# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 1 of 34 

### Transmittal Information

ACSS Publication Number 8008222

- 001

ATA Service Bulletin 9003500

- 34

- 6015



## NAVIGATION

- TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM

- TCAS 3000SP COMPUTER UNIT

– Part No. 9003500

- 10001,

- 10002,

- 10003

, and

- 10 004 , Part No. 9003500

- 55001,

- 55002,

- 55003, and

- 55004

, and Part No. 9003500

- 65001,

- 65002,

- 65003, and

- 65004

– Updates TCAS 3000SP (Surveillance Processor) Computer Units to Part Number 9003500

- 10005

, - 55005 , or

- 65005

. Install s New SafeRouteTM Operating Software Part No. 9000660

- 013

, from Master Media, Part No. 9400001

- 011F to Incorporate Updates to Interference Limiting Functionality

.

EXPORT ADMINISTRATION REGULATIONS ( EAR ) NOTICE

This technic al 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,

use d , or disclosed to others without the written authorizati on 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

- 011F

. The CF car d installs new o perating software, Part No. 9000660

- 013

, which upgrades TCAS 3000SP (Surveillance Processor) Computer Units as shown in the list that follows :

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 2 of 34 Summ ary (Cont)

Unit Part No. Before Modification Unit Part No. After Modification

9003500

- 10001,

- 10002,

- 10003, or

- 10004 to 9003500

- 10005

9003500

- 55 001

, - 55 002,

- 55 003, or

- 55 004 to 9003500

- 55005

9003500

- 65 001,

- 65 002,

- 65 003, or

- 65 004 to 9003500

- 65005

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

- 013

. Notes:

1. Aircraft Configuration Files (ACF) vary by installation. The ACSS Service Center loads only “generic” ACF files as part of final test. After installing the updated TCAS 3000SP Computer Unit in the aircraft, the operator must load the correct ACF files into the TCAS 3000SP Computer Unit.

2. The work described in this Service Bulletin can be completed on board the aircraft or on a TCAS 2000 Manual Test Station (MTS)

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 3 of 34 REVISION HISTORY

Revisions to ATA Service Bulletin No. 9003500

- 34

- 6015 (ACSS Pub. No. 8008222

- 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.

2

, 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 infor mation 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 r eferred 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

, 19 Added note to make sure aircraft is on t he ground during part number verification. Also added Step m) to choose the applicable unit.

24 Updated note in Section F , Step (6) to mak e sure that HW Mod D is identified.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 4 of 34 Revision Page Change Made
1 (Cont.) 27 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

..

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 5 of 34 1. PLANNING INFORMATION

A. Effectivit y This Service Bulletin is applicable to Part Numbers 9003500

- 10001,

- 10002,

- 10003,

or

- 10004 , Part No. 9003500

- 55 001,

- 55 002,

- 55 003, or

- 55 004

, a nd Part No. 9003500

- 65 001,

- 65 002,

- 65 003, or

- 65 004

.

B. Concurrent Requirements
Hardware Modification D must b e done before or at the same time as this conversion / modification.

**•** ACSS Publication No. 8008 296

- 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 use d 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 No. 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

- 013 , 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 Unit s to Part No. 9003500

- 10005

, - 55005 , or

- 65005

.

D. Description This Service Bulletin gives instructions for installing new Operational Software Part No. 9000660

- 013 , from Compact Flash (CF) card, Part No. 9400001

- 011F

, 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 identi fy the new dash number.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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 appro ved 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 modi fied TCAS 3000SP unit on aircraft as identified below:

Aircraft Previously Equipped With... New Approved Part N o s

.

9003500

- 10001,

- 10002,

- 10003, or

- 10004 to 9003500

- 100 05

9003500

- 55 001

, - 55 002,

- 55 003, or

- 55 004 to 9003500

- 55005

9003500

- 65 001,

- 65 002,

- 65 003, or

- 65 004 to 9003500

- 65005

After completing this FAA

- approved modific ation, 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 t his Service Bulletin is done on board the aircraft, ap proximately 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 u sing manual test procedures.

H. Weight and Balance This modification does not change weight and balance

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 7 of 34 I. Electrical Load Data This modification does not change electrical load data

.

