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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 34

TITLE: NAVIGATION - GENERAL - REPLACE THE THIRD THALES PITOT

PROBE BY A GOODRICH PITOT PROBE

MODIFICATION No.: 151182P18009

This page transmits Revision No.01 of Service Bulletin No.A320-34-1463

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 01 issued to add aircraft MSN 2445 for operator ANZ.

CHANGES

SUMMARY

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

CONCURRENT REQUIREMENTS CONCURRENT REQUIREMENTS UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

CONCURRENT REQUIREMENTS CONCURRENT SB LIST UPDATED R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

APPROVAL APPROVAL UPDATED R

FILLING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

REVISION No.: 01 - May 15/12 Page: 1

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REVISION TRANSMITTAL SHEET

HISTORY OF PREVIOUS REVISIONS

No previous revision

REVISION SEQUENCE

ORIGINAL: Mar 09/10

REVISION No. : 01 - May 15/12

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

REVISION No.: 01 - May 15/12 Page: 2

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SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

ATA SYSTEM: 34

TITLE: NAVIGATION - GENERAL - REPLACE THE THIRD THALES PITOT

PROBE BY A GOODRICH PITOT PROBE

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 151182P18009

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

This Service Bulletin is issued further to an operator’s request.

This Service Bulletin replaces the THALES pitot probe 9DA2, PN C16195BA, by a GOODRICH pitot

probe PN 0851HL, on the F/O side.

Accomplishment of this Service Bulletin will satisfy the operator’s request.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE OPTIONAL (1) CANCELS INSPECTION SB NO

POTENTIAL AD NO A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin for convenience or option.

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SUMMARY

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB Pitot Probe

EFFECTIVITY

This Service Bulletin is applicable to this (these) operator(s) :

AFR ANZ SBI UDC

NOTE: This Service Bulletin is written for the operators listed above. The modification in this

Service Bulletin can be done by other operators. If other operators want to do this

modification, use the RFC/RMO procedure and write to :

AIRBUS

CUSTOMER SERVICES DIRECTORATE

SC Department

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

CONCURRENT REQUIREMENTS

For MSN 0044 0061 0063 0102 0115 0144-0145 0155 0186-0187 0214 0227 0235-0237 0239 0270

0278 0285-0287 0337 0352 0377 0491 0498 0509 0521 0529 0544 0598 0600 0608 0618 0625 0637

0777 0796 0938 0985 0998 1000 1020 1025 1036 1133 1151 1169 1176 1190 1201 1216 1267 1271

1299 1344 1404 1415 1444 1449 1471 1476 1502 1505 1524 1616 1622 1640 1645 1658 1677 1691

1699 1733 1859 1873 1879 1885 1894 1900 1924 1938 1949 2035 2059 2071 2081 2100 2109 2140

2213 2228 2279 2317 2344 2350 2445 2456 2582 2601 2686 2705 2716 2721 2750 2918 2938 2951

2961 2967 2972 3008-3009 3051 3065 3098 3372 3399 3401 3419-3420 3441 3470 3777 3795 3814

3825 3859 3884 3930 4063 4084 4105 4137 4139

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin(s):

Service Bulletin No. A320-34-1456

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

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SUMMARY

HARD YES

SOFT NO

OBRM NO

MANPOWER

Task 341463-831-801-001: Modification

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

APPENDICES

None

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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SUMMARY

This Page Intentionally Left Blank

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 34

TITLE: NAVIGATION - GENERAL - REPLACE THE THIRD THALES PITOT

PROBE BY A GOODRICH PITOT PROBE

MODIFICATION No.: 151182P18009

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the

property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with

any information contained in it. It is delivered on the express condition that said document and the

information contained in it shall be treated as confidential, shall not be used for any purpose other than

that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall

not be duplicated in any manner (except for the purposes of performing the tasks described hereunder

and provided that any recipient of such document shall comply with the conditions herein), without

