@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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 54

TITLE: NACELLES/PYLONS - GENERAL - INSPECTION OF FORWARD

CORNER FITTING OF PYLON AFT SECONDARY STRUCTURE.

MODIFICATION No.: None

This page transmits Revision No.03 of Service Bulletin No.A320-54-1022

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No.03 issued to:

- delete the topic Test for the Inspection of the Lower and Medium Spars, to improve the removal

and the installation of the Aft Lower Fairing and to create 2 configurations to differentiate CFM and

IAE engines.

- revise the compliance time to take into account current fleet situation.

- change the compliance from recommended to mandatory.

CHANGES

FRONT MATTER

NACELLES/PYLONS - GENERAL -

INSPECTION OF FORWARD CORNER

FITTING OF PYLON AFT SECONDARY

STRUCTURE.

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

EFFECTIVITY OPERATOR LIST UPDATED R

REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE

UPDATED

R

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 1

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REVISION TRANSMITTAL SHEET

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

PLANNING INFORMATION

EFFECTIVITY Paragraph modified to update the MSN of the

effectivity.

R

Configuration definition CONFIGURATION LIST UPDATED R

CONF 001 CONFIGURATION DEFINITION UPDATED

CONFIGURATION DESCRIPTION UPDATED

R

CONF 002 CONFIGURATION ADDED N

REASON

History HISTORY UPDATED R

Objective/Action OBJECTIVE/ACTION UPDATED R

Advantages ADVANTAGES UPDATED R

DESCRIPTION DESCRIPTION UPDATED R

COMPLIANCE

Classification CLASSIFICATION UPDATED R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED

CONFIGURATION UPDATED

R

Accomplishment Timescale ACCOMPLISHMENT TIMESCALE ADDED N

APPROVAL APPROVAL UPDATED R

MANPOWER MANPOWER UPDATED

CONFIGURATION UPDATED

R

MANPOWER ADDED N

REFERENCES REFERENCED DOCUMENTATION UPDATED

CONFIGURATION UPDATED

R

REFERENCED DOCUMENTATION ADDED N

ACCOMPLISHMENT INSTRUCTIONS

TASK 541022- 832-801-001-Inspection of

the Corner Fittings

TASK SOLUTION UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 541022-910-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-839-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-910-001-001 SUBTASK SOLUTION ADDED N

Subtask 541022-839-004-001 SUBTASK SOLUTION ADDED N

Subtask 541022-941-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-941-001-001 SUBTASK SOLUTION ADDED N

Subtask 541022-220-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

ZONE UPDATED

LOCATION UPDATED

MANPOWER RESSOURCE UPDATED

R

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 2

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REVISION TRANSMITTAL SHEET

Subtask 541022-220-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

MANPOWER RESSOURCE UPDATED

R

Subtask 541022-220-001-001 SUBTASK SOLUTION ADDED N

Subtask 541022-220-002-001 SUBTASK SOLUTION ADDED N

Subtask 541022-942-001-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-942-001-001 SUBTASK SOLUTION ADDED N

TASK 541022- 832-802-001-Inspection of

the Lower and Medium Spars

TASK SOLUTION UPDATED

NOTE UPDATED

CONFIGURATION UPDATED

R

Task associated data - 001 CONFIGURATION UPDATED

MAN HOURS UPDATED

ELAPSED TIME UPDATED

R

Task associated data - 002 TASK ASSOCIATED DATA ADDED N

Subtask 541022-910-002-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-839-005-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-910-002-001 SUBTASK SOLUTION ADDED N

Subtask 541022-839-005-001 SUBTASK SOLUTION ADDED N

Subtask 541022-941-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 541022-941-003-002 SUBTASK SOLUTION ADDED N

Subtask 541022-220-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-220-004-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

R

Subtask 541022-220-003-001 SUBTASK SOLUTION ADDED N

Subtask 541022-220-004-001 SUBTASK SOLUTION ADDED N

Subtask 541022-700-003-001 SUBTASK SOLUTION DELETED FOR

APPLICABLE MSN

D

Subtask 541022-942-003-001 SUBTASK SOLUTION UPDATED

CONFIGURATION UPDATED

REFERENCED DOCUMENTATION UPDATED

REFERENCES UPDATED

R

Subtask 541022-942-003-002 SUBTASK SOLUTION ADDED N

Fig. A-FBAAA

Fig. A-FBAAA Sheet 02 SHEET UPDATED R

Fig. A-FBAAA Sheet 03 SHEET UPDATED R

Fig. A-FBCAA FIGURE SOLUTION UPDATED R

Fig. A-FBCAA Sheet 01 SHEET UPDATED R

Fig. A-FBCAA Sheet 02 SHEET UPDATED R

Fig. A-FBCAA Sheet 03 SHEET UPDATED R

Fig. A-FBCAA Sheet 04 SHEET UPDATED R

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

Fig. A-FBCAA Sheet 05 SHEET ADDED N

Fig. A-FRAAA

Fig. A-FRAAA Sheet 01 SHEET UPDATED R

Fig. A-FRBAA

Fig. A-FRBAA Sheet 01 SHEET UPDATED R

Appendix 02 - Elapsed Time Assumption of the Inspection of the Lower and Medium Spars

Fig. A-FADAA FIGURE SOLUTION UPDATED

CONFIGURATION UPDATED

R

Fig. A-FADAA Sheet 01 SHEET UPDATED R

Fig. A-FADAB FIGURE SOLUTION ADDED N

Fig. A-FADAB Sheet 01 SHEET ADDED 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

Revision No 01 issued to update the accomplishment timescale of this Service Bulletin, to simplify

the inspection flowchart, to update the effectivity and to add the RH in accomplishment timescale

paragraph.

Revision No 02 issued to update the accomplishment timescale and to add the inspection of the lower

and medium spars.

REVISION SEQUENCE

ORIGINAL: Jul 07/09

REVISION No. : 01 - Sep 29/11

REVISION No. : 02 - Jul 12/13

REVISION No. : 03 - Apr 15/14

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 4

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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.

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 54

TITLE: NACELLES/PYLONS - GENERAL - INSPECTION OF FORWARD

CORNER FITTING OF PYLON AFT SECONDARY STRUCTURE.

**CONF ALL

MODIFICATIONS

None

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

Several operators reported cracks on the two corner fittings at Rib 11 lower attachment level, in the

pylon aft fixed secondary structure. Cracks have been found on the lateral face (lateral panel side) and

could extend up to the forward face (Rib 11 side). Cracks could occur on aircraft having accumulated

only 8,000 Flight Hours (FH).

Investigation have highlighted that cracks may be due to static failure under phenomenon of stress

corrosion. The corner fittings allow the transfer of internal loads between the spars, the lateral panels

and the lower fitting.

New fittings made of aluminium alloy 7175T7351 instead of 2024T351 and having thicker faces with

shot peened surfaces, have been designed and introduced in production via Mod No. 38067P10459

(INSTALL NEW CORNER FITTINGS TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS

(SERIAL SOL)) and retrofit via Service Bulletin No. A320-54-1019 (Mod No. 38067P10500 (INSTALL

NEW CORNER FITTINGS TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS (SB SOL))).

Challenged analysis concluded that damaged Aft Fixed Fairing Structure with both corner fittings

completely cracked is still airworthy. Based on new analyses, the figures of this inspection are changed.

The Aft Pylon Fairing with both fittings broken will experience higher level of loads on the adjacent

structures : hence, lower and center spars are inspected if corner fittings are found cracked.

This service Bulletin mandates repetitive detailed inspection of the four corner fittings per aircraft to

ensure crack detection in case of crack findings. This Service Bulletin recommends lower and medium

spars inspection for deformation or crack.

