@A318/A319/A320/A321

SERVICE BULLETIN

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: 35

TITLE: MULTIPROG - CREW OXYGEN - INSPECTION OF OXYGEN PIPE FOR

CORROSION

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Some production oxygen pipe assemblies located within the crew oxygen distribution system have been

found to be affected by internal corrosion.

The potentially corroded oxygen pipe assembly is installed at the end of the Right Hand (RH) crew

distribution line just upstream of the First Officer and RH Observer oxygen mask boxes.

This condition could lead to no or insufficient oxygen supply to one flight crew member since corrosion

particles may obstruct the crew oxygen mask filter and could under some conditions lead to an increase

of the fire risk.

As the affected batches of oxygen pipes have been identified, this Inspection Service Bulletin details the

work required to check all the potentially impacted aircraft for corrosion and to replace the pipe if

necessary.

Accomplishment of this Inspection Service Bulletin permits:

- determining if the pipe is part of the affected batches of potentially corroded pipes,

- replacing it if necessary.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED YES PAX COMFORT AFFECTED YES

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational

disruptions.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Component COMPA01 1 See SB PIPE

Component COMPA02 1 See SB WASHER, RING

EFFECTIVITY

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

ABY AFL AFR ALK AVA AXM AZA BER C2C CCA CEB CES CHH

CQH CRK CSC DKH DLH ETD EZY FHY FLI GAP GFA GMI GOW

IGO JBU JJP JST LAN NKS NLY PAL QTR RJA SBI SFJ SLK

SVA SWR TAI TAM TGW THY TNA VOI VRD WZZ

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 351069-832-848-001: Inspection

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

APPENDICES

Appendix 01: Inspection Report

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

**CONF ALL

A

Z125 Z126 − 

PIPE TO BE INSPECTED

A

FR9

FR11

FR13

N_SB_351069_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 3

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 4

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

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: 35

TITLE: MULTIPROG - CREW OXYGEN - INSPECTION OF OXYGEN PIPE FOR

CORROSION

MODIFICATION No.: None

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

319-111 319-112 319-115 319-133 320-214 320-216 320-232 320-233

321-211 321-231 321-232

(2) Effectivity by MSN

4987 4997 5013-5014 5022 5032 5039 5041-5042 5045 5047 5049-5050 5052-5060

5062-5065 5067-5070 5072-5081 5083-5090 5092-5096 5099 5101-5109 5111-5120

5122-5130 5132-5138 5140 5143-5144 5146 5148

(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.

