# ACSS Service Bulletin 9003500-34-6016 Copy: No revision named ("U.S. DOT/FAA - Service Information - 3"), 34 pages: PDF https://openairdocs.org/files/sha256/74/50/745026826d3e415a9b730e5dc71672236c9a19a6ab89c9576b6b6641ca6692f3; text https://openairdocs.org/service-documents/acss/sb-9003500-34-6016/file/745026826d3e.md. Rights: © Aviation Communication & Surveillance Systems, LLC. Filed by the FAA in regulations.gov docket FAA-2010-1204; AD 2012-02-08 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [ACSS](https://openairdocs.org/service-documents/acss.md) - Type: Service bulletin (Service Bulletin) - Number: 9003500-34-6016 - Page: https://openairdocs.org/service-documents/acss/sb-9003500-34-6016 ## ADs that cite it (1) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2012-02-08](https://openairdocs.org/ad/2012-02-08.md), effective Mar 13, 2012: No revision named Also cited in [1 proposed AD](https://openairdocs.org/service-documents/acss/sb-9003500-34-6016/proposed.md). ## Text (34 pages) Rights: © Aviation Communication & Surveillance Systems, LLC. Filed by the FAA in regulations.gov docket FAA-2010-1204; AD 2012-02-08 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 1 of 34 Transmittal Information ACSS Publication Number 8008223-001 ATA Service Bulletin 9003500-34-6016 NAVIGATION - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM - TCAS 3000SP COMPUTER UNIT – Part No. 9003500-10802 – Updates TCAS 3000SP (Surveillance Processor) Computer Units to Part Number 9003500-10803. Installs New SafeRoute™ Operating Software Part No. 9000660-015, from Master Media, Part No. 9400001-013F to Incorporate Updates to Interference Limiting Functionality. EXPORT ADMINISTRATION REGULATIONS (EAR) NOTICE This technical data is controlled under the Export Administration Regulations (EAR) ECCN 7E994 and may not be exported to a Foreign Person, either in the U.S. or abroad, without the proper authorization of the U.S. Department of Commerce. LEGAL NOTICE This document and the information disclosed herein are proprietary data of Aviation Communication and 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 and Surveillance Systems, LLC. This document is being furnished in confidence by Aviation Communication and Surveillance Systems, LLC. The information disclosed herein falls within exemption (b) (4), Freedom of Information Act, (5 USC 552), and the prohibitions of the Disclosure of Confidential Information Generally (18 USC 1905). Implementation of this software update described in this Service Bulletin involves changes to software. The software required to effect this update is copyrighted by ACSS. License to use this software to perform the modifications set forth in this Service Bulletin shall be granted by ACSS in accordance with terms and conditions to be entered into between ACSS and the customer. SUMMARY This Service Bulletin gives instructions for the installation of new TCAS 3000SP Operating Software from Master Media Compact Flash card (CF), Part No. 9400001-013F. The CF card installs new operating software, Part No. 9000660-015, which upgrades TCAS 3000SP (Surveillance Processor) Computer Unit Part No. 9003500-10802 to Part No. 9003500-10803. ### Page 2 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 2 of 34 SUMMARY (Cont.) Refer to Section 1.C on Page 5 for a list of the changes that are a part of new TCAS Product Software, Part No. 9000660-015. NOTE: The work described in this Service Bulletin can be completed on board the aircraft or on a TCAS 2000 Manual Test Station (MTS). ### Page 3 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 3 of 34 REVISION HISTORY Revisions to ATA Service Bulletin No. 9003500-34-6016 (ACSS Pub. No. 8008223-001) are summarized in Table 2 below. Table 1. Service Bulletin Revisions Revision Date of Release Initial Release May 27, 2010 Revision 1 February 4, 2011 NOTE: This Service Bulletin obeys ASD-STE100 Simplified Technical English guidelines and ATA iSpec2200 specifications, wherever practicable. Table 2. Revisions Summary Revision Page Change Made 1 VAR Made minor changes in the document to agree with current ACSS format and style standards. 1 Added Export Administration Regulations (EAR) notice. 1, 8, 12 Removed references to Part Availability. 5 Removed the first sentence in the first paragraph in Section 1.B. Added Concurrent Requirement. HW Mod D must be done before or at the same time as this conversion / modification. 5, 7, 19, 25 Removed Section L. Test Program information is available in other sections of the Service Bulletin or in the “Testing and Fault Isolation” section of the Component Maintenance Manual (CMM). Removed all references to test procedures/software that are included in the CMM and referred operators to the CMM. 12 Updated Table 4 to include options for updating labels that have a 2D barcode and those that do not. 13 Added new information to Section C. (2). This section identifies commercially available items supplied by the operator. 15 Removed misplaced duplicate Warning. 