J. Software Accomplishment Summary
Software is chang ed by this conversion/modifi cation.

Work a ctivities and procedur es 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 (SDI M), 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.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 8 of 34 2. MATERIAL INFOR MATION

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. I f a copy of the Software is necessary , ACSS must be in possession of a completed Software License Agreement before it will ship the Softw are.
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 Ser vice 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 load ing 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 c urrent 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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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 Servi ce Bulletin: ATA Part No. 9003500

- 34

- 6015 (ACSS Pub No. 8008222

- 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. 7 th 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 Surveill ance 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

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 10 of 34 

### ACSS SERVICE BULLETIN MATE RIALS 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 Agree ment for the software being ordered. Based on the information in this order form, ACSS Order Administration will complete the Appendix a nd/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 lis t 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 Bulle tin section, ‘Material Necessary for Each Component’ )

Part Number Description Quantity

NOTE: Each Compact Flash Card /Diskette is capable of performing an unlimited nu mber of upgrades. Please order a minimum quantity to meet your needs.

B ILL 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 7 th Avenue Phoenix , AZ 85027

- 4741, USA Phone: 623.445.7040 Fax: 623.445.7004 Email: acss.orderadmin@L

- 3com.com

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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.acsscustomerservi ces.com/CustomerServices

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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 Bulle tin.

Table 4 . Material to Be Purchased

New Part Number Name Old Part Number Qty. Instructions/ Disposition

9400001

- 011F New Surveillance Processor Operational Software (Master Med ia) See Table 9 on Page 27 1 1, 2, 6

9400005

- 010F SafeRoute ACF File for Rel 2.8 (767) See Table 9 on Page 27 A/N 1, 2, 6

9100012

- 00107F Safe R oute ASDB Config 7 See Table 9 on Page 27 A/N 1, 2, 6

Software Te ar Off Labels

9000359

- 173 Label for 10005 units N/A A/N 1, 2, 3, 4 , 7

Software Tear Off Labels (2D Compatible)

9000359

- 273 TCAS 3000SP , Label (for

- 10005 units)

N/A A/N 1, 2, 3 , 5, 7 9000359

- 274 TCAS 3000SP , Label (for

- 55005 units)

9000359

- 275 TCAS 3000SP , Label (for

- 65005 units)

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. Necessary only for units that have Product ID labe ls that do not include a 2D barcode.

5. Necessary only for units that have Product ID labels that include a 2D barcode.

6. Each Compact Flash Card (CF) can install an unlimited number of upgrades. Order a minimum quantity to satisfy your needs. A nominal cha rge can be applicable to Compact Flash Cards.

7. Labels are made of white polyester material.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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 MATE RIALS 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 Mat erial

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 = A s 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.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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. Descr iption

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. See Note 2 below.

OR

Method 3

– Part Number Verification with Remote ACSS VSI/TRA display

200F

- 0 0083 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

. R efer to Note 3

.

9000903

- 001 1 Software Configuration File for Surveillance Processor During Manufacturing Test Procedure. Refer to Note 3

.
**A/N = As Necessary**

IN STRUCTIONS/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 a n email to crc.acss@l

- 3com.com or telephone the Customer Response Center at (623) 445

- 7070.

3. For order information, refer to Section 2.A

, Pric e and Availability , starting on Page 8

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 15 of 34 3. ACCOMPLISHMENT INSTR UCTIONS

A. General Information



### CAUTION

ALL DISASSEMBLY AND MODIFICATION PROCEDURES MUST BE COMPLETED AT AN ANTISTATIC WORKSTATION

. REFER TO ESTABLISHED ANTISTATI C 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 Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8002231

- 002 (ATA No. 34

- 43

- 26)

.

**•** Surveillance Processor System Description and Installation Manua l (SDIM), ACSS Pub. No. 8007091

- 001 (ATA No. 34

- 43

- 25)

.

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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 16 of 34 B. Prep aration
(1) Choose an Implementation Method Before starting t his s oftware upgrade, refer to the Decision Chart shown in Figure 1 on Page 29 and choose a method for implementation of th is u pgrade

. (2) Examine the installed TCAS 3000SP Product Software Part Number Before starting t his 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.

F or a list of initial and new software part numbers

, r efer to the tables st arting on Pages 27

.


### C AUTION

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 SY STEM POWER CYCLE WHILE YOU ARE REPROGRAMMING THE COMPUTER UNIT. THIS WILL RESULT IN A PROGRAMMING FAILURE.

Method 1

Software Verification with a n I nstalled VSI/TRA, CDTI, or other display that can show extended test data (Cockpit only)

. NOTE: Access to Extende d 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

, C ode 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, ACSS Pub . No. 8007091

- 001 (A TA No. 34

- 43

- 25)

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 17 of 34 b) Examine the displayed software part number to m ake 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 )

.

