# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 

### Transmittal Information

ACSS Publication Number 8008235

- 001

ATA Service Bulletin 9003000

- 34

- 6006



## NAVIGATION

- TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM

- TCAS 3000 COMPUTER UNIT

– Part No. 9003000

- 10001,

- 10002, and

- 10003

, Part No. 9003000

- 55001,

- 55002, and

- 55003

, and Part No. 9003000

- 65001,

- 65002, and

- 65003

– Updates TCAS 3000 Computer Unit s to Part No. 9003000

- 10004

, - 55004

, or

- 65004

. Install s New Operating Software

, Part No. 9000354

- 005 from Master Media, Part No. 9300001

- 005F

, to Incorporate Updates to Interference Limiting Functionality

.

EXPORT ADMINISTRATION REGULATIONS NOTICE

This technical da ta 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 t he 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 US C 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 copyr ighted 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 3 000 Operating Software from Master Media Compact Flash (CF) C ard , Part No. 9300001

- 005F

. The CF card installs n ew o perating software, Part No. 9000354

- 005

, which upgrades TCAS 3000 Computer Units as shown in the list that follows :

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Summary (Cont)

Unit Part No. Before Modifica tion Unit Part No. After Modification

9003000

- 10001,

- 10002, or

- 10003 to 9003000

- 10004

9003000

- 55001,

- 55002, or

- 55003 to 9003000

- 55004

9003000

- 65001,

- 65002, or

- 65003 to 9003000

- 65004

Refer to Section 1.C on Page 5 for a list of the changes that are a part of new TCAS 3000 Product Software, Part No. 9000354

- 005

. NOTE: The work described in this Service Bulletin can be completed onboard the aircraft

or on a TCAS 2000 Manual Test Station (MTS)

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 REVIS ION HISTORY

This is the initial release of ATA Service Bulletin No. 9003000

- 34

- 6006 (ACSS Pub. No. 8008235

- 001 ).

Table 1

. Service Bulletin Revi sions

Revision Date of Release

Initial Release June 4, 2010

Revision 0 1 February 1, 2011

Revision 02 February 3, 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 stand ards.

1 Added Export Administration Regulations (EAR) statement.

5 Added Concurrent Requirement. HW Mod B must be done before or at the same time as this con version / modification

. 7

, 20

, 24 Removed Section L. Test Program information is available in other sections of the Service Bulletin or in the “Testing and Fault Is olation” section of the CMM

. Removed all references to test procedures/software that are included in the CMM . R eferred operators to the CMM.

12

, 33 Updated Table 4 to i nclude options for updating labels that have a 2D barcode and those that do not. Added new figure to non

- 2D barcode

- compatible tear

- off label.

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

15 Removed misplaced duplicate Warning.

18 Added note to make sure aircraft is on the ground during part number verification. Added Step m) to choose the applicable unit.

25 Added Table 8 to identify field names used for part number validation when the different tools are used.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Revision Page Change Made
1 (Cont.) 29 Added Figure 3 to show CVI Part Number Verification Tool

– Dialog Box. Updated Figure 4

. CVI Part Number Verification Tool

– Verification Window

. 2 5 Removed the first sentence in the first paragraph in Section 1.B

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 1. PLANNING INFORMATION

A. Effectivity This Service Bulletin is applicable to Part Numbers

, 9003000

- 1 0001,

- 10002, and

- 10003

, Part No. 9003000

- 55001,

- 55002, and

- 55003

, a nd Part No. 9003000

- 65001,

- 65002, and

- 65003

.

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

**•** ACSS Publication No. 800829 7

- 001 (ATA Service Bulletin No. 9003 0 00

- 34

- 000 3 )

– Installs an update to the TCAS 3000 Boot Code.

If a TCAS 2000 Manual Test Station (MTS) i s used to load the operational software, one of the Service Bulletins that follow must be done before or in conjunction with this Bulletin :

**•** Installation of Hardware Modification F is re quired

. Hardware Mod F replaces a Windows NT PC with a Windows XP PC o n the Manual Test Station (MTS). Refer to ATA Service Bulletin No. T336255

- 34

- 0006 ( ACSS Pub. No. 8007849

- 001 ).