18 Added note to make sure aircraft is on the ground during part number verification. Added Step m) to choose the applicable unit. 24 Updated note in Section F, Step (6) to make sure that HW Mod D is identified. ### Page 4 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 4 of 34 Revision Page Change Made 1 (Cont.) 27, 28 Added Table 8. Updated Table 9 and Table 10 to show field names for part number validation when the CVI Tool is used. 31 Replaced Figure 3 with new Figure showing CVI Part Number Verification Tool – Dialog Box. Updated Figure 4. CVI Part Number Verification Tool – Verification Window ### Page 5 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 5 of 34 1. PLANNING INFORMATION A. Effectivity This Service Bulletin is applicable to Part Numbers 9003500-10802. B. Concurrent Requirements Hardware Modification D must be done before or at the same time as this conversion / modification. • ACSS Publication No. 8008296-001 (ATA Service Bulletin No. 9003500-34-0006) – Installs an update to the Surveillance Processor Boot Code. If a TCAS 2000 Manual Test Station (MTS) is used to load the operational software, one of the Service Bulletins that follow must be done before or in conjunction with this Bulletin: • ACSS ATE Service Bulletin No. 8007622-001 (ATA Service Bulletin No. 9003500-34-6000) - installs test program 9000767-001 for PC with Windows NT operating system or • ACSS ATE Service Bulletin 8008093-001 (ATA Service Bulletin No. 9003500-34- 6009) - installs test program 9000950-001 for PC with Windows XP operating system. C. Reason New Operational Software, Part No. 9000660-015, incorporates updates to the Interference Limiting functionality. These updates improve tracking of nearby Mode-S intruders in high density environments. Customers upgrading from older software versions of TCAS will also gain the benefit of minor changes that have been incorporated into later software releases. This Service Bulletin updates TCAS 3000SP Computer Units to Part No. 9003500-10803. D. Description This Service Bulletin gives instructions for installing new Operational Software Part No. 9000660-015, from Compact Flash (CF) card, Part No. 9400001-013F, on board the aircraft or by final Acceptance Test on a TCAS 2000 Manual Test Station (MTS). This Service Bulletin also includes instructions for installing a new software tear-off label on the front of the unit to identify the new dash number. ### Page 6 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 6 of 34 NOTE: Some units have Product Identification labels made of metalized polyester material. New tear-off labels are all made with white polyester. A mixture of materials on an updated Product Identification Label is permitted. When this software upgrade is done at an ACSS-Authorized Service Center, new ACSS labels can be installed, if necessary. E. Compliance This Service Bulletin is highly recommended because it has an effect on aircraft safety. This Service Bulletin has been written in support of a potential FAA Airworthiness Directive. Do this conversion as soon as possible. The FAA Airworthiness Directive will identify the compliance schedule. F. Approval / Authorization Granted The content of this Service Bulletin is reviewed and approved by the FAA. This Service Bulletin includes the information that follows: (1) Gives TCAS 3000SP unit modification instructions from the manufacturer. (2) Gives authorization for the installation and operation of the modified TCAS 3000SP unit on aircraft as identified below: Aircraft Previously Equipped With… New Approved Part Nos. 9003500-10802 to 9003500-10803 After completing this FAA-approved modification, it is the responsibility of the aircraft operator to get “Return to Service” authorization, if necessary, from the applicable regulatory authorities. G. Manpower When the modification described in this Service Bulletin is done on board the aircraft, approximately 0.5 work hours are necessary to complete the work. Approximately 0.5 work hours are necessary when the modification is done on a TCAS 2000 Manual Test Station (MTS). Approximately 1.0 work-hour is necessary to complete Final Test of the unit using manual test procedures. H. Weight and Balance This modification does not change weight and balance. I. Electrical Load Data This modification does not change electrical load data. ### Page 7 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 7 of 34 J. Software Accomplishment Summary Software is changed by this conversion/modification. Work activities and procedures described in this software update meet the requirements of RTCA Document DO-178B, Software Considerations in Airborne Systems and Equipment Certification. K. References (1) Reference Documents The document identified in Table 3 is for reference only and is not necessary to implement this Service Bulletin. Subsequent revisions to the document are permitted. Table 3. Reference Documents Document Number Revision Title FAA Best Practices Document 22 Dec. 2000 Scrap or Salvageable Parts and Materials (2) Related Service Bulletins None L. Other Publications Affected As a consequence of this Service Bulletin, ACSS will revise the documents in the list that follows: • Surveillance Processor Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8002231-002 (ATA No. 34-43-26) • Surveillance Processor System Description and Installation Manual (SDIM), ACSS Pub. No. 8007091-001 (ATA No. 34-43-25). The Airworthiness Analysis is not changed. The Testing is not changed. M. Interchangeability or Intermixability of Parts This is not applicable to the changes outlined in the Service Bulletin. ### Page 8 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 8 of 34 2. MATERIAL INFORMATION A. Price and Availability (1) Software License Agreement New Product Software is necessary for the update described in this Service Bulletin. ACSS must be in possession of a completed ACSS Software License Agreement before it will ship an order. A signed Software License Agreement is not usually necessary for software upgrades done at