# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 

### Transmittal Information

ACSS Publication Number 8008221

- 001
ATA Service Bulletin 9003500

- 34

- 6014



## NAVIGATION

- TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM

- TCAS 3000SP COMPUTER UNIT

– Part No. 9003500

- 10900,

- 10 901

, and

- 10 90 2

, Part No. 9003500

- 55900,

- 55901

, and

- 55902

, Part No. 9003500

- 57901, and Part No. 9003500

- 65900,

- 65901

, and

- 65902

– Updates TCAS 3000SP (Surveillance Processor) Computer Unit s to Part No. 9003500

- 10904

, - 55904 , or

- 65904

. Install s New SafeRouteTM Operating Software Part No. 9000660

- 014

, from Master Media, Part No. 9400001

- 012F 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, use d

, 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 Bull etin gives instructions for the installation of new TCAS 3000SP Operating Software from Master Media Compact Flash card (CF) , Part No. 9400001

- 012F

. The CF card in stalls new o perating software, Part No. 9000660

- 014

, 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

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Summary (Cont)

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

9003500

- 10900,

- 10901, or

- 10902 to 9003500

- 10904

9003500

- 55900,

- 55901 or

- 55902 or

- 57901 to 9003500

- 55904

9003500

- 65900,

- 65901 or

- 65902 to 9003500

- 65904

Refer to Section 1.C on Page 5 for a list of the changes that are a part of new T CAS Product Software, Part No. 9000660

- 014

. NOTE: 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

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 REVISION HISTORY

Revisions to AT A Service Bulletin No. 9003500

- 34

- 6014 (ACSS Pub. No. 8008221

- 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 Simplifie d 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 stan dards.

1 Added Export Administration Regulations (EAR) notice.

1

, 8

, 12 Removed references to Part Availability.

5 Removed the first sentence in the first par agraph 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

, 20

, 26 Removed Section L, “Documents Necessary to Complete This Bulletin.” This information is available in other sections of the Service Bulletin or in the “Testing and Fault Isolation” section of the Component Maintena nce Manual (CMM). Removed other references to test procedures/software that is included in the CMM. 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. Added Old Software Part Numbers in the applicable column and added a note to refer the operator to the tables starting on Page 28

. 13 Added new information to Section 2.C(2) . This section identifies commercially available items supplied by the operator.

15 Removed misplaced duplicate Warning.

17

, 17

, 18

, 20 Updated the last step in each Part Number Verification Method to refer the operator to the applicable part number reference table.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Revision Page Change Made 1 (Cont.) 19 Added note to make sure aircraft is on the ground during part number verification. Added Step m) to choose the applicable unit.

25 Updated note in Section F , Step (6) to make sure that HW Mod D is identified.

23 Added note to Section 3.D , Step (12) . In some cases, the hardware part number may be

- 5 5, not

- 57. The embedded Hardware Part Number can only be changed on a Manual Test Station (MTS). It is not necessary for successful part number verification.

24 Updated installation instructions for updating labels that ha ve 2D barcodes and those that do not

. 28 thru 31 Added four new software part number reference tables to make it easier to identify results obtained when using different software verification me thods.
Added a note after Table 9

, Table 11 , and Table 13 to explain that new part numbers released after the release of Part No. 9400001

- 012F are not included in the related tab le

. 34 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

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 1. PLANNI NG INFORMATION

A. Effectivity This Service Bulletin is applicable to Part Numbers 9003500

- 10900,

- 10901, and

- 10902, Part No. 9003500

- 55900,

- 55901

, and

- 55902, Part No. 57901

, a nd Part No. 9003500

- 65900,

- 65901

, and

- 65902

.

B. Concurrent Requirements
Hardware M odification D must be 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 S tation (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 p rogram 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

- 014 , incorporates updates to the Interference Limiting functionality. These updates improve trac king 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

- 10904

, - 55904 , or

- 65904

.

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

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

- 012F , 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 th e unit to identify the new dash number.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 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 perm itted. 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 re viewed 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 opera tion of the modified TCAS 3000SP unit on aircraft as identified below:

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

.
9003500

- 10 900,

- 10901, or

- 10902 to 9003500

- 10904

9003500

- 55900,

- 55901 or

- 55902

or 9003500

- 57901 to 9003500

- 55904

9003500

- 65900,

- 65901 or

- 65902 to 9003500

- 65904

After completing this FAA

- approved m odification, 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 aircra ft, 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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 I. Electrical Load Data This modification does not change electrical load data

.