**•** ACSS Publication No. 8007761

- 001 (ATA Service Bulletin No. 9003000

- 34

- 6004 ) which installs test program 9000949

- 001 for PC with Windows XP operating system.

C. Reason New Operational Software, Part No. 9000354

- 005 , incorporates updates to the Interference Limiting functionality. These updates improve t racking 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 3000 Computer Unit s ( CU ) to Part No. 9003000

- 10004

, - 55004 , or

- 65004

.

D. Description This Service Bulletin gives instructions for installing new Operational Software

, Part No. 9000354

- 005 , from Compact Flash (CF) card, Part No. 9300001

- 005F

, onboard the aircraft or by final Acceptance Test on a TCAS 2000 Manual Test Station (MTS)

. This Service Bulletin also includes instructions fo r installing a new software tear

- off label on the front of the unit to identify the new dash number.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 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

ma terials on an updated Product Identification Label is permitted. When this software upgrade is done at a n 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 / Authoriza tion Granted The content of this Service Bulletin is reviewed and approved by the FAA

. This Service Bulletin includes the information that follows:
(1) Gives TCAS 3000 unit modification instructions from the manufacture r. (2) Gives authorization for the installation and operation of the modified TCAS 3000 unit on aircraft as identified below:

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

.

9003000

- 10001,

- 10002, or

- 10003 to 9003000

- 10004

9003000

- 55001,

- 55002, or

- 55003 to 9003000

- 55004

9003000

- 65001,

- 65002, or

- 65003 to 9003000

- 65004

After completing this FAA

- approved modification, it is the responsibility of the aircraft operator to get “Return to Service” authorization, if necessary, from the applicable regulatory authorities.

G. Manpower
When the modification described in this Service Bulletin is done onboard the aircraft, approximately 0.5 work hours are necessary to complete the work. Approximately 0.5 work hours are necessary when the modification is done on a TCAS 2000 Manual Test Station (MTS)

. Approximate ly 1.0 work

- hour is necessary to complete Final Test of the unit using manual test procedures.

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

.

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

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 J. Software Ac complishment 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 Certificati on

.

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 :

**•** TCAS 3000 Computer Unit Component Ma intenance Manual (CMM), ACSS Pub. No. 8005744

- 001 (ATA No. 34

- 43

- 24) )

**•** TCAS 3000 System Description and Installation Manual (SDIM), ACSS Pub. No. 8003529

- 001 (ATA No. 34

- 43

- 23)

. 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: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 2. MATERIAL INFORMATION

A. Price and Availability
(1) Software License Agreement

New Product Software is necessary for the update described in this Service Bulletin. ACSS must be in possession of a completed ACSS Software License Agreement before it will ship an order

. A signed Software License Agreement is not usually necessary for software upgrades done at an ACSS Authorized Service Center. I f a copy of the Software is necessary , ACSS must be in possession of a completed Software License A greement before it will ship the Software.

If a current Software License Agreement is on file at ACSS, only an Addendum to this Agreement is necessary for this Software upgrade.
(2) Pricing and Availability

Refer to Section 2.C

, Table 4 on Page 12 for parts availability. Pricing for this Service Bulletin is available from :
ACSS Order Administration or ACSS Service Center

For contact information , refer to Paragraph 2.A(3)

, Placing an Order

. Pricing for this Service Bulletin is different for customers who use on

- board data loading or their own shop procedures to complete this upgrade. ACSS has different pricing for units that customers send to ACSS for this upgrade.

