@A318/A319/A320/A321

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: 54

TITLE: NACELLES/PYLONS - GENERAL - INSTALL NEW CORNER FITTINGS

TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS.

MODIFICATION No.: 38067P10500

This page transmits Revision No.02 of Service Bulletin No.A320-54-1019

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 02 issued to:

- Change the compliance from desirable to recommended.

- Update the effectivity.

- Modify the Test procedure.

This Service Bulletin has been validated at original issue on A320 aircraft with Manufacturer Serial

Number (MSN) 0383.

Aircraft with Manufacturer Serial Number (MSN) 0383 complies fully with the requirements of the

current issue of the Service Bulletin.

CHANGES

Revised text and layout changes of this revision are not identified with revision bars.

The main changes of this revision are:

- Modification of the Evaluation Table

- Modification of the PROCEDURE Topic

. Removal of the Drain Pipes moved to PREPARATION paragraph

. Installation of the Drain Pipes moved to CLOSE-UP paragraph

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 1

5

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

- Modification of the TEST Topic

. Notes added in the Test procedure

SUMMARY

MODIFICATIONS Minor editorial or document structure change N

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

Minor editorial or document structure change N

GENERAL EVALUATION Minor editorial or document structure change N

MATERIAL PRICE INFORMATION Minor editorial or document structure change N

EFFECTIVITY Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REFERENCES / REPERCUSSIONS Minor editorial or document structure change N

NATURE OF THE WORK Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

APPENDICES Minor editorial or document structure change N

Fig. A-FSAAA Minor editorial or document structure change N

Fig. A-FSAAA Sheet 01 Minor editorial or document structure change N

PLANNING INFORMATION

EFFECTIVITY Minor editorial or document structure change N

Configuration definition Minor editorial or document structure change N

CONF 001 Minor editorial or document structure change N

Material Effectivity Minor editorial or document structure change N

Minor editorial or document structure change N

CONCURRENT REQUIREMENTS Minor editorial or document structure change N

REASON Minor editorial or document structure change N

History Minor editorial or document structure change N

Objective/Action Minor editorial or document structure change N

Advantages Minor editorial or document structure change N

Operational/Maintenance

Consequences

Minor editorial or document structure change N

DESCRIPTION Minor editorial or document structure change N

COMPLIANCE Minor editorial or document structure change N

Classification Minor editorial or document structure change N

Accomplishment Timescale Minor editorial or document structure change N

APPROVAL Minor editorial or document structure change N

Minor editorial or document structure change N

MANPOWER Minor editorial or document structure change N

Minor editorial or document structure change N

WEIGHT AND BALANCE Minor editorial or document structure change N

ELECTRICAL LOAD DATA Minor editorial or document structure change N

REFERENCES Minor editorial or document structure change N

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 2

5

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Minor editorial or document structure change N

PUBLICATION AFFECTED Minor editorial or document structure change N

Minor editorial or document structure change N

INTERCHANGEABILITY/MIXABILITY Minor editorial or document structure change N

SPARES Minor editorial or document structure change N

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY Minor editorial or document structure change N

Procurement Addresses Minor editorial or document structure change N

Price and Availability Minor editorial or document structure change N

INDUSTRY SUPPORT INFORMATION Minor editorial or document structure change N

LIST OF COMPONENTS Minor editorial or document structure change N

Kit 541019A01R01 Minor editorial or document structure change N

LIST OF MATERIALS - OPERATOR

SUPPLIED

Minor editorial or document structure change N

Consumable Materials Minor editorial or document structure change N

Consumable CMLA01 Minor editorial or document structure change N

Components Minor editorial or document structure change N

Component COMPA01 Minor editorial or document structure change N

Equipment Minor editorial or document structure change N

PARTS TO BE RE-IDENTIFIED BY

OPERATOR

Minor editorial or document structure change N

TOOLING Minor editorial or document structure change N

ACCOMPLISHMENT INSTRUCTIONS

TASK 541019- 831-801-001-

MODIFICATION

Minor editorial or document structure change N

Task associated data - 001 Minor editorial or document structure change N

Subtask 541019-910-001-001 Minor editorial or document structure change N

Subtask 541019-839-001-001 Minor editorial or document structure change N

Subtask 541019-941-003-001 Minor editorial or document structure change N

Subtask 541019-941-001-001 Minor editorial or document structure change N

Subtask 541019-941-002-001 Minor editorial or document structure change N

Subtask 541019-831-002-001 Minor editorial or document structure change N

Subtask 541019-831-003-001 Minor editorial or document structure change N

Subtask 541019-831-004-001 Minor editorial or document structure change N

Subtask 541019-831-005-001 Minor editorial or document structure change N

Subtask 541019-700-001-001 Minor editorial or document structure change N

Subtask 541019-942-001-001 Minor editorial or document structure change N

Subtask 541019-942-002-001 Minor editorial or document structure change N

Fig. A-FBAAA Minor editorial or document structure change N

Fig. A-FBAAA Sheet 01 Minor editorial or document structure change N

Fig. A-FBAAA Sheet 02 Minor editorial or document structure change N

Fig. A-FBAAA Sheet 03 Minor editorial or document structure change N

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 3

5

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-FBAAA Sheet 04 Minor editorial or document structure change N

Fig. A-FBAAA Sheet 05 Minor editorial or document structure change N

Fig. A-FBBAA Minor editorial or document structure change N

Fig. A-FBBAA Sheet 01 Minor editorial or document structure change N

Fig. A-FBBAA Sheet 02 Minor editorial or document structure change N

Fig. A-FBBAA Sheet 03 Minor editorial or document structure change N

Fig. A-FBBAA Sheet 04 Minor editorial or document structure change N

Fig. A-FBBAA Sheet 05 Minor editorial or document structure change N

Fig. A-FBCAA Minor editorial or document structure change N

Fig. A-FBCAA Sheet 01 Minor editorial or document structure change N

Fig. A-FBCAA Sheet 02 Minor editorial or document structure change N

Fig. A-FBCAA Sheet 03 Minor editorial or document structure change N

Fig. A-FBDAA Minor editorial or document structure change N

Fig. A-FBDAA Sheet 01 Minor editorial or document structure change N

Fig. A-FBDAA Sheet 02 Minor editorial or document structure change N

Fig. A-FBDAA Sheet 03 Minor editorial or document structure change N

Appendix 01 - Elapsed Time Assumption

APPENDIX CONTENT Minor editorial or document structure change N

Fig. A-FAAAA Minor editorial or document structure change N

Fig. A-FAAAA Sheet 01 Minor editorial or document structure change N

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.

HISTORY OF PREVIOUS REVISIONS

This Service Bulletin has been validated on A320 aircraft MSN 0383.

Revision No. 01 issued to include minor improvements after validation.

REVISION SEQUENCE

ORIGINAL: Nov 20/07

REVISION No. : 01 - Apr 10/08

REVISION No. : 02 - Apr 15/14

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 4

5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.
@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: 54

TITLE: NACELLES/PYLONS - GENERAL - INSTALL NEW CORNER FITTINGS

TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS.

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 38067P10500

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

Several operators reported cracks on the two corner fittings at RIB11 lower attachment level, in the

pylon aft fixed secondary structure.

Improved fittings, having thicker faces with shot peened surfaces, have been designed and introduced

in production.

This Service Bulletin recommends the replacement of the two corner fittings by new improved fittings for

in-service aircraft.

Accomplishment of this Service Bulletin will prevent cracking occurrence at this location.

Due to access requirements to the area, AIRBUS informs of an improvement of the aft fixed secondary

structure : accomplishment of Service Bulletin No. A320-54-1013 (Mod. No. 31705P7399) could be

performed simultaneously.

Accomplishment of this Service Bulletin cancels the requirements of Inspection Service Bulletin No.

A320-54-1022.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB YES

POTENTIAL AD NO A/C OPERATION AFFECTED NO

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 1

5

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

SERVICE BULLETIN

SUMMARY

EVALUATION TABLE

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

BOOKLET AVAILABLE YES VALIDATION ON AIRCRAFT YES

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

disruptions.

This Service Bulletin has been validated at original issue on A320 aircraft with Manufacturer Serial

Number (MSN) 0383.

Aircraft with Manufacturer Serial Number (MSN) 0383 complies fully with the requirements of the

current issue of the Service Bulletin.

A booklet including photographs taken during the validation of this Service Bulletin is available on

AIRBUS|World - Maintenance and Engineering - AirN@v engineering (in the concerned SB file).

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 541019A01R01 2 2,400.00 Corner, Rivet

Component COMPA01 2 See SB Rivet

EFFECTIVITY

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

03X 15S 15T 17W 19R 26S 29S 31V 31X 32Q 35U 36R 38W

46U 52T 53Z 59Z 66X 69X 73W 74T 80X 85T 86W 86Z 89Q

91X 92Q 94W 95V 95W 98W AAF AAR AAW AAY ABL ABQ ABY

ACA ACI ADH AEE AFL AFR AGC AGY AHY AIB AIC AIJ ALK

AMC AMU ANA ANR ANZ APZ ARR ART ARU ATR AUA AUH AVA

AWC AWM AWW AXM AZA AZI AZW B2V BAW BEC BEL BER BGF

BGH BGY BHP BIE BKP BQB BRS C9G CCA CEB CEF CES CHH

CIB CQH CQN CSA CSC CSN CSZ CTN CTV CYP D2F DAL DCS

DKH DLH DNV DQA DRK DTR EAA EDW EIN ETD ETJ EVA EZD

EZY F2I FFT FHY FIN FLI FPY FRN FTZ G2X G4I G8E GAP

GBB GCR GLG GMI GMR GWI GZQ HAY HDA HFY HKE HKJ HRM

HVN I2L I2T IBE IBS IND IRA IRM ISS IZG JAT JAV JBU

JSA JST JZR KAC KCA KFR KGL KHO KHV KKK KMF KNE KZR

LAN LBT LFO LLC LLM LLP LMJ LMU LZB MAU MDL MEA MLD

MLM MLR MMA MML MON MRJ MSC MSR MXA MYX NIA NKS NLV

NLY NMA NMB NVD NVR NWS OAW OHY ORF OZW PAL PIC PTI

PTR QAF QTR R1T RBA RBG RCT RFJ RJA RJD RNV RYW RZO

S2A SAA SAI SAS SBI SDM SFJ SFW SGG SHJ SHU SKU SLK

SMX SND SNX SOL SUD SVR SVW SWM SWR SYR TAE TAI TAK

TAM TAP TAR TBJ TBZ TCW TCX TGW THY TNA TVS TWJ TXP

UAL UEA ULG USA VAR VIM VIV VJC VKG VLE VLG VLK VOI

VRD VRE VVC WGT WHT WOW WRC WTJ WZZ

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 2

5

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

SERVICE BULLETIN

SUMMARY

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED None

LIFE LIMIT No

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 541019-831-801-001: MODIFICATION

TOTAL MANHOURS 59.00

ELAPSED TIME (HOURS) 29.50

APPENDICES

Appendix 01 - Elapsed Time Assumption

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 3

5

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

SERVICE BULLETIN

SUMMARY

**CONF ALL

REPLACEMENT OF THE

CORNER FITTINGS

Z475 Z476 − 

Z485 Z486 − 

A

A

LH SHOWN

RH SYMMETRICAL 1

NOTE:

B

RIB11

RIB12

RIB14

RIB15

B

A 1

N_SB_541019_5_SAAA_01_00

Figure A-FSAAA - Sheet 01

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 4

5

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: 54

TITLE: NACELLES/PYLONS - GENERAL - INSTALL NEW CORNER FITTINGS

TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS.

MODIFICATION No.: 38067P10500

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.

NOTE: This Service Bulletin is only applicable to aircraft on which Mod. No.

33844P8341 (IMPROVE AERODYNAMIC SHAPE OF CFM PYLON), Mod.No.

33687P8297 (IMPROVE THE AERODYNAMIC SHAPE OF A318 PW

PYLON), Mod. No. 33847P8340 (IMPROVE AERODYNAMIC SHAPE OF IAE

PYLON) and Mod. No. 38067P10459 (INSTALL NEW CORNER FITTINGS

TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS) are not

embodied.