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

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 i n 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 Re vision 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 Manu al (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.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 2. MATERIA L 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. I f a copy of the Software is necessary , ACSS must be in possession of a completed Software License Agreement before it will ship th e 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 A CSS 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 da ta 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 bas ed 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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 (3) Placing an Order
Use a standard Purchase Or der (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 thi s Service Bulletin: ATA Service Bulletin No. 9003500

- 34

- 6014 (ACSS Pub No. 8008221

- 001 )

**•** Aircraft Type

**•** Unit Original Part Number

**•** Unit Serial Number(s)

**•** Price of modific ation 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.)

**•** Qua ntity 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) At tn: 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 Communi cation 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

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 

### ACSS SER VICE 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 Ap pendix to the Agreement 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 Li cense 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 O rder 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 appli cable Service Bulletin 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.

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 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

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 B. Industry Support Information ACSS will not reimburse labor hours for integration of this conversion/modification.
ACSS ’s on

- line electronic sys tem 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://ww w.acsscustomerservices.com/CustomerServices

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 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

- 012F New Surveillance Processor Operational S oftware (Master Media) 9400001

- 003 F
9400001

- 006F
9400008

- 001F
9400001

- 010F
9400001

- 008F 1 1, 2, 4 , 8

Software Tear Off Labels

9000359

- 176 TCAS 3000SP , La bel for

- 10904 units N/A A/N 1, 2, 3 , 5, 7

Software Tear Off Labels (2D Compatible)

9000359

- 276 TCAS 3000SP , La bel (for

- 10904 units)

N/A A/N 1, 2, 3

, 6, 7 9000359

- 277 TCAS 3000SP , Label (for

- 55904 units)

9000359

- 278 TCAS 3000SP , Label (for

- 65904 units)

A/N = As Necessary

INSTRUCT IONS/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 fu ll 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 charg e can be applicable to Compact Flash Cards.

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

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 INSTRUCTIONS/DISPOSITION (Cont.)

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

7. Labels are made of white polyester material.

8. Refer to Table 8

, Table 10 , and Table 12 for detailed part number information.

(2) Material Su pplied 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 SPECIFIE D 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 a s 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%)

- Opt ional

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.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 F. Tooling The items identified in Table 6 below are necessary to do the proc edures 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

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 Verification Tool Refer to Note 3

.
9000903

- 001 1 Software Configuration File for Surveillance Pr ocessor 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 a n email to crc.acss@l

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

- 7070.

3. For order informati on, refer to Section 2.A

, Price and Availability , starting on Page 8

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 3. ACCOMPLISHMENT INSTR UCTIONS

A. General Information



### CAUTION

ALL DI SASSEMBLY 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, Tab les, 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 (AT A 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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 B. Preparation (1) Choose an Implementation Method Before starting t his s oftware upgrade, refer to the Decision Chart shown in Figure 1 on Page 32 and choose a method for implementation of th is u pgrade

. (2) Examine the installed TCAS 3000SP Product Software Part Number s. Before starting t his Sof tware 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 lis t of initial and new software part numbers

, r efer to the tables st arting on Pages 28

. 

### 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 Verificati on with a n I nstalled 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

- initi ated 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 I SOLATION section of the Surveillance Processor System Description and Installation Manual (SDIM), ACSS Pub. No. 8007091

- 001 (ATA No. 34

- 43

- 25)

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 b) Examine the displayed software part number to m ake sure the installed part numbers agree with the part numbers in the applicable reference tables.

**•** For installed software part numbers b efore this modification, refer to Table 8 on Page 28

.

**•** For installed software part numbers after this modification, refer to Table 9 on Page 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 car d. 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 bl ank 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 35

. 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 tha t 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 ope n the text file and

see part numbers for the newly installed software

. h) Do a check to make sure to make sure the installed part numbers agree with the part numbers in the applicable reference tables.

**•** For installed software part numbers b efore this modifica tion, refer to Table 10 on Page 29

.