Accomplishment of this Service Bulletin will allow early detection of cracking or deformation occurrence

at level of rib11 corner fittings and spar.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 1

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SERVICE BULLETIN

SUMMARY

Application of Service Bulletin No. A320-54-1019 is the terminative action for this repetitive Inspection

Service Bulletin No. A320-54-1022.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

MATERIAL PRICE INFORMATION

No Material

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 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

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 2

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SERVICE BULLETIN

SUMMARY

AOT None

SIL 54-032

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER OIT SE 999.0006/14

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 541022-832-801-001: Inspection of the Corner Fittings

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

Task 541022-832-802-001: Inspection of the Lower and Medium Spars

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

**CONF 002

Task 541022-832-801-001: Inspection of the Corner Fittings

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

Task 541022-832-802-001: Inspection of the Lower and Medium Spars

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

APPENDICES

**CONF ALL

Appendix 01 - Elapsed Time Assumption of the Inspection of the Corner Fittings

Appendix 02 - Elapsed Time Assumption of the Inspection of the Lower and Medium Spars

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

RIB11

RIB12

Z475 Z476 − 

A

A

Z485 Z486 − 

B

AREA TO BE INSPECTED

B

A

N_SB_541022_5_SAAA_01_04

Figure A-FSAAA - Sheet 01

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 4

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 54

TITLE: NACELLES/PYLONS - GENERAL - INSPECTION OF FORWARD

CORNER FITTING OF PYLON AFT SECONDARY STRUCTURE.

MODIFICATION No.: None

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: This Service Bulletin is valid for aircraft on which Mod No. 33687P8297

(IMPROVE AERODYNAMIC SHAPE OF PW PYLON), 33844P8341

(IMPROVE AERODYNAMIC SHAPE OF CFM PYLON), 33847P8340

(IMPROVE AERODYNAMIC SHAPE OF IAE PYLON), 38067P10459

(INSTALL NEW CORNER FITTINGS TO SOLVE CRACK PROBLEM ON ALL

ENGINE PYLONS (SERIAL SOL)) are not embodied and which have not

embodied Service Bulletin A320-54-1019.

(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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 1

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

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 1873

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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 2

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OPERATOR MSN

73W 0087

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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 3

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OPERATOR MSN

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 1668 1718 2593 2624 2629 2907

AIJ 0707 1132 1162 1179 1244 1259 1308 1322 1747 1780 2048 2189

2227 2539 3021

ALK 2345 2564 2584 2908

AMC 2113 2122 2142 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

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 2826 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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 4

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SERVICE BULLETIN

OPERATOR MSN

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

BGF 3188

BGH 1087 2844 2863 3139

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

2171 2182 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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 5

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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 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: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 6

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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 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 2158

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: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 7

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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 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 0995 1121 1175 1597 1744

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 2730 2793

MRJ 0530 1202 1300 1353

MSC 2937 2966 3282 3323

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

2073 2079 2088 2094

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 8

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SERVICE BULLETIN

OPERATOR MSN

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

SFJ 2658 3025

SFW 0734 0994 1018

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 9

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SERVICE BULLETIN

OPERATOR MSN

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 2553 2610

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

TVS 2180

TWJ 2550

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 10

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SERVICE BULLETIN

OPERATOR MSN

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

VRE 1429 2213 2228

VVC 1306 1454 1564 1725 1867

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 11

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SERVICE BULLETIN

OPERATOR MSN

WGT 1212

WHT 1256 2440 2675

WOW 2457

WRC 0235 0645 0684 0781 1869 2462 2682

WTJ 0548

WZZ 1834 1892 1902

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 12

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0029 0059 0068 0069 0070 0071 0072 0073 0078 0083 0084

0085 0086 0087 0088 0093 0094 0104 0110 0111 0112 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 0167 0171 0172