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

(1) Models

318-111 319-111 319-113 319-115 320-211 320-212 320-214 320-232

321-111 321-211 321-212

(2) Effectivity by MSN

0044 0061 0063 0102 0115 0144-0145 0155 0186-0187 0214 0227 0235-0237 0239

0270 0278 0285-0287 0337 0352 0377 0491 0498 0509 0521 0529 0544 0598 0600

0608 0618 0625 0637 0777 0796 0938 0985 0998 1000 1020 1025 1036 1133 1151

1169 1176 1190 1201 1216 1267 1271 1299 1344 1404 1415 1444 1449 1471 1476

1502 1505 1524 1616 1622 1640 1645 1658 1677 1691 1699 1733 1859 1873 1879

1885 1894 1900 1924 1938 1949 2035 2059 2071 2081 2100 2109 2140 2213 2228

2279 2317 2344 2350 2445 2456 2582 2601 2686 2705 2716 2721 2750 2918 2938

2951 2961 2967 2972 3008-3009 3051 3065 3098 3372 3399 3401 3419-3420 3441

3470 3777 3795 3814 3825 3859 3884 3930 4063 4084 4105 4137 4139

(3) Effectivity by Operator

The Operator/MSN relationship is provided for information only and is correct at the time

of issue in accordance with the information available to AIRBUS. Any future changes

resulting from transfer of an aircraft from one operator to another will not be reflected in

this list unless the Service Bulletin is revised for another reason.

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OPERATOR MSN

AFR 0044 0061 0063 0102 0115 0144 0145 0155 0186 0187 0214 0227

0236 0237 0239 0270 0278 0285 0286 0287 0337 0352 0377 0491

0498 0509 0521 0529 0544 0598 0600 0608 0618 0625 0637 0777

0796 0938 0985 0998 1000 1020 1025 1036 1133 1151 1169 1176

1190 1201 1216 1267 1271 1299 1344 1404 1415 1444 1449 1471

1476 1502 1505 1524 1616 1622 1640 1645 1658 1677 1691 1699

1733 1859 1873 1879 1885 1894 1900 1924 1938 1949 2035 2059

2071 2081 2100 2109 2140 2213 2228 2317 2344 2350 2456 2582

2601 2686 2705 2716 2721 2750 2918 2938 2951 2961 2967 2972

3008 3009 3051 3065 3098 3372 3399 3401 3419 3420 3441 3470

3777 3795 3814 3825 3859 3884 3930 4063 4084 4105 4137 4139

ANZ 2445

SBI 2279

UDC 0235

(4) Configuration by MSN

MSN CONFIGURATION

0044 0061 0063 0102 0115 0144 0145 0155 0186 0187 0214

0227 0235 0236 0237 0239 0270 0278 0285 0286 0287 0337

0352 0377 0491 0498 0509 0521 0529 0544 0598 0600 0608

0618 0625 0637 0777 0796 0938 0985 0998 1000 1020 1025

1036 1133 1151 1169 1176 1190 1201 1216 1267 1271 1299

1344 1404 1415 1444 1449 1471 1476 1502 1505 1524 1616

1622 1640 1645 1658 1677 1691 1699 1733 1859 1873 1879

1885 1894 1900 1924 1938 1949 2035 2059 2071 2081 2100

2109 2140 2213 2228 2279 2317 2344 2350 2445 2456 2582

2601 2686 2705 2716 2721 2750 2918 2938 2951 2961 2967

2972 3008 3009 3051 3065 3098 3372 3399 3401 3419 3420

3441 3470 3777 3795 3814 3825 3859 3884 3930 4063 4084

4105 4137 4139

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

B. CONCURRENT REQUIREMENTS

For MSN 0044 0061 0063 0102 0115 0144-0145 0155 0186-0187 0214 0227 0235-0237

0239 0270 0278 0285-0287 0337 0352 0377 0491 0498 0509 0521 0529 0544 0598 0600

0608 0618 0625 0637 0777 0796 0938 0985 0998 1000 1020 1025 1036 1133 1151 1169

1176 1190 1201 1216 1267 1271 1299 1344 1404 1415 1444 1449 1471 1476 1502 1505

1524 1616 1622 1640 1645 1658 1677 1691 1699 1733 1859 1873 1879 1885 1894 1900

1924 1938 1949 2035 2059 2071 2081 2100 2109 2140 2213 2228 2279 2317 2344 2350

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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2445 2456 2582 2601 2686 2705 2716 2721 2750 2918 2938 2951 2961 2967 2972

3008-3009 3051 3065 3098 3372 3399 3401 3419-3420 3441 3470 3777 3795 3814 3825

3859 3884 3930 4063 4084 4105 4137 4139

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of

the following Service Bulletin(s):

Service Bulletin No. A320-34-1456

C. REASON

(1) History

This Service Bulletin is issued further to an operator’s request.

