.6 07_30 4.9.5 07_70 4.9.10 09_10 4.11.10 04_07 4.5.7 07_31 4.9.5 07_71 4.9.11 09_11 4.11.11 05_01 4.6.1 07_32 4.9.5 07_72 4.9.12 09_12 4.11.12 05_02 4.6.2 07_33 4.9.5 08_01 4.10.1 09_13 4.11.13 ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 18 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D Test 09_14 Through Test 15_11 Test TRD Test TRD Test TRD Test TRD Number Para. Number Para. Number Para. Number Para. 09_14 4.11.14 11_14 4.13.14 12_06 4.14.6 12_50 4.14.50 09_15 4.11.15 11_15 4.13.15 12_07 4.14.7 12_51 4.14.51 09_16 4.11.16 11_16 4.13.16 12_08 4.14.8 12_52 4.14.52 09_17 4.11.17 11_17 4.13.17 12_09 4.14.9 13_01 4.15.1 09_18 4.11.18 11_18 4.13.18 12_10 4.14.10 13_02 4.15.2 09_19 4.11.19 11_19 4.13.19 12_11 4.14.11 13_03 4.15.3 09_20 4.11.20 11_20 4.13.20 12_12 4.14.12 13_04 4.15.4 09_21 4.11.21 11_21 4.13.21 12_13 4.14.13 13_05 4.15.5 09_22 4.11.22 11_22 4.13.22 12_14 4.14.14 13_06 4.15.6 09_23 4.11.23 11_23 4.13.23 12_15 4.14.15 13_07 4.15.7 09_24 4.11.24 11_24 4.13.24 12_16 4.14.16 13_08 4.15.8 09_25 4.11.25 11_25 4.13.25 12_17 4.14.17 13_09 4.15.9 09_26 4.11.26 11_26 4.13.26 12_18 4.14.18 13_10 4.15.10 09_27 4.11.27 11_27 4.13.27 12_19 4.14.19 13_11 4.15.11 09_28 4.11.28 11_28 4.13.28 12_20 4.14.20 13_12 4.15.12 09_29 4.11.29 11_29 4.13.29 12_21 4.14.21 13_13 4.15.13 09_30 4.11.30 11_30 4.13.30 12_22 4.14.22 13_14 4.15.14 09_31 4.11.31 11_31 4.13.31 12_23 4.14.23 13_15 4.15.15 09_32 4.11.32 11_32 4.13.32 12_24 4.14.24 13_16 4.15.16 10_01 4.12.1 11_33 4.13.33 12_25 4.14.25 13_17 4.15.17 10_02 4.12.2 11_34 4.13.34 12_26 4.14.26 13_18 4.15.18 10_03 4.12.3 11_35 4.13.35 12_27 4.14.27 14_01 4.16.1 10_04 4.12.4 11_36 4.13.36 12_28 4.14.28 14_02 4.16.2 10_05 4.12.5 11_37 4.13.37 12_29 4.14.29 14_03 4.16.3 10_06 4.12.6 11_38 4.13.38 12_30 4.14.30 14_04 4.16.4 10_07 4.12.7 11_39 4.13.39 12_31 4.14.31 14_05 4.16.5 10_08 4.12.8 11_40 4.13.40 12_32 4.14.32 14_06 4.16.6 10_09 4.12.9 11_41 4.13.41 12_33 4.14.33 14_07 4.17.1 10_10 4.12.10 11_42 4.13.42 12_34 4.14.34 14_08 4.17.2 10_11 4.12.11 11_43 4.13.43 12_35 4.14.35 14_09 4.17.3 10_12 4.12.12 11_44 4.13.44 12_36 4.14.36 14_10 4.17.4 11_01 4.13.1 11_45 4.13.45 12_37 4.14.37 14_11 4.17.5 11_02 4.13.2 11_46 4.13.46 12_38 4.14.38 14_12 4.17.6 11_03 4.13.3 11_47 4.13.47 12_39 4.14.39 15_01 4.18.1 11_04 4.13.4 11_48 4.13.48 12_40 4.14.40 15_02 4.18.2 11_05 4.13.5 11_49 4.13.49 12_41 4.14.41 15_03 4.18.3 11_06 4.13.6 11_50 4.13.50 12_42 4.14.42 15_04 4.18.4 11_07 4.13.7 11_51 4.13.51 12_43 4.14.43 15_05 4.18.5 11_08 4.13.8 11_52 4.13.52 12_44 4.14.44 15_06 4.18.6 11_09 4.13.9 12_01 4.14.1 12_45 4.14.45 15_07 4.18.7 11_10 4.13.10 12_02 4.14.2 12_46 4.14.46 15_08 4.18.8 11_11 4.13.11 12_03 4.14.3 12_47 4.14.47 15_09 4.18.9 11_12 4.13.12 12_04 4.14.4 12_48 4.14.48 15_10 4.18.10 11_13 4.13.13 12_05 4.14.5 12_49 4.14.49 15_11 4.18.11 ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 19 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D Test 15_12 Through Test 20_20 15_12 4.18.12 16_30 4.20.12 20_01 4.24.1 16_01 4.19.1 16_31 4.20.13 20_02 4.24.2 16_02 4.19.2 16_32 4.20.14 20_03 4.25.1 16_03 4.19.3 16_33 4.20.15 20_04 4.25.2 16_04 4.19.4 16_34 4.20.16 20_05 4.25.3 16_05 4.19.5 16_35 4.20.17 20_06 4.25.4 16_06 4.19.6 16_36 4.20.18 20_07 4.25.5 16_07 4.19.7 17_01 4.21.1 20_08 4.25.6 16_08 4.19.8 17_02 4.21.2-5 20_09 4.25.7 16_09 4.19.9 17_03 4.21.6-9 20_10 4.25.8 16_10 4.19.10 17_04 4.21.10 20_11 4.25.9 16_11 4.19.11 17_05 4.21.11-14 20_12 4.25.10 16_12 4.19.12 17_06 4.21.15-18 20_13 4.25.11 16_13 4.19.13 18_01 4.22.1 20_14 4.25.12 16_14 4.19.14 18_02 4.22.2 20_15 4.25.13 16_15 4.19.15 18_03 4.22.3 20_16 4.25.14 16_16 4.19.16 18_04 4.22.4 20_17 4.25.15 16_17 4.19.17 18_05 4.22.5 20_18 4.25.16-18 16_18 4.19.18 18_06 4.22.6 20_19 4.25.19 16_19 4.20.1 18_07 4.22.7 20_20 4.25.20 16_20 4.20.2 18_08 4.22.8 16_21 4.20.3 18_09 4.22.9 16_22 4.20.4 18_10 4.22.10 16_23 4.20.5 18_11 4.22.11 16_24 4.20.6 18_12 4.22.12 16_25 4.20.7 18_13 4.22.13 16_26 4.20.8 18_14 4.22.14 16_27 4.20.9 18_15 4.22.15 16_28 4.20.10 18_16 4.22.16 16_29 4.20.11 19_01 4.23.1 ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 20 Proprietary notice on the title page.

Doc Number ACCEPTANCE TEST PROCEDURE FOR TCAS 3000 Revision 8002217-001 D END OF DOCUMENT ACSS Use or disclosure of the information on this sheet is subject to the proprietary Page 21 Proprietary notice on the title page.


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Document Modified: 2006-02-01 22:05:25
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