0173 0174 0175 0176 0181 0182 0183 0185 0189 0190 0192

0195 0197 0199 0200 0201 0202 0203 0205 0206 0207 0208

0209 0210 0211 0212 0213 0214 0216 0217 0218 0219 0220

0223 0224 0229 0231 0232 0233 0234 0235 0237 0239 0240

0241 0242 0244 0248 0253 0254 0255 0262 0263 0264 0265

0266 0267 0268 0269 0270 0272 0273 0274 0277 0279 0281

0282 0284 0285 0287 0289 0290 0293 0294 0297 0298 0299

0300 0301 0302 0303 0306 0307 0309 0311 0312 0318 0319

0323 0324 0325 0328 0329 0330 0331 0333 0339 0340 0341

0342 0343 0345 0346 0349 0350 0355 0356 0358 0359 0360

0367 0370 0371 0372 0375 0378 0380 0381 0382 0383 0384

0387 0388 0390 0391 0395 0399 0400 0401 0402 0403 0404

0407 0408 0409 0410 0413 0417 0418 0419 0420 0421 0422

0426 0427 0434 0436 0438 0445 0459 0466 0477 0482 0488

0491 0494 0495 0497 0498 0501 0507 0509 0511 0513 0514

0515 0516 0517 0519 0520 0521 0522 0524 0525 0526 0528

0529 0531 0532 0533 0534 0535 0537 0541 0544 0545 0546

0548 0549 0552 0553 0554 0559 0562 0566 0569 0570 0572

0574 0576 0577 0578 0579 0581 0583 0585 0586 0588 0593

0594 0596 0598 0599 0600 0603 0605 0607 0608 0609 0610

0611 0612 0616 0617 0618 0619 0621 0622 0623 0625 0627

0629 0630 0634 0635 0636 0637 0639 0641 0642 0643 0644

0645 0646 0647 0648 0649 0650 0651 0653 0654 0656 0657

0658 0660 0662 0664 0665 0666 0669 0670 0672 0673 0674

0675 0677 0679 0681 0682 0684 0685 0688 0689 0691 0693

0694 0695 0697 0700 0701 0703 0706 0707 0711 0713 0714

0716 0717 0719 0721 0723 0724 0726 0727 0728 0729 0730

0732 0734 0735 0736 0737 0738 0740 0742 0744 0745 0749

0750 0752 0754 0755 0757 0761 0763 0764 0765 0766 0767

0768 0769 0772 0773 0774 0775 0776 0777 0778 0779 0781

0782 0785 0786 0790 0793 0794 0795 0796 0797 0799 0800

0801 0807 0808 0809 0813 0814 0815 0817 0818 0819 0821

0823 0827 0828 0829 0830 0831 0832 0833 0837 0838 0840

0841 0844 0845 0846 0848 0852 0853 0854 0860 0861 0863

0868 0869 0870 0875 0876 0879 0880 0883 0884 0885 0888

0890 0891 0894 0896 0897 0903 0904 0905 0906 0907 0909

0911 0914 0917 0920 0921 0922 0923 0925 0926 0929 0933

0935 0936 0937 0938 0939 0940 0941 0942 0945 0946 0947

0949 0951 0957 0958 0959 0960 0961 0962 0964 0967 0970

0971 0972 0973 0975 0978 0979 0981 0982 0984 0985 0986

0987 0988 0991 0992 0994 0995 0996 0997 0998 0999 1000

1002 1005 1006 1009 1011 1012 1016 1017 1018 1019 1020

1021 1023 1025 1026 1027 1028 1029 1030 1033 1034 1036

1037 1038 1040 1041 1046 1047 1048 1051 1052 1054 1055

002

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 13

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SERVICE BULLETIN

MSN CONFIGURATION

1058 1059 1061 1062 1063 1065 1067 1068 1069 1070 1071

1072 1073 1077 1078 1081 1084 1086 1087 1089 1090 1091

1093 1094 1095 1097 1099 1100 1101 1102 1106 1107 1108

1109 1112 1114 1119 1120 1121 1122 1124 1125 1126 1127

1129 1130 1131 1132 1133 1134 1135 1136 1137 1138 1141

1144 1145 1147 1148 1149 1150 1151 1152 1154 1155 1157

1160 1162 1164 1165 1167 1168 1169 1170 1171 1172 1175

1176 1179 1180 1181 1182 1184 1185 1187 1189 1190 1191

1198 1200 1201 1203 1205 1206 1208 1209 1210 1213 1216

1217 1219 1220 1221 1224 1226 1229 1230 1231 1233 1237

1238 1241 1242 1244 1245 1247 1249 1250 1252 1254 1255

1259 1262 1263 1264 1265 1267 1268 1269 1271 1275 1277

1283 1285 1286 1287 1288 1289 1292 1294 1296 1297 1298

1299 1301 1303 1305 1306 1307 1308 1309 1310 1311 1312

1313 1314 1315 1316 1317 1318 1319 1320 1322 1324 1325

1326 1328 1330 1331 1336 1337 1340 1342 1344 1345 1346

1347 1348 1352 1354 1357 1358 1360 1361 1362 1364 1365

1367 1369 1370 1371 1372 1377 1378 1379 1381 1382 1385

1386 1387 1388 1389 1390 1391 1392 1393 1394 1396 1399

1402 1403 1404 1405 1412 1413 1414 1415 1416 1417 1425

1429 1430 1431 1434 1436 1437 1439 1441 1442 1443 1444

1447 1448 1449 1450 1451 1453 1454 1455 1456 1457 1458

1461 1462 1465 1467 1470 1471 1472 1473 1476 1478 1479

1480 1481 1483 1484 1485 1488 1489 1492 1493 1494 1496

1498 1499 1501 1502 1503 1504 1505 1515 1516 1517 1519

1520 1521 1524 1525 1530 1531 1532 1535 1536 1539 1540

1541 1542 1543 1544 1549 1550 1551 1553 1554 1556 1560

1562 1564 1567 1570 1571 1572 1577 1578 1579 1582 1583

1588 1592 1597 1598 1599 1601 1602 1603 1605 1607 1611

1612 1615 1616 1618 1622 1623 1625 1629 1630 1632 1633

1634 1637 1638 1639 1640 1641 1645 1646 1651 1654 1655

1657 1658 1659 1662 1666 1667 1668 1673 1674 1677 1678

1679 1681 1683 1684 1685 1686 1691 1692 1693 1694 1699

1700 1701 1704 1706 1709 1712 1713 1714 1716 1717 1718

1719 1720 1722 1724 1725 1726 1733 1735 1736 1738 1740

1742 1743 1744 1745 1746 1747 1748 1750 1751 1752 1753

1756 1757 1759 1761 1762 1765 1766 1767 1769 1770 1772

1774 1775 1777 1778 1779 1780 1781 1783 1786 1787 1789

1791 1793 1795 1796 1797 1799 1800 1803 1805 1806 1808

1809 1810 1811 1812 1815 1816 1819 1820 1824 1828 1833

1836 1838 1839 1841 1846 1851 1852 1853 1859 1860 1863

1864 1866 1867 1870 1872 1873 1874 1875 1876 1879 1881

1882 1884 1885 1886 1887 1889 1890 1894 1897 1900 1901

1905 1906 1908 1911 1913 1916 1920 1921 1923 1924 1925

1929 1931 1932 1936 1937 1938 1940 1942 1943 1949 1951

1954 1959 1960 1961 1963 1964 1965 1966 1968 1972 1973

1975 1976 1978 1980 1981 1982 1983 1988 1989 1990 1994

1997 1999 2001 2002 2003 2005 2009 2010 2011 2012 2013

2017 2018 2019 2022 2024 2026 2028 2030 2033 2034 2035

2036 2037 2039 2043 2046 2047 2048 2049 2050 2052 2053

2054 2056 2057 2059 2060 2061 2062 2064 2065 2066 2068

002

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 14

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SERVICE BULLETIN

MSN CONFIGURATION

2069 2071 2072 2074 2076 2078 2081 2082 2083 2086 2087

2091 2092 2093 2095 2100 2101 2103 2104 2106 2109 2113

2114 2115 2116 2117 2119 2120 2122 2123 2124 2126 2127

2129 2131 2133 2134 2140 2142 2143 2144 2145 2146 2151

2154 2155 2158 2162 2163 2165 2166 2170 2171 2174 2175

2176 2178 2179 2180 2181 2182 2183 2184 2186 2187 2189

2191 2196 2198 2199 2206 2207 2208 2209 2212 2213 2214

2217 2219 2220 2221 2222 2224 2225 2227 2228 2230 2233

2235 2236 2237 2239 2240 2241 2242 2243 2244 2245 2248

2249 2250 2251 2253 2256 2258 2260 2262 2264 2265 2266

2269 2270 2271 2272 2274 2278 2279 2283 2285 2287 2289

2291 2293 2294 2298 2300 2306 2309 2311 2315 2317 2318

2319 2325 2327 2328 2330 2332 2333 2337 2342 2344 2346

2347 2349 2350 2353 2354 2357 2358 2360 2361 2364 2365

2367 2369 2370 2373 2374 2377 2378 2380 2381 2382 2385

2387 2388 2390 2391 2392 2394 2398 2399 2400 2402 2406

2407 2409 2411 2412 2416 2419 2420 2425 2427 2432 2436

2437 2439 2440 2442 2446 2448 2450 2451 2456 2460 2463

2464 2465 2471 2472 2474 2477 2478 2481 2483 2484 2486

2487 2488 2492 2493 2494 2495 2497 2498 2499 2503 2506

2507 2508 2511 2512 2514 2516 2518 2519 2523 2525 2527

2528 2529 2532 2538 2539 2540 2541 2542 2543 2544 2545

2546 2547 2548 2549 2550 2551 2552 2554 2555 2556 2557

2558 2561 2562 2563 2565 2569 2575 2578 2581 2582 2583

2584 2586 2588 2591 2592 2593 2596 2599 2601 2605 2606

2607 2611 2612 2616 2617 2618 2619 2620 2623 2624 2625

2627 2628 2629 2632 2633 2635 2636 2637 2638 2641 2644