(1) Models

318-111 318-112 319-111 319-112 319-113 319-114 319-115 319-131

319-132 319-133 320-211 320-212 320-214 320-216 320-231 320-232

320-233 321-111 321-112 321-131 321-211 321-212 321-213 321-231

321-232

(2) Effectivity by MSN

0029 0045-0047 0049-0057 0059 0064-0078 0080-0088 0090 0093-0096 0099 0104

0110-0119 0121-0127 0135 0137-0138 0140-0142 0147-0150 0152-0154 0157-0162

0164-0168 0171-0176 0178-0179 0181-0183 0185 0189-0190 0192 0194-0195

0197-0203 0205-0214 0216-0220 0223-0224 0229-0235 0237 0239-0244 0248-0249

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 1

5

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

SERVICE BULLETIN

0251-0256 0259-0270 0272-0277 0279 0281-0282 0284-0285 0287 0289-0303

0306-0309 0311-0312 0314 0316-0325 0328-0333 0339-0343 0345-0347 0349-0351

0353-0362 0364 0366-0368 0370-0373 0375-0376 0378 0380-0388 0390-0391 0393

0395-0396 0398-0410 0412-0424 0426-0432 0434-0436 0438-0439 0441-0442

0444-0445 0447-0452 0454-0460 0462-0466 0468-0477 0479-0480 0482-0535

0537-0546 0548-0589 0591-0600 0603-0614 0616-0623 0625 0627 0629-0631

0633-0670 0672-0707 0709 0711-0752 0754-0788 0790-0955 0957-1043 1045-1112

1114-1185 1187-1217 1219-1277 1279-1332 1334-1373 1375-1463 1465-1659

1661-1675 1677-1728 1730-1767 1769-1812 1814-1821 1823-1829 1831-1918

1920-1929 1931-1938 1940-1984 1986-1990 1993-2024 2026-2050 2052-2110

2112-2217 2219-2275 2277-2423 2425-2499 2501-2721 2723-2780 2782-2801

2803-2813 2815-2831 2833-2847 2849-2870 2872-2879 2881-2899 2901-2930

2932-2944 2946-2954 2956-2969 2971-2976 2978-2991 2993 2995-3000 3002-3028

3031-3032 3035-3037 3040-3047 3049-3061 3063-3065 3067-3071 3073 3075-3086

3088 3090 3093-3104 3106 3109 3111-3114 3116-3118 3121-3122 3124-3126 3129

3131-3142 3144-3145 3147-3148 3151-3156 3159 3161-3162 3165 3168-3169

3173-3176 3179-3186 3188-3189 3192 3194-3195 3198-3204 3206-3209 3211 3215

3218-3219 3221 3223-3224 3226 3231-3232 3234 3236-3237 3239 3242 3244-3246

3253 3255 3257 3261 3268 3272 3275 3277 3279 3282-3283 3285 3289 3291-3293

3296-3297 3299 3303 3315-3316 3318 3320-3321 3323 3327 3332 3337-3338 3341

3345-3346 3349-3350 3353 3355 3361 3363 3366 3368 3370 3376-3380 3383

(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

03X 2421

15S 1589

15T 0764 1494 2910

17W 3046

19R 0421

26S 0368 0424 0438

29S 0291 0292

31V 0164 0332 0343 0420 0436 0605 1048

31X 2192

32Q 1283

35U 0088 0199 0240 0241 0264

36R 1305

38W 1194

46U 2906 2952 2982 3275 3296 3332

52T 1599

53Z 1468

59Z 1556

66X 0558 0561 1098

69X 0219 0449 0588 0733

73W 0087

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 2

5

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

SERVICE BULLETIN

OPERATOR MSN

74T 2165

80X 2748

85T 0234

86W 0384

86Z 0168 0460 0497 2874

89Q 0400

91X 2837

92Q 0279 0395

94W 1818

95V 3379

95W 2949

98W 0441

AAF 0639 1006 1846 2870 3136 3242 3289

AAR 0802 1174 1356 1511 1670 1734 2041 2110 2226 2247 2290 2397

2459 2808 2840 3244 3297

AAW 3224 3236

AAY 1229 1255 1262 1288 1292 1318 1347 2224 2319 2387

ABL 1227 1636 1970 2045 2943

ABQ 1467

ABY 2764 3246

ACA 0059 0068 0073 0084 0122 0126 0127 0141 0149 0150 0154 0159

0174 0175 0183 0210 0231 0232 0233 0242 0248 0253 0254 0255

0265 0277 0284 0290 0309 0324 0330 0341 0378 0403 0404 0546

0572 0634 0656 0670 0672 0682 0688 0691 0693 0695 0697 0711

0719 0721 0728 0732 0736 0740 0742 0752 0757 0769 0773 0779

0785 0800 0813 0817 0829 0831 0840 0845 1562 1577 1602 1611

1623 1632 1638 1673 1726 1742 1748 1772 1783 1811 1853 1864

1874 1940 2018 2145

ACI 2152

ADH 3138 3161

AEE 2468 2828 3162 3316

AFL 2052 2069 2072 2091 2106 2116 2133 2144 2151 2163 2233 2243

2330 2337 2342 2875 2903 2912 2920 2947 2957 2965 3052 3063

AFR 0115 0214 0237 0239 0285 0287 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 1879 1894 1900