**•** For installed software part numbers after this modification, refer to Table 11 on Page 29

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Method 3
Software 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 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 33

. a) Push and hold the self

- test button on the controller for 8 seconds or longer. b) Do a check to make sure to make sure the installed part numbers agree with the part numbers in the applicable reference tables.

**•** For installed software part numbers b efore this modif ication, refer to Table 8 on Page 28

.

**•** For installed software part numbers after this modification, refer to Table 9 on Page 28

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Method 4
Softwar e 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 applicable version of the 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 p ower 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

. 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 Software Configuration File Part No. 9000903

- 001 , in to 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) P ut the CVI Part Num ber 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 f ind 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 34

. 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 34

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 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 to make sure the installed part numbers agree with the pa rt numbers in the applicable reference tables.

**•** For installed software part numbers b efore this modification, refer to Table 12 on Page 31

.

**•** For installed software part numbers after this modification, refer to Table 13 on Page 31

.
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

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 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 8 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

- 012F

. (2) Apply power to the TCAS 3000SP CU

. W ait until all LEDs go off

. (3) Open the CF card protective door on the front panel of the unit. See Figure 5 on Page 35

. NOTE: Hold the 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, a ll LEDs will come on and the TCAS 3000SP C U 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.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Table 7 . Software Installation LED Display
LED Disp lay 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 XF ER 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 Proc essor . If the files are not changed, Step (5) occur s 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 3000 SP Computer Unit and remove the card. (9) Close the CF card protective door. Result: All LEDs come on and the TCAS 3000SP Computer Unit restart s

. (10) When all LEDs go off

, the unit is ready

. (11) R emove power from the TCAS 3000SP CU

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 (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

. NOTE: The H ardware Part Number (

- 55XXX or

- 57XXX) is embedded in the TCAS 3000SP Computer Unit and cannot be changed in the field. It

can only be changed on a Manual Tes t Station (MTS). This embedded Part Number is used for End Item Test ing at ACSS and is not necessary for successful verification of the software/firmware part numbers

.

If ATA Service Bulletin 9003500

- 34

- 0004 ( ACSS Publication Number 8008143

- 001 ) was do ne to upgrade TCAS 3000SP CU, Part No. 9003500

- 55901 to Part No. 9003500

- 5 7 901, it is possible that the Part Number Verification procedure given in Step (12) above wil l continue to show the hardware part number as Part Number 9003500

- 55 xxx , not 9003500

- 57 xxx

. (13) R emove power from the TCAS 3000SP Computer Unit and disconnect all PC Interface cable connections.

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.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 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 APPLI CABLE 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

- 10904

, - 55904 , or

- 65904

. (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

- 10904 9000359

- 276 9000359

- 176

9003500

- 55904 9000359

- 277 N/A

9003500

- 65904 9000359

- 278 N/A

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 Mo d part of the Product Identification Label on the front of the CU . See Figure 6 and Figure 7 on Page 36

. (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

m odifications are installed with this upgrade

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 (6) Use a black indelible i nk 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 37

. NOTE: Some units will have Hardware Mod A identified on the Product Identification Label. For other units, the newly installed media , Part No. 9400001

- 012F , includes the updates necessary for Hardware Mod A

, Hardware Mod B, and Hardware Mod C

. A CSS 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 Requi rements , 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

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 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 S oftware, 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 Mainte nance 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 modifi cation 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 Upd ate

- A t 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 ca n 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 24 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) For new part number 9003500

- 10904 , if there is no 2D barcode on the label, use the instructions in Section 3.F ( Identification Label Update

– On Board the Aircr aft or On a Bench System ) on Page 24 to update the Product Identification Label. See Figure 6 on Page 36 for reference OR c) If the label includes a 2D barcode, use ACSS P ub. No. 8007628

- 001 (ATA Service Bulletin No. 9003500

- 34

- 0001) to replace the entire Product Identification Label with a new ACSS 2D barcode label. See Figure 7 on Page 36

. NOTE: Do not put marks on the SW Mod status table . No software modifications are installed with this upgrade

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 (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 37