NOTE: 1. A shop Bench Test Fee is applicable for those units sent to ACSS for this Software upgrade and will be based on current catalog pricing.
NOTE: 2. Other repairs will be quoted separately. Plea se speak or write to an ACSS Customer Order Administrator for scheduling information before sending a unit for repair or modification

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 (3) Placing an Order

Use a standard Purchase Order (PO) form, or complete the ACSS Service Bulletin Materials Order Form (OA

- 009) shown on Page 10 . To expedite your order, include all of the information in the list that follows :

**•** A Purchase Order Number

**•** Reference to this Service Bulletin: ATA Service Bulletin No. 9003000

- 34

- 6006 (ACSS Pub No. 8008235

- 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

**•** Freig ht 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 t o give sufficient time for documentation validation and order preparation

. When sending units to an ACSS Service Center, send Purchase Orders to: Aviation Communication and Surveillance Systems (ACSS) Attn: Customer Order Administration 19810 N. 7th Ave Ph oenix, AZ 85027

- 4741 USA Phone: (623) 445

- 7030 Fax: (623) 445

- 7002

or e

- mail: acss.phxrepair@L

- 3com.com

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 

### ACSS SERVICE BULLETIN MATERIALS ORDER FORM

To secure the rights to use ACSS software, ACSS requires t he completion of a Software License Agreement and Appendix. If a current Software License Agreement exists with ACSS, the customer is only required to sign an Appendix to the Agreement for t he software being ordered. Based on the information in this order form, ACSS Order Administration will complete the Appendix and/or the Software License Agreement and forward it to the customer for signatures.
The Software License Agreement, or Appendix, must be signed and received by ACSS prior to shipment of the order.

ALL of the following information MUST be completed for ACSS to quickly and efficiently process this software order.

Customer Name * Customer Purchase Order Number Date

Unit Original Part Number Customer Contact Name Customer Contact Email Address

A/C Type Applicable ACSS Service Bulletin Pub. No. Price of Modification for each Unit

Unit Serial Number(s) Attach additional sheets as necessary to list all of the serial numbers being updated by this software order.

* This complet ed form may be used as the formal Purchase Order (PO) or may be used as an information sheet attached to the PO.

PARTS BEING ORDERED (as listed in the applicable Service Bulletin section, ‘Material Necessary for Each Component’ )

Part Number Description Qua ntity

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 Specia l 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: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 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 Technic al Newsletters are available at the ACSS Customer Services web site

. Go to : http://www.acsscustomerservices.com/CustomerServices

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 C. Material Necessary for Each Component
(1) Material to be Purch ased

The items listed in Table 4 below are necessary to complete this Service Bulletin.

Table 4

. Material to Be Purchased

New Part Number Keywo rd (Description) Former Part Number Qty. Instructions/ Disposition Parts Availability

9300001

- 005F New TCAS 3000 Operational Software ( Master Media ) See Table 9 on Page 25 A/N 1

, 2

, 4 August 5, 2011

Software Tear O ff Labels

9000820

- 014 TCAS 3000 , Label (for

- 10004 units )

N/A A/N 1

, 2

, 3

, 5

, 7 August 5, 2011 9000820

- 015 TCAS 3000 , Label (for

- 55004 units)

9000820

- 016 TCAS 3000 , Label (for

- 65004 units)

Software Tear Off Labels (2D Comp atible)

9000820

- 011 TCAS 3000 , Label (for

- 10004 units)

N/A A/N 1

, 2

, 3

, 6

, 7 August 5, 2011 9000820

- 012 TCAS 3000 , Label (for

- 55004 units)

9000820

- 013 TCAS 3000 , Label (for

- 65004 units)

A/N = As Necessary

INSTRUCTIONS/DISPOSITION

1. For correc t disposal of used parts, refer to FAA Best Practices document, Scrap or Salvageable Parts and Materials, local regulatory agency, or local Repair Station policy.

2. Make sure quantities are correct and verifiable.

3. Include a full list of serial numbers for the units to be modified to make sure you receive the correct identification plates.

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

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

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

7. Labels are made of white polyester material.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 (2) Material Supplied by the Op erator



### WARNING
BEFORE USING A MATERIAL, REFER TO THE MANUFACTURER’S MATERIAL SAFETY DATA SHEETS FOR SAFETY INFORMATION. SOME MATERIALS CAN BE DANGEROUS.