1924 1938 1949 2035 2059 2071 2081 2100 2109 2140 2317 2344

2350 2456 2582 2601 2686 2705 2716 2721 2750 2918 2938 2951

2961 2967 2972 3008 3009 3051 3098

AGC 0190

AGY 0351

AHY 0331 2487 2516 2588 2685 2788 2846 2853 2865 2991 3006

AIB 0138

AIC 0045 0046 0047 0049 0050 0051 0056 0057 0074 0075 0080 0090

0095 0096 0396 0398 0416 0423 0431 0432 0451 0469 0486 0490

0492 0499 2593 2624 2629 2907

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 3

5

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

SERVICE BULLETIN

OPERATOR MSN

AIJ 0707 1132 1162 1179 1244 1259 1308 1322 1747 1780 2048 2227

2539 3021

ALK 2345 2564 2584 2908

AMC 2113 2122 2142 2189 2291 2332 2382 2665 2768 3056 3068

AMU 0620 0631 0805 0908 0928 1758 1790 1850 1893 1912 1926 1962

ANA 0167 0212 0300 0328 0383 0413 0482 0501 0507 0531 0534 0549

0554 0658 0669 0685

ANR 0726

ANZ 2085 2090 2112 2130 2148 2153 2173 2257 2297 2445 2533 2594

2663

APZ 0747

ARR 0913 1439

ART 0142 0244 0311 0333 0359 0426 0533 0936 1873

ARU 0573 0582

ATR 0314 0373 0393

AUA 0552 0570 0581 0768 0776 0797 0920 0935 1137 1150 1189 1385

1387 1458 1478 1504 1553 1678 1735 1931 1937 2009 2131 2174

2262 2416 2494 2547 2652

AUH 2403

AVA 1612 1634 2066 2328 2333 2358 2367 2377 2394 2523 2544 2552

2575 2662

AWC 2791

AWM 0765

AWW 0557 0597

AXM 2425 2612 2633 2656 2683 2699 2760 2816 2842 2881 2885 2944

2989 3000 3117 3140 3154 3173 3182 3194 3201 3223 3232 3261

3277 3291 3299 3327 3338 3353 3370

AZA 0434 0477 0488 0494 0495 0513 0514 0515 0516 0524 0526 0532

0576 0583 0586 0593 0599 0819 0848 0940 0951 0959 0999 1138

1168 1217 1220 1448 1457 1473 1480 1489 1722 1740 1745 1770

1779 2033 2057 2074 2083 2086 2101 2127 2869 2932 3076 3079

3080

AZI 0527

AZW 0630 1973

B2V 0185

BAW 1014 1082 1115 1118 1142 1177 1193 1197 1222 1225 1232 1236

1239 1258 1261 1279 1295 1329 1338 1380 1384 1418 1423 1424

1440 1445 1466 1510 1513 1529 1537 1558 1574 1590 1594 1604

1606 1661 1665 1687 1689 1690 1696 1708 1711 1754 1760 1782

1814 1829 1871 1883 1899 1907 1910 1958 1987 2038 2040 2098

2188 2190 2194 2305 2320 2323 2324 2351 2363 2389 2429 2441

2466 2536 2653 2694 2697 2720 2799 2981 3049 3081

BEC 3199

BEL 0644 1086 1102 1160 1336 1388 1441 1493 1797 1838 1885 1963

2196 2230 2392 2400 2810 3255

BER 1629 1961 1966 1988 1994 2003 2005 2619 3055 3093 3121

BGF 3188

BGH 1087 2844 2863 3139

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 4

5

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

SERVICE BULLETIN

OPERATOR MSN

BGY 1450 1723 2118

BHP 2968 3245

BIE 0519 0827 0891

BKP 2254 2310 2366 2417 2509 2531 2634 2648 2660 2664 2783

BQB 1703

BRS 2263

C9G 0772 1727 2335

CCA 0876 0921 1296 2000 2007 2015 2172 2202 2205 2237 2269 2285

2293 2298 2454 2499 2508 2525 2532 2545 2551 2559 2614 2643

2805 2819 2839 2847 2890 3195 3200 3215 3221 3226 3337

CEB 2556 2586 2625 2638 2786 2790 2821 2831 2852 2876 3272

CEF 2801 3085

CES 0665 0754 0828 0838 0854 0897 0909 0925 0939 0967 0984 0986

1005 1028 1030 1041 1070 1072 1093 1108 1285 1303 1312 1316

1330 1345 1357 1361 1377 1386 1532 1541 1542 1551 1601 1603

1639 1906 1911 1964 1981 2022 2034 2036 2049 2056 2068 2155

2199 2212 2219 2221 2235 2239 2244 2274 2309 2315 2437 2451

2478 2493 2498 2543 2549 2562 2591 2606 2627 2693 2757 2825

2882 2895 3168 3186

CHH 2475 2557 2561 2581 2611 2617 2644 2733 2746 2849 2891 2985

3285

CIB 0774 0809 0884 0894 0905 0957 0971 1381 1402 1416 1437 1607

1968

CQH 0978 1686 1769 1852 1920 2939 3014 3023

CQN 0696 0698 0704 0705

CSA 2719 2758 2789 3031 3043 3060 3094 3097

CSC 0540 0550 0551 0556 0591 0878 0902 0915 0919 1007 1013 2313

2348 2396 2431 2510 2534 2597 2639 3114 3116 3124

CSN 0712 0718 0720 0722 0849 0859 0881 0895 0900 0950 0966 1035

1039 1057 1596 1614 1776 1788 1971 1974 1986 1995 2004 2008

2067 2080 2200 2203 2232 2273 2354 2361 2371 2408 2426 2435

2484 2505 2506 2511 2519 2521 2530 2541 2546 2554 2555 2558

2574 2579 2637 2667 2680 2689 2701 2708 2713 2714 2741 2743

2759 2767 2770 2772 2796 2809 2815 2824 2834 2855 2861 2877

2899 2901 2915 2936 2940 2948 2950 2960 2969 2971 2986 3020

3067 3075 3112 3144

CSZ 2672 2684 2841 2905 2909 2935 2973 2980 3131 3132 3153 3206

3366 3383

CTN 0767 0833 1009 1029 1237 1252

CTV 0839 0892 1635 2598 2692 3147 3148

CYP 0256 2108 2275 2334 2343 2359

D2F 1668 1718

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 5

5

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

SERVICE BULLETIN

OPERATOR MSN

DAL 0118 0121 0125 0152 0153 0160 0171 0192 0197 0206 0208 0213

0262 0263 0272 0273 0281 0282 0297 0298 0306 0307 0318 0319

0329 0339 0340 0355 0358 0360 0367 0372 0380 0381 0387 0388

0399 0408 0410 0417 0418 0766 0778 0786 0801 0807 0818 0830

0832 0846 0903 0907 0911 0923 0962 0964 0981 0988 0996 1011

1037 1058 1062 1191 1230 1249 1324 1325 1346 1392 1414 1434

1453 1456 1483 1498 1501 1520 1535 1543 1549 1567 1570 1582

1633 1641 1646 1659 1662 1683 1685 1693 1709 1714 1738 1746

1752 1766 1774 1789 1796 1800 1810 1812 1815 1820 1824 1828

1833 1839 1875 1897 1923 1959 1976 1982 1990 2002 2013 2026

2039 2047 2082 2087 2092 2095

DCS 1053

DKH 2975 3027 3234 3268 3368

DLH 0069 0070 0071 0072 0078 0083 0086 0093 0094 0104 0110 0111

0116 0117 0135 0137 0161 0172 0201 0202 0209 0216 0267 0268

0269 0346 0412 0458 0468 0473 0474 0484 0493 0502 0505 0518

0560 0563 0564 0567 0595 0609 0610 0616 0623 0627 0636 0641

0651 0652 0679 0689 0692 0694 0699 0700 0717 0723 0729 0738

0744 0853 0860 0875 0887 0901 1016 1080 1161 1172 1188 1214

1260 1273 1337 1365 1367

DNV 1630 1805 1808 1841 2093 2179 2241 2751 3065 3179

DQA 2347

DRK 2306 2346

DTR 0444

EAA 0386 0445

EDW 0942 0947 1026 2024

EIN 0926 1023 1094 1242 1394 1443 1983 2001 2191 2206 2217 2250

2256 2272 2294 2364 2374 2399 2409 2411 2432 2486 2542 2583

2635 3054 3102 3129 3169 3318 3345 3377

ETD 0350 1140 1159 1944 1945 1947 1955 2167 3004 3050

ETJ 0325 0428

EVA 3363

EZD 0667 0743 0872 0874 1074 1286 2137 2141 2147 2576 2826 2926

2956 3018 3064

EZY 2037 2043 2050 2053 2062 2120 2170 2181 2184 2245 2265 2271

2289 2300 2353 2360 2370 2385 2398 2402 2412 2420 2427 2450

2463 2471 2477 2481 2492 2495 2503 2512 2514 2527 2528 2538

2565 2578 2605 2636 2646 2677 2681 2691 2702 2709 2715 2727

2729 2735 2742 2744 2754 2765 2769 2777 2779 2782 2795 2803

2812 2818 2827 2829 2854 2860 2866 2873 2884 2923 2946 2959

3003 3036 3041 3053 3059 3061 3082 3084 3088 3090 3118 3122

3134 3137 3176 3184

F2I 0085 0148 0220 0230 0243 0249 0251 0270 0294 0301 0391 0724

0758 0976 1010

FFT 1515 1579 1583 1615 1684 1759 1781 1786 1803 1806 1860 1943

1980 1997 2010 2012 2017 2019 2030 2103 2198 2209 2236 2240

2253 2258 2260 2287 2318 2325 2406 2448 2483 2518 2695 2806

2836 2857

FHY 0580 0771 0855 2524 2804

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 6

5

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

SERVICE BULLETIN

OPERATOR MSN

FIN 0941 0961 1073 1107 1184 1185 1241 1309 1352 1364 1405 1470

1544 1588 1712 1913 1916 1978 1989 2065 2124 2146 2154 2208

2266

FLI 2186

FPY 0112 0189 0342

FRN 0647 0660

FTZ 1068 1145 2176

G2X 0347 0674

G4I 1157 1795 2507

G8E 0349 0594 2700 2763

GAP 0706 0745 2162 2183

GBB 0067

GCR 2338

GLG 1866 1872 1882 1925 2078 2126

GMI 0970 0995 3019 3202

GMR 1407 2128

GWI 0147 0162 0200 0217 0218 0382 0401 0646 0654 0794 1077 1084

1089 1136 1147 1155 1170 1209 1277 2607 2628 2632 2813 2833

2976 3011

GZQ 1878

HAY 0716 0888 2745

HDA 0633 0756 0784 0812 0930 0993 1024 1253 1695 1721 1984 2021

2229 2238 2428

HFY 1004

HKE 2717

HKJ 2706 3073

HRM 0517 0535 0642 0666

HVN 0619 0648 0650 2255 2261 2267 2303 2974 3005 3013 3022 3198

3315 3355

I2L 0293 0371 0427 0579 0760 0816 1719

I2T 1631 1682

IBE 0158 0173 0176 0207 0223 0224 0266 0274 0323 0356 1021 1027

1047 1154 1362 1572 1655 1674 1681 1716 1793 1809 1836 2115

2220 2225 2242 2264 2270 2311 2357 2365 2381 2391 2472 2488

2563 2599 2736 2756 2889 2996 3078 3209 3320 3380

IBS 1059 1067 1099 1101 1119 1516 1530 2104 2143 2248 2807

IND 0357

IRA 0303 0312 0345 0575 0857 2054

IRM 0354

ISS 0737 0749 1125 1198 1823 1896 2102

IZG 0376 0407

JAT 2277 2621 2645

JAV 0029 2061

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 7