OPERATOR MSN

ABY 5143

AFL 5059

AFR 5084 5129

ALK 5086

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

OPERATOR MSN

AVA 5057 5119

AXM 5137

AZA 5130

BER 5126 5133

C2C 5088

CCA 4997 5014 5032 5054 5124

CEB 5045 5067

CES 4987 5047 5053 5063 5135 5136 5144

CHH 5105 5117

CQH 5022 5108

CRK 5072 5114

CSC 5041

DKH 5013 5070

DLH 5049 5087 5122

ETD 5095

EZY 5052 5056 5064 5104 5111 5113 5116 5138 5146

FHY 5096

FLI 5079

GAP 5103

GFA 5074

GMI 5085

GOW 5112

IGO 5076 5080 5090 5092 5094

JBU 5060 5148

JJP 5093

JST 5039

LAN 5125

NKS 5042 5132

NLY 5115

PAL 5081 5140

QTR 5078 5127

RJA 5099 5128

SBI 5106 5134

SFJ 5102

SLK 5050 5089

SVA 5065

SWR 5069

TAI 5068

TAM 5101 5107 5109

TGW 5073 5120

THY 5077 5083 5118

TNA 5055

VOI 5062

VRD 5058

WZZ 5075 5123

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

4987 4997 5013 5014 5022 5032 5039 5041 5042 5045 5047

5049 5050 5052 5053 5054 5055 5056 5057 5058 5059 5060

5062 5063 5064 5065 5067 5068 5069 5070 5072 5073 5074

5075 5076 5077 5078 5079 5080 5081 5083 5084 5085 5086

5087 5088 5089 5090 5092 5093 5094 5095 5096 5099 5101

5102 5103 5104 5105 5106 5107 5108 5109 5111 5112 5113

5114 5115 5116 5117 5118 5119 5120 5122 5123 5124 5125

5126 5127 5128 5129 5130 5132 5133 5134 5135 5136 5137

5138 5140 5143 5144 5146 5148

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

Component COMPA01 1

Component COMPA02 1

Consumable CMLA01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Some production oxygen pipe assemblies located within the crew oxygen distribution

system have been found to be affected by internal corrosion.

The potentially corroded oxygen pipe assembly is installed at the end of the Right Hand

(RH) crew distribution line just upstream of the First Officer and RH Observer oxygen

mask boxes.

This condition could lead to no or insufficient oxygen supply to one flight crew member

since corrosion particles may obstruct the crew oxygen mask filter and could under

some conditions lead to an increase of the fire risk.

(2) Objective/Action

As the affected batches of oxygen pipes have been identified, this Inspection Service

Bulletin details the work required to check all the potentially impacted aircraft for

corrosion and to replace the pipe if necessary.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 3

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(3) Advantages

Accomplishment of this Inspection Service Bulletin permits:

- determining if the pipe is part of the affected batches of potentially corroded pipes,

- replacing it if necessary.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 351069-832-848-001: Inspection

(1) Inspect the Crew Oxygen Pipe between FR 9 and FR 13.

(2) Flush the affected parts with nitrogen and replace the Crew Oxygen Pipe.

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available but within 7500 Flight Hours (FH) or 2 years

after issuance of this Inspection Service Bulletin.

This Service Bulletin has been classified Recommended. It is expected that an

Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA)

will be issued to change this classification to Mandatory. It is anticipated that the AD will

confirm the 7500 Flight Hours (FH) or 2 years given above but reference should be

made to the AD for confirmation of the mandated accomplishment timescale.

F. APPROVAL

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

Organisation Approval No. EASA.21J.031.

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.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 4

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

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 351069-832-848-001: Inspection

Get Access 0.50

On Aircraft

Inspect the Crew Oxygen Pipe between FR 9 and FR

13.

0.50

Flush the affected parts with nitrogen and replace the

Crew Oxygen Pipe.

3.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-53

12-34-24 20-21-11 35-00-00

35-10-00 35-12-41 52-10-00

52-41-00

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-42-00 51-43-00 51-75-12

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 5

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 6

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Component COMPA01 AIRBUS Material, Logistics and Suppliers

IFD - In Flight Desk

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 4012

For ordering by E-mail:

ifd.spares@airbus.com

AIRBUS Material, Logistics and Suppliers do not stock standard hardware as competitive

multiple suppliers ensure access to minimum prices AIRBUS recommends Customers

with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to

B/E Aerospace. The address is:

Component COMPA02 B/E AEROSPACE INC

CONSUMABLES MANAGEMENT

10000 NW 15th Terrace Miami

FL 33172

USA

Tel EMEA: +49 (0) 40 822 285 31500

Tel US: +1 305 925 2600

Tel ASIA: +1 310 900 1300

Fax EMEA: +49 (0) 40 822 285 31010

Fax US: +1 305 507 7191

Fax ASIA: +1 310 819 1200

SITA: MIAMMCR

E-Mail: AOGdesk_CMG@beaerospace.com

internet: http://www.beconsumables.com

or, alternatively any other source on the open

market.

(2) Price and Availability

No AIRBUS kit will be provided.

Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be

purchased by a spares purchase order.

Operator supplied standard hardware parts required to accomplish this Service Bulletin

are to be supplied from the Operator’s stock.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 7

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will not provide industry support for accomplishment of this Service Bulletin.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Nitrogen,(gaseous) 19-014 As required

(2) Components

Component COMPA01

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

NOTES

1 D3511032000640 1 PIPE (1) D3511032000640

NOTE: The above list of components is not an AIRBUS kit, the required parts

shall be ordered as necessary through the given channel.