### CAUTION

DO NOT USE MATERIALS THAT ARE NOT EQUIVALENT TO MATERIALS SPECIFIED BY ACSS. MATE RIALS 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 S ervice Bulletin. Equivalent alternatives are permitted for items in the table

. Table 5 . Operator Supplied Material

Part/Specification Number Qty. Keyword

HAZARD CODE 130D A/N Solvent, isopropyl alcohol (99%)

- Optional

source

HA ZARD 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: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 F. Tooling
The items identified in Table 6 below are necessary to do the procedures in this Service Bulletin. Equivalent alternatives are permitted. If the work described in this Service Bulletin is done using a TCAS 2000 Manual Test Station (MTS) , also refer to Section 1.B

, Concurrent Requirements , on Page 5

. Table 6

. Tooling

Part/Specification Number Qty. Description

Method 5

– Part Number Verification with Compact Flash Card and PC

Ope rator

- 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 2

– Part Number Verification with Remote ACSS VSI/TRA display

200F

- 00083 1 Adapter Cable

OR

Method 4

– Part Number Verification with ACSS CVI Part Numb er 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

- 003 1 Software Configuration Fi le for TCAS 3000 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 Mat erials, 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 i nformation, refer to Section 2.A

, Price and Availability , starting on Page 8

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 3. ACCOMPLISHMENT INSTR UCTIONS

A. General Information



### CAUTION

ALL DISASSEMBLY AND MODIFICATI ON PROCEDURES MUST BE COMPLETED AT AN ANTISTATIC WORKSTATION

. REFER TO ESTABLISHED ANTISTATIC PROCEDURES.



### CAUTION

THIS EQUIPMENT CONTAINS MOISTURE SENSITIVE PARTS. SPECIAL HANDLING IS NECESSARY.

NOTE: 1. The Paragraphs, Items, Tables, and/or Figure numbers given in this Service Bulletin can be found in one of the two manuals in the list below:

**•** TCAS 3000 System Desc ription and Installation Manual (SDIM), ACSS Pub. No. 8003529

- 001 (ATA No. 34

- 43

- 23)

.

**•** TCAS 3000 Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8005744

- 001 (ATA No. 34

- 43

- 24)

. NOTE: 2. Before doing the work in this Service Bulletin, make sure you can read the TCAS 3000 CU software part numbers from a maintenance connection

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 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 27 and choose a method for implementation of th is u pgrade

. (2) Examine the installed TCAS 3000 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 an d new software part numbers

, r efer to the tables st arting on Pages 25

.


### CAUTION

MAKE SURE THE AIRCRAFT HAS GEAR DOWN AND “WEIGHT ON WHEELS” DURING PART NUMBER VERIFICATION OR WHILE REPROGRAMMING THE TCAS 3000 CU ONBOARD THE AIRCRAFT.



### CAUTION

DO NOT START A TCAS SYSTEM POWER CYCLE WHILE YOU ARE REPROGRAMMING THE CU

. T HIS 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 Extended Test Mode is available only on the ground with the transponder i n 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 t o the FAULT ISOLATION section of the TCAS 3000 System Description and Installation Manual (SDIM), ACSS Pub. No. 8003529

- 001 (ATA No. 34

- 43

- 23)

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 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 )

.

Method 2

Software Verification with a R emote ACSS VSI/TRA display

. NOTE: 1. This method is valid ONLY if an ACSS VSI/TRA is used.
NOTE: 2. The external VSI method will not work if pin RMP 12C (Honeywell BCA EFIS output format) is grounded as part of the aircraft in stallation.
NOTE: 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 t est mode, connect the VSI/TRA to the J1 front connector on the TCAS 3000 CU with an adapter cable (Part No. 200F −00083). See Figure 2 on Page 28

. a) Push and hold the self

- test button on the controller for 8 seconds or longer.
b) Make sure the installed software part numbers agree with the part numbers in Table 9 ( Installed Software Part Numbers Before This Modification ) or Table 10 ( Installed Software Part Numbers After this Modification )

.