2646 2652 2654 2656 2658 2662 2665 2668 2672 2674 2675

2677 2678 2681 2683 2684 2685 2686 2691 2693 2695 2696

2699 2700 2702 2705 2706 2707 2708 2709 2712 2715 2716

2719 2721 2726 2727 2729 2733 2735 2736 2740 2742 2743

2744 2745 2746 2748 2749 2750 2751 2754 2756 2757 2758

2760 2761 2762 2763 2764 2765 2768 2769 2770 2773 2774

2776 2777 2778 2779 2782 2785 2786 2788 2789 2790 2792

2794 2795 2796 2798 2800 2801 2803 2805 2806 2807 2810

2811 2812 2816 2818 2819 2820 2821 2822 2824 2825 2826

2827 2829 2830 2831 2834 2835 2836 2837 2839 2841 2842

2843 2846 2847 2849 2851 2852 2853 2854 2855 2857 2860

2861 2865 2866 2867 2869 2870 2873 2875 2876 2877 2878

2879 2881 2882 2884 2885 2889 2890 2891 2895 2897 2899

2902 2903 2905 2907 2909 2910 2912 2913 2915 2918 2920

2921 2923 2924 2925 2926 2930 2932 2935 2937 2938 2939

2944 2946 2947 2949 2950 2951 2954 2956 2957 2959 2960

2961 2962 2964 2965 2966 2967 2968 2972 2973 2975 2980

2985 2986 2988 2989 2991 2993 2995 2996 2998 3000 3002

3003 3006 3008 3009 3014 3016 3018 3019 3021 3023 3024

3025 3027 3028 3031 3035 3036 3037 3040 3041 3043 3044

3046 3047 3051 3052 3053 3054 3055 3056 3058 3059 3060

3061 3063 3064 3065 3068 3070 3073 3076 3078 3079 3080

3082 3083 3084 3085 3088 3090 3093 3094 3095 3096 3097

3098 3099 3100 3101 3102 3109 3111 3117 3118 3121 3122

002

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 15

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SERVICE BULLETIN

MSN CONFIGURATION

3129 3131 3132 3133 3134 3135 3136 3137 3138 3139 3140

3145 3147 3148 3151 3152 3153 3154 3155 3161 3168 3169

3173 3174 3176 3179 3180 3181 3182 3184 3186 3188 3189

3194 3199 3201 3202 3203 3204 3206 3209 3211 3215 3218

3221 3223 3224 3226 3232 3234 3236 3237 3242 3245 3246

3255 3261 3268 3272 3277 3282 3285 3289 3291 3293 3299

3318 3320 3321 3323 3327 3337 3338 3345 3346 3349 3353

3361 3363 3366 3368 3370 3376 3377 3380 3383

002

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 16

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SERVICE BULLETIN

MSN CONFIGURATION

0045 0046 0047 0049 0050 0051 0052 0053 0054 0055 0056

0057 0064 0065 0066 0067 0074 0075 0076 0077 0080 0081

0082 0090 0095 0096 0099 0113 0114 0164 0165 0166 0168

0178 0179 0194 0198 0230 0243 0249 0251 0252 0256 0259

0260 0261 0275 0276 0291 0292 0295 0296 0308 0314 0316

0317 0320 0321 0322 0332 0347 0351 0353 0354 0357 0361

0362 0364 0366 0368 0373 0376 0385 0386 0393 0396 0398

0405 0406 0412 0414 0415 0416 0423 0424 0428 0429 0430

0431 0432 0435 0439 0441 0442 0444 0447 0448 0449 0450

0451 0452 0454 0455 0456 0457 0458 0460 0462 0463 0464

0465 0468 0469 0470 0471 0472 0473 0474 0475 0476 0479

0480 0483 0484 0485 0486 0487 0489 0490 0492 0493 0496

0499 0500 0502 0503 0504 0505 0506 0508 0510 0512 0518

0523 0527 0530 0538 0539 0540 0542 0543 0550 0551 0555

0556 0557 0558 0560 0561 0563 0564 0565 0567 0568 0571

0573 0575 0580 0582 0584 0587 0589 0591 0592 0595 0597

0604 0606 0613 0614 0620 0631 0633 0638 0640 0652 0655

0659 0661 0663 0667 0668 0676 0678 0680 0683 0686 0687

0690 0692 0696 0698 0699 0702 0704 0705 0709 0712 0715

0718 0720 0722 0725 0731 0733 0739 0741 0743 0746 0747

0748 0751 0756 0758 0759 0760 0762 0770 0771 0780 0783

0784 0787 0788 0791 0792 0798 0802 0803 0804 0805 0806

0810 0811 0812 0816 0820 0822 0824 0825 0826 0834 0835

0836 0839 0842 0843 0847 0849 0850 0851 0855 0856 0857

0858 0859 0862 0864 0865 0866 0867 0871 0872 0873 0874

0877 0878 0881 0882 0886 0887 0889 0892 0893 0895 0898

0899 0900 0901 0902 0908 0910 0912 0913 0915 0916 0918

0919 0924 0927 0928 0930 0931 0932 0934 0943 0944 0948

0950 0952 0953 0954 0955 0963 0965 0966 0968 0969 0974

0976 0977 0980 0983 0989 0990 0993 1001 1003 1004 1007

1008 1010 1013 1014 1015 1022 1024 1031 1032 1035 1039

1042 1043 1045 1049 1050 1053 1056 1057 1060 1064 1066

1074 1075 1076 1079 1080 1082 1083 1085 1088 1092 1096

1098 1103 1104 1105 1110 1111 1115 1116 1117 1118 1123

1128 1139 1140 1142 1143 1146 1153 1156 1158 1159 1161

1163 1166 1173 1174 1177 1178 1183 1188 1192 1193 1194

1195 1196 1197 1199 1202 1204 1207 1211 1212 1214 1215

1222 1223 1225 1227 1228 1232 1234 1235 1236 1239 1240

1243 1246 1248 1251 1253 1256 1257 1258 1260 1261 1266

1270 1272 1273 1274 1276 1279 1280 1281 1282 1284 1290

1291 1293 1295 1300 1302 1304 1321 1323 1327 1329 1332

1334 1335 1338 1339 1341 1343 1349 1350 1351 1353 1355

1356 1359 1363 1366 1368 1373 1375 1376 1380 1383 1384

1395 1397 1398 1400 1401 1406 1407 1408 1409 1410 1411

1418 1419 1420 1421 1422 1423 1424 1426 1427 1428 1432

1433 1435 1438 1440 1445 1446 1452 1459 1460 1463 1466

1468 1469 1474 1475 1477 1482 1486 1487 1490 1491 1495

1497 1500 1506 1507 1508 1509 1510 1511 1512 1513 1514

1518 1522 1523 1526 1527 1528 1529 1533 1534 1537 1538

1545 1546 1547 1548 1552 1555 1557 1558 1559 1561 1563

1565 1566 1568 1569 1573 1574 1575 1576 1580 1581 1584

001

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 17

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SERVICE BULLETIN

MSN CONFIGURATION

1585 1586 1587 1589 1590 1591 1593 1594 1595 1596 1600

1604 1606 1608 1609 1610 1613 1614 1617 1619 1620 1621

1624 1626 1627 1628 1631 1635 1636 1642 1643 1644 1647

1648 1649 1650 1652 1653 1656 1661 1663 1664 1665 1669

1670 1671 1672 1675 1680 1682 1687 1688 1689 1690 1695

1696 1697 1698 1702 1703 1705 1707 1708 1710 1711 1715

1721 1723 1727 1728 1730 1731 1732 1734 1737 1739 1741

1749 1754 1755 1758 1760 1763 1764 1771 1773 1776 1782

1784 1785 1788 1790 1792 1794 1798 1801 1802 1804 1807

1814 1817 1818 1821 1823 1825 1826 1827 1829 1831 1832

1834 1835 1837 1840 1842 1843 1844 1845 1847 1848 1849

1850 1854 1855 1856 1857 1858 1861 1862 1865 1868 1869

1871 1877 1878 1880 1883 1888 1891 1892 1893 1895 1896

1898 1899 1902 1903 1904 1907 1909 1910 1912 1914 1915

1917 1918 1922 1926 1927 1928 1933 1934 1935 1941 1944

1945 1946 1947 1948 1950 1952 1953 1955 1956 1957 1958

1962 1967 1969 1970 1971 1974 1977 1979 1984 1986 1987

1993 1995 1996 1998 2000 2004 2006 2007 2008 2014 2015

2016 2020 2021 2023 2027 2029 2031 2032 2038 2040 2041

2042 2044 2045 2055 2058 2063 2067 2070 2073 2075 2077

2079 2080 2084 2085 2088 2089 2090 2094 2096 2097 2098

2099 2102 2105 2107 2108 2110 2112 2118 2121 2125 2128

2130 2132 2135 2136 2137 2138 2139 2141 2147 2148 2149

2150 2152 2153 2156 2157 2159 2160 2161 2164 2167 2168

2169 2172 2173 2177 2185 2188 2190 2192 2193 2194 2195

2197 2200 2201 2202 2203 2204 2205 2210 2211 2215 2216

2223 2226 2229 2231 2232 2234 2238 2246 2247 2252 2254

2255 2257 2259 2261 2263 2267 2268 2273 2275 2277 2280

2281 2282 2284 2286 2288 2290 2292 2295 2296 2297 2299

2301 2302 2303 2304 2305 2307 2308 2310 2312 2313 2314

2316 2320 2321 2322 2323 2324 2326 2329 2331 2334 2335

2336 2338 2339 2340 2341 2343 2345 2348 2351 2352 2355

2356 2359 2362 2363 2366 2368 2371 2372 2375 2376 2379

2383 2384 2386 2389 2393 2395 2396 2397 2401 2403 2404

2405 2408 2410 2413 2414 2415 2417 2418 2421 2422 2423

2426 2428 2429 2430 2431 2433 2434 2435 2438 2441 2443

2444 2445 2447 2449 2452 2453 2454 2455 2457 2458 2459