Component COMPA02

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

NOTES

3 AN960C816 1 WASHER

5 NSA835070-5C 6 RING

7 NSA935401-05 5 TIE

NOTE: If you find part numbers of hardware components in the related kit(s)

which you cannot identify in the LIST OF COMPONENTS of this Service

Bulletin, refer to Standards Manual (SM). The SM will give you the

correct part number to part number relationship.

NOTE: The above list of components is not an AIRBUS kit, the required parts

shall be ordered as necessary through the given channel.

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 8

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

F. TOOLING

None

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 9

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 10

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 351069-832-848-001 - Inspection

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: KEEP ALL HYDROCARBONS (FUELS, LUBRICANTS, ETC.) AWAY FROM ALL

SOURCE OF OXYGEN. OXYGEN BECOMES EXPLOSIVE WHEN IT TOUCHES

HYDROCARBONS.

WARNING: CLEAN THE TOOLS AND MAKE SURE YOUR HANDS ARE CLEAN TO

PREVENT CONTAMINATION OF THE OXYGEN SYSTEM.

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.

NOTE: The purpose of flow charts is to supplement the information given in the Procedure

and Compliance paragraphs and not to serve as the primary source for tasks or

compliance times given in this Service Bulletin.

Task Associated Data

Zone

120 210

Modified FIN

5765HM 5766HM

Access

Door 812 831 841

Manpower

TOTAL MANHOURS 5.50

ELAPSED TIME (HOURS) 5.50

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 11

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

A. GENERAL

(1) Subtask 351069-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001

06-31-53, Page Block 001

Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-42-00

51-43-00

51-75-12

(a) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.

(c) To torque tighten the standard threaded fasteners, refer to AMM Task

20-21-11-911-001.

(d) Obtain alternative and substitute fasteners data, in accordance with SRM 51-43-00.

(e) Renew the protective finish in accordance with refer to SRM 51-75-12.

(f) Remove and install fasteners in accordance with SRM 51-42-00.

(2) Subtask 351069-839-001-001 - 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.

B. PREPARATION

(1) Subtask 351069-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

Task 52-10-00-010-001

Task 52-41-00-010-002

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

12-34-24-869-002.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 12

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(b) Put the access platform(s) in position at the passenger/crew door(s) 831 or 841 and

at the avionics compartment door 812.

(c) Open the passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page Block

001 and AMM Task 52-10-00-010-001.

(d) Open the avionics compartment door 812, refer to AMM 06-41-53, Page Block 001

and AMM Task 52-41-00-010-002.

C. PROCEDURE

(1) Subtask 351069-832-001-001 - Inspect the Crew Oxygen Pipe between FR 9 and FR

13.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 812

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FFAAA

Flow Chart

Sheet 01

(a) At the threshold given in the PLANNING INFORMATION paragraph E.(2):

Do a General Visual Inspection of the crew oxygen pipe.

Refer to Fig. A-FBAAA Sheet 01

Refer to Fig. A-FFAAA Sheet 01

1 Check the batch number of the crew oxygen pipe PN D3511032000640:

19356252, 40008586, 40076689, 40187414, 40292749, 40405164, 40649383,

40724994, 40820410, 40911832

a If the crew oxygen pipe is part of the affected batches:

<1> Do SUBTASK 351069-833-001 001 Flush the affected parts with

nitrogen and replace the Crew Oxygen Pipe.

b If the crew oxygen pipe is not part of the affected batches:

<1> No further action is required.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 13

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(2) Subtask 351069-833-001-001 - Flush the affected parts with nitrogen and replace

the Crew Oxygen Pipe.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 812

210 Access Door 831, Door 841

Manpower Resources

Manhours 3.50

Minimum number of person 1

Subtask elapsed time 3.50

Skills AIRFRAME

Material necessary to do the job

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 D3511032000640 1 PIPE

NOTE: The above list of components is not an AIRBUS kit, the required parts

shall be ordered as necessary through the given channel.

