@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: 25

TITLE: EQUIPMENT/FURNISHINGS - PASSENGER SUPPLY CHANNEL -

INSPECTION AND REWORK FOR JIFFY CONNECTOR

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

AIRBUS has discovered a potential issue with the jiffy joint connectors on the Passenger Service Unit

(PSU) cable installation. Some of the connectors have been found to be not properly locked. If the

connectors become disengaged during flight, malfunction of the passenger oxygen box can occur.

This Service Bulletin is published to advise operators of A320 and A321 aircraft of the issue of AIRBUS

Operation and Cabin Electronics Service Bulletin No. Z315H-25-004, which gives the procedures for

the special detailed inspection and if necessary, rework and potential replacement of the jiffy joint

connectors.

The accomplishment of this Service Bulletin will ensure that the jiffy joint connectors are inspected and

rectified if the connectors are found to be disengaged.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES 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 YES

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

disruptions.

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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

Component COMPD01 1 See SB Tie-wrap

EFFECTIVITY

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

AAR AFL AIJ ANZ APJ AVA AXM BAW CBJ CHB CSC CSN DLH

EVE EZY FFT GOW IGO JJP JST JZR KZR LAN NKS NLY SFJ

TAM TAR THY USA VLG VOI 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 YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 251B20-832-848-001: Inspection

TOTAL MANHOURS 4.25

ELAPSED TIME (HOURS) 4.25

Additional manhours related to Vendor SB; refer to:

Do a Special Detailed Inspection of the Jiffy Joint

Connectors

AIRBUS Service Bulletin No.

Z315H-25-004

Rework the Jiffy Joint Connectors AIRBUS Service Bulletin No.

Z315H-25-004

APPENDICES

None

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

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SUMMARY

**CONF ALL

A

Z240

Z250

Z230

B

TYPICAL

NOTE:

AREA TO BE INSPECTED

B

A

N_SB_251B20_6_SAAA_01_01

Figure A-GSAAA - Sheet 01

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

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SUMMARY

This Page Intentionally Left Blank

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

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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: 25

TITLE: EQUIPMENT/FURNISHINGS - PASSENGER SUPPLY CHANNEL -

INSPECTION AND REWORK FOR JIFFY CONNECTOR

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

NOTE: This modification is applicable by Service Bulletin only.

(1) Models

320-214 320-216 320-232 320-233 321-211 321-231

(2) Effectivity by MSN

5583 5598 5602 5604 5608 5610 5613-5622 5624-5627 5629-5632 5634-5636 5638

5640-5644 5646-5649 5651-5653 5655 5657-5661 5663 5665 5667 5670 5672-5673

5675

(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

AAR 5636

AFL 5614

AIJ 5653 5665

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OPERATOR MSN

ANZ 5629

APJ 5640

AVA 5622 5632

AXM 5619 5627 5657

BAW 5634

CBJ 5630

CHB 5626

CSC 5646 5647 5670

CSN 5602 5655

DLH 5635 5658

EVE 5642

EZY 5638

FFT 5661

GOW 5675

IGO 5641

JJP 5598 5618 5649

JST 5631

JZR 5625

KZR 5613

LAN 5583

NKS 5624 5672

NLY 5648

SFJ 5652

TAM 5621 5643

TAR 5610

THY 5663 5667

USA 5644 5659

VLG 5616 5620 5673

VOI 5651

WZZ 5604 5608 5615 5617 5660

(4) Configuration by MSN

MSN CONFIGURATION

5583 5598 5602 5604 5608 5610 5613 5614 5615 5616 5617

5618 5619 5620 5621 5622 5624 5625 5626 5627 5629 5630

5631 5632 5634 5635 5636 5638 5640 5641 5642 5643 5644

5646 5647 5648 5649 5651 5652 5653 5655 5657 5658 5659

5660 5661 5663 5665 5667 5670 5672 5673 5675

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.

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(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Component COMPD01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

AIRBUS has discovered a potential issue with the jiffy joint connectors on the Passenger

Service Unit (PSU) cable installation. Some of the connectors have been found to be not

properly locked. If the connectors become disengaged during flight, malfunction of the

passenger oxygen box can occur.