an ACSS Authorized Service Center. If a copy of the Software is necessary, ACSS must be in possession of a completed Software License Agreement before it will ship the Software. If a current Software License Agreement is on file at ACSS, only an Addendum to this Agreement is necessary for this Software upgrade. (2) Pricing and Availability Pricing for this Service Bulletin is available from: ACSS Order Administration or ACSS Service Center For contact information, refer to Paragraph 2.A(3), Placing an Order. Pricing for this Service Bulletin is different for customers who use on-board data loading or their own shop procedures to complete this upgrade. ACSS has different pricing for units that customers send to ACSS for this upgrade. NOTE: 1. A shop Bench Test Fee is applicable for those units sent to ACSS for this Software upgrade and will be based on current catalog pricing. NOTE: 2. Other repairs will be quoted separately. Please speak or write to an ACSS Customer Order Administrator for scheduling information before sending a unit for repair or modification. ### Page 9 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 9 of 34 (3) Placing an Order Use a standard Purchase Order (PO) form, or complete the ACSS Service Bulletin Materials Order Form (OA-009) shown on Page 10. To expedite your order, include all of the information in the list that follows: • A Purchase Order Number • Reference to this Service Bulletin: ATA Part No. 9003500-34-6016 (ACSS Pub No. 8008223-001) • Aircraft Type • Unit Original Part Number • Unit Serial Number(s) • Price of modification for each unit • Part Number(s) being ordered (Refer to Table 4 on Page 12 for a list of part numbers and order only those parts that are applicable to the unit to be updated.) • Quantity ordered • Bill-to address/instructions • Ship-to address/instructions • Freight carrier Account number and special shipping instructions When ordering software and/or parts, send Purchase Orders to: Aviation Communication and Surveillance Systems (ACSS) Attn: Customer Order Administration 19810 N. 7th Ave Phoenix, AZ 85027-4741 USA Phone: (623) 445-7040 Fax: (623) 445-7004 or e-mail: acss.orderadmin@L-3com.com NOTE: All orders are subject to a standard lead time of 2 weeks to give sufficient time for documentation validation and order preparation. When sending units to an ACSS Service Center, send Purchase Orders to: Aviation Communication and Surveillance Systems (ACSS) Attn: Customer Order Administration 19810 N. 7th Ave Phoenix, AZ 85027-4741 USA Phone: (623) 445-7030 Fax: (623) 445-7002 or e-mail: acss.phxrepair@L-3com.com ### Page 10 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 10 of 34 ACSS SERVICE BULLETIN MATERIALS ORDER FORM To secure the rights to use ACSS software, ACSS requires the completion of a Software License Agreement and Appendix. If a current Software License Agreement exists with ACSS, the customer is only required to sign an Appendix to the Agreement for t he software being ordered. Based on the information in this order form, ACSS Order Administration will complete the Appendix and/or the Software License Agreement and forward it to the customer for signatures. The Software License Agreement, or Appendix, must be signed and received by ACSS prior to shipment of the order. ALL of the following information MUST be completed for ACSS to quickly and efficiently process this software order. Customer Name * Customer Purchase Order Number Date Unit Original Part Number Customer Contact Name Customer Contact Email Address A/C Type Applicable ACSS Service Bulletin Pub. No. Price of Modification for each Unit Unit Serial Number(s) Attach additional sheets as necessary to list all of the serial numbers being updated by this software order. * This completed form may be used as the formal Purchase Order (PO) or may be used as an information sheet attached to the PO. PARTS BEING ORDERED (as listed in the applicable Service Bulletin section, ‘Material Necessary for Each Component’) Part Number Description Quantity NOTE: Each Compact Flash Card/Diskette is capable of performing an unlimited number of upgrades. Please order a minimum quantity to meet your needs. BILL TO ADDRESS SHIP TO ADDRESS Freight Carrier and Account Number Special Shipping Instructions SUBMIT THIS ORDER TO: Aviation Communication and Surveillance Systems (ACSS), LLC Attn: Customer Order Administration 19810 North 7th Avenue Phoenix, AZ 85027-4741, USA Phone: 623.445.7040 Fax: 623.445.7004 Email: acss.orderadmin@L-3com.com ### Page 11 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 11 of 34 B. Industry Support Information ACSS will not reimburse labor hours for integration of this conversion/modification. ACSS’s on-line electronic system gives customers access to a variety of product-related publications. Service Bulletins and Technical Newsletters are available at the ACSS Customer Services web site. Go to: http://www.acsscustomerservices.com/CustomerServices. ### Page 12 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 12 of 34 C. Material Necessary for Each Component (1) Material to be Purchased The items listed in Table 4 below are necessary to complete this Service Bulletin. Table 4. Material to Be Purchased New Part Number Name Old Part Number Qty. Instructions/Disposition 9400001-013F New Surveillance Processor Operational Software (Master Media) 9400001-009F A/N 1, 2, 4 Software Tear Off Labels for -10803 units 9000359-174 TCAS 3000SP, Label N/A A/N 1, 2, 3, 5, 7 9000359-251 TCAS 3000SP, Label (2D Compatible) N/A A/N 1, 2, 3, 6, 7 A/N = As Necessary INSTRUCTIONS/DISPOSITION 1. For correct disposal of used parts, refer to FAA Best Practices document, Scrap or Salvageable Parts and Materials, local regulatory agency, or local Repair Station policy. 