Component COMPA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

3 AN960C816 1 WASHER

5 NSA835070-5C 6 RING

7 NSA935401-05 5 TIE

NOTE: The above list of components is not an AIRBUS kit, the required parts

shall be ordered as necessary through the given channel.

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Nitrogen,(gaseous) 19-014 As required

References

Aircraft Maintenance Manual (AMM) Task 35-00-00-860-001

Fig. A-FBBAA

Removal/Installation of the pipes

Sheet 01

Fig. A-FBCAA

Removal/Installation of the pipes

between the Tee and the Crew Oxygen

Mask

Sheet 01

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 14

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(a) Remove the crew oxygen pipe:

Refer to Fig. A-FBBAA Sheet 01

1 Washer Item (3) Discard

1 Nut Item (4) Retain

2 Ring For Flared Tube Item (5) Discard

5 Tie-Cable Item (7) Discard

2 Electrical Conduit Item (6) Retain

1 Union Item (12) Retain

3 Screw Item (8) Retain

3 Washer Item (9) Retain

3 Clamp Item (10) Retain

1 Strip-Bonding Item (11) Retain

1 Pipe D3511032000640 Item (1) Discard

(b) Open connections (if not in use) have to be closed with oxygen clean blind plugs at

all times.

(c) Remove all parts of the distribution system between the discarded pipe and the

crew oxygen mask stowage box:

Refer to AMM Task 35-00-00-860-001

Refer to Fig. A-FBCAA Sheet 01

4 Ring For Flared Tube Item (5) Discard

FIN 5765HM

1 Hose Item (13) Retain

FIN 5766HM

1 Hose Item (13) Retain

1 Tee Item (2) Retain

(d)

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 15

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

WARNING: DO NOT EXCEED 30PSIG (2,1KG/CM2) OF PRESSURE AT THE

NOZZLE WHEN USING COMPRESSED AIR OR NITROGEN IN

THIS CLEANING PROCESS. ALSO WEAR STURDY GOGGLES

OR A FACE SHIELD. PARTICLES OR LIQUID DROPLETS

PROPELLED BY HIGH PRESURE CAN CAUSE PERMANENT

EYE INJURY.

Flush the parts with nitrogen in the shop to remove potential particles within.

NOTE: Flush the parts with:

Nitrogen,(gaseous) 19-014 As required

(e) Install the flushed parts:

Refer to AMM Task 35-00-00-860-001

Refer to Fig. A-FBCAA Sheet 01

1 Tee Item (2) Retained at

removal

FIN 5765HM

1 Hose Item (13) Retained at

removal

FIN 5766HM

1 Hose Item (13) Retained at

removal

4 Ring For Flared Tube NSA835070-5C Item 5

(f) Install a new crew oxygen pipe not affected by this Inspection Service Bulletin:

Refer to Fig. A-FBBAA Sheet 01

1 Pipe D3511032000640 Item 1

3 Clamp Item (10) Retained at

removal

1 Strip-Bonding Item (11) Retained at

removal

3 Washer Item (9) Retained at

removal

3 Screw Item (8) Retained at

removal

2 Electrical Conduit Item (6) Retained at

removal

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 16

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

5 Tie-Cable NSA935401-05 Item 7

1 Union Item (12) Retained at

removal

1 Washer AN960C816 Item 3

2 Ring For Flared Tube NSA835070-5C Item 5

1 Nut Item (4) Retained at

removal

D. TEST

(1) Subtask 351069-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 35-10-00-790-001

Task 35-12-41-400-001

(a) Job Set-up:

1 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breakers

as specified in the installation of the Oxygen-Mask Stowage-Box, AMM Task

35-12-41-400-001.