5

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

SERVICE BULLETIN

OPERATOR MSN

JBU 1123 1156 1173 1235 1240 1257 1270 1280 1302 1327 1398 1446

1452 1506 1528 1546 1557 1610 1650 1705 1739 1784 1785 1849

1861 1898 1904 1915 1917 1927 1948 2006 2020 2031 2042 2063

2075 2099 2125 2132 2136 2149 2150 2159 2160 2177 2201 2215

2231 2246 2259 2280 2284 2286 2307 2314 2336 2352 2368 2384

2386 2415 2447 2449 2461 2489 2491 2504 2520 2535 2577 2580

2640 2647 2671 2710 2725 2755

JSA 2316 2356 2423 2453 2604

JST 1195 1408 2169 2185 2197 2292 2299 2322 2329 2455 2515 2526

2537 2573 2587 2608 2642 2651 2703 2766 2787

JZR 2792 2822

KAC 0181 0182 0195 2046

KCA 0662

KFR 2650

KGL 0663 0668 0787 0852 0954 1060 1293 1554 2029 2077

KHO 0414

KHV 2480

KKK 0604 0614 0675 0761 0808 0823 0968 0974 1124 1438 1451 1503

1624 1730 1950 1953 2747 2753

KMF 0480

KNE 1942 1965 2123 2171 2182 2569 2776 3218 3361

KZR 1042 1204 3141

LAN 1304 1332 1351 1355 1491 1512 1526 1548 1568 1626 1854 1858

1877 1903 2089 2096 2295 2304 2321 2572 2585 2845 2858 2864

2872 2886 2887 2892 2894

LBT 0793 0937 1121 1175 1597 1744 2158

LFO 0659

LLC 0415 0990 1715 2987

LLM 1054 1918 1956 1967 1969 1993 2413 2419 2439

LLP 0739 0883 0914 1411 2016

LMJ 1868

LMU 0977 1366

LZB 2540 2596 3028

MAU 1592 1936

MDL 2600

MEA 1977 2055

MLD 0622 0741

MLM 2592

MLR 1946 2731 3106

MMA 0113 0114 0295 0316 0973 1180 1247 1791

MML 1706 1750

MON 0864 0983 1015 1045 1081 1153 1207 1320 1370 1413 1421 1428

1433 1571 1605 1637 1707 1763 1794 1941 2105 2234 2553 2610

2730 2793

MRJ 0530 1202 1300 1353

MSC 2937 2966 3282 3323

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 8

5

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

SERVICE BULLETIN

OPERATOR MSN

MSR 0165 0166 0178 0194 0198 0322 0366 0680 0687 0715 0725 2070

2073 2079 2088 2094

MXA 0252 0259 0260 0261 0275 0276 0296 0320 0321 0353

MYX 0566

NIA 3183 3219

NKS 2433 2470 2473 2476 2485 2490 2560 2567 2590 2603 2622 2673

2679 2698 2704 2711 2723 2797 2893 2898 2929 2942 2963 2978

2983 3007 3017 3026 3165

NLV 1998 2496 2502

NLY 2529 2668 2749 2867 2902

NMA 1697 1732 2676

NMB 3346

NVD 0211 0299 0375 0409 0419 0466 0528 0709 1778

NVR 2211 2216 2410

NWS 1219 1233 1276 1843 2649 2927 2933

OAW 1886

OHY 0364 0385 0455 0471 0496 0543 0640 0661 0676 0792 0806 0810

0811 0835 0912 0916 0963 1008 1482 1509 2571 2688

ORF 2566

OZW 0429 1922

PAL 2878 2925 2954

PIC 2331 2340 2670 2922 3012

PTI 1263

PTR 0459 0537

QAF 0927 1335

QTR 1487 1566 1648 1656 1773 1895 1928 1957 2097 2107 2121 2138

2161 2288 2341

R1T 1908

RBA 2023 2032 2135 2139 2195 3071

RBG 3152

RCT 1017

RFJ 0814

RJA 2953

RJD 1618

RNV 0229

RYW 0569

RZO 0795 2011 2390

S2A 0932 0943 2376

SAA 2268 2281 2308 2326 2355 2375 2379 2418 2438 2469 2501

SAI 0542 0877 1497 2027

SAS 1183 1383 1587 1619 1642 1675 1798 1807 1817 1848 2817 2850

2856 2883 2888 2911 2958 2990 3086 3159 3192 3231 3292

SBI 1071 1078 1090 1091 1126 1129 1131 1149 1164 1167 1819 1870

2028 2064 2076 2279 2369 2373 2464 2474 2618 2623 2641 2726

3070

SDM 0525 0649 1130 1488 1560 1578 1654 1657 1679 1743 1753 1761

1767 1851 1863 1876 1890 2465 2497 2879 2913 2930 2964 3044

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 9

5

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

SERVICE BULLETIN

OPERATOR MSN

SFJ 2658 3025

SFW 0734 0994 1018

SGG 0799 0879 1390

SHJ 0910

SHU 2222

SKU 0179 0406 0447 1400 1523 2119 2129 2214 2249 2251 2283 2378

2380 2436 2460 2548

SLK 0899 0969 1228 1422 1561 1698 2058 2252 2517 2568 2775 3104

SMX 2995

SND 1880 1999

SNX 0289

SOL 0302

SUD 3040

SVR 0140 0157 0203 0735 0775 0815 0841 0991 1012 1063 1152 1199

1484 1720 1751 1777 1884 1901 1905 2117 2166 2175 2187 2278

2327 2349 2707 2998 3099 3189

SVW 2921 3100 3133

SWM 0430 0476

SWR 0520 0522 0541 0545 0553 0559 0562 0574 0577 0578 0585 0596

0603 0612 0621 0635 0643 0664 0673 0681 0701 0703 0713 0727

0782 0987 1144 1762 1951 2134

SYR 0886 0918 1032 1076 1085 1117

TAE 0657 0934 0946 0949 1339 1368 1500 1934 2084 2659

TAI 1066 1334 1598 1625 1952 2282 2301 2339 2434 2444 2687 2862

2917 3042 3057 3103 3113 3378

TAK 2442 2446

TAM 1092 1096 1103 1139 1143 1158 1215 1246 1251 1376 1459 1486

1518 1575 1580 1591 1593 1595 1608 1613 1628 1652 1663 1672

1692 1717 1757 1771 1775 1801 1802 1804 1825 1826 1827 1831

1832 1835 1837 1855 1857 1888 1891 2014 2044 2372 2393 2467

2513 2661 2734 2737 2784 2838 2859 2896 2904 2924 3002 3032

3035 3047 3058 3111 3156 3180 3211

TAP 0629 0750 0755 0763 0790 0821 0837 0870 0906 0917 0933 0945

0960 0979 0982 1034 1100 1106 1120 1127 1165 1181 1206 1231

1307 1399 1667 1713 1756 1765 1799 1816 2178

TAR 0119 0123 0124 0205 0370 0390 0402 0511 0869 0880 0958 0975

1187 1479 1700 3096

TBJ 1485

TBZ 0361 0362 0405

TCW 0653 1787 1929 1975 2362

TCX 0677 1238 1250 2060 2114

TGW 2724 2728

THY 1002 1856 1909 1996 2156 2164 2395 2401 2404 2414 2452 2522

2602 2609 2626 2631 2655 2738 2739 2823 2868 2916 2919 2928

2934 2941 2984 2999 3010 3015 3126 3142 3185 3207 3208 3239

3257 3283 3303 3341 3350

TNA 0538 0555 0606 0731 0746 0791 0822 2914

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 10

5

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

SERVICE BULLETIN

OPERATOR MSN

TVS 2180

TWJ 2550

TXP 0607 0611 0617

UAL 0435 0439 0442 0450 0452 0454 0456 0457 0462 0463 0464 0465

0470 0472 0475 0479 0483 0485 0487 0489 0500 0503 0504 0506

0508 0510 0512 0523 0539 0568 0571 0587 0589 0592 0613 0638

0655 0678 0683 0686 0690 0702 0748 0751 0759 0780 0783 0788

0798 0804 0820 0824 0825 0826 0834 0836 0842 0843 0847 0850

0851 0858 0862 0865 0867 0871 0873 0882 0893 0898 0944 0948

0952 0955 0965 0980 0989 1001 1022 1031 1104 1105 1128 1146

1163 1192 1211 1243 1248 1266 1272 1282 1290 1291 1321 1341

1343 1359 1363 1401 1409 1420 1426 1427 1432 1435 1460 1469

1474 1475 1477 1495 1507 1508 1514 1522 1533 1538 1545 1555

1559 1569 1573 1581 1584 1585 1586 1600 1609 1617 1620 1627

1647 1649 1653 1664 1669 1671 1680 1688 1702 1728 1731 1737

1741 1755 1821 1840 1842 1845 1847 1865

UEA 2654 2696 2762 2774 2820 2835 3024

ULG 0308

USA 0052 0053 0054 0055 0064 0065 0066 0076 0077 0081 0082 0099

0317 0448 0565 0584 0762 0770 0803 0844 0856 0861 0863 0866

0868 0885 0889 0890 0896 0904 0922 0924 0929 0931 0953 0972

0997 1003 1019 1033 1038 1040 1043 1046 1049 1050 1051 1052

1055 1056 1061 1064 1065 1069 1075 1079 1083 1088 1095 1097

1109 1110 1111 1112 1114 1116 1122 1134 1135 1141 1148 1166

1178 1182 1196 1203 1205 1223 1224 1234 1245 1254 1264 1265

1268 1269 1274 1275 1281 1284 1287 1289 1294 1297 1298 1301

1310 1311 1313 1314 1315 1317 1319 1323 1326 1328 1331 1340

1342 1348 1350 1354 1358 1360 1369 1371 1373 1375 1378 1382

1389 1391 1393 1395 1397 1403 1406 1410 1412 1417 1419 1425

1431 1436 1442 1447 1455 1462 1463 1465 1472 1481 1490 1492

1496 1499 1517 1519 1521 1525 1527 1531 1534 1536 1539 1547

1552 1563 1565 1576 1621 1643 1644 1651 1666 1701 1704 1710

1724 1764 1792 1844 1935 2193 2302 2312 2405 2422 2430 2458

2482 2570 2595 2613 2615 2630 2669 2690

VAR 2383 2718

VIM 2732 3125

VIV 2157 2210 2443 2752

VJC 2712

VKG 1881 1887 1889 1921 1932 1954 1960 1972

VLE 1226

VLG 0992 1171 1208 1210 1221 1349 1372 1396 1430 1461 1540 1550

1694 1736 1749 1862 1914 1933 1979 2168 2207 2223 2388 2407

2479 2589 2620 2678 2761 2785 2794 2798 2843 2897 2962 2988

3083 3095 3109 3145 3151 3174 3203 3237 3293 3321 3376

VLK 0422 0714 0730 1200 1213 1379

VOI 2204 2296 2657 2666 2771 2780 2979 2997 3045 3069 3077 3175

3253 3279

VRD 2616 2674 2740 2773 2778 2800 2811 2830 2851 2993 3016 3037

3101 3135 3155 3181 3204 3349

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 11

5

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

SERVICE BULLETIN

OPERATOR MSN

VRE 1429 2213 2228

VVC 1306 1454 1564 1725 1867

WGT 1212

WHT 1256 2440 2675

WOW 2457

WRC 0235 0645 0684 0781 1869 2462 2682

WTJ 0548

WZZ 1834 1892 1902

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 12

5

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

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0029 0045 0046 0047 0049 0050 0051 0052 0053 0054 0055