2. Make sure quantities are correct and verifiable. 3. Include a full list of serial numbers for the units to be modified to make sure you receive the correct identification plates. 4. Each Compact Flash Card (CF) can install an unlimited number of upgrades. Order a minimum quantity to satisfy your needs. A nominal charge can be applicable to Compact Flash Cards. 5. Necessary only for units that have Product ID labels that do not include a 2D barcode. 6. Necessary only for units that have Product ID labels that include a 2D barcode. 7. Labels are made of white polyester material. ### Page 13 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 13 of 34 (2) Material Supplied by the Operator WARNING BEFORE USING A MATERIAL, REFER TO THE MANUFACTURER’S MATERIAL SAFETY DATA SHEETS FOR SAFETY INFORMATION. SOME MATERIALS CAN BE DANGEROUS. CAUTION DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO MATERIALS SPECIFIED BY ACSS. MATERIALS THAT ARE NOT EQUIVALENT CAN CAUSE DAMAGE TO THE EQUIPMENT AND CAN VOID ANY WARRANTY. The items identified in Table 5 on Page 13 are commercially available. Do not order them as part of this Service Bulletin. Equivalent alternatives are permitted for items in the table. Table 5. Operator Supplied Material Part/Specification Number Qty. Keyword HAZARD CODE 130D A/N Solvent, isopropyl alcohol (99%) - Optional source HAZARD CODE 203B A/N Ink, black marking, dye-based marker. No. 33003 Marker, Action, 33 Fine. ITW Dymon, Olathe KS (CAGE 1QZC4) A/N = As Necessary D. Material Necessary for Each Spare Same as Section 2.C, Material Necessary for Each Component. E. Re-identified Parts This reference is not applicable. ### Page 14 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 14 of 34 F. Tooling The items identified in Table 6 below are necessary to do the procedures in this Service Bulletin. Equivalent alternatives are permitted. Table 6. Tooling Part/Specification Number Qty. Description Method 2 – Part Number Verification with Compact Flash Card and PC Operator-supplied 1 Windows-based PC Operator-supplied A/N A blank CF card Various 1 A commercially available CF Read/Write Drive A/N A header file used to read the installed software part numbers. Refer to Note 2. OR Method 3 – Part Number Verification with Remote ACSS VSI/TRA display Part/Specification Number Qty. Description 200F-00083 1 Adapter Cable OR Method 4 – Part Number Verification with ACSS CVI Part Number Verification Tool RS-232 (Part No. T336255-88) 1 PC Interface Cable 9001089-001 1 CVI Part Number Versification Tool. Refer to Note 3. 9000903-001 1 Software Configuration File for Surveillance Processor During Manufacturing Test Procedure. Refer to Note 3. A/N = As Necessary INSTRUCTIONS/DISPOSITION 1. For correct disposal of used parts, refer to FAA Best Practices document, Scrap or Salvageable Parts and Materials, local regulatory agency, or local Repair Station policy. 2. To request a copy of the header file, send an email to crc.acss@l-3com.com or telephone the Customer Response Center at (623) 445-7070. 3. For order information, refer to Section2.A, Price and Availability, starting on Page 8. ### Page 15 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 15 of 34 3. ACCOMPLISHMENT INSTRUCTIONS A. General Information CAUTION ALL DISASSEMBLY AND MODIFICATION PROCEDURES MUST BE COMPLETED AT AN ANTISTATIC WORKSTATION. REFER TO ESTABLISHED ANTISTATIC PROCEDURES. CAUTION THIS EQUIPMENT CONTAINS MOISTURE SENSITIVE PARTS. SPECIAL HANDLING IS NECESSARY. NOTE: 1. The Paragraphs, Items, Tables, and/or Figure numbers given in this Service Bulletin can be found in one of the two manuals in the list below: • Surveillance Processor System Description and Installation Manual (SDIM), ACSS Pub. No. 8007091-001 (ATA No. 34-43-25) • Surveillance Processor Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8002231-002 (ATA No. 34-43-26) NOTE: 2. Before doing the work in this Service Bulletin, make sure you can read the TCAS 3000SP Computer Unit software part numbers from a maintenance connection. ### Page 16 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 16 of 34 B. Preparation (1) Choose an Implementation Method Before starting this software upgrade, refer to the Decision Chart shown in Figure 1 on Page 29 and choose a method for implementation of this upgrade. (2) Examine the installed TCAS 3000SP Product Software Part Number. Before starting this Software upgrade, use one of the Methods below to make sure that verification of the software part number(s) is possible. If the method you use gives a satisfactory result, use the same method to make sure the new software installed successfully. For a list of initial and new software part numbers, refer to the tables starting on Pages 27. CAUTION MAKE SURE THE AIRCRAFT HAS GEAR DOWN AND “WEIGHT ON WHEELS” DURING PART NUMBER VERIFICATION OR WHILE REPROGRAMMING THE TCAS 3000SP COMPUTER UNIT ON BOARD THE AIRCRAFT. CAUTION DO NOT START A TCAS SYSTEM POWER CYCLE WHILE YOU ARE REPROGRAMMING THE COMPUTER UNIT. THIS WILL RESULT IN A PROGRAMMING FAILURE. Method 1 Software Verification with an Installed VSI/TRA, CDTI, or other display that can show extended test data (Cockpit only). NOTE: Access to Extended Test Mode is available only on the ground with the transponder in STANDBY mode. The aircraft