2461 2462 2466 2467 2468 2469 2470 2473 2475 2476 2479

2480 2482 2485 2489 2490 2491 2496 2501 2502 2504 2505

2509 2510 2513 2515 2517 2520 2521 2522 2524 2526 2530

2531 2533 2534 2535 2536 2537 2553 2559 2560 2564 2566

2567 2568 2570 2571 2572 2573 2574 2576 2577 2579 2580

2585 2587 2589 2590 2594 2595 2597 2598 2600 2602 2603

2604 2608 2609 2610 2613 2614 2615 2621 2622 2626 2630

2631 2634 2639 2640 2642 2643 2645 2647 2648 2649 2650

2651 2653 2655 2657 2659 2660 2661 2663 2664 2666 2667

2669 2670 2671 2673 2676 2679 2680 2682 2687 2688 2689

2690 2692 2694 2697 2698 2701 2703 2704 2710 2711 2713

2714 2717 2718 2720 2723 2724 2725 2728 2730 2731 2732

2734 2737 2738 2739 2741 2747 2752 2753 2755 2759 2766

2767 2771 2772 2775 2780 2783 2784 2787 2791 2793 2797

001

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 18

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SERVICE BULLETIN

MSN CONFIGURATION

2799 2804 2808 2809 2813 2815 2817 2823 2828 2833 2838

2840 2844 2845 2850 2856 2858 2859 2862 2863 2864 2868

2872 2874 2883 2886 2887 2888 2892 2893 2894 2896 2898

2901 2904 2906 2908 2911 2914 2916 2917 2919 2922 2927

2928 2929 2933 2934 2936 2940 2941 2942 2943 2948 2952

2953 2958 2963 2969 2971 2974 2976 2978 2979 2981 2982

2983 2984 2987 2990 2997 2999 3004 3005 3007 3010 3011

3012 3013 3015 3017 3020 3022 3026 3032 3042 3045 3049

3050 3057 3067 3069 3071 3075 3077 3081 3086 3103 3104

3106 3112 3113 3114 3116 3124 3125 3126 3141 3142 3144

3156 3159 3162 3165 3175 3183 3185 3192 3195 3198 3200

3207 3208 3219 3231 3239 3244 3253 3257 3275 3279 3283

3292 3296 3297 3303 3315 3316 3332 3341 3350 3355 3378

3379

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft on which IAE engines are installed.

**CONF 002

Config. 002 is valid for aircraft on which CFM engines are installed.

(6) Material Effectivity

None

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

Several operators reported cracks on the two corner fittings at Rib 11 lower attachment

level, in the pylon aft fixed secondary structure. Cracks have been found on the lateral

face (lateral panel side) and could extend up to the forward face (Rib 11 side). Cracks

could occur on aircraft having accumulated only 8,000 Flight Hours (FH).

Investigation have highlighted that cracks may be due to static failure under

phenomenon of stress corrosion. The corner fittings allow the transfer of internal loads

between the spars, the lateral panels and the lower fitting.

New fittings made of aluminium alloy 7175T7351 instead of 2024T351 and having

thicker faces with shot peened surfaces, have been designed and introduced in

production via Mod No. 38067P10459 (INSTALL NEW CORNER FITTINGS TO SOLVE

CRACK PROBLEM ON ALL ENGINE PYLONS (SERIAL SOL)) and retrofit via Service

Bulletin No. A320-54-1019 (Mod No. 38067P10500 (INSTALL NEW CORNER FITTINGS

TO SOLVE CRACK PROBLEM ON ALL ENGINE PYLONS (SB SOL))).

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 19

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Challenged analysis concluded that damaged Aft Fixed Fairing Structure with both

corner fittings completely cracked is still airworthy. Based on new analyses, the figures

of this inspection are changed. The Aft Pylon Fairing with both fittings broken will

experience higher level of loads on the adjacent structures : hence, lower and center

spars are inspected if corner fittings are found cracked.

(2) Objective/Action

This service Bulletin mandates repetitive detailed inspection of the four corner fittings

per aircraft to ensure crack detection in case of crack findings. This Service Bulletin

recommends lower and medium spars inspection for deformation or crack.

(3) Advantages

Accomplishment of this Service Bulletin will allow early detection of cracking or

deformation occurrence at level of rib11 corner fittings and spar.

Application of Service Bulletin No. A320-54-1019 is the terminative action for this

repetitive Inspection Service Bulletin No. A320-54-1022.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 541022-832-801-001: Inspection of the Corner Fittings

(1) Do a detailed Inspection of Forward Corner Fittings of Pylon AFT Secondary

Structure LH

(2) Do a detailed Inspection of Forward Corner Fittings of Pylon AFT Secondary

Structure RH

Task 541022-832-802-001: Inspection of the Lower and Medium Spars

(1) Do a detailed Inspection of the Lower and Medium Spars of the LH Pylon

(2) Do a detailed Inspection of the Lower and Medium Spars of the RH Pylon

**CONF 002

Task 541022-832-801-001: Inspection of the Corner Fittings

(1) Do a detailed Inspection of Forward Corner Fittings of Pylon AFT Secondary

Structure LH

(2) Do a detailed Inspection of Forward Corner Fittings of Pylon AFT Secondary

Structure RH

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 20

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Task 541022-832-802-001: Inspection of the Lower and Medium Spars

(1) Do a detailed Inspection of the Lower and Medium Spars of the LH Pylon

(2) Do a detailed Inspection of the Lower and Medium Spars of the RH Pylon

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

**CONF 001

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

Compliance Time Condition Action

Threshold Grace period Repetitive Interval

All aircraft Do a detailed

inspection of

corner fittings.

Refer to TASK

541022-832-801

001 Inspection of

the Corner Fittings

Whichever occurs

later :

- 15000FC /

22500FH from

first flight (see

NOTE (*))

For aircraft:

- below

40000FC/60000FH

from first flight

(see NOTE (*)):

5000FC/7500FH

from SB

issuance date

(see NOTE

(*)) without

exceeding

40750FC/60750FH

from first flight

(see NOTE (*))

- above

40000FC/60000FH

from first flight

(see NOTE (*)):

750FC/750FH

from SB

issuance date

(see NOTE (*))

None

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 21

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SERVICE BULLETIN

Compliance Time Condition Action

Threshold Grace period Repetitive Interval

No crack found on

corner fitting

Do the inspection

again. Refer to

TASK

541022-832-801

001 Inspection of

the Corner Fittings

None None 15000FC /

22500FH (see

NOTE (*))

Crack found on

corner fitting

Do a detail

inspection of the

lower and medium

spars for crack and

deformation

detection in the

splicing area with

corner fitting

between Ribs 11

and 12. Refer to

TASK

541022-832-802

001 Inspection of

the Lower and

Medium Spars

Before next flight None None

No damage found Accomplish

Service Bulletin

No.A320-54-1019

5,000FC/7,500FH

(see NOTE (*))

None None

Damage found Contact Airbus and

apply instructions

approved by Airbus

Before next flight None None

Table 1: Detailed Inspection of the Corner Fittings

NOTE (*): Flight Cycle (FC) or Flight Hours (FH) whichever occurs first.

**CONF 002

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 22

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Compliance Time Condition Action

Threshold Grace period Repetitive Interval

All aircraft Do a detailed

inspection of

corner fittings.