0056 0057 0059 0064 0065 0066 0067 0068 0069 0070 0071

0072 0073 0074 0075 0076 0077 0078 0080 0081 0082 0083

0084 0085 0086 0087 0088 0090 0093 0094 0095 0096 0099

0104 0110 0111 0112 0113 0114 0115 0116 0117 0118 0119

0121 0122 0123 0124 0125 0126 0127 0135 0137 0138 0140

0141 0142 0147 0148 0149 0150 0152 0153 0154 0157 0158

0159 0160 0161 0162 0164 0165 0166 0167 0168 0171 0172

0173 0174 0175 0176 0178 0179 0181 0182 0183 0185 0189

0190 0192 0194 0195 0197 0198 0199 0200 0201 0202 0203

0205 0206 0207 0208 0209 0210 0211 0212 0213 0214 0216

0217 0218 0219 0220 0223 0224 0229 0230 0231 0232 0233

0234 0235 0237 0239 0240 0241 0242 0243 0244 0248 0249

0251 0252 0253 0254 0255 0256 0259 0260 0261 0262 0263

0264 0265 0266 0267 0268 0269 0270 0272 0273 0274 0275

0276 0277 0279 0281 0282 0284 0285 0287 0289 0290 0291

0292 0293 0294 0295 0296 0297 0298 0299 0300 0301 0302

0303 0306 0307 0308 0309 0311 0312 0314 0316 0317 0318

0319 0320 0321 0322 0323 0324 0325 0328 0329 0330 0331

0332 0333 0339 0340 0341 0342 0343 0345 0346 0347 0349

0350 0351 0353 0354 0355 0356 0357 0358 0359 0360 0361

0362 0364 0366 0367 0368 0370 0371 0372 0373 0375 0376

0378 0380 0381 0382 0383 0384 0385 0386 0387 0388 0390

0391 0393 0395 0396 0398 0399 0400 0401 0402 0403 0404

0405 0406 0407 0408 0409 0410 0412 0413 0414 0415 0416

0417 0418 0419 0420 0421 0422 0423 0424 0426 0427 0428

0429 0430 0431 0432 0434 0435 0436 0438 0439 0441 0442

0444 0445 0447 0448 0449 0450 0451 0452 0454 0455 0456

0457 0458 0459 0460 0462 0463 0464 0465 0466 0468 0469

0470 0471 0472 0473 0474 0475 0476 0477 0479 0480 0482

0483 0484 0485 0486 0487 0488 0489 0490 0491 0492 0493

0494 0495 0496 0497 0498 0499 0500 0501 0502 0503 0504

0505 0506 0507 0508 0509 0510 0511 0512 0513 0514 0515

0516 0517 0518 0519 0520 0521 0522 0523 0524 0525 0526

0527 0528 0529 0530 0531 0532 0533 0534 0535 0537 0538

0539 0540 0541 0542 0543 0544 0545 0546 0548 0549 0550

0551 0552 0553 0554 0555 0556 0557 0558 0559 0560 0561

0562 0563 0564 0565 0566 0567 0568 0569 0570 0571 0572

0573 0574 0575 0576 0577 0578 0579 0580 0581 0582 0583

0584 0585 0586 0587 0588 0589 0591 0592 0593 0594 0595

0596 0597 0598 0599 0600 0603 0604 0605 0606 0607 0608

0609 0610 0611 0612 0613 0614 0616 0617 0618 0619 0620

0621 0622 0623 0625 0627 0629 0630 0631 0633 0634 0635

0636 0637 0638 0639 0640 0641 0642 0643 0644 0645 0646

0647 0648 0649 0650 0651 0652 0653 0654 0655 0656 0657

0658 0659 0660 0661 0662 0663 0664 0665 0666 0667 0668

0669 0670 0672 0673 0674 0675 0676 0677 0678 0679 0680

0681 0682 0683 0684 0685 0686 0687 0688 0689 0690 0691

0692 0693 0694 0695 0696 0697 0698 0699 0700 0701 0702

001

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 13

5

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

SERVICE BULLETIN

MSN CONFIGURATION

0703 0704 0705 0706 0707 0709 0711 0712 0713 0714 0715

0716 0717 0718 0719 0720 0721 0722 0723 0724 0725 0726

0727 0728 0729 0730 0731 0732 0733 0734 0735 0736 0737

0738 0739 0740 0741 0742 0743 0744 0745 0746 0747 0748

0749 0750 0751 0752 0754 0755 0756 0757 0758 0759 0760

0761 0762 0763 0764 0765 0766 0767 0768 0769 0770 0771

0772 0773 0774 0775 0776 0777 0778 0779 0780 0781 0782

0783 0784 0785 0786 0787 0788 0790 0791 0792 0793 0794

0795 0796 0797 0798 0799 0800 0801 0802 0803 0804 0805

0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816

0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827

0828 0829 0830 0831 0832 0833 0834 0835 0836 0837 0838

0839 0840 0841 0842 0843 0844 0845 0846 0847 0848 0849

0850 0851 0852 0853 0854 0855 0856 0857 0858 0859 0860

0861 0862 0863 0864 0865 0866 0867 0868 0869 0870 0871

0872 0873 0874 0875 0876 0877 0878 0879 0880 0881 0882

0883 0884 0885 0886 0887 0888 0889 0890 0891 0892 0893

0894 0895 0896 0897 0898 0899 0900 0901 0902 0903 0904

0905 0906 0907 0908 0909 0910 0911 0912 0913 0914 0915

0916 0917 0918 0919 0920 0921 0922 0923 0924 0925 0926

0927 0928 0929 0930 0931 0932 0933 0934 0935 0936 0937

0938 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948

0949 0950 0951 0952 0953 0954 0955 0957 0958 0959 0960

0961 0962 0963 0964 0965 0966 0967 0968 0969 0970 0971

0972 0973 0974 0975 0976 0977 0978 0979 0980 0981 0982

0983 0984 0985 0986 0987 0988 0989 0990 0991 0992 0993

0994 0995 0996 0997 0998 0999 1000 1001 1002 1003 1004

1005 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015

1016 1017 1018 1019 1020 1021 1022 1023 1024 1025 1026

1027 1028 1029 1030 1031 1032 1033 1034 1035 1036 1037

1038 1039 1040 1041 1042 1043 1045 1046 1047 1048 1049

1050 1051 1052 1053 1054 1055 1056 1057 1058 1059 1060

1061 1062 1063 1064 1065 1066 1067 1068 1069 1070 1071

1072 1073 1074 1075 1076 1077 1078 1079 1080 1081 1082

1083 1084 1085 1086 1087 1088 1089 1090 1091 1092 1093

1094 1095 1096 1097 1098 1099 1100 1101 1102 1103 1104

1105 1106 1107 1108 1109 1110 1111 1112 1114 1115 1116

1117 1118 1119 1120 1121 1122 1123 1124 1125 1126 1127

1128 1129 1130 1131 1132 1133 1134 1135 1136 1137 1138

1139 1140 1141 1142 1143 1144 1145 1146 1147 1148 1149

1150 1151 1152 1153 1154 1155 1156 1157 1158 1159 1160

1161 1162 1163 1164 1165 1166 1167 1168 1169 1170 1171

1172 1173 1174 1175 1176 1177 1178 1179 1180 1181 1182

1183 1184 1185 1187 1188 1189 1190 1191 1192 1193 1194

1195 1196 1197 1198 1199 1200 1201 1202 1203 1204 1205

1206 1207 1208 1209 1210 1211 1212 1213 1214 1215 1216

1217 1219 1220 1221 1222 1223 1224 1225 1226 1227 1228

1229 1230 1231 1232 1233 1234 1235 1236 1237 1238 1239

1240 1241 1242 1243 1244 1245 1246 1247 1248 1249 1250

1251 1252 1253 1254 1255 1256 1257 1258 1259 1260 1261

1262 1263 1264 1265 1266 1267 1268 1269 1270 1271 1272

001

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 14

5

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

SERVICE BULLETIN

MSN CONFIGURATION

1273 1274 1275 1276 1277 1279 1280 1281 1282 1283 1284

1285 1286 1287 1288 1289 1290 1291 1292 1293 1294 1295

1296 1297 1298 1299 1300 1301 1302 1303 1304 1305 1306

1307 1308 1309 1310 1311 1312 1313 1314 1315 1316 1317

1318 1319 1320 1321 1322 1323 1324 1325 1326 1327 1328

1329 1330 1331 1332 1334 1335 1336 1337 1338 1339 1340

1341 1342 1343 1344 1345 1346 1347 1348 1349 1350 1351

1352 1353 1354 1355 1356 1357 1358 1359 1360 1361 1362

1363 1364 1365 1366 1367 1368 1369 1370 1371 1372 1373

1375 1376 1377 1378 1379 1380 1381 1382 1383 1384 1385

1386 1387 1388 1389 1390 1391 1392 1393 1394 1395 1396

1397 1398 1399 1400 1401 1402 1403 1404 1405 1406 1407

1408 1409 1410 1411 1412 1413 1414 1415 1416 1417 1418

1419 1420 1421 1422 1423 1424 1425 1426 1427 1428 1429

1430 1431 1432 1433 1434 1435 1436 1437 1438 1439 1440

1441 1442 1443 1444 1445 1446 1447 1448 1449 1450 1451

1452 1453 1454 1455 1456 1457 1458 1459 1460 1461 1462

1463 1465 1466 1467 1468 1469 1470 1471 1472 1473 1474

1475 1476 1477 1478 1479 1480 1481 1482 1483 1484 1485

1486 1487 1488 1489 1490 1491 1492 1493 1494 1495 1496

1497 1498 1499 1500 1501 1502 1503 1504 1505 1506 1507

1508 1509 1510 1511 1512 1513 1514 1515 1516 1517 1518

1519 1520 1521 1522 1523 1524 1525 1526 1527 1528 1529

1530 1531 1532 1533 1534 1535 1536 1537 1538 1539 1540

1541 1542 1543 1544 1545 1546 1547 1548 1549 1550 1551

1552 1553 1554 1555 1556 1557 1558 1559 1560 1561 1562

1563 1564 1565 1566 1567 1568 1569 1570 1571 1572 1573

1574 1575 1576 1577 1578 1579 1580 1581 1582 1583 1584

1585 1586 1587 1588 1589 1590 1591 1592 1593 1594 1595

1596 1597 1598 1599 1600 1601 1602 1603 1604 1605 1606

1607 1608 1609 1610 1611 1612 1613 1614 1615 1616 1617

1618 1619 1620 1621 1622 1623 1624 1625 1626 1627 1628

1629 1630 1631 1632 1633 1634 1635 1636 1637 1638 1639

1640 1641 1642 1643 1644 1645 1646 1647 1648 1649 1650

1651 1652 1653 1654 1655 1656 1657 1658 1659 1661 1662

1663 1664 1665 1666 1667 1668 1669 1670 1671 1672 1673

1674 1675 1677 1678 1679 1680 1681 1682 1683 1684 1685

1686 1687 1688 1689 1690 1691 1692 1693 1694 1695 1696

1697 1698 1699 1700 1701 1702 1703 1704 1705 1706 1707

1708 1709 1710 1711 1712 1713 1714 1715 1716 1717 1718

1719 1720 1721 1722 1723 1724 1725 1726 1727 1728 1730

1731 1732 1733 1734 1735 1736 1737 1738 1739 1740 1741

1742 1743 1744 1745 1746 1747 1748 1749 1750 1751 1752

1753 1754 1755 1756 1757 1758 1759 1760 1761 1762 1763

1764 1765 1766 1767 1769 1770 1771 1772 1773 1774 1775

1776 1777 1778 1779 1780 1781 1782 1783 1784 1785 1786

1787 1788 1789 1790 1791 1792 1793 1794 1795 1796 1797

1798 1799 1800 1801 1802 1803 1804 1805 1806 1807 1808

1809 1810 1811 1812 1814 1815 1816 1817 1818 1819 1820

1821 1823 1824 1825 1826 1827 1828 1829 1831 1832 1833

1834 1835 1836 1837 1838 1839 1840 1841 1842 1843 1844

001

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 15

5

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

SERVICE BULLETIN

MSN CONFIGURATION

1845 1846 1847 1848 1849 1850 1851 1852 1853 1854 1855

1856 1857 1858 1859 1860 1861 1862 1863 1864 1865 1866

1867 1868 1869 1870 1871 1872 1873 1874 1875 1876 1877

1878 1879 1880 1881 1882 1883 1884 1885 1886 1887 1888

1889 1890 1891 1892 1893 1894 1895 1896 1897 1898 1899

1900 1901 1902 1903 1904 1905 1906 1907 1908 1909 1910

1911 1912 1913 1914 1915 1916 1917 1918 1920 1921 1922

1923 1924 1925 1926 1927 1928 1929 1931 1932 1933 1934

1935 1936 1937 1938 1940 1941 1942 1943 1944 1945 1946

1947 1948 1949 1950 1951 1952 1953 1954 1955 1956 1957

1958 1959 1960 1961 1962 1963 1964 1965 1966 1967 1968

1969 1970 1971 1972 1973 1974 1975 1976 1977 1978 1979

1980 1981 1982 1983 1984 1986 1987 1988 1989 1990 1993

1994 1995 1996 1997 1998 1999 2000 2001 2002 2003 2004

2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015

2016 2017 2018 2019 2020 2021 2022 2023 2024 2026 2027

2028 2029 2030 2031 2032 2033 2034 2035 2036 2037 2038

2039 2040 2041 2042 2043 2044 2045 2046 2047 2048 2049

2050 2052 2053 2054 2055 2056 2057 2058 2059 2060 2061

2062 2063 2064 2065 2066 2067 2068 2069 2070 2071 2072

2073 2074 2075 2076 2077 2078 2079 2080 2081 2082 2083

2084 2085 2086 2087 2088 2089 2090 2091 2092 2093 2094

2095 2096 2097 2098 2099 2100 2101 2102 2103 2104 2105

2106 2107 2108 2109 2110 2112 2113 2114 2115 2116 2117

2118 2119 2120 2121 2122 2123 2124 2125 2126 2127 2128

2129 2130 2131 2132 2133 2134 2135 2136 2137 2138 2139

2140 2141 2142 2143 2144 2145 2146 2147 2148 2149 2150

2151 2152 2153 2154 2155 2156 2157 2158 2159 2160 2161

2162 2163 2164 2165 2166 2167 2168 2169 2170 2171 2172

2173 2174 2175 2176 2177 2178 2179 2180 2181 2182 2183

2184 2185 2186 2187 2188 2189 2190 2191 2192 2193 2194

2195 2196 2197 2198 2199 2200 2201 2202 2203 2204 2205

2206 2207 2208 2209 2210 2211 2212 2213 2214 2215 2216

2217 2219 2220 2221 2222 2223 2224 2225 2226 2227 2228

2229 2230 2231 2232 2233 2234 2235 2236 2237 2238 2239

2240 2241 2242 2243 2244 2245 2246 2247 2248 2249 2250

2251 2252 2253 2254 2255 2256 2257 2258 2259 2260 2261

2262 2263 2264 2265 2266 2267 2268 2269 2270 2271 2272

2273 2274 2275 2277 2278 2279 2280 2281 2282 2283 2284

2285 2286 2287 2288 2289 2290 2291 2292 2293 2294 2295

2296 2297 2298 2299 2300 2301 2302 2303 2304 2305 2306

2307 2308 2309 2310 2311 2312 2313 2314 2315 2316 2317

2318 2319 2320 2321 2322 2323 2324 2325 2326 2327 2328

2329 2330 2331 2332 2333 2334 2335 2336 2337 2338 2339

2340 2341 2342 2343 2344 2345 2346 2347 2348 2349 2350

2351 2352 2353 2354 2355 2356 2357 2358 2359 2360 2361

2362 2363 2364 2365 2366 2367 2368 2369 2370 2371 2372

2373 2374 2375 2376 2377 2378 2379 2380 2381 2382 2383

2384 2385 2386 2387 2388 2389 2390 2391 2392 2393 2394

2395 2396 2397 2398 2399 2400 2401 2402 2403 2404 2405

2406 2407 2408 2409 2410 2411 2412 2413 2414 2415 2416

001

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 16

5

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

SERVICE BULLETIN

MSN CONFIGURATION

2417 2418 2419 2420 2421 2422 2423 2425 2426 2427 2428

2429 2430 2431 2432 2433 2434 2435 2436 2437 2438 2439

2440 2441 2442 2443 2444 2445 2446 2447 2448 2449 2450

2451 2452 2453 2454 2455 2456 2457 2458 2459 2460 2461

2462 2463 2464 2465 2466 2467 2468 2469 2470 2471 2472

2473 2474 2475 2476 2477 2478 2479 2480 2481 2482 2483

2484 2485 2486 2487 2488 2489 2490 2491 2492 2493 2494

2495 2496 2497 2498 2499 2501 2502 2503 2504 2505 2506

2507 2508 2509 2510 2511 2512 2513 2514 2515 2516 2517

2518 2519 2520 2521 2522 2523 2524 2525 2526 2527 2528

2529 2530 2531 2532 2533 2534 2535 2536 2537 2538 2539

2540 2541 2542 2543 2544 2545 2546 2547 2548 2549 2550

2551 2552 2553 2554 2555 2556 2557 2558 2559 2560 2561

2562 2563 2564 2565 2566 2567 2568 2569 2570 2571 2572

2573 2574 2575 2576 2577 2578 2579 2580 2581 2582 2583

2584 2585 2586 2587 2588 2589 2590 2591 2592 2593 2594

2595 2596 2597 2598 2599 2600 2601 2602 2603 2604 2605

2606 2607 2608 2609 2610 2611 2612 2613 2614 2615 2616

2617 2618 2619 2620 2621 2622 2623 2624 2625 2626 2627

2628 2629 2630 2631 2632 2633 2634 2635 2636 2637 2638

2639 2640 2641 2642 2643 2644 2645 2646 2647 2648 2649

2650 2651 2652 2653 2654 2655 2656 2657 2658 2659 2660

2661 2662 2663 2664 2665 2666 2667 2668 2669 2670 2671

2672 2673 2674 2675 2676 2677 2678 2679 2680 2681 2682

2683 2684 2685 2686 2687 2688 2689 2690 2691 2692 2693

2694 2695 2696 2697 2698 2699 2700 2701 2702 2703 2704

2705 2706 2707 2708 2709 2710 2711 2712 2713 2714 2715

2716 2717 2718 2719 2720 2721 2723 2724 2725 2726 2727

2728 2729 2730 2731 2732 2733 2734 2735 2736 2737 2738

2739 2740 2741 2742 2743 2744 2745 2746 2747 2748 2749

2750 2751 2752 2753 2754 2755 2756 2757 2758 2759 2760

2761 2762 2763 2764 2765 2766 2767 2768 2769 2770 2771

2772 2773 2774 2775 2776 2777 2778 2779 2780 2782 2783

2784 2785 2786 2787 2788 2789 2790 2791 2792 2793 2794

2795 2796 2797 2798 2799 2800 2801 2803 2804 2805 2806

2807 2808 2809 2810 2811 2812 2813 2815 2816 2817 2818

2819 2820 2821 2822 2823 2824 2825 2826 2827 2828 2829

2830 2831 2833 2834 2835 2836 2837 2838 2839 2840 2841

2842 2843 2844 2845 2846 2847 2849 2850 2851 2852 2853

2854 2855 2856 2857 2858 2859 2860 2861 2862 2863 2864

2865 2866 2867 2868 2869 2870 2872 2873 2874 2875 2876

2877 2878 2879 2881 2882 2883 2884 2885 2886 2887 2888

2889 2890 2891 2892 2893 2894 2895 2896 2897 2898 2899

2901 2902 2903 2904 2905 2906 2907 2908 2909 2910 2911

2912 2913 2914 2915 2916 2917 2918 2919 2920 2921 2922

2923 2924 2925 2926 2927 2928 2929 2930 2932 2933 2934

2935 2936 2937 2938 2939 2940 2941 2942 2943 2944 2946

2947 2948 2949 2950 2951 2952 2953 2954 2956 2957 2958

2959 2960 2961 2962 2963 2964 2965 2966 2967 2968 2969

2971 2972 2973 2974 2975 2976 2978 2979 2980 2981 2982

2983 2984 2985 2986 2987 2988 2989 2990 2991 2993 2995

001

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 17

5

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

SERVICE BULLETIN

MSN CONFIGURATION

2996 2997 2998 2999 3000 3002 3003 3004 3005 3006 3007

3008 3009 3010 3011 3012 3013 3014 3015 3016 3017 3018

3019 3020 3021 3022 3023 3024 3025 3026 3027 3028 3031

3032 3035 3036 3037 3040 3041 3042 3043 3044 3045 3046

3047 3049 3050 3051 3052 3053 3054 3055 3056 3057 3058

3059 3060 3061 3063 3064 3065 3067 3068 3069 3070 3071

3073 3075 3076 3077 3078 3079 3080 3081 3082 3083 3084

3085 3086 3088 3090 3093 3094 3095 3096 3097 3098 3099

3100 3101 3102 3103 3104 3106 3109 3111 3112 3113 3114

3116 3117 3118 3121 3122 3124 3125 3126 3129 3131 3132

3133 3134 3135 3136 3137 3138 3139 3140 3141 3142 3144

3145 3147 3148 3151 3152 3153 3154 3155 3156 3159 3161

3162 3165 3168 3169 3173 3174 3175 3176 3179 3180 3181

3182 3183 3184 3185 3186 3188 3189 3192 3194 3195 3198

3199 3200 3201 3202 3203 3204 3206 3207 3208 3209 3211

3215 3218 3219 3221 3223 3224 3226 3231 3232 3234 3236

3237 3239 3242 3244 3245 3246 3253 3255 3257 3261 3268

3272 3275 3277 3279 3282 3283 3285 3289 3291 3292 3293

3296 3297 3299 3303 3315 3316 3318 3320 3321 3323 3327

3332 3337 3338 3341 3345 3346 3349 3350 3353 3355 3361

3363 3366 3368 3370 3376 3377 3378 3379 3380 3383

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

Kit 541019A01R01 2

Component COMPA01 2

Consumable CMLA01 1

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Several operators reported cracks on the two corner fittings at RIB11 lower attachment

level, in the pylon aft fixed secondary structure.