configuration must include a cockpit-initiated self−test that starts when the operator pushes and holds the TCAS TEST switch for 8−seconds. a) Use the extended test mode menu to show the System Status Page, Code 0013, and examine the installed version of the operating software. Refer to the FAULT ISOLATION section of the Surveillance Processor System Description and Installation Manual (SDIM), ACSS Pub. No. 8007091-001 (ATA No. 34-43-25). ### Page 17 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 17 of 34 b) Examine the displayed software part number to make sure the installed part numbers agree with the part numbers in Table 9 (Installed Software Part Numbers Before This Modification) or Table 10 (Installed Software Part Numbers After this Modification) on Page 27 and 28. Method 2 (Preferred Method) Software Verification with a Standalone PC with an installed or connected CF Card Read/Write Drive and a blank CF card. a) Procure a header file from ACSS Customer Services. Refer to Note 2 in Table 6 on Page 14 for contact information. b) Make a copy of the header file and write it to the blank CF card. NOTE: Refer to the CF Read/Write Drive manufacturer’s operating instructions. c) Open the CF card protective door on the front panel of the TCAS 3000SP Computer Unit. See Figure 5 on Page 32. d) Put the CF card into the slot. Make sure that the disk manufacturer’s label with barcode points towards the front panel LEDs. NOTE: DO NOT FORCE THE CARD INTO THE CU. Result: The XFER IN PROCESS LED blinks to show that the unit is reading the CF card. Data transfer from the LRU is complete when the XFER IN PROCESS LED goes off and the C/F LOAD STATUS LED is continuous green. e) When the data transfer is complete, push the CF ejector button to remove the CF card and close the CF card protective door. f) Start the PC and put the CF card into the CF card reader. Refer to the manufacturer’s instructions to see the card’s contents. • A text file (LOG.OUT) shows on the display. g) Use a text editor (Microsoft® Word or WordPad) to open the text file and see part numbers for the newly installed software. h) Do a check to make sure the installed software part numbers agree with the part numbers in Table 9 (Installed Software Part Numbers Before This Modification) or Table 10 (Installed Software Part Numbers After this Modification) on Page 27 and 28. ### Page 18 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 18 of 34 Method 3 Software Verification with a Remote ACSS VSI/TRA display. Notes: 1. This method is valid ONLY if an ACSS VSI/TRA is used. 2. The external VSI method will not work if pin RMP 12C (Honeywell BCA EFIS output format) is grounded as part of the aircraft installation. 3. A CMC/CFDS-initiated extended self−test is not recognized at the 8−second time period. Extended self-test is available only with some approved TCAS control panels. The specified aircraft configuration must include a cockpit-initiated self−test that starts when the TCAS TEST switch is pushed and held for 8−seconds. On some aircraft, you can use a remotely-connected VSI/TRA, Part No. 4067241-843, -844, -845, -860, -861, -862, -880, -881, -882, -890, -891, or -892 to do software verification. During extended test mode, connect the VSI/TRA to the J1 front connector on the TCAS 3000SP Computer unit with an adapter cable (Part No. 200F−00083). See Figure 2 on Page 30. a) Push and hold the self-test button on the controller for 8 seconds or longer. b) Make sure the installed software part numbers agree with the part numbers in Table 9 (Installed Software Part Numbers Before This Modification) or Table 10 (Installed Software Part Numbers After this Modification) on Page 27 and 28. Method 4 Software Verification with CVI Part Number Verification Tool. NOTE: Before starting verification, make sure that the aircraft is on the ground and that the unit under test is set to ground mode. a) Acquire a copy of the CVI Part Number Verification Tool, Part No. 9001089-001, and the applicable Software Configuration File Part No. 9000903-001, from ACSS Customer Services. Refer to Note 2 in Table 6 on Page 14 for contact information. b) Procure or assemble an RS-232 cable, Part No. T336255-88. Refer to Table 6 on Page 14. c) Stop the PC and remove power from the TCAS 3000SP CU. d) Connect the RS-232 cable from the PC (9-pin connector) to the J1 front connector (53-pin connector) on the TCAS 3000SP CU. e) Apply power to the TCAS 3000SP CU. f) Start the PC and Microsoft Windows operation. ### Page 19 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 19 of 34 g) Use standard Windows procedures to make a folder on Local Disk drive(C:) and change the folder name to “9001089”. h) Put the CD that contains Configuration File Part No. 9000903-001, into the CD drive. i) Use standard Windows procedures to copy the configuration text (.ini) file from the CD into directory c:\9001089. j) Eject the CD. k) Put the CVI Part Number Verification Tool disk, Part No. 9001089-001, into the CD drive. Result: The program will run automatically and open the testexec window. NOTE: If the program fails to load, go to Start => Run. You can type D:\9001089.exe in the Open field or browse to find the file, 9001089.exe. l) Choose 9001089.exe and double-click to activate the program. m) In the Select Unit dialog box, choose the applicable unit under test; for example, Surv Proc. See Figure 3 on Page 31. Result: The LabWindows/CVI Test Executive 9001089 window opens. n) Choose the applicable part number and software mod from the Select P/N