Method 3

Software Verification with the CFDS (Central F ault Display System) or CMC (Central Maintenance Computer) type maintenance programs. If the aircraft is equipped with an OMS (Onboard Maintenance System), the aircraft’s CFDS or CMC can be used to display fault information, including the current version o f the operating software. Use the aircraft

- specific AMM (Aircraft Maintenance Manual) and refer to the OMS program. If you us e this method to verify the initial operating software part number, check that the part numbers displayed match the part numbers l isted in Table 9 on Page 25 . If you are verifying the newly installed software, refer to Table 10 on Page 26 for part numbers.

NOTE: Fault data is ac cessible only when the aircraft is on the ground.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Method 4

Software Verification with CVI Part Number Verification Tool

. NOTE: Before starting verification, make sure that the aircraft is on the ground and that the unit under test is set to ground mode.
a) Acquir e a copy of the CVI Part Number Verification Tool, Part No. 9001089

- 001

, and Configuration File, Part No. 9000903

- 003 from ACSS Order Administration

. Refer to Note 3 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 3000 CU

. d) Connect the RS

- 232 cable from the PC (9

- pin connector) to the J1 front connector (53

- pin connector) on the TCAS 3000 CU.
e) Apply power to the TCAS 3000 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 ” on the appli cable drive

. h) Put the CD that contains Configuration File

, Part No. 9000903

- 003 , into the CD drive.
i) Use standard Windows procedures to copy the configuration text (.ini) file from the CD into directory 

### C : \ 900 1089

. j) Eject the CD.
k) Put the CVI Part Number Verification Tool disk, Part No. 9001089

- 001 , into the CD drive

. Result: The program will run automatically and open the testexec window.

NOTE: If the program fails to load, go to Start => Run

. You can type D: \ 900108 9.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, TCAS 3000

. See Figure 3 on Page 29

. Result: The LabWindows/CVI Test Executive 9001089 window opens.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 n) Choose the applicable part number from the Select P/N dropdown menu and click Start

. See Figure 4 on Page 29

. 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 s a PASS/FAIL indication.
o) Do a check to m ake sure the installed software part numbers a gree 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 5

Software Verification with a Standalone PC with an installed or connected CF Card Read/Write Drive and a blank CF card.
a) Get a header file from ACSS Customer Services. Refer to Note 3 in Table 6 on Page 14 for contact information.
b) Make a copy of the header file and write it to the blank CF card.

NOTE: R efer to the CF Read/Write Drive manufacturer’s operating instructions.
c) Op en the CF card protective door on the front panel of the TCAS 3000 CU

. See Figure 5 on Page 30

. 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 extinguishes 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 a nd close the CF card protective door.
f) Start the PC and put the CF card into the CF card reader. Refer to the manufacturer’s instructions to see the card’s contents.

**•** A text file ( 

### LOG.OUT ) shows on the display

. g) Use a text editor (Microsoft® Word or WordPad) to open the text file and

see part numbers for the newly installed software

. Refer to Table 8 on Page 25 for header file field names.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 h) Do a check to m ake sure the installed software part numbers agre e 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 6 If an upgraded TCAS 2000 Manual Test Station (MTS) 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 TCAS 3000 Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 80 05744

- 001 (ATA No. 34

- 43

- 24) for test procedure information

.

C. Disassembly/Inspection/Removal
No disassembly necessary

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 D. Modification Procedures

– Onboard 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 on Page 25 for a list of Initial Software Part Numbers.
Use the proce dure that follows to install the software from a CF (Compact Flash) card to the TCAS 3000 CU installed on the aircraft.