(2) Objective/Action

This Service Bulletin is published to advise operators of A320 and A321 aircraft of the

issue of AIRBUS Operation and Cabin Electronics Service Bulletin No. Z315H-25-004,

which gives the procedures for the special detailed inspection and if necessary, rework

and potential replacement of the jiffy joint connectors.

(3) Advantages

The accomplishment of this Service Bulletin will ensure that the jiffy joint connectors are

inspected and rectified if the connectors are found to be disengaged.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 251B20-832-848-001: Inspection

(1) Do a Check of the Affected PSU Part Numbers and Serial Numbers

(2) Remove the Tie-wraps from the Area of Inspection

(3) Do a Special Detailed Inspection of the Jiffy Joint Connectors

(4) Rework the Jiffy Joint Connectors

(5) Install the Tie-wraps in the Area of Inspection

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

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SERVICE BULLETIN

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 within

26 months, whichever occurs first, from the initial Service Bulletin date.

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 (thresholds and/or intervals and/or date) 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.

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 251B20-832-848-001: Inspection

Get Access 1.00

On Aircraft

Do a Check of the Affected PSU Part Numbers and

Serial Numbers

0.25

Remove the Tie-wraps from the Area of Inspection 0.50

Install the Tie-wraps in the Area of Inspection 0.50

Tests 1.00

Close-Up 1.00

TOTAL MANHOURS 4.25

ELAPSED TIME (HOURS) 4.25

Additional manhours related to Vendor SB; refer to:

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Task 251B20-832-848-001: Inspection

Do a Special Detailed Inspection of the Jiffy Joint

Connectors

AIRBUS Service Bulletin No.

Z315H-25-004

Rework the Jiffy Joint Connectors AIRBUS Service Bulletin No.

Z315H-25-004

NOTE: The manpower estimate for the removal of the tie-wraps, inspection of the jiffy

joint connectors and the installation of the tie-wraps is approximately 1 hour

for each affected PSU. The total manpower estimate will vary for each A/C,

refer to the list of affected PSU part numbers and serial numbers in AIRBUS

Service Bulletin No. Z315H-25-004 to determine the total number of affected

PSUs.

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 20-16-00 23-73-45

35-23-00

Elec. Std. Practices Manual (ESPM) 20-25-41 20-25-42 20-25-51

20-33-44 20-55-00

Standards Manual (SM)

Vendor Service Bulletin (VSB) AIRBUS Service Bulletin No.

Z315H-25-004

K. PUBLICATION AFFECTED

None

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

No Material Set

B. INDUSTRY SUPPORT INFORMATION

Refer to AIRBUS Operation and Cabin Electronics Service Bulletin No. Z315H-25-004 for the

industry support terms of the Vendor Service Bulletin parts and labor.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

Component COMPD01

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

NOTES

1 NSA935401-04 3 TIE (1)

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 (1): 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

F. TOOLING

(1) Tooling - Price and Availability

None

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(2) Tools

To accomplish the Inspection Task of this Service Bulletin it is necessary to use

the tools listed in AIRBUS Operation and Cabin Electronics Service Bulletin No.

Z315H-25-004 and in ESPM tasks:

- ESPM 20-33-44

- ESPM 20-25-51

- ESPM 20-25-42 (tool 81969-14).

(3) Special Tools

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 251B20-832-848-001 - Inspection

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.

NOTE: The accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words ’refer to’ are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. When the words ’in accordance with’ are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: This Service Bulletin is classified mandatory or expected to be classified mandatory

by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these

accomplishment instructions are Required for Compliance (RC) and must be done

to comply with the AD. Other paragraphs are recommended and may be deviated

from, done as part of other actions or done with accepted methods different from

those given in the Service Bulletin, as long as the RC paragraphs can be done and

the aircraft can be put back into a serviceable condition.

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.

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Task Associated Data

Zone

200 230 240 250

Manpower

TOTAL MANHOURS 4.25

ELAPSED TIME (HOURS) 4.25

Additional manhours related to Vendor SB; refer to:

AIRBUS Service Bulletin No. Z315H-25-004

A. GENERAL

(1) Subtask 251B20-910-201-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-53, Page Block 001

Task 20-16-00-912-001

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

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

(c) For the identification of access panels, refer to AMM 06-41-53, Page Block 001.