dropdown menu and click Start. See Figure 4 on Page 31. Result: The Test Display field shows a list of installed software part numbers that are applicable to the unit part number you chose and give a PASS/FAIL indication. o) Do a check to make sure the installed software part numbers agree with the part numbers in Table 9 (Installed Software Part Numbers Before This Modification) or Table 10 (Installed Software Part Numbers After this Modification) on Page 27 and 28. Method 5 If an upgraded TCAS 2000 Manual Test Station is used to install this upgrade, the correct Manufacturing Test Software must be installed. Refer to Section 1.B, Concurrent Requirements. Refer to the TESTING AND FAULT ISOLATION section of Volume II of the Surveillance Processor Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8002231-002 (ATA No. 34-43-26) for test procedure information. C. Disassembly/Inspection/Removal No disassembly necessary. ### Page 20 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 20 of 34 D. Modification Procedures – On Board the Aircraft or on a Bench System NOTE: Before starting this modification, use one of the Software Verification Methods in Section 3.B(2) on Page 16 to make sure you can read the installed software part numbers. Refer to Table 9 on Page 27 for a list of Initial Software Part Numbers. Use the procedure that follows to install the software from a CF (Compact Flash) card to the TCAS 3000SP Computer Unit (CU) installed on the aircraft. NOTE: Before uploading the software, make sure that the aircraft is on the ground. This software cannot be uploaded while the aircraft is airborne. (1) Procure new Surveillance Processor Master Media CF card, Part No. 9400001- 013F. (2) Apply power to the TCAS 3000SP CU. Wait until all LEDs go off. (3) Open the CF card protective door on the front panel of the unit. See Figure 5 on Page 32. NOTE: Hold the Surveillance Processor Master Media CF card with the ACSS product label pointing to the left side of the unit and the manufacturer’s label (with barcode) pointing to the right (i.e., in the direction of the front panel LEDs). (4) Put the CF card into the slot. NOTE: DO NOT FORCE THE CARD INTO THE CU. Result: If the CF card is put into the CU correctly, all LEDs will come on and the TCAS 3000SP CU will restart. (5) Monitor the LEDs on the front panel while the new product software uploads from the CF card. The LEDs will continue to cycle until all of the software files on the CF card are loaded onto the TCAS 3000SP Computer unit. ### Page 21 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 21 of 34 Table 7. Software Installation LED Display LED Display What it means All LEDs come on. The TCAS 3000SP CU is restarting. All LEDs go off and the XFER IN PROCESS LED blinks. The TCAS 3000SP CU is reading the CF card. The XFER IN PROCESS LED is continuous green. The TCAS 3000SP CU is loading the contents of the CF card. Note: The loading process takes approximately 5 minutes. The C/F LOAD STATUS LED is continuous green. The software upload is complete. The C/F LOAD STATUS LED is red. The software upload failed. (6) Step (5) will repeat if the DL or FPGA files on the new CF card are different from files already loaded on the Surveillance Processor. If the files are not changed, Step (5) occurs one time only. (7) When the upload is complete and successful, the CF Load Status LED changes to a continuous green. NOTE: A red C/F LOAD STATUS LED on the front panel shows that the upload was not successful. The LED correlations are identified in Table 7, above. (8) Push the CF ejector button on the front panel of the TCAS 3000SP Computer Unit and remove the card. (9) Close the CF card protective door. Result: All LEDs come on and the TCAS 3000SP Computer Unit restarts. (10) When all LEDs go off, the unit is ready. (11) Remove power from the TCAS 3000SP CU. (12) Make sure that the part numbers of the new software are correct. Use the same Verification method you used to do a check of the initial software part numbers. Refer to Paragraph 3.B(2) on Page 16. (13) Remove power from the TCAS 3000SP Computer Unit and disconnect all PC Interface cable connections. ### Page 22 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 22 of 34 E. Return to Service Use the System Self−Test procedures referred to in the ADJUSTMENT/TEST System Self-Tests section of the Surveillance Processor System Description and Installation Manual (SDIM), ACSS Pub. No. 8007091-001 (ATA No. 34-43-25). Refer to the AMM (Aircraft Maintenance Manual) specified for the aircraft. ### Page 23 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 23 of 34 F. Identification Label Update – On Board the Aircraft or on a Bench System WARNING WHEN HANDLING SOLVENTS, MAKE SURE THERE IS SUFFICIENT VENTILATION IN THE WORK AREA. USE APPLICABLE PRECAUTIONS TO PREVENT INHALATION OF VAPORS AND EXPOSURE OF FUMES TO FLAME. After you are sure that installation of the new product software was successful, use the applicable procedure below to update the identification label(s) on the TCAS 3000SP CU. The new TCAS 3000SP part numbers will be 9003500-10803. (1) Procure the applicable preprinted software tear-off label. Refer to the chart below and to Table 4 on Page 12 to identify which labels are necessary: Unit Part No. 2D Barcode on ID Label No 2D Barcode on ID Label 9003500-10803 9000359-251 9000359-174 NOTE: Some CUs have Product Identification labels made of metalized polyester material. New tear-off labels are all made with white polyester. A mixture of materials on an