NOTE: Before uploading the software , make sur e that the aircraft is on the ground

. This software cannot be uploaded while the aircraft is airborne.
(1) Procure new TCAS 3000 Master Media CF C ard , Part No. 9300001

- 005F

. (2) Apply power to the TCAS 3000 CU

. W ait until all LEDs are extinguished.
(3) Open the CF card protective door on the front panel of the unit. See Figure 5 on Page 30

. NOTE: Hold the TCAS 3000 Master Media CF card with the ACSS product label pointing to the left side of the unit and the manufacturer’s label (with barcode) pointing to the right (i.e., in the direction of the front panel LEDs).
(4) Put the CF card into the slot

. NOTE: DO NOT FORCE THE CARD INTO THE CU

. Result: If the CF card is put into the CU correctly, a ll LEDs will illuminate and the TCAS 3000 CU will restart

. (5) Monitor the LEDs on the front panel while the new product software uploads from the CF card

. The LEDs will continue to cycle until all of the software files on the CF card are loaded onto the TCAS 3000 CU

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Table 7

. Software Installation LED Display

LED Display What it means

All LEDs come on

. The TCAS 3000 CU is restarting.

Al l LEDs go off and the XFER IN PROCESS LED blinks. The TCAS 3000 CU is reading the CF card.

The XFER IN PROCESS LED is continuous green

. The TCAS 3000 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 TCAS 3000

. 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 LE D 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 CU and remove the card.
(9) Close the CF card protective door.

Result: All LEDs come on and the TCAS 3000 CU restart s

. (10) When all LEDs go off

, the unit is ready

. (11) 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

. (12) R emove power from the TCAS 3000 CU and disconnect all PC Interface cable connection s.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 E. Return to Service
Use the System Self −Test procedures referred to in the ADJUSTMENT/TEST System Self

- Tests section of the TCAS 3000 System Description and Installat ion Manual (SDIM), ACSS Pub. No. 8003529

- 001 (ATA No. 34

- 43

- 23)

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

F. Identification Label Update

– Onboard the Aircraft or On a Bench System



### WARNING WHEN HANDLING SOLVENTS, MAKE SURE THERE IS SUFFICIENT VENTILATION IN THE WORK AREA. USE APPLICABLE PRECAUTIONS TO PREVENT INHALATION OF VAPORS AND EXPOSURE OF FUMES TO FLAME.

After you are sure that installation of the new product software was successful, use the applicable procedure below to update the identification label(s) on the TCAS 3000 CU

. The new TCAS 3000 P art No’ s will be 9003000

- 10004

, - 55004 , or

- 65004

. (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

9003000

- 10004 9000820

- 011 9000820

- 014

9003000

- 55004 9000820

- 012 9000820

- 015

9003000

- 65004 9000820

- 013 9000820

- 016

NOTE: Some CU s 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
pe rmitted.
(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 7 and Figure 8 on Page 32

. (3) Keep the label you removed in Step (2) above

. Refer to local policy for correct disposal instructions

. (4) Carefully cl ean 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 correct 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: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 G. Modification Procedures

– At Service Center with a TCAS 2000 MTS

When a TCAS 2000 Manual Test Station (MTS) is used to install n ew 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 TCAS 3000 Com puter Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8005744

- 001 (ATA No. 34

- 43

- 24) for test procedure information

. (2) During functional testing, use the procedures and instructions in the TCAS 3000 CMM to complete the software modificati on described in this Service Bulletin.

Refer to the Acceptance Test Procedure for TCAS 3000 , ACSS Pub. No. 8002217

- 001 , Appendix A, for software loading procedures

H. Identification Label Update

- At an ACSS

- Authorized Service Center
If the work described in this Service Bulletin is done at an ACSS

- Authorized Service Center, the full Product Identification Label can be replaced to show the new part number.