Method 2 (Preferred Method)

Software Verification with a Standalone PC wit h 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 con tact 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 (Micr osoft® Word or WordPad) to open the text file and

see part numbers for the newly installed software

. h) Do a check to m ake 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 )

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 18 of 34 Method 3

Softw are Verification with a R emote 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 C MC/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 wh en 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 te st 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 Modific ation ) or Table 10 ( Installed Software Part Numbers After this Modification )

.

Method 4

Software Verification with CVI Part Number Verification Tool

. NOTE: Before starting veri fication, 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 W indows operation

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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 name it “ 9001089 ”.
h) Put the CD that contains Configuration File Part No. 9000903

- 001 , into the CD drive.
i) Use st andard 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 an d 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
program 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 a nd 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 u nit part number you chose and give a PASS/FAIL indication.
o) Do a check to m ake sure the installed software part numbers agree with the part numbers in Table 9 ( Installed Sof tware Part Numbers Before This Modification ) or Table 10 ( Installed Software Part Numbers After this Modification )

.

Method 5

If an upgraded TCAS 2000 Manual Test Station i s 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 secti on 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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 20 of 34 D. Modification Procedures

– On Board the Aircraft or o n 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 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) In stall the new TCAS 3000SP Operational Software.
a) Procure new Surveillance Processor Master Media CF card , Part No. 9400001

- 011F

. b) Apply power to the TCAS 3000SP CU

. W ait until all LEDs go off

. c) Open the CF card protective door on the front panel of the unit. See Figure 5 on Page 32

. NOTE: Hold the CF card with the ACSS product label facing the left side of the unit and the manufacturer’s label (with barcode) facing to the right (i.e., towards the front panel LEDs).
d) Put the CF card into the slot

. NOTE: DO NOT FORCE THE CARD INTO THE CU.

NOTE: Result: If the CF card is put int o the CU correctly, a ll LEDs will

come on and the TCAS 3000SP C U will restart

. e) 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 o f the software files on the CF card are loaded onto the TCAS 3000SP Computer unit.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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

. Th e software upload failed.

f) Step e) 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 e) occur s one time only

. g) 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 is an indication that the upload was not successful. The LED correlations are identified in Table 7

, above

. h) Push the CF ejector button on the front panel of the TCAS 3000SP Computer Un it and remove the card.
i) Close the CF card protective door. Result: All LEDs come on and the TCAS 3000SP Computer Unit restart s

. j) When all LEDs go off

, the unit is ready

. (2) Install the SafeRouteTM ACF File.
a) Procure new TCAS 3000SP ACF File, Part No. 9400005

- 010F

. b) Use Steps 3.D(1)b) thru 3.D(1)j) starting on Page 20 to install the ACF File.
(3) Install the SafeRoute ASDB File.
a) Procure new TCAS 3000SP ASDB File, Part No. 9100012

- 00107F

. b) Do Step 3.D(2 ) again to install the ASDB Software.
(4) R emove power from the TCAS 3000SP CU

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 22 of 34 (5) 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 s oftware part numbers. Refer to Paragraph 3.B(2) on Page 16

. (6) R emove power from the TCAS 3000SP Computer Unit and disconnect all PC Interface cable connecti ons.

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. 8007 091

- 001 (ATA No. 34

- 43

- 25)

. Refer to the AMM (Aircraft Maintenance Manual) specified for the aircraft.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 23 of 34 F. Identification Label Update

– On Board the Aircraft or o n a Bench System



### WARNING WHEN HANDLING SOLVENTS, MAKE SURE THERE IS SUFFICIENT VENTILATION I N 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 9003 5 00

- 10005

, - 55005 , or

- 65005

. (1) Examine the Product Identification Label on the front of the unit and procure the correct software tear

- off label(s). 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

- 10005 9000359

- 273 9000359

- 173

9003500

- 55005 9000359

- 274 N/A

9003500

- 65005 9000359

- 275 N/A

NOTE: Some CUs have Pr oduct 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 l abel 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 procedures

. (4) Carefully clean the software label area with isopropyl alcohol and give the surface sufficient time to dry

. (5) Remove the Software Mo d 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

m odifications are installed with this upgrad e

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 24 of 34 (6) Use a black indelible ink marker 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

- 011F , 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.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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 use d 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 Com puter 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 c omplete 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 procedur es

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 Pro duct 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 Ai rcraft 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

- 0 02 (ATA No. 34

- 43

- 26)

.