updated Product Identification Label is permitted. (2) Use a utility knife or razorblade to carefully remove only the bottom software Mod part of the Product Identification Label on the front of the CU. See Figure 6 and Figure 7 on Page 33. (3) Keep the label you removed in Step (2) above. Refer to local policy for correct disposal instructions. (4) Carefully clean the software label area with isopropyl alcohol and give the surface sufficient time to dry. (5) Remove the Software Mod Tear-off Label from its backing and install the label in the same location as the label you removed in Step (2) above. NOTE: Do not put marks on the SW Mod status table. No software Modifications are installed with this upgrade. ### Page 24 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 24 of 34 (6) Use a black indelible pen to completely conceal the letters A, B, C, and D in the Hardware Mod block of the Product Identification label. See Figure 9 on Page 34. NOTE: Some units will have Hardware Mod A identified on the Product Identification Label. For other units, the newly installed media, Part No. 9400001-013F, includes the updates necessary for Hardware Mod A, Hardware Mod B, and Hardware Mod C. ACSS Pub. No. 8008296-001 installs the updates necessary for Hardware Mod D and must be done before starting the modification referred to in this Service Bulletin. Refer to Section 1.B, Concurrent Requirements, on Page 5. The label must be updated to show the new Hardware Mod status. ### Page 25 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 25 of 34 G. Modification Procedures – At a Service Center with a TCAS 2000 MTS When a TCAS 2000 Manual Test Station (MTS) is used to install new Product Software, use the procedure that follows: (1) Do a Final Test to make sure all system parameters are fully functional. Refer to the TESTING AND FAULT ISOLATION section of Surveillance Processor Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8002231-002 (ATA No. 34-43-26) for test procedure information. (2) During functional testing, use the procedures and instructions in the TCAS 3000SP CMM to complete the software modification described in this Service Bulletin. Refer to the Acceptance Test Procedure for Surveillance Processor, ACSS Pub. No. 8002217-002, Appendix A, for software loading procedures H. Identification Label Update - At an ACSS-Authorized Service Center If the work described in this Service Bulletin is done at an ACSS-Authorized Service Center, the full Product Identification Label can be replaced to show the new part number. NOTE: Full Product Identification Labels can only be installed at an ACSS- Authorized Service Center. All other Service Centers must obey the instructions in Section 3.F (Identification Label Update – On Board the Aircraft or on a Bench System) on Page 23 to update existing Product Identification Labels. (1) Identify and examine the Identification Labels on the front of the TCAS 3000SP CU. Choose one of the steps below to update the Product Identification Label: a) If replacement of the full label is necessary, refer to the Surveillance Processor Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8002231-002 (ATA No. 34-43-26). OR b) If there is no 2D barcode on the label, use the instructions in Section 3.F (Identification Label Update – On Board the Aircraft or on a Bench System) on Page 23 to update Product Identification Labels. See Figure 6 on Page 33 for reference. OR c) If the label includes a 2D barcode, use ACSS Pub. No. 8007628-001 (ATA Service Bulletin No. 9003500-34-0001) to replace the entire Product Identification Label with the new ACSS 2D barcode label. See Figure 7 on Page 33. ### Page 26 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 26 of 34 (2) Use a black indelible pen to completely conceal the letters A, B, C, and D in the Hardware Mod block of the Product Identification label. See Figure 9 on Page 34. NOTE: Do not put marks on the SW Mod status table. No software modifications are installed with this upgrade. This completes the upgrade of TCAS 3000SP Computer Unit, Part No. 9003500-10802 to Part No. 9003500-10803. ### Page 27 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 27 of 34 Table 8. Field Reference Table for Part Number Verification Software Field Names Method 2 LOG.OUT Header File See Note below. Method 4 CVI Tool See Note below. OP I Software Application Software Appl Software P/N OP II Software – P2 OP SW PN P1 Data Loader Data Loader Copy 1 Data Load Copy 1 P/N P2 Data Loader – P2 Data Loader 1 P/N IO FPGA I/O FPGA Copy 1 IO FPGA Copy 1 P/N RF FPGA RF FPGA RF FPGA P/N ACF Configuration Settings Part Number Config Settings P/N ASDB ASDB ASDB P/N NOTE: It is possible that the Verification Method you choose will not output every installed part number shown in the tables that follow. The purpose for doing a validation before starting the modification is to make sure that the tool you use can communicate with the LRU. It is not necessary to do a verification of every part number when doing this step. Table 9. Installed Software Part Numbers Before This Modification Affected Part No. 9003500 -10802 Master Media Part No. 9400001-009F Field Names Part Number CRC OP I Software 9000660-010 31F5098F P1 Data Loader 9000355-102 D95461F8 RF FPGA 9003536-005 1BE4D4AB ACF 9000776-006 79662FCC ASDB 9200002-00105 373FEA3F ### Page 28 Service Bulletin Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 28 of 34 Table 10. Installed Software Part Numbers After this Modification Affected Part No. 9003500 -10803 Master