NOTE: Full Product Identification Labels can only be installed at an ACSS

Authorized Service Center. All other Service Centers must obey the instructions in Section 3.F ( Identification Label Update

– Onboard the Aircraft or On a Bench System ) on Page 23 to update existing Product Identification Labels. Identify and examine the Identification Labels on the front of the TCAS 3000 CU

. Choose one of the steps below to update the Product Identification Label:
(1) If replacement of the full Product Identification Label is necessary, refer to the TCAS 3000 Computer Unit Component Maintenance Manual (CMM), ACSS Pub. No. 8005744

- 001 (ATA No. 34

- 43

- 24)

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

– Onboard the Aircraft or On a Bench System ) on Page 23 to update Product Identification Labels. See Figure 7 on Page 32 for reference

. (3) If the label includes a 2D barcode, use ACSS Pub. No. 8007621

- 0 01 (ATA Service Bulletin No. 9003000

- 34

- 0002 ) to replace the entire Product Identification Label with the new ACSS 2D barcode label. See Figure 8 on Page 32

. This completes the upgrade of TCAS 3000 CU

, Part No. 9003000

- 10001,

- 10002, and

- 10003

, Part No. 9003000

- 55001,

- 55002, and

- 55003

, a nd Part No. 9003000

- 65001,

- 65002, and

- 65003 to 9003000

- 10004

, - 55004 , or

- 65004

.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Table 8

. Field Reference Table for Part Number Verification

Software Field Names Method 5 LOG.OUT Header File See Note below. Method 4 CVI Tool See Note below.

OP I Software Application Software Appl Software P/N

P1 Data Loader Data Loader Copy 1 Data Load Copy 1 P/N

IO FPGA I / O FPGA Copy 1 IO FPGA Copy 1 P/N

RF FPGA RF FPGA RF FPGA 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 us e can communicate with the LRU . It is not necessary to do a verification of every part number when doing this step.

Table 9

. Installed Software Part Numbers Before This Modification

Affected Part No. 9003000 - 10001

- 55001

- 65001 - 10002

- 55002

- 65002 - 10003

- 55003

- 65003

Master Media Part No. 9300001

- 002F 9300001

- 003F 9300001

- 004F

Field Names Part Number

OP I Software 9000354

- 001 9000354

- 002 9000354

- 003

P1 Data Loader 9000355

- 001 90 00355

- 001 9000355

- 001

IO FPGA 9003025

- 001 9003025

- 001 9003025

- 001

RF FPGA 9003026

- 002 9003026

- 002 9003026

- 002

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Table 10

. Installed Software Part Numbers After this Modification

Affected Part No.

- 10004

, - 55004 , or

- 65004

Master Media Part No. 9300001

- 005F

Field Names Part Number CRC

OP I Softwar e 9000354

- 005 D 233397C

P1 Data Loader 9000355

- 001 CBA53

IO FPGA 9003025

- 001 E4D78D

RF FPGA 9003026

- 002 A2260964

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Figure 1

. TCAS 3000 CU Decision Chart

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Figure 2

. Remote VSI/TRA to TCAS 3000 CU Interconnect TCAS 3000 Compute r Unit

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Figure 3

. CVI Part Number Verification Tool

– Dialog Box

Figure 4

. CVI Part Number Verification Tool

– Verification Window Click TCAS 3000

Choose the applicable end item part number from the drop

- down list.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Figure 5 : Compact Flash Card Or ientation for TCAS 3000 CU CF Manufacturer’s Label (with barcode) Front Panel LEDs

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

Card Ejector button

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Figure 6 . Location of Compact Flash Card Ejector Eject Button

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Figure 7

. Exam ple of a TCAS 3000 Computer Unit 6MCU Label ( Without 2D Barcode)

Figure 8

. Example of a TCAS 3000 Computer Unit 6MCU Label (With 2D Barco de) Remove only the bottom part of the original Product I D 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 Install new software tear

- off label below original Product ID label.

# Service Bulletin

Release Date: June 4, 2010 ATA Service Bulletin No

. 9003000

- 34

- 6006 Revision 02 : February 3, 2011 ACSS Pub lication No. 8008235

- 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 33 Figure 9

. Example of a Software Tear

- Off Label for the

TCAS 3000 Compute r Unit (2D Barcode Compatible)

Figure 10

. Example of a Software Tear

- Off Label f or the TCAS 3000 Compute r Unit Before installing the new software
tear

- off label, make sure the new dash number is

– XX004

.

Before installing the new software
tear

- off label, make sure the new dash number is

– XX004

.