Refer to TASK

541022-832-801

001 Inspection of

the Corner Fittings

Whichever occurs

later :

- 15000FC /

22500FH from

first flight (see

NOTE (*))

For aircraft:

- below

40000FC/60000FH

from first flight

(see NOTE (*)):

5000FC/7500FH

from SB

issuance date

(see NOTE

(*)) without

exceeding

40750FC/60750FH

from first flight

(see NOTE (*))

- above

40000FC/60000FH

from first flight

(see NOTE (*)):

750FC/750FH

from SB

issuance date

(see NOTE (*))

None

No crack found on

corner fitting

Do the inspection

again. Refer to

TASK

541022-832-801

001 Inspection of

the Corner Fittings

None None 15000FC /

22500FH (see

NOTE (*))

Crack found on

corner fitting

Do a detail

inspection of the

lower and medium

spars for crack and

deformation

detection in the

splicing area with

corner fitting

between Ribs 11

and 12. Refer to

TASK

541022-832-802

001 Inspection of

the Lower and

Medium Spars

Before next flight None None

No damage found Accomplish

Service Bulletin

No.A320-54-1019

5,000FC/7,500FH

(see NOTE (*))

None None

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 23

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Compliance Time Condition Action

Threshold Grace period Repetitive Interval

Damage found Contact Airbus and

apply instructions

approved by Airbus

Before next flight None None

Table 1: Detailed Inspection of the Corner Fittings

NOTE (*): Flight Cycle (FC) or Flight Hours (FH) whichever occurs first.

**CONF ALL

F. APPROVAL

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

Organization Approval No. EASA 21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

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

Appendix 01 - Elapsed Time Assumption of the Inspection of the Corner Fittings and

Appendix 02 - Elapsed Time Assumption of the Inspection of the Lower and Medium Spars .

**CONF 001

Task 541022-832-801-001: Inspection of the Corner Fittings

Get Access 2.00

On Aircraft

Do a detailed Inspection of Forward Corner Fittings of

Pylon AFT Secondary Structure LH

2.00

Do a detailed Inspection of Forward Corner Fittings of

Pylon AFT Secondary Structure RH

2.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

Task 541022-832-802-001: Inspection of the Lower and Medium Spars

Get Access 2.00

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 24

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Task 541022-832-802-001: Inspection of the Lower and Medium Spars

On Aircraft

Do a detailed Inspection of the Lower and Medium

Spars of the LH Pylon

2.00

Do a detailed Inspection of the Lower and Medium

Spars of the RH Pylon

2.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

**CONF 002

Task 541022-832-801-001: Inspection of the Corner Fittings

Get Access 2.00

On Aircraft

Do a detailed Inspection of Forward Corner Fittings of

Pylon AFT Secondary Structure LH

2.00

Do a detailed Inspection of Forward Corner Fittings of

Pylon AFT Secondary Structure RH

2.00

Close-Up 2.00

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

Task 541022-832-802-001: Inspection of the Lower and Medium Spars

Get Access 4.00

On Aircraft

Do a detailed Inspection of the Lower and Medium

Spars of the LH Pylon

2.00

Do a detailed Inspection of the Lower and Medium

Spars of the RH Pylon

2.00

Close-Up 4.00

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

**CONF ALL

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

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J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-40-00 06-41-54

12-34-24 54-56-00

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

Service Bulletin (SB) A320-54-1019

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-40-00 06-41-54

12-34-24 54-56-00

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

Service Bulletin (SB) A320-54-1019

**CONF ALL

K. PUBLICATION AFFECTED

Maintenance Planning Document (MPD) 545172-01-1

Structural Repair Manual (SRM) 54-54-17

L. INTERCHANGEABILITY/MIXABILITY

Not Applicable

M. SPARES

None

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

None

(2) Price and Availability

None

B. INDUSTRY SUPPORT INFORMATION

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

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 27

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This Page Intentionally Left Blank

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 541022-832-801-001 - Inspection of the Corner Fittings

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

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

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

operator has an accepted alternative procedure, the accepted alternative procedure

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

the procedure in the AIRBUS document must be used.

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

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

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

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

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

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

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

NOTE: This Service Bulletin is mandated or expected to be mandated by an Airworthiness

Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions

are Required for Compliance (RC) and must be done to comply with the AD. Other

paragraphs are recommended and may be deviated from, done as part of other

actions or done with accepted methods different from those given in the Service

Bulletin, as long as the RC paragraphs can be done and the aircraft can be put

back into a serviceable condition.

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

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

compliance times given in this Service Bulletin.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 29

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Task Associated Data

**CONF 001

Zone

475 476 485 486

Access

Panel 475AL 476AR 485AL 486AR

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

**CONF 002

Zone

475 476 485 486

Access

Panel 475AL 476AR 485AL 486AR

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 541022-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-40-00, Page Block 001

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

(b) For the identification of access panels, refer to AMM 06-40-00, Page Block 001.

(2) Subtask 541022-839-004-001 - 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: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 30

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**CONF 002

(1) Subtask 541022-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-40-00, Page Block 001

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

(b) For the identification of access panels, refer to AMM 06-40-00, Page Block 001.

(2) Subtask 541022-839-004-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 541022-941-001-001 - Job Set-Up

Work Zones and Access Panels

Zone Access/Work location

485 Access Panel 485AL

486 Access Panel 486AR

475 Access Panel 475AL

476 Access Panel 476AR

Manpower Resources

Skills NON SPECIFIC

References

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

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.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

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- 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 the access platform(s) in position.

(d) Remove the panels of the pylons 475AL, 476AR or 485AL, 486AR, refer to AMM

06-41-54, Page Block 001.

**CONF 002

(1) Subtask 541022-941-001-001 - Job Set-Up

Work Zones and Access Panels

Zone Access/Work location

485 Access Panel 485AL

486 Access Panel 486AR

475 Access Panel 475AL

476 Access Panel 476AR

Manpower Resources

Skills NON SPECIFIC

References

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

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.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 32

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- 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 the access platform(s) in position.

(d) Remove the panels of the pylons 475AL, 476AR or 485AL, 486AR, refer to AMM

06-41-54, Page Block 001.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 541022-220-001-001 - Do a detailed Inspection of Forward Corner Fittings

of Pylon AFT Secondary Structure LH

Work Zones and Access Panels

Zone Access/Work location

485

486

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Service Bulletin (SB) A320-54-1019

Fig. A-FBAAA

Area to be Inspected - Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report - Corner Fittings

Sheet 01

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

1 Do a Detailed Inspection of the corner fittings

Refer to Fig. A-FBAAA

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

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Refer to Fig. A-FFAAA

2 If no crack is found on the corner fitting:

a Do the inspection again at the interval given in PLANNING

INFORMATION Paragraph E.(2), refer to TASK 541022-832-801 001

Inspection of the Corner Fittings

3 If crack is found on the corner fitting:

a Do TASK 541022-832-802 001 Inspection of the Lower and Medium

Spars

(b) Please fill in the inspection report, refer to Fig. A-FRAAA Sheet 01

(2) Subtask 541022-220-002-001 - Do a detailed Inspection of Forward Corner Fittings

of Pylon AFT Secondary Structure RH

Work Zones and Access Panels

Zone Access/Work location

485

486

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Service Bulletin (SB) A320-54-1019

Fig. A-FBAAA

Area to be Inspected - Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report - Corner Fittings

Sheet 01

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

1 Do a Detailed Inspection of the corner fittings

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 34

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2 If no crack is found on the corner fitting:

a Do the inspection again at the interval given in PLANNING

INFORMATION Paragraph E.(2), refer to TASK 541022-832-801 001

Inspection of the Corner Fittings

3 If crack is found on the corner fitting:

a Do TASK 541022-832-802 001 Inspection of the Lower and Medium

Spars

(b) Please fill in the inspection report, refer to Fig. A-FRAAA Sheet 01

**CONF 002

(1) Subtask 541022-220-001-001 - Do a detailed Inspection of Forward Corner Fittings

of Pylon AFT Secondary Structure LH

Work Zones and Access Panels

Zone Access/Work location

485

486

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Service Bulletin (SB) A320-54-1019