Media Part No. 9400001-013F Field Names Part Number CRC OP I Software 9000660-015 DC48D1DB P1 Data Loader 9000355-103 CDE19B90 RF FPGA 9003536-006 A2281243 ACF 9000776-008 8692EE7E ASDB 9200002-00107 7A7AFB3B NOTE: TCAS 3000SP Product Software that is released after the release of Part No. 9400001-013F is not included in Table 10 above. ### Page 29 (OCR) ACSS® Thales Company on Service Bulletin Decision Logic if updating SafeRoute ™ Operational Software onboard aircraft is an option Can you read the installed OP Software Part Number on board the aircraft? (Refer to Section 3.B for Method options) Yes No Update Unit Onboard Aircraft Update completed at Service Center Read installed Part Numbers (if Send unit to Service available) on cockpit system Center for update Upload new software from Service Center updates Compact Flash Card and returns unit Verify upload by reading new software Part Number Perform system Return-to-Service Customer installs updated unit in aircraft Install new software Tear-Off AA9003500-001-DF label or identify new Software Mod on Product ID Label Customer completes aircraft certification documentation update with authorities Figure 1. TCAS 3000SP (Surveillance Processor) Computer Decision Chart Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7"h Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 29 of 34 ### Page 30 (OCR) ACSS® lemmunication compar Service Bulletin J1 MOUNTING CONNECTOR TRAY (ARINC 615) VSI/TRA 4067241-843-844 -845 -860 TCAS -861 -862 3000SP -880-881 Computer 882-890 Unit -891 -892 ADAPTER CABLE (P/N 200F-00083) 41-PIN MATING 53-PIN MATING CONNECTOR CONNECTOR (ARINC 615) Figure 2. Remote VSI/TRA to TCAS 3000SP Computer Interconnect Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7"h Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 30 of 34 ### Page 31 (OCR) ACSS® Thales Company on compar Service Bulletin "Surv Proc" is the Surveillance Processor, Part No. 9003500-XXXXX E Select Unit AA9001089-00-002 Select type of unit TCAS 3000 Surv ProcL Cancel Figure 3. CVI Part Number Verification Tool - Dialog Box # LabWindows/CVI Test Executive 9001089_REV_- Ele Beport Sequence Test Applications Description: Sequence File: Login Level: Current Time: TCAS 3000 Load Software |Check_SW_Load3000≤ Developer 10:44:51 Sequence Display: RS232 Com Display: 30 20 Load/Verify OP SW 30_21 Verify UT PN 30 _22 HW Config SW PN 30 24 APP SH PN 30_25 APP SW CRC 30_26 Boot SW PM 30_27 Boot SW CRC Test Display: Choose the applicable end item part number from the drop-down list. NO DOPWr AA9001089-00-001 Select P/N = 9003000-10001- Start QUIT Figure 4. CVI Part Number Verification Tool - Verification Window Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7"h Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 31 of 34 ### Page 32 (OCR) ACSS® Thales ommunication compar Service Bulletin Protective door for CF Card Slot NR 900 1WY D3 TCAS PASS DISE TA Front Panel LEDS TCAS Card Ejector button FAIL DISP RA TOP XXXX ANT RAD Identification label Product SO 1600 Emi Cal. (WIC WT 15.61 Lbs 379758 INSP# BOT ANT XPDA BuS ALT C/F Load Status LED C/F LOAD XPER STATUS DATA LOADER PROCES CF Manufacturer's PUSH TO TEST Label (with barcode) Figure 5: Compact Flash Card Orientation for TCAS 3000 and TCAS 3000SP CU Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7th Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 32 of 34 ### Page 33 (OCR) ACSS® lemmunication compar Service Bulletin ACSS 19810 N 7TH AVE PHOENIX AZ USA Install new software MFR 1WYD3 INSP # DATE tear-off label below WT Lbs original Product ID label. SER FCC ID P8CT3K-4M MOD ABCDEFGHJKLMNPRSTU H/W PNR 9003500- MADE IN USA AA9000359-501-K' Remove only the bottom part of the original Product ID label. TCAS SOFTWARE DO-178B LEVEL B MOD ABCDEFGHJ KLMNPRSTU Figure 6. Example of a TCAS 3000SP Computer Unit 4MCU Label (No 2D Barcode) ACSS 19810 N 7TH AVE PHOENIX AZ USA Install new software MFR 1WYD3 INSP # DATE tear-off label below original Product ID WT Lbs label. SER FCC ID P8CT3K-4M 2D Barcode H/W ABCDEFGHJ KLMNPRSTU MOD _---- PNR 9003500- MADE IN USA the bottom part Remove only AА 9000359-001-J of the original Product ID label. TCAS SOFTWARE DO-178B LEVEL B MOD ABCDEFGHJKLMNPRSTU Figure 7. Example of a TCAS 3000SP Computer Unit 4MCU Label (With 2D Barcode Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7"h Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 33 of 34 ### Page 34 (OCR) ACSS® Thales Company on compar Service Bulletin Before installing the new software tear-off label, make sure the new dash number is -10803. PNR 9003500- MADE IN USA TCAS SOFTWARE DO-178B LEVEL B MOD AA 9000359-003-J AB CDEFGHJ KLMNPRSTU Figure 8. Example of a Software Tear-Off Label for the TCAS 3000SP Computer Unit (2D-Compatible) ACSS 19810 N 7TH AVE PHOENIX AZ USA Mod A, Mod B , Black ink conceals Mod C, and MFR 1WYD3 INSP # DATE WT Lbs New dash number is Mod D on the H/W FCC ID P8CT3K-4M -10803 MOD table. SER MOD HW OOOO EFGH J KLM NPRSTU PNR 9003500- MADE IN USA TCAS SOFTWARE DO-178B LEVEL B MOD AA 9000359-001-J AB CDEFGHJ KLMNPRSTU Figure 9. Example of Generic TCAS 3000SP Product Identification Label with New Software Tear-Off Label Installed and Hardware Modifications Identified Release Date: May 27, 2010 ATA Service Bulletin No. 9003500-34-6016 Revision 01: February 4, 2011 ACSS Publication No. 8008223-001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC 19810 North 7"h Avenue, Phoenix, AZ 85027-4741 Printed in U.S.A. Page 34 of 34 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.