(d) For circuit breaker safety practices, refer to AMM Task 20-16-00-912-001.

(2) Subtask 251B20-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 251B20-941-201-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

230

240

250

Manpower Resources

Skills NON SPECIFIC

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References

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

Task 23-73-45-000-001

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position.

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

12-34-24-869-002.

(b) Do the job set-up for the removal of PSUs, refer to AMM Task 23-73-45-000-001.

C. PROCEDURE

(1) Subtask 251B20-200-201-001 - Do a Check of the Affected PSU Part Numbers and

Serial Numbers

Work Zones and Access Panels

Zone Access/Work location

230

240

250

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills ELECTRICAL

References

Vendor Service Bulletin (VSB) AIRBUS Z315H-25-004

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(a) Identify the part number and the serial number of each installed PSU in accordance

with AIRBUS Service Bulletin No. Z315H-25-004.

1 If the installed PSUs are not listed in the Appendix ’Affected PSU Part

Numbers and Serial Numbers’ in AIRBUS Service Bulletin No. Z315H-25-004:

a Go to SUBTASK 251B20-720-201 001 Functional Test .

2 For each installed PSU listed in the Appendix ’Affected PSU Part Numbers

and Serial Numbers’ in AIRBUS Service Bulletin No. Z315H-25-004:

a Go to SUBTASK 251B20-020-201 001 Remove the Tie-wraps from the

Area of Inspection .

(2) Subtask 251B20-020-201-001 - Remove the Tie-wraps from the Area of Inspection

Work Zones and Access Panels

Zone Access/Work location

230

240

250

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

References

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-44

Fig. A-GBAAA

Removal and Installation of the Tiewraps from the Inspection Area

Sheet 01

(a) Remove the tie-wraps from the area of inspection, refer to ESPM 20-33-44 and

ESPM 20-25-51.

1 As shown in Fig. A-GBAAA Sheet 01, remove:

3 Tie-Cable NSA935401-04 Item (1) Discard

(3) Subtask 251B20-832-201-001 - Do a Special Detailed Inspection of the Jiffy Joint

Connectors

Work Zones and Access Panels

Zone Access/Work location

230

240

250

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References

Vendor Service Bulletin (VSB) AIRBUS Z315H-25-004

Fig. A-GFAAA

Flow Chart

Sheet 01

Fig. A-GRAAA

Inspection Report

Sheet 01

(a) Do a Special Detailed Inspection of the unit side of the jiffy joint connectors in

accordance with AIRBUS Service Bulletin No. Z315H-25-004.

Refer also to Fig. A-GFAAA Sheet 01.

1 If there are no findings, go to step 3(b).

2 If there are findings, go to SUBTASK 251B20-833-201 001 Rework the Jiffy

Joint Connectors .

(b) Do a Special Detailed Inspection of the A/C side of the jiffy joint connectors in

accordance with AIRBUS Service Bulletin No. Z315H-25-004.

Refer also to Fig. A-GFAAA Sheet 01.

1 If there are no findings, go to SUBTASK 251B20-420-201 001 Install the Tiewraps in the Area of Inspection .

2 If there are findings, go to SUBTASK 251B20-833-201 001 Rework the Jiffy

Joint Connectors .

(c) Record all inspection results, and contact AIRBUS, refer to Fig. A-GRAAA Sheet

01.

(4) Subtask 251B20-833-201-001 - Rework the Jiffy Joint Connectors

Work Zones and Access Panels

Zone Access/Work location

230

240

250

References

Elec. Std. Practices Manual (ESPM) 20-25-41

Vendor Service Bulletin (VSB) AIRBUS Z315H-25-004

(a) If disconnected jiffy joint connectors are found on the unit side, do the rework

procedure of the jiffy joint connectors in accordance with AIRBUS Service Bulletin

No. Z315H-25-004 or ESPM 20-25-41.

(b) If disconnected jiffy joint connectors are found on the A/C side, do the rework

procedure of the jiffy joint connectors in accordance with AIRBUS Service Bulletin

No. Z315H-25-004.

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(c) If after the rework the connection does not engage correctly, do the replacement

of the jiffy joint connectors in accordance with AIRBUS Service Bulletin No.