Improved fittings, having thicker faces with shot peened surfaces, have been designed

and introduced in production.

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 18

5

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

SERVICE BULLETIN

(2) Objective/Action

This Service Bulletin recommends the replacement of the two corner fittings by new

improved fittings for in-service aircraft.

(3) Advantages

Accomplishment of this Service Bulletin will prevent cracking occurrence at this location.

Due to access requirements to the area, AIRBUS informs of an improvement of the aft

fixed secondary structure : accomplishment of Service Bulletin No. A320-54-1013 (Mod.

No. 31705P7399) could be performed simultaneously.

(4) Operational/Maintenance Consequences

Accomplishment of this Service Bulletin cancels the requirements of Inspection Service

Bulletin No. A320-54-1022.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

Task 541019-831-801-001: MODIFICATION

(1) Remove the Corner Fittings on LH Pylon

(2) Remove the Corner Fittings on RH Pylon

(3) Install the Corner Fittings on LH Pylon

(4) Install the Corner Fittings on RH Pylon

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.

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: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 19

5

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.

For an explanation of the manhours and elapsed time, refer to the Gantt Chart given in

Appendix 01 - Elapsed Time Assumption .

Task 541019-831-801-001: MODIFICATION

Get Access 20.00

On Aircraft

Remove the Corner Fittings on LH Pylon 2.50

Remove the Corner Fittings on RH Pylon 2.50

Install the Corner Fittings on LH Pylon 6.00

Install the Corner Fittings on RH Pylon 6.00

Close-Up 22.00

TOTAL MANHOURS 59.00

ELAPSED TIME (HOURS) 29.50

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-41-54 12-34-24 20-21-11

54-54-00 54-55-00 54-56-00

Consumable Material List (CML)

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-40-00 51-42-00 51-43-00

51-44-00 51-47-00

K. PUBLICATION AFFECTED

Structural Repair Manual (SRM) 54-54-17

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 20

5

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:

Kit 541019A01R01 AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 2590

For ordering by E-mail: airbus.kit@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 COMPA01 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

Kit 541019A01R01

Cost 1,200.00 USD

Availability 150 calendar days from receipt of order

The availability given above is the standard lead time from the date of your purchase

order. If items are required before this time, please include a retrofit planning schedule

with your order so that we can try to comply with your requirements.

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 21

5

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

SERVICE BULLETIN

The sales terms (costs and availability) are estimated in relation to economic conditions.

The latest valid price and lead time for ordering purposes shall be obtained through the

AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.

Component COMPA01

Operator supplied standard hardware parts required to accomplish this Service Bulletin

are to be supplied from the operator’s stock.

B. INDUSTRY SUPPORT INFORMATION

As a special policy applied to this Service Bulletin, AIRBUS will provide a 20% reduction to

the applicable kits sales prices given in the paragraph ’Price and Availability’ for orders placed

before Dec 31/16.

As a special policy applied to this Service Bulletin, for the accomplishment of this modification

before Dec 31/16, AIRBUS will credit a 20% reduction to the applicable operator supplied

standard hardware parts sales prices for claims received not later than 90 days after

completion of the last affected aircraft of your fleet.

C. LIST OF COMPONENTS

Kit 541019A01R01

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

NOTES

1 D0041092120000 1 CORNER

2 D0041092120100 1 CORNER

12 NSA5414-40-18 6 RIVET

20 NAS1726-4E 10 NUT

21 ASNA2050DXJ4020 18 RIVET

22 NSA5415-40-18 4 RIVET

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.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-Fuel Tank Fillet 06ABB1 As required

Non Hardening Jointing PuttyMedium Temp. Area06LCG9 As required

Non Aqueous Cleaner - General 08BAA9 As required

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 22

5

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

SERVICE BULLETIN

(2) Components

Component COMPA01

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

NOTES

23 ASNA2051DCJ3620 2 RIVET

24 NSA5414-36-18 6 RIVET

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

F. TOOLING

None

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 23

5

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

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 24

5

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

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 541019-831-801-001 - 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.

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.

Task Associated Data

Zone

470 480

Access

Panel 475AL 476AR 485AL 486AR

Manpower

TOTAL MANHOURS 59.00

ELAPSED TIME (HOURS) 29.50

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 25

5

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

SERVICE BULLETIN

A. GENERAL

(1) Subtask 541019-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

Task 20-21-11-911-001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-40-00

51-42-00

51-43-00

51-44-00

51-47-00

(a) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to

the Consumable Material List (CML).

(b) For the identification of access panels, refer to AMM 06-41-54, Page Block 001.

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

(d) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.

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

(f) If alternative and substitute fasteners have to be used, you must make sure that the

associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating

Part" column.

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

20-21-11-911-001.

(h) Obtain fasteners spacing and margin data, in accordance with SRM 51-47-00.

(i) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(2) Subtask 541019-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 26

5

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

SERVICE BULLETIN

B. PREPARATION

(1) Subtask 541019-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

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

(a) The following items 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.

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

12-34-24-869-002.

(c) Put an access platform in position.

(2) Subtask 541019-941-001-001 - Get Access at LH Pylon

Work Zones and Access Panels

Zone Access/Work location

470 Access Panel 475AL, Panel 476AR

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

Task 54-54-00-000-001

Task 54-55-00-000-001

Task 54-56-00-000-001

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 27

5

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

SERVICE BULLETIN

References

Fig. A-FBDAA

Removal/Installation of the Drain Pipes

Sheet 01

Sheet 02

Sheet 03

(a) Remove the access panels 475AL and 476AR for access, refer to AMM 06-41-54

Page Block 001.

(b) Remove the Aft Movable Fairing for access, refer to AMM Task 54-55-00-000-001.

(c) Remove the Lower Fairing for access, refer to AMM Task 54-56-00-000-001.

(d) Remove the Aft Fixed Fairing, refer to AMM Task 54-54-00-000-001.

(e) Depending on aircraft configuration, remove the Drain Pipes for access, refer to

Fig. A-FBDAA.

1 Remove:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 02.

1 Pipe Item (30) Retain

1 Pipe Item (31) Retain

2 Or remove:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03.

1 Pipe Item (32) Retain

1 Pipe Item (33) Retain

1 Pipe Item (35) Retain

1 Pipe Item (36) Retain

1 Drain Clamp Item (34) Retain

attached with

3 Screw Item (38) Retain

3 Washer Item (39) Retain

(3) Subtask 541019-941-002-001 - Get Access at RH Pylon

Work Zones and Access Panels

Zone Access/Work location

480 Access Panel 485AL, Panel 486AR

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 28

5

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

SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

Task 54-54-00-000-001

Task 54-55-00-000-001

Task 54-56-00-000-001

Fig. A-FBDAA

Removal/Installation of the Drain Pipes

Sheet 01

Sheet 02

Sheet 03

(a) Remove the access panels 485AL and 486AR for access, refer to AMM 06-41-54

Page Block 001.

(b) Remove the Aft Movable Fairing for access, refer to AMM Task 54-55-00-000-001.

(c) Remove the Lower Fairing for access, refer to AMM Task 54-56-00-000-001.

(d) Remove the Aft Fixed Fairing, refer to AMM Task 54-54-00-000-001.

(e) Depending on aircraft configuration, remove the Drain Pipes for access, refer to

Fig. A-FBDAA.

1 Remove:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 02.

1 Pipe Item (30) Retain

1 Pipe Item (31) Retain

2 Or remove:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03.

1 Pipe Item (32) Retain

1 Pipe Item (33) Retain

1 Pipe Item (35) Retain

1 Pipe Item (36) Retain

1 Drain Clamp Item (34) Retain

attached with

3 Screw Item (38) Retain

3 Washer Item (39) Retain

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 29

5

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

SERVICE BULLETIN

C. PROCEDURE

(1) Subtask 541019-831-002-001 - Remove the Corner Fittings on LH Pylon

Work Zones and Access Panels

Zone Access/Work location

470

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills AIRFRAME

Material necessary to do the job

Kit 541019A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 D0041092120000 1 CORNER

2 D0041092120100 1 CORNER

References

Structural Repair Manual (SRM) 51-42-00

51-44-00

51-47-00

Fig. A-FBAAA

Removal of the Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBBAA

Installation of the New Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBCAA

Removal/Installation of the Fasteners of

RIB11

Sheet 01

Sheet 02

Sheet 03

(a) Remove the corner fittings:

Refer to Figure Fig. A-FBAAA, Fig. A-FBBAA and Fig. A-FBCAA.

In accordance with SRM 51-42-00.

In accordance with SRM 51-44-00.

In accordance with SRM 51-47-00.

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 30

5

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

SERVICE BULLETIN

1 Remove the lower fitting:

Refer to Figure Fig. A-FBAAA, Sheets Fig. A-FBAAA Sheet 02 thru Fig. AFBAAA Sheet 04

a Remove :

1 Lower Fitting Item (5) Retain

attached with

4 Screw Item (18) Retain

6 Screw Item (17) Retain

10 Nut Item (20) Discard

2 Remove the fasteners from the Rib 11:

Refer to Fig. A-FBCAA Sheet 01 thru Fig. A-FBCAA Sheet 03 and Fig. AFBAAA Sheet 01 thru Fig. A-FBAAA Sheet 02.

a Remove :

2 Rivet Item (23) Discard

6 Rivet Item (24) Discard

2 Rivet Item (21) Discard

NOTE: For a better access, move the Rib 11 without removal

(max 20 mm (0.787 in.)).

3 Remove the corner fittings Item (1) :

Refer to Fig. A-FBAAA Sheet 01 thru Fig. A-FBAAA Sheet 05.

a Remove:

1 Corner Fitting Item (1) Discard

attached with

3 Rivet Item (11) Discard

2 Rivet Item (14) Discard

8 Rivet Item (15) Discard

4 Temporarily put in position the new Corner Fitting Item 1 on the structure:

Refer to Fig. A-FBBAA Sheet 01 thru Fig. A-FBBAA Sheet 05

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 31

5

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

SERVICE BULLETIN

1 Corner Fitting D0041092120000 Item 1

- Drill the holes on the new Corner Fitting Item 1 to align with the existing

holes of the structure.

- Remove the new Corner Fitting Item 1.

- Temporarily put in position the new Corner Fitting Item 1.

5 Remove the corner fittings Item (2) :

Refer to Fig. A-FBAAA Sheet 01 thru Fig. A-FBAAA Sheet 05.

a Remove:

1 Corner Fitting Item (2) Discard

attached with

3 Rivet Item (11) Discard

2 Rivet Item (14) Discard

8 Rivet Item (15) Discard

1 Rivet Item (21) Discard

6 Temporarily put in position the new Corner Fitting Item 2 on the structure:

Refer to Fig. A-FBBAA Sheet 01 thru Fig. A-FBBAA Sheet 05

1 Corner Fitting D0041092120100 Item 2

- Drill the holes on the new Corner Fitting Item 2 to align with the existing

holes of the structure.

- Remove the new Corner Fitting Item 2.