Fig. A-FBAAA

Area to be Inspected - Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report - Corner Fittings

Sheet 01

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

1 Do a Detailed Inspection of the corner fittings

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 35

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2 If no crack is found on the corner fitting:

a Do the inspection again at the interval given in PLANNING

INFORMATION Paragraph E.(2), refer to TASK 541022-832-801 001

Inspection of the Corner Fittings

3 If crack is found on the corner fitting:

a Do TASK 541022-832-802 001 Inspection of the Lower and Medium

Spars

(b) Please fill in the inspection report, refer to Fig. A-FRAAA Sheet 01

(2) Subtask 541022-220-002-001 - Do a detailed Inspection of Forward Corner Fittings

of Pylon AFT Secondary Structure RH

Work Zones and Access Panels

Zone Access/Work location

485

486

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Service Bulletin (SB) A320-54-1019

Fig. A-FBAAA

Area to be Inspected - Corner Fitting

Sheet 01

Sheet 02

Sheet 03

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRAAA

Inspection Report - Corner Fittings

Sheet 01

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

1 Do a Detailed Inspection of the corner fittings

Refer to Fig. A-FBAAA

Refer to Fig. A-FFAAA

2 If no crack is found on the corner fitting:

a Do the inspection again at the interval given in PLANNING

INFORMATION Paragraph E.(2), refer to TASK 541022-832-801 001

Inspection of the Corner Fittings

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

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3 If crack is found on the corner fitting:

a Do TASK 541022-832-802 001 Inspection of the Lower and Medium

Spars

(b) Please fill in the inspection report, refer to Fig. A-FRAAA Sheet 01

**CONF ALL

D. TEST

**CONF 001

None

**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 541022-942-001-001 - Close-Up

Work Zones and Access Panels

Zone Access/Work location

475 Access Panel 475AL

476 Access Panel 476AR

485 Access Panel 485AL

486 Access Panel 486AR

Manpower Resources

Skills NON SPECIFIC

References

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

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

equipment.

(b) Install the panels of the pylons 475AL, 476AR or 485AL, 486AR, refer to AMM

06-41-54, Page Block 001.

(c) Remove the access platform(s).

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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 37

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**CONF 002

(1) Subtask 541022-942-001-001 - Close-Up

Work Zones and Access Panels

Zone Access/Work location

475 Access Panel 475AL

476 Access Panel 476AR

485 Access Panel 485AL

486 Access Panel 486AR

Manpower Resources

Skills NON SPECIFIC

References

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

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

equipment.

(b) Install the panels of the pylons 475AL, 476AR or 485AL, 486AR, refer to AMM

06-41-54, Page Block 001.

(c) Remove the access platform(s).

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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 38

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Task 541022-832-802-001 - Inspection of the Lower and Medium Spars

**CONF ALL

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

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

THIS:

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

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

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

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

operator has an accepted alternative procedure, the accepted alternative procedure

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

the procedure in the AIRBUS document must be used.

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

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

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

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

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

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

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

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

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

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

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

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

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

the aircraft can be put back into a serviceable condition.

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

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

compliance times given in this Service Bulletin.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 39

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Task Associated Data

**CONF 001

Zone

470 480

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 4.00

**CONF 002

Zone

470 475 476 480

Manpower

TOTAL MANHOURS 12.00

ELAPSED TIME (HOURS) 6.00

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 541022-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-40-00, Page Block 001

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

(b) For the identification of access panels, refer to AMM 06-40-00, Page Block 001.

(2) Subtask 541022-839-005-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 541022-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 40

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References

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

06-40-00, Page Block 001

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

(b) For the identification of access panels, refer to AMM 06-40-00, Page Block 001.

(2) Subtask 541022-839-005-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 541022-941-003-001 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

470

480

Manpower Resources

Skills AIRFRAME

References

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

Task 54-56-00-000-002

(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.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 41

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- 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 the access platform(s) in position.

(d) Remove the LH and/or RH Aft Lower fairing, refer to AMM Task 54-56-00-000-002.

**CONF 002

(1) Subtask 541022-941-003-002 - Job Set-up

Work Zones and Access Panels

Zone Access/Work location

475 Work location Panel 475AL

476 Work location Panel 476AR

Manpower Resources

Skills AIRFRAME

References

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

Task 54-56-00-000-001

(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 the access platform(s) in position.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 42

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(d) Remove the LH and/or RH Aft Lower fairing, refer to AMM Task 54-56-00-000-001.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 541022-220-003-001 - Do a detailed Inspection of the Lower and Medium

Spars of the LH Pylon

Work Zones and Access Panels

Zone Access/Work location

470

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Fig. A-FBCAA

Area to be inspected - Lower and

Medium spars

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRBAA

Inspection Report - Lower and Medium

Spars

Sheet 01

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

1 Do a Detailed Inspection of the Lower and Medium Spars.

Refer to Fig. A-FBCAA

Refer to Fig. A-FFAAA

a If no damage is found :

<1> Accomplish Service Bulletin No. A320-54-1019 at the threshold

given in PLANNING INFORMATION paragraph E.2.

b If damage is found such as crack or deformation :

<1> Contact Airbus and apply instructions approved by Airbus before

next flight.

(b) Please fill in the Inspection report, refer to Fig. A-FRBAA Sheet 01

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 43

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(2) Subtask 541022-220-004-001 - Do a detailed Inspection of the Lower and Medium

Spars of the RH Pylon

Work Zones and Access Panels

Zone Access/Work location

480

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Fig. A-FBCAA

Area to be inspected - Lower and

Medium spars

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRBAA

Inspection Report - Lower and Medium

Spars

Sheet 01

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

1 Do a Detailed Inspection of the Lower and Medium Spars.

Refer to Fig. A-FBCAA

Refer to Fig. A-FFAAA

a If no damage is found :

<1> Accomplish Service Bulletin No. A320-54-1019 at the threshold

given in PLANNING INFORMATION paragraph E.2.

b If damage is found such as crack or deformation :

<1> Contact Airbus and apply instructions approved by Airbus before

next flight.

(b) Please fill in the Inspection report, refer to Fig. A-FRBAA Sheet 01

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 44

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**CONF 002

(1) Subtask 541022-220-003-001 - Do a detailed Inspection of the Lower and Medium

Spars of the LH Pylon

Work Zones and Access Panels

Zone Access/Work location

470

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Fig. A-FBCAA

Area to be inspected - Lower and

Medium spars

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRBAA

Inspection Report - Lower and Medium

Spars

Sheet 01

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

1 Do a Detailed Inspection of the Lower and Medium Spars.

Refer to Fig. A-FBCAA

Refer to Fig. A-FFAAA

a If no damage is found :

<1> Accomplish Service Bulletin No. A320-54-1019 at the threshold

given in PLANNING INFORMATION paragraph E.2.

b If damage is found such as crack or deformation :

<1> Contact Airbus and apply instructions approved by Airbus before

next flight.

(b) Please fill in the Inspection report, refer to Fig. A-FRBAA Sheet 01

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 45

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(2) Subtask 541022-220-004-001 - Do a detailed Inspection of the Lower and Medium

Spars of the RH Pylon

Work Zones and Access Panels

Zone Access/Work location

480

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills NON SPECIFIC

References

Fig. A-FBCAA

Area to be inspected - Lower and

Medium spars

Sheet 01

Sheet 02

Sheet 03

Sheet 04

Sheet 05

Fig. A-FFAAA

Flow Chart

Sheet 01

Fig. A-FRBAA

Inspection Report - Lower and Medium

Spars

Sheet 01

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

1 Do a Detailed Inspection of the Lower and Medium Spars.

Refer to Fig. A-FBCAA

Refer to Fig. A-FFAAA

a If no damage is found :

<1> Accomplish Service Bulletin No. A320-54-1019 at the threshold

given in PLANNING INFORMATION paragraph E.2.

b If damage is found such as crack or deformation :

<1> Contact Airbus and apply instructions approved by Airbus before

next flight.