. This completes the upgrade of TCAS 3000SP Computer Unit

, 9003500

- 10900,

- 10901, and

- 10902

, Part No. 9003500

- 55900

, - 55901 and

- 55902

, Part No. 9003500

- 57901, and Part No. 9003500

- 65900,

- 65901, and

- 65902 to Part No. 9003500

- 10904

, - 55904 , or

- 65904

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Table 8

. Installed Software Part Numbers Before This Modification ( Using Method 1 or Method 3 )

Affected Part No. 9003500 - 10900

- 55900

- 65900 - 1 0901

- 55901

- 65901 - 10901 - 55901

- 65901

- 57901 - 10902

- 55902

- 65902

Master Media Part No. 9400001

- 003 F 9400001

- 006F (HW Mod A) 9400008

- 001F (SW Mod A) 9400001

- 010F (HW Mod B) 9400001

- 008F

Field Names Part Number s

OP I Software 9000660

- 003 9000660

- 006 90 00660

- 006 9000660

- 006 9000660

- 009

OP II Software 9000774

- 001 9000774

- 001 9000774

- 001 9000774

- 001 9000774

- 001

P1 Data Loader 9000355

- 101 9000355

- 102 9000355

- 102 9000355

- 102 9000355

- 102

P2 Data Loader 9000775

- 001 9000775

- 001 9000775

- 001 9000775

- 001 900077 5

- 001

IO FPGA 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001

RF FPGA 9003536

- 001 9003536

- 003 9003536

- 003 9003536

- 005 9003536

- 005

ACF 9000777

- 001 9000777

- 002 9000777

- 002 9000777

- 002 9000776

- 007

ASDB 9200002

- 00101 9200002

- 00103 9200002

- 00104 9200002

- 00103 9200002

- 00105

Table 9

. Installed Software Part Numbers After this Modification (Using Method 1 or Method 3 )

Affected Part No. 9 003500

- 10904,

- 55904, and

- 65 9 04

Master Media Part No. 9400001

- 012F

Field Names Part Number CRC

OP I Software 9000660

- 014 DC48D1DB

OP II Software 9000 774

- 001 36B78460

P1 Data Loader 9000355

- 103 CDE19B90

P2 Data Loader 9000775

- 001 96B22CA5

IO FPGA 9003535

- 001 8BAD7032

RF FPGA 9003536

- 006 A2281243

ACF 9000776

- 011 50DD6C73

ASDB 9200002

- 00107 7A7AFB3B

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

- 012F is not included in Table 9 above

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Table 10

. Installed Software Part Numbers Before This Modification ( Using Method 2 )

Affected Part No. 9003500 - 10900

- 55900

- 65900 - 10901

- 55901

- 65901 - 10901 - 55901

- 65901

- 57901 - 10902

- 55902

- 65902

Master Media Part No

. 9400001

- 003 F 9400001

- 006F (HW Mod A) 9400008

- 001F (SW Mod A) 9400001

- 010F (HW Mod B) 9400001

- 008F

Field Names Part Number s
Application Software 9000660

- 003 9000660

- 006 9000660

- 006 9000660

- 006 9000660

- 009

ASDB 9200002

- 00101 9200002

- 00103 9200002

- 00104 9200002

- 00103 9200002

- 00105

BOOT 9000356

- 101

or

- 202 9000356

- 201 9000356

- 201 9000356

- 201 9000356

- 201

Data Loader Copy 1 9000355

- 101 9000355

- 102 9000355

- 102 9000355

- 102 9000355

- 102

Data Loader Copy 2 9000355

- 101 9000355

- 102 9000355

- 102 9000355

- 102 90003 55

- 102

Hardware Refer to the Note in Paragraph 3.D(12) on Page 23

. I / O FPGA Copy 1 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001

I / O FPGA Copy 2 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001

RF FPGA 9003536

- 001 9003536

- 003 9003536

- 003 9003536

- 005 9003536

- 005
Configuration Settings Part Number 9000777

- 001 9000777

- 002 9000777

- 002 9000777

- 002 9000776

- 007

Table 11

. Installed Software Part Numbe rs After this Modification (Using Method 2 )