(2) Objective/Action

This Service Bulletin replaces the THALES pitot probe 9DA2, PN C16195BA, by a

GOODRICH pitot probe PN 0851HL, on the F/O side.

(3) Advantages

Accomplishment of this Service Bulletin will satisfy the operator’s request.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 341463-831-801-001: Modification

(1) Replace the pitot probe 9DA2

E. COMPLIANCE

(1) Classification

OPTIONAL: Service Bulletin for convenience or option.

(2) Accomplishment Timescale

In accordance with operators’ maintenance schedule.

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organization Approval No. EASA.21J.031.

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

Task 341463-831-801-001: Modification

Get Access 0.50

On Aircraft

Replace the pitot probe 9DA2 0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 12-34-24 34-11-15

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-55-00

Service Bulletin (SB) A320-34-1456

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

Illustrated Parts Catalog (IPC) 34-11-01 34-11-15

L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Probe-Pitot C16195BA 0851HL 03 Not

Applicable

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NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

M. SPARES

Probe-Pitot C16195BA

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Equipment BFEA01 Vendor parts are to be purchased from :

ROSEMOUNT AEROSPACE INC

DBA GOODRICH SENSOR SYSTEMS DIV.

14300 JUDICIAL ROAD

MN 55306-4890 BURNSVILLE

USA

(2) Price and Availability

Sales terms must be agreed between the Customer and AIRBUS in accordance with the

RFC (or RFC/RMO) procedure.

B. INDUSTRY SUPPORT INFORMATION

Refer to the paragraph: ’Price and Availability’.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

None

(3) Equipment

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE

NOTES

0851HL 1 PROBE C16195BA 03

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

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F. TOOLING

None

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 341463-831-801-001 - Modification

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC. AS

NECESSARY ON WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

Task Associated Data

Zone

120

Modified FIN

9DA2

Access

Door 822

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

A. GENERAL

(1) Subtask 341463-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

(a) Write in the applicable aircraft records that you have done all the work given in this

Service Bulletin.

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B. PREPARATION

(1) Subtask 341463-941-001-001 - External preparation

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

(a) Make sure that the aircraft is electrically grounded (Refer to AMM Task

12-34-24-869-002).

(2) Subtask 341463-941-002-001 - Preparation Procedure

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-15-000-001

(a) Do the preparation procedure as specified in the removal of the pitot probe (9DA2)

(Refer to AMM Task 34-11-15-000-001).

C. PROCEDURE

(1) Subtask 341463-831-001-001 - Replace the pitot probe 9DA2

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

0851HL 1 PROBE

References

Aircraft Maintenance Manual (AMM) Task 34-11-15-000-001

Task 34-11-15-400-001

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(a) Remove :

(Refer to AMM Task 34-11-15-000-001)

FIN 9DA2

1 Probe-Pitot C16195BA

(b) Install :

(Refer to AMM Task 34-11-15-400-001)

FIN 9DA2

1 Probe-Pitot 0851HL

D. TEST

(1) Subtask 341463-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-15-400-001

(a) Do the test after the installation of the pitot probe (9DA2) (Refer to AMM Task

34-11-15-400-001).

E. CLOSE-UP

(1) Subtask 341463-942-001-001 - Close-up Procedure

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 34-11-15-400-001

(a) Make sure that the work areas are clean and clear of tools and other items of

equipment.

(b) Do the close-up procedure as specified in the installation of the pitot probe (9DA2)

(Refer to AMM Task 34-11-15-400-001).

(c) Restore the systems and the aircraft to normal operating condition.

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REPORTING SHEET

TITLE: NAVIGATION - GENERAL - REPLACE THE THIRD THALES PITOT

PROBE BY A GOODRICH PITOT PROBE

MODIFICATION No.: 151182P18009

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Mar 09/10 SERVICE BULLETIN No.: A320-34-1463

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