7 Remove the corner fitting Item 1.

(2) Subtask 541019-831-003-001 - Remove the Corner Fittings on RH Pylon

Work Zones and Access Panels

Zone Access/Work location

480

Manpower Resources

Manhours 2.50

Minimum number of person 1

Subtask elapsed time 2.50

Skills AIRFRAME

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 32

5

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

SERVICE BULLETIN

Material necessary to do the job

Kit 541019A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 D0041092120000 1 CORNER

2 D0041092120100 1 CORNER

References

Structural Repair Manual (SRM) 51-42-00

51-44-00

51-47-00

Fig. A-FBAAA

Removal of the Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBBAA

Installation of the New Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBCAA

Removal/Installation of the Fasteners of

RIB11

Sheet 01

Sheet 02

Sheet 03

(a) Remove the Corner fittings:

Refer to Figure Fig. A-FBAAA, Fig. A-FBBAA and Fig. A-FBCAA.

In accordance with SRM 51-42-00.

In accordance with SRM 51-44-00.

In accordance with SRM 51-47-00.

1 Remove the lower fitting:

Refer to Figure Fig. A-FBAAA, Sheets Fig. A-FBAAA Sheet 02 thru Fig. AFBAAA Sheet 04.

a Remove :

1 Lower Fitting Item (5) Retain

attached with

4 Screw Item (18) Retain

6 Screw Item (17) Retain

10 Nut Item (20) Discard

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 33

5

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

SERVICE BULLETIN

2 Remove the fasteners from the Rib 11:

Refer to Fig. A-FBCAA Sheet 01 thru Fig. A-FBCAA Sheet 03 and Fig. AFBAAA Sheet 01 thru Fig. A-FBAAA Sheet 02.

a Remove :

2 Rivet Item (23) Discard

6 Rivet Item (24) Discard

2 Rivet Item (21) Discard

NOTE: For a better access, move the Rib 11 without removal

(max 20 mm (0.787 in.)).

3 Remove the corner fittings Item (1) :

Refer toFig. A-FBAAA Sheet 01 thru Fig. A-FBAAA Sheet 05.

a Remove:

1 Corner Fitting Item (1) Discard

attached with

3 Rivet Item (11) Discard

2 Rivet Item (14) Discard

8 Rivet Item (15) Discard

4 Temporarily put in position the new Corner Fitting Item 1 on the structure:

Refer to Fig. A-FBBAA Sheet 01 thru Fig. A-FBBAA Sheet 05

1 Corner Fitting D0041092120000 Item 1

- Drill the holes on the new Corner Fitting Item 1 to align with the existing

holes of the structure.

- Remove the new Corner Fitting Item 1.

- Temporarily put in position the new Corner Fitting Item 1.

5 Remove the corner fittings Item (2) :

Refer to Fig. A-FBAAA Sheet 01 thru Fig. A-FBAAA Sheet 05.

a Remove:

1 Corner Fitting Item (2) Discard

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 34

5

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

SERVICE BULLETIN

attached with

3 Rivet Item (11) Discard

2 Rivet Item (14) Discard

8 Rivet Item (15) Discard

1 Rivet Item (21) Discard

6 Temporarily put in position the new Corner Fitting Item 2 on the structure:

Refer to Fig. A-FBBAA Sheet 01 thru Fig. A-FBBAA Sheet 05

1 Corner Fitting D0041092120100 Item 2

- Drill the holes on the new Corner Fitting Item 2 to align with the existing

holes of the structure.

- Remove the new Corner Fitting Item 2.

7 Remove the Corner Fitting Item 1.

(3) Subtask 541019-831-004-001 - Install the Corner Fittings on LH Pylon

Work Zones and Access Panels

Zone Access/Work location

470

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills AIRFRAME

Material necessary to do the job

Kit 541019A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 D0041092120000 1 CORNER

2 D0041092120100 1 CORNER

12 NSA5414-40-18 6 RIVET

20 NAS1726-4E 10 NUT

21 ASNA2050DXJ4020 18 RIVET

22 NSA5415-40-18 4 RIVET

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 35

5

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

SERVICE BULLETIN

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

23 ASNA2051DCJ3620 2 RIVET

24 NSA5414-36-18 6 RIVET

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

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Hardening Jointing

Putty-Medium Temp. Area

06LCG9 As required

Non Aqueous Cleaner -

General

08BAA9 As required

References

Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-42-00

51-43-00

Fig. A-FBBAA

Installation of the New Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBCAA

Removal/Installation of the Fasteners of

RIB11

Sheet 01

Sheet 02

Sheet 03

(a) Install the new Corner Fittings:

Refer to Fig. A-FBBAA and Fig. A-FBCAA.

In accordance with SRM 51-42-00.

In accordance with SRM 51-43-00.

Refer to AMM Task 20-21-11-911-001.

1 Clean the surfaces with:

Non Aqueous

Cleaner - General

08BAA9 As required

2 Install the new Corner Fittings:

Refer to Fig. A-FBBAA Sheet 02 thru Fig. A-FBBAA Sheet 05.

1 Corner Fitting D0041092120000 Item 1

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 36

5

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

SERVICE BULLETIN

1 Corner Fitting D0041092120100 Item 2

with

6 Rivet NSA5414-40-18 Item 12

18 Rivet ASNA2050DXJ4020 Item 21

4 Rivet NSA5415-40-18 Item 22

NOTE: Apply to the interface of the corner fittings Item 1 and 2 and

the structure (refer to Fig. A-FBBAA Sheet 03):

Non Hardening

Jointing PuttyMedium Temp.

Area

06LCG9 As required

NOTE: Wet install all fasteners with (refer to Fig. A-FBBAA Sheet 02

thru Fig. A-FBBAA Sheet 05):

Polysulfide SealantFuel Tank Fillet06ABB1 As required

3 Install the fasteners of Rib 11:

Refer to Fig. A-FBCAA Sheet 01 thru Fig. A-FBCAA Sheet 03.

2 Rivet ASNA2051DCJ3620 Item 23

6 Rivet NSA5414-36-18 Item 24

NOTE: Items 23 and 24 are not supplied in the Kit 541019A01R01.

NOTE: Apply at the interface of the Rib 11 and the structure (refer to

Fig. A-FBCAA Sheet 02 and Fig. A-FBCAA Sheet 03):

Non Hardening

Jointing PuttyMedium Temp.

Area

06LCG9 As required

NOTE: Wet install all fasteners with (refer to Fig. A-FBCAA Sheet 02

and Fig. A-FBCAA Sheet 03):

Polysulfide SealantFuel Tank Fillet06ABB1 As required

4 Install the Lower Fitting:

Refer to Fig. A-FBBAA Sheet 02 thru Fig. A-FBBAA Sheet 04.

1 Lower Fitting Item (5) Retained at

removal

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 37

5

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

SERVICE BULLETIN

with

4 Screw Item (18) Retained at

removal

6 Screw Item (17) Retained at

removal

10 Nut NAS1726-4E Item 20

NOTE: Apply to the interface of the lower fitting Item (5) and the

structure (refer to Fig. A-FBBAA Sheet 02 thru Fig. A-FBBAA

Sheet 04):

Non Hardening

Jointing PuttyMedium Temp.

Area

06LCG9 As required

NOTE: Wet install all fasteners with (refer to Fig. A-FBBAA Sheet 02

thru Fig. A-FBBAA Sheet 04):

Polysulfide SealantFuel Tank Fillet06ABB1 As required

(4) Subtask 541019-831-005-001 - Install the Corner Fittings on RH Pylon

Work Zones and Access Panels

Zone Access/Work location

480

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills AIRFRAME

Material necessary to do the job

Kit 541019A01R01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 D0041092120000 1 CORNER

2 D0041092120100 1 CORNER

12 NSA5414-40-18 6 RIVET

20 NAS1726-4E 10 NUT

21 ASNA2050DXJ4020 18 RIVET

22 NSA5415-40-18 4 RIVET

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 38

5

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

SERVICE BULLETIN

Component COMPA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

23 ASNA2051DCJ3620 2 RIVET

24 NSA5414-36-18 6 RIVET

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

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

Non Hardening Jointing

Putty-Medium Temp. Area

06LCG9 As required

Non Aqueous Cleaner -

General

08BAA9 As required

References

Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-42-00

51-43-00

Fig. A-FBBAA

Installation of the New Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FBCAA

Removal/Installation of the Fasteners of

RIB11

Sheet 01

Sheet 02

Sheet 03

(a) Install the new Corner Fittings:

Refer to Fig. A-FBBAA and Fig. A-FBCAA.

In accordance with SRM 51-42-00.

In accordance with SRM 51-43-00.

Refer to AMM Task 20-21-11-911-001.

1 Clean the surfaces with:

Non Aqueous

Cleaner - General

08BAA9 As required

2 Install the new Corner Fittings:

Refer to Fig. A-FBBAA Sheet 02 thru Fig. A-FBBAA Sheet 05.

1 Corner Fitting D0041092120000 Item 1

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 39

5

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

SERVICE BULLETIN

1 Corner Fitting D0041092120100 Item 2

with

6 Rivet NSA5414-40-18 Item 12

18 Rivet ASNA2050DXJ4020 Item 21

4 Rivet NSA5415-40-18 Item 22

NOTE: Apply to the interface of the corner fittings Item 1 and 2 and

the structure (refer to Fig. A-FBBAA Sheet 03):

Non Hardening

Jointing PuttyMedium Temp.

Area

06LCG9 As required

NOTE: Wet install all fasteners with (refer toFig. A-FBBAA Sheet 02

thru Fig. A-FBBAA Sheet 05):

Polysulfide SealantFuel Tank Fillet06ABB1 As required

3 Install the fasteners of Rib 11:

Refer to Fig. A-FBCAA Sheet 01 thru Fig. A-FBCAA Sheet 03.

2 Rivet ASNA2051DCJ3620 Item 23

6 Rivet NSA5414-36-18 Item 24

NOTE: Items 23 and 24 are not supplied in the Kit 541019A01R01.

NOTE: Apply to the interface of the Rib 11 and the structure (refer to

Fig. A-FBCAA Sheet 02 and Fig. A-FBCAA Sheet 03):

Non Hardening

Jointing PuttyMedium Temp.

Area

06LCG9 As required

NOTE: Wet install all fasteners with (refer to Fig. A-FBCAA Sheet 02

and Fig. A-FBCAA Sheet 03):

Polysulfide SealantFuel Tank Fillet06ABB1 As required

4 Install the Lower Fitting:

Refer to Fig. A-FBBAA Sheet 02 thru Fig. A-FBBAA Sheet 04.

1 Lower Fitting Item (5) Retained at

removal

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 40

5

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

SERVICE BULLETIN

with

4 Screw Item (18) Retained at

removal

6 Screw Item (17) Retained at

removal

10 Nut NAS1726-4E Item 20

NOTE: Apply to the interface of the lower fitting Item (5) and the

structure (refer to Fig. A-FBBAA Sheet 02 thru Fig. A-FBBAA

Sheet 04):

Non Hardening

Jointing PuttyMedium Temp.

Area

06LCG9 As required

NOTE: Wet install all fasteners with (refer to Fig. A-FBBAA Sheet 02

thru Fig. A-FBBAA Sheet 04):

Polysulfide SealantFuel Tank Fillet06ABB1 As required

D. TEST

(1) Subtask 541019-700-001-001

Work Zones and Access Panels

Zone Access/Work location

470

480

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-54-00-400-001

NOTE: This Service Bulletin requires the accomplishment of the following Tests

which are given in subtasks included in the topic CLOSE UP. The

manhours for the tests are included in the referenced Service Bulletin

subtasks.

- Remove the Safety clips and tags and close the circuit breakers as specified after

the installation of the aft fixed fairing, refer to AMM Task 54-54-00-400-001.

- Do the test procedure as specified after the installation of the aft fixed fairing, refer

to AMM Task 54-54-00-400-001.

NOTE: Test procedure is only valid for above mentioned AMM task including

removal/installation of hydraulic lines.

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 41

5

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

SERVICE BULLETIN

E. CLOSE-UP

(1) Subtask 541019-942-001-001 - Close-up at LH Pylon

Work Zones and Access Panels

Zone Access/Work location

470 Access Panel 475AL, Panel 476AR

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

Task 54-54-00-400-001

Task 54-55-00-400-001

Task 54-56-00-400-001

Fig. A-FBDAA

Removal/Installation of the Drain Pipes

Sheet 01

Sheet 02

Sheet 03

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

equipment.