Affected Part No. 9003500

- 10904,

- 55904, and

- 65 9 04

Master Media Part No. 9400001

- 012F

Field Name Part Number CRC
Application Software 9000660

- 014 DC48D1DB

ASDB 9200002

- 00107 7A7AFB3B

BOOT 9000356

- 20 2 01 0E 21 AA

Data Loader Copy 1 9000355

- 103 CDE19B90

Data Loader Copy 2 9000355

- 103 CDE19B90

I / O FPGA Copy 1 900353 5

- 001 8BAD7032

I / O FPGA Copy 2 9003535

- 001 8BAD7032

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Affected Part No. 9003500

- 10904,

- 55904, and

- 65 9 04

Master Media Part No. 9400001

- 012F

Field Name Part Number CRC

RF FPGA 9003536

- 006 A2281243
Configuration Settings Part Number 9000776

- 011 50DD6C73

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

. 9400001

- 012F is not included in Table 11 above

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Table 12

. Installed Software Part Numbers Before This Modification ( Using Method 4 )

Affected Part No. 9003500 - 10900

- 55900

- 65900 - 10901

- 55901

- 65901 - 10901 - 55901

- 65901

- 57901 - 10902

- 55902

- 65902

Master Media Part No. 9400001

- 003 F 9400001

- 006F (HW Mod A) 9400008

- 001F (SW Mod A) 9400001

- 010F (HW Mod B) 9400001

- 008F

Field Names Part Number s
Appl Software P/N 9000660

- 003 9000660

- 006 9000660

- 006 9000660

- 006 9000660

- 009

P2 OP SW PN 9000774

- 001 9000774

- 001 9000774

- 001 9000774

- 001 9000774

- 001
Data Load Copy 1 P/N 9000355

- 101 9000355

- 102 9000355

- 102 9000355

- 102 9000355

- 102

P2 Data Loader 1 P/N 9000775

- 001 9000775

- 001 9000775

- 001 9000775

- 001 9000775

- 001

IO FPGA Copy 1 P/N 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001 9003535

- 001

RF FPGA P/N 9003536

- 001 9003536

- 003 9003536

- 003 9003 536

- 005 9003536

- 005
Config Settings P/N 9000777

- 001 9000777

- 002 9000777

- 002 9000777

- 002 9000776

- 007

ASDB P/N 9200002

- 00101 9200002

- 00103 9200002

- 00104 9200002

- 00103 9200002

- 00105

Table 13

. Installed Software Part Numbers After this Modification (Using Method 4 )

Affected Part No. 9003500

- 10904,

- 55904, and

- 65 9 04

Master Media Part No. 9400001

- 012F

Field Names Part Number CRC

Appl S oftware P/N 9000660

- 014 DC48D1DB

P2 OP SW PN 9000774

- 001 36B78460
Data Load Copy 1 P/N 9000355

- 103 CDE19B90

P2 Data Loader 1 P/N 9000775

- 001 96B22CA5

IO FPGA Copy 1 P/N 9003535

- 001 8BAD7032

RF FPGA 900 3536

- 006 A2281243
Config Settings P/N 9000776

- 011 50DD6C73

ASDB P/N 9200002

- 00107 7A7AFB3B

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

- 012F is not included in Table 13 above

.

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Figure 1

. TCAS 3000SP (Surveillance Processor) Computer Decision Chart

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 Figure 2 . Remote VSI/TRA to TCAS 3000SP Computer Interconnect TCAS 3000SP Computer Unit

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 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 37 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

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U. S.A. Page 35 of 37 Figure 5 : Compact Flash Card Orientation for TCAS 3000 and TCAS 3000SP CU CF Manufacturer’s Label (with barcode) Front Panel LEDs

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

Car d Ejector button

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U. S.A. Page 36 of 37 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 Barcode

# Service Bulletin

Release Date: May 27, 2010 ATA Service Bulletin No

. 9003500

- 34

- 6014 Revision 01: February 4, 2011 ACSS Pub lication No. 8008221

- 001 Copyright 2011 Aviation Communication & Surveillance Systems, LLC

19810 N orth 7 th Avenue, Phoenix, AZ 85027

- 4741 Printed in U. S.A. Page 37 of 37 Figure 8

. Example of a Software Tear

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

- Compatible)

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

- Off Label Installed and Hardware Modifications Identified New d ash number is

- XX904

. Black ink conceals Mod A , Mod B, Mod C

, and Mod D on the H/W MOD table. B efore install ing the new software tear

- off label, make sure the new dash number is

- XX 904

.