(b) Procedure:

1 Do the test procedure as specified in the installation of the Oxygen-Mask

Stowage-Box, AMM Task 35-12-41-400-001.

2 If the pipe has been replaced, do the Leakage Test of the LP Oxygen System

for the Crew, refer to AMM Task 35-10-00-790-001

E. CLOSE-UP

(1) Subtask 351069-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 52-10-00-410-001

Task 52-41-00-410-002

(a) Close the passenger/crew door(s) 831 or 841, refer to AMM 06-41-53, Page Block

001 and AMM Task 52-10-00-410-001.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 17

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

(b) Close the avionics compartment door 812, refer to AMM 06-41-53, Page Block 001

and AMM Task 52-41-00-410-002.

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating conditions.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 18

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

A

Z125 Z126 − 

PIPE TO BE INSPECTED

A

FR9

FR11

FR13

B

B

N_SB_351069_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Area to be inspected

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 19

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

A

Z125 Z126 − 

A

FR9

FR11

FR13

B

B

(2)

(3)

(4)

(5)

(6)

(7)

(7)

(8)

(9)

(10)

(8)

(9)

(10)

(11) (8)

(9)

(10)

(1)

1

(6)

7

7

5

(12)

3

5

(5)

7

7

(7)

(7)

N_SB_351069_5_BBAA_01_01

Figure A-FBBAA - Sheet 01

Removal/Installation of the pipes

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 20

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

FR11

FR10

FR9

B

(5)

(13)

(5)

5

(2)

(13)

(5)

A

Z210

A

B

5

5

5

(5)

N_SB_351069_5_BCAA_01_00

Figure A-FBCAA - Sheet 01

Removal/Installation of the pipes between the Tee and the Crew Oxygen Mask

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 21

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

**CONF ALL

BATCHES?

IS THE PIPE

PART OF THE AFFECTED YES

OXYGEN PIPE PN D3511032000640

DO A GENERAL VISUAL INSPECTION OF THE CREW

NO

REFER TO SUBTASK 351069−833−001−001

QUESTION

ACTION

FINDING

AT THE THRESHOLD GIVEN IN THE PLANNING

OXYGEN PIPE PN D3511032000640

CHECK BATCH NUMBER OF THE CREW

PIPE PN D3511032000640

REPLACE THE CREW OXYGEN

NO FURTHER ACTION

REFER TO TASK 351069−832−001−001

INFORMATION PARAGRAPH E.(2).

N_SB_351069_5_FAAA_01_00

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 22

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

Appendix 01: Inspection Report

**CONF ALL

The results of the inspection, including no findings, replacement or actions to be done, must be

forwarded to AIRBUS Department SEEC2, on the attached inspection report sheet.

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

Appendix 01: Inspection Report

**CONF ALL

YES

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A320−35−1069

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEEC2

PASSENGER/CREW FACILITIES AND

INSPECTION METHOD :

EMERGENCY EQUIPMENT

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 44 25 GENERAL VISUAL

19356252

D3511032000640 IS PART OF

THE AFFECTED BATCHES

CREW OXYGEN PIPE PN

NO

INSPECTION

40008586

40076689

40187414

40292749

40405164

40649383

40724994

40820410

40911832

OXYGEN PIPE REPLACED YES NO

PRECISE BATCH NUMBER OF

THE CREW OXYGEN PIPE

IF PIPE IS AFFECTED,

(PN D3511032000640)

N_SB_351069_5_RAAA_01_00

Figure A-FRAAA - Sheet 01

Inspection Report Sheet

DATE: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 2

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

REPORTING SHEET

TITLE: MULTIPROG - CREW OXYGEN - INSPECTION OF OXYGEN PIPE FOR

CORROSION

MODIFICATION No.: None

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: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@A318/A319/A320/A321

SERVICE BULLETIN

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: Apr 26/13 SERVICE BULLETIN No.: A320-35-1069

REVISION No.: 00 - Apr 26/13 Page: 1

6

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.