(b) Depending on aircraft configuration, install the Drain Pipes, refer to Fig. A-FBDAA.

1 Install:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 02.

1 Pipe Item (30) Retained at

removal

1 Pipe Item (31) Retained at

removal

2 Or install:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03.

1 Pipe Item (32) Retained at

removal

1 Pipe Item (33) Retained at

removal

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 42

5

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

SERVICE BULLETIN

1 Pipe Item (35) Retained at

removal

1 Pipe Item (36) Retained at

removal

1 Drain Clamp Item (34) Retained at

removal

with

3 Screw Item (38) Retained at

removal

3 Washer Item (39) Retained at

removal

NOTE: Apply to the interface of the drain clamp Item (34) and the

structure (refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA

Sheet 03):

Polysulfide SealantFuel Tank Fillet06ABB1 As required

(c) Install the aft fixed fairing, refer to AMM Task 54-54-00-400-001.

(d) Install the lower fairing, refer to AMM Task 54-56-00-400-001.

(e) Install the aft movable fairing, refer to AMM Task 54-55-00-400-001.

(f) Install the access panels 475AL and 476AR, refer to AMM 06-41-54 Page Block

001.

(g) Remove the access platform in position.

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

(2) Subtask 541019-942-002-001 - Close-up at RH Pylon

Work Zones and Access Panels

Zone Access/Work location

480 Access Panel 485AL, Panel 486AR

Manpower Resources

Skills NON SPECIFIC

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 43

5

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

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Polysulfide Sealant-Fuel

Tank Fillet

06ABB1 As required

References

Aircraft Maintenance Manual (AMM) 06-41-54, Page Block 001

Task 54-54-00-400-001

Task 54-55-00-400-001

Task 54-56-00-400-001

Fig. A-FBDAA

Removal/Installation of the Drain Pipes

Sheet 01

Sheet 02

Sheet 03

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

equipment.

(b) Depending on aircraft configuration, install the Drain Pipes, refer to Fig. A-FBDAA.

1 Install:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 02.

1 Pipe Item (30) Retained at

removal

1 Pipe Item (31) Retained at

removal

2 Or install:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03.

1 Pipe Item (32) Retained at

removal

1 Pipe Item (33) Retained at

removal

1 Pipe Item (35) Retained at

removal

1 Pipe Item (36) Retained at

removal

1 Drain Clamp Item (34) Retained at

removal

with

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 44

5

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

SERVICE BULLETIN

3 Screw Item (38) Retained at

removal

3 Washer Item (39) Retained at

removal

NOTE: Apply to the interface of the drain clamp Item (34) and the

structure:

Refer to Fig. A-FBDAA Sheet 01 and Fig. A-FBDAA Sheet 03.

Polysulfide SealantFuel Tank Fillet06ABB1 As required

(c) Install the aft fixed fairing, refer to AMM Task 54-54-00-400-001.

(d) Install the lower fairing, refer to AMM Task 54-56-00-400-001.

(e) Install the aft movable fairing, refer to AMM Task 54-55-00-400-001.

(f) Install the access panels 485AL and 486AR, refer to AMM 06-41-54 Page Block

001.

(g) Remove the access platform in position.

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

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 45

5

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

SERVICE BULLETIN

**CONF ALL

Z475 Z476 − 

Z485 Z486 − 

A

A

B

A

LH SHOWN

RH SYMMETRICAL 1

1

NOTE:

B

C

N_SB_541019_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Removal of the Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 46

5

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

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING REAR

(18)

(20)

(18)

(20)

PYLON AXIS

(21) (21)

A

A

C

N_SB_541019_5_BAAA_02_00

Figure A-FBAAA - Sheet 02

Removal of the Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 47

5

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

SERVICE BULLETIN

**CONF ALL

A−A

SECTION

(11) (5)

B B

D

N_SB_541019_5_BAAA_03_01

Figure A-FBAAA - Sheet 03

Removal of the Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 48

5

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

SERVICE BULLETIN

**CONF ALL

PYLON AXIS

(17)

(20)

(17)

(20)

(1)

(2)

(14)

(14)

(5)

B−B

SECTION

N_SB_541019_5_BAAA_04_00

Figure A-FBAAA - Sheet 04

Removal of the Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 49

5

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

SERVICE BULLETIN

**CONF ALL

(15)

(15)

PYLON AXIS

NII DATUM

TOP VIEW

D

N_SB_541019_5_BAAA_05_00

Figure A-FBAAA - Sheet 05

Removal of the Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 50

5

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

SERVICE BULLETIN

**CONF ALL

Z475 Z476 − 

Z485 Z486 − 

A

A

LH SHOWN

RH SYMMETRICAL 1

NOTE:

B

C

B

A 1

N_SB_541019_5_BBAA_01_00

Figure A-FBBAA - Sheet 01

Installation of the New Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 51

5

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

SERVICE BULLETIN

**CONF ALL

VIEW LOOKING REAR

MIN MAX

HOLE

SYMBOL ITEM

HOLE DIAMETER

DESCRIPTION REMARKS

SCREW

PN

RETAINED AT REMOVAL

NAS1726−4E

NOT APPLICABLE

NOT APPLICABLE

NUT

RIVET 4.01 mm

(0.158 in)

4.11 mm

(0.162 in) ASNA2050DXJ4020

6.339 mm

(0.250 in)

6.379 mm

(0.251 in) 20

21

(18)

PYLON AXIS

A

A

C

APPLY MAT. No 06ABB1 FOR WET ASSEMBLY

NOTE:

N_SB_541019_5_BBAA_02_00

Figure A-FBBAA - Sheet 02

Installation of the New Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 52

5

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

SERVICE BULLETIN

**CONF ALL

1

F

HEAD ON HIDDEN SIDE

APPLY MAT. No 06LCG9

APPLY MAT. No 6ABB1 FOR WET ASSEMBLY

(5)

A−A

SECTION

B B

D

1

1

MIN MAX

HOLE

SYMBOL ITEM

HOLE DIAMETER

PN DESCRIPTION REMARKS

NSA5414−40−18 RIVET NOT APPLICABLE 4.05 mm

(0.159 in)

4.15 mm

(0.163 in) F

12

NOTE:

N_SB_541019_5_BBAA_03_01

Figure A-FBBAA - Sheet 03

Installation of the New Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 53

5

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

SERVICE BULLETIN

**CONF ALL

MIN MAX

HOLE

SYMBOL ITEM

HOLE DIAMETER

DESCRIPTION REMARKS

SCREW

PN

RETAINED AT REMOVAL

NAS1726−4E

NOT APPLICABLE

NOT APPLICABLE

NUT

RIVET 4.05 mm

(0.159 in)

4.15 mm

(0.163 in) NSA5415−40−18

6.339 mm

(0.250 in)

6.379 mm

(0.251 in) 20

21

(17)

PYLON AXIS

B−B

SECTION

2

1

(5)

APPLY MAT. No 06ABB1 FOR WET ASSEMBLY

NOTE:

N_SB_541019_5_BBAA_04_00

Figure A-FBBAA - Sheet 04

Installation of the New Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 54

5

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

SERVICE BULLETIN

**CONF ALL

MIN MAX

HOLE

SYMBOL ITEM

HOLE DIAMETER

PN DESCRIPTION REMARKS

RIVET NOT APPLICABLE 4.01 mm

(0.158 in)

4.11 mm

(0.162 in) 21 ASNA2050DXJ4020

PYLON AXIS

NII DATUM

TOP VIEW

D

APPLY MAT. No 06ABB1 FOR WET ASSEMBLY

NOTE:

N_SB_541019_5_BBAA_05_00

Figure A-FBBAA - Sheet 05

Installation of the New Corner Fitting

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 55

5

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

SERVICE BULLETIN

**CONF ALL

Z475 Z476 − 

Z485 Z486 − 

A

A

LH SHOWN

RH SYMMETRICAL 1

NOTE:

B

B

B

A

A

B

A 1

N_SB_541019_5_BCAA_01_00

Figure A-FBCAA - Sheet 01

Removal/Installation of the Fasteners of RIB11

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 56

5

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

SERVICE BULLETIN

**CONF ALL

HOLE

SYMBOL ITEM PN DESCRIPTION REMARKS

NSA5414−36−18 RIVET NOT APPLICABLE

F

MOVE THE RIB11 WITHOUT REMOVAL

MAX 20 mm (0.787 in)

A−A

SECTION

RH SHOWN

LH SYMMETRICAL 1

NOTE:

1

F

HEAD ON HIDDEN SIDE

APPLY MAT. No 06ABB1 FOR WET ASSEMBLY

APPLY MAT. No 06LCG9 TO THE INTERFACE OF RIB11 AND THE STRUCTURE

24

(24)

N_SB_541019_5_BCAA_02_01

Figure A-FBCAA - Sheet 02

Removal/Installation of the Fasteners of RIB11

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 57

5

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

SERVICE BULLETIN

**CONF ALL

HOLE

SYMBOL ITEM PN DESCRIPTION REMARKS

ASNA2051DCL3620 RIVET NOT APPLICABLE

F

RH SHOWN

LH SYMMETRICAL 1

NOTE:

F

HEAD ON HIDDEN SIDE

APPLY MAT. No 06ABB1 FOR WET ASSEMBLY

APPLY MAT. No 06LCG9 TO THE INTERFACE OF RIB11 AND THE STRUCTURE

B−B

SECTION

1

23

(23)

N_SB_541019_5_BCAA_03_00

Figure A-FBCAA - Sheet 03

Removal/Installation of the Fasteners of RIB11

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 58

5

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

SERVICE BULLETIN

**CONF ALL

Z475 Z476 − 

Z485 Z486 − 

A

A

LH SHOWN

RH SYMMETRICAL 1

NOTE:

B

C

B

A 1

D

N_SB_541019_5_BDAA_01_00

Figure A-FBDAA - Sheet 01

Removal/Installation of the Drain Pipes

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 59

5

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

SERVICE BULLETIN

**CONF ALL

DEPENDING ON AIRCRAFT

CONFIGURATION

(30) (31)

C

N_SB_541019_5_BDAA_02_00

Figure A-FBDAA - Sheet 02

Removal/Installation of the Drain Pipes

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 60

5

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

SERVICE BULLETIN

**CONF ALL

(38)

(39)

(36)

(34)

(35) (38)

(39)

(38)

(39)

(32) (33)

APPLY MAT. No 06ABB1 TO THE INTERFACE OF THE ITEM (34) AND THE STRUCTURE

1

DEPENDING ON AIRCRAFT

CONFIGURATION

D

E

F

E

1

NOTE:

F

N_SB_541019_5_BDAA_03_00

Figure A-FBDAA - Sheet 03

Removal/Installation of the Drain Pipes

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 61

5

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

SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 62

5

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

SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

**CONF ALL

For an explanation of the manhours and elapsed time, refer to the following Gantt Chart.

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 1

5

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

SERVICE BULLETIN

Appendix 01 - Elapsed Time Assumption

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320−54−1019

SB ELAPSED TIME

(HOURS)

GET ACCESS AT LH PYLON

MH ET/S

TOTAL MANHOURS (MH)

SB ELAPSED TIME (ET)

59.00

29.50

STEPS

10.00 10.00

0 5 10 15 20 25 30

GET ACCESS AT RH PYLON 10.00 10.00

FITTINGS ON LH SIDE

2.50 2.50

FITTINGS ON RH SIDE

2.50 2.50

ON LH SIDE

6.00 6.00

CLOSE−UP AT LH PYLON 11.00 11.00

CLOSE−UP AT RH PYLON 11.00 11.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

PER

1

1

1

1

1

1

1

ON RH SIDE

6.00 6.00 1

:

:

REMOVAL OF THE CORNER 

REMOVAL OF THE CORNER 

CORNER FITTINGS

CORNER FITTINGS 

NOTE:

INSTALLATION OF THE 

INSTALLATION OF THE 

01

02

01

02 IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

N_SB_541019_5_AAAA_01_00

Figure A-FAAAA - Sheet 01

Gantt Chart

DATE: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 2

5

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

SERVICE BULLETIN

REPORTING SHEET

TITLE: NACELLES/PYLONS - GENERAL - INSTALL NEW CORNER FITTINGS

TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS.

MODIFICATION No.: 38067P10500

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: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 1

5

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: Nov 20/07 SERVICE BULLETIN No.: A320-54-1019

REVISION No.: 02 - Apr 15/14 Page: 1

5

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