OR
b) For new part number 9003500

- 10005 , i f 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 the Product Identification Label. 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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 26 of 3 4 (2) Use a black indelible ink marker 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

. This completes the upgrade of TCAS 3000SP Computer Unit

, Part No. 9003500

- 10001

, - 1000 2

, - 10 003 and

- 10 004

, Part No. 9003500

- 55001,

- 55002,

- 55003 and

- 5 5004 , and Part No. 9003500

- 65001,

- 65002,

- 65003 and

- 65004 to Part N o. 9003500

- 10005

, - 55005 , or

- 65005

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th 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 be low.

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 Thi s Modification

Affected Part No. 9003500

- 10001

- 55001

- 65001 - 10002

- 55002

- 65002 - 10003

- 55003

- 65003 - 10004

- 55004

- 65004

Master Media (MM) Part No. 9400001

- 00 2 (SW Mod A) 9400001

- 00 4 F 9400001

- 0 05 F 9400001

- 00 7 F

Field Names Part Number

OP I Software 9000660

- 002 9000660

- 004 9000660

- 005 9000660

- 008

P1 Data Loader 9000355

- 101 9000355

- 101 9000355

- 102 9000355

- 102

RF FPGA 9003536

- 001 9003536

- 001 9003536

- 003 9003536

- 005

ACF MM Part No. 940000 5

- 00 1F 9400005

- 003F 9400005

- 0 05 F 940000 5

- 00 5 F

ACF 9000776

- 001 9000776

- 003 9000776

- 00 5 9000776

- 00 5

ASDB MM Part No. 9100012

- 00101 9100012

- 00102 9100012

- 00103 9400001

- 008F

ASDB 9200002

- 0010 1 9200002

- 00102 9200002

- 0010 3 9200002

- 0010 3

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 28 of 34 Table 10

. Installed Software Part Numbers After this Modif ication

Affected Part No. 9003500

- 10005,

- 55005, and

- 65005
Master Media (MM) Part No. 9400001

- 011F

Field Names Part Number

OP I Software 9000660

- 013 D C48D1DB

P1 Data Loader 9000355

- 103 CDE19B90

RF FPGA 9003536

- 006 A2281243

ACF Master Media Part No. 9400005

- 010F

ACF 9000776

- 010 45 AB DC 5E

ASDB Master Media Part No. 9100012

- 00107F

ASDB 9200002

- 00107 7A 7A FB 3B

NOTE: TCAS 3000SP Product Software that is released after the release of Part No. 9400001

- 011F is not included in Table 10 above

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 29 of 34 Figure 1

. TCAS 3000SP (Surveillance Processor) Computer Decision Chart

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 30 of 34 Figure 2 . Remote VSI/TRA to TCAS 3000SP Computer Interc onnect TCAS 3000SP Computer Unit

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 31 of 34 Figure 3

. CVI Part Number Verification Tool

– Dialog Box

Figure 4

. CVI Part Number Verification Tool

– Verification Window “Surv Proc” is the Surveillance Processor, Part No. 9003500

- XXXXX

Choose the applicable end item part

number from the drop

- down list.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 32 of 34 Figure 5 : Compact Fl ash Card Orientation for TCAS 3000 and TCAS 3000SP CU CF Manufacturer’s Label (with barcode) F ront Panel LEDs

C/F Load Status LED Product Identification label Protect ive door for CF Card Slot

Card Ejector button

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 33 of 34 Figure 6

. Example of a TCAS 3000SP Computer Unit 4MCU Label ( Without 2D Barcode)

Figure 7

. Example of a TCAS 3000SP Computer Unit 4MCU Label (With 2D Barcode) Remove only the bottom part of the original Product ID label. Install new software
tear

- off label below original Product ID label.

Remove only the bottom part of the original Product ID label. Install new software
tear

- off label below original Product ID label. 2D Ba rcode

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6015 Revision 01: February 4, 2011 ACSS Pub lication No. 8008222

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U.S.A. Page 34 of 34 Figure 8

. Example of a Software Tear

- Off Label for the TCAS 3000 SP Compute r Unit (2D

- Compatible)

Figure 9 . Example of Generic TCAS 3000SP Product Identification Label with New Software Tear

- Off Label Installed and Hardware Modifications Identified B efore install ing the new software tear

- off label, make sure the new dash number is

– XX 005

.

New d ash number is

- XX005

. Black ink conceals Mod A , Mod B, Mod C, and Mod D on the H/W MOD table.