Z315H-25-004.

(5) Subtask 251B20-420-201-001 - Install the Tie-wraps in the Area of Inspection

Work Zones and Access Panels

Zone Access/Work location

230

240

250

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills ELECTRICAL

Material necessary to do the job

Component COMPD01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 NSA935401-04 3 TIE (1)

NOTE (1): The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

Elec. Std. Practices Manual (ESPM) 20-25-51

20-33-44

Fig. A-GBAAA

Removal and Installation of the Tiewraps from the Inspection Area

Sheet 01

(a) Install the tie-wraps in the area of inspection, refer to ESPM 20-33-44 and ESPM

20-25-51.

1 As shown in Fig. A-GBAAA Sheet 01, install:

3 Tie-Cable NSA935401-04 Item 1

D. TEST

(1) Subtask 251B20-720-201-001 - Functional Test

Work Zones and Access Panels

Zone Access/Work location

200

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Manpower Resources

Skills CABIN

References

Aircraft Maintenance Manual (AMM) Task 35-23-00-710-001

(a) Do the functional test as specified in the AMM task Functional Test of the Manual

Mask Release, refer to AMM Task 35-23-00-710-001.

E. CLOSE-UP

(1) Subtask 251B20-942-201-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

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

equipment.

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

REVISION No.: 00 - Oct 09/14 Page: 15

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SERVICE BULLETIN

**CONF ALL

IDENTIFY THE PSU AFFECTED IN 

IS THE PSU AFFECTED? NO

YES

BEFORE THE THRESHOLD GIVEN IN THE PLANNING INFORMATION

PARAGRAPH 1.E.(2) GET ACCESS TO THE APPLICABLE PSU

YES

DO THE SPECIAL DETAILED

IS THE CONNECTION

MADE CORRECTLY? NO

DO THE REWORK OF

THE JIFFY CONNECTORS

DO THE IDENTIFICATION OF

THE REWORKED PSUs

IS THE LAST PSU

INSPECTED? YES

RETURN THE A/C 

TO SERVICEABLE

DO THE FUNCTIONAL

TEST OF THE MANUAL

OXYGEN MASK RELEASE CONDITION

NO

DO THE INSPECTION OF

THE NEXT PSU

COMPLETE THE REPORTING

SHEET AND SEND IT TO AIRBUS

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.

INSPECTION OF THE JIFFY

JOINT CONNECTIONS

ACCORDANCE WITH THE VSB

N_SB_251B20_6_FAAA_01_02

Figure A-GFAAA - Sheet 01

Flow Chart

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

REVISION No.: 00 - Oct 09/14 Page: 16

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SERVICE BULLETIN

**CONF ALL

A

Z240

Z250

Z230

B

TYPICAL

B

A

(1)1

N_SB_251B20_6_BAAA_01_00

Figure A-GBAAA - Sheet 01

Removal and Installation of the Tie-wraps from the Inspection Area

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

REVISION No.: 00 - Oct 09/14 Page: 17

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SERVICE BULLETIN

**CONF ALL

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A320−25−1B20

INSPECTION REPORT

FINDINGS : YES NO

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEEC1

CABIN ELECTRONICS SYSTEMS

INSPECTION METHOD: SPECIAL DETAILED

INSPECTION

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 44 25

LH CABIN PSU

LOCATION OF

DISENGAGED

CONNECTOR

PART NUMBER SERIAL NUMBER

RH CABIN PSU

LOCATION OF

DISENGAGED

CONNECTOR

PART NUMBER SERIAL NUMBER

N_SB_251B20_6_RAAA_01_00

Figure A-GRAAA - Sheet 01

Inspection Report

DATE: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

REVISION No.: 00 - Oct 09/14 Page: 18

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SERVICE BULLETIN

REPORTING SHEET

TITLE: EQUIPMENT/FURNISHINGS - PASSENGER SUPPLY CHANNEL -

INSPECTION AND REWORK FOR JIFFY CONNECTOR

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: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

REVISION No.: 00 - Oct 09/14 Page: 1

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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: Oct 09/14 SERVICE BULLETIN No.: A320-25-1B20

REVISION No.: 00 - Oct 09/14 Page: 1

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