(b) Please fill in the Inspection report, refer to Fig. A-FRBAA Sheet 01

**CONF ALL

D. TEST

**CONF 001

None

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 46

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**CONF 002

None

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 541022-942-003-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

470

480

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 54-56-00-400-002

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

equipment.

(b) Install the removed Aft Lower Fairing, refer to AMM Task 54-56-00-400-002.

(c) Remove the access platform(s).

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

**CONF 002

(1) Subtask 541022-942-003-002 - Close-up

Work Zones and Access Panels

Zone Access/Work location

470

480

Manpower Resources

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 54-56-00-400-001

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

equipment.

(b) Install the removed Aft Lower Fairing, refer to AMM Task 54-56-00-400-001.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 47

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(c) Remove the access platform(s).

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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 48

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**CONF ALL

RIB11

RIB12

Z475 Z476 − 

A

A

Z485 Z486 − 

B

AREA TO BE INSPECTED

B

A

C

N_SB_541022_5_BAAA_01_04

Figure A-FBAAA - Sheet 01

Area to be Inspected - Corner Fitting

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 49

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**CONF ALL

RIB11

CORNER FITTING

CORNER FITTING

TOP VIEW

PYLON AXIS

D

D

TYPICAL CRACK

LH SHOWN

RH SYMMETRICAL

C

D

(MEDIUM SPAR NOT REPRESENTED)

A A

B B

N_SB_541022_5_BAAA_02_08

Figure A-FBAAA - Sheet 02

Area to be Inspected - Corner Fitting

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 50

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**CONF ALL

TYPICAL CRACKS

TYPICAL CRACKS

RIB11

CORNER FITTING

CORNER FITTING

FWD

FWD

RIB11 A A

B B

N_SB_541022_5_BAAA_03_05

Figure A-FBAAA - Sheet 03

Area to be Inspected - Corner Fitting

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 51

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**CONF ALL

RIB11

RIB12

Z475 Z476 − 

A

A

Z485 Z486 − 

B

AREA TO BE INSPECTED

B

A

C

A

A

D

D

N_SB_541022_5_BCAA_01_03

Figure A-FBCAA - Sheet 01

Area to be inspected - Lower and Medium spars

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 52

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**CONF ALL

RIB11

TOP VIEW

PYLON AXIS

C

NOTE:

01 INSPECTION AREA ON MEDIUM SPAR UPPER SURFACE BETWEEN RIB11 AND HALF WAY TO RIB12

OF MEDIUM SPAR

01

FASTENERS NOT AFFECTED

UPPER AREA

N_SB_541022_5_BCAA_02_04

Figure A-FBCAA - Sheet 02

Area to be inspected - Lower and Medium spars

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 53

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**CONF ALL

RIB11

CORNER FITTING

CORNER FITTING

PYLON AXIS

TOP VIEW

NOTE:

01 INSPECTION AREA ON LOWER SPAR UPPER SURFACE BETWEEN RIB11 AND HALF WAY TO RIB12

OF LOWER SPAR

01

A A

B B

C C

N_SB_541022_5_BCAA_03_04

Figure A-FBCAA - Sheet 03

Area to be inspected - Lower and Medium spars

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 54

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**CONF ALL

RIB11

PYLON AXIS

BOTTOM VIEW

NOTE:

01 INSPECTION AREA ON LOWER SPAR LOWER SURFACE BETWEEN RIB11 AND HALF WAY TO RIB12

OF LOWER SPAR

01

FASTENERS NOT AFFECTED

D D

N_SB_541022_5_BCAA_04_02

Figure A-FBCAA - Sheet 04

Area to be inspected - Lower and Medium spars

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 55

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**CONF ALL

RIB11

FWD

RIB11

FWD

LOWER SPAR TO BE INSPECTED

ON UPPER AND LOWER SURFACE

MEDIUM SPAR

AREA TO BE INSPECTED

ON UPPER SURFACE

LOWER SPAR TO BE INSPECTED

ON UPPER AND LOWER SURFACE

MEDIUM SPAR

AREA TO BE INSPECTED

ON UPPER SURFACE

B B

C C

NOTE:

FASTENERS NOT AFFECTED N_SB_541022_5_BCAA_05_01

Figure A-FBCAA - Sheet 05

Area to be inspected - Lower and Medium spars

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 56

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**CONF ALL

QUESTION

ACTION

FINDING

REFER TO TASK 541022−832−801−001

CRACK FOUND

NO YES

DO THE INSPECTION AGAIN

AT THE INTERVAL

DO A DETAILED INSPECTION OF CORNER FITTINGS

CONTACT AIRBUS AND APPLY

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2).

ON CORNER FITTINGS AT

AFT FIXED FAIRING

STRUCTURE

GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.(2).

REFER TO TASK 541022−832−801−001

DO A DETAILED INSPECTION OF THE

LOWER AND MEDIUM SPAR FOR CRACK

DEFORMATION DETECTION IN THE

SPLICING AREA WITH CORNER FITTING

NO DAMAGE FOUND YES

ACCOMPLISH SERVICE BULLETIN

No A320−54−1019

AT THE THRESHOLD GIVEN IN THE

PLANNING INFORMATION PARAGRAPH E.(2).

BETWEEN RIBS 11 AND 12

REFER TO TASK 541022−832−802−001

NOTE:

THE PURPOSE OF FLOW CHARTS IS TO SUPPLEMENT THE INFORMATION GIVEN IN THE PROCEDURE

AND COMPLIANCE PARAGRAPHS AND NOT TO SERVE AS THE PRIMARY SOURCE FOR TASKS OR

COMPLIANCE TIMES GIVEN IN THIS SERVICE BULLETIN.

INSTRUCTIONS APPROVED BY

AIRBUS BEFORE NEXT FLIGHT

N_SB_541022_5_FAAA_01_05

Figure A-FFAAA - Sheet 01

Flow Chart

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 57

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**CONF ALL

PRESENCE OF CRACK(S)

YES NO

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A320−54−1022

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRUCTURE − ENGINE PYLON

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

DETAILED INSPECTION FAX +33 (0)5 61 93 36 14

ON CORNER

FITTINGS AT AFT FIXED

CORNER FITTING

CORNER FITTING

PYLON AXIS

PYLON LH

PYLON AXIS

PYLON RH

AREA WILL BE REPAIRED IN ACCORDANCE WITH :

SERVICE BULLETIN No. 54−1019

PLEASE RECORD OTHER FINDINGS :

RIB11

RIB11

FAIRING STRUCTURE

FITTING

CORNER

INBOARD

YES NO

FITTING

CORNER

OUTBOARD

PRESENCE OF CRACK(S)

YES NO

ON CORNER

FITTINGS AT AFT FIXED

FAIRING STRUCTURE

FITTING

CORNER

INBOARD

YES NO

FITTING

CORNER

OUTBOARD

INBOARD

OUTBOARD

CORNER FITTING

INBOARD

CORNER FITTING

OUTBOARD

E−mail: structure.sbinspectionresult@airbus.com

N_SB_541022_5_RAAA_01_04

Figure A-FRAAA - Sheet 01

Inspection Report - Corner Fittings

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 58

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**CONF ALL

INSPECTION REPORT

SERVICE BULLETIN No. :

A/C MSN :

FLIGHT CYCLES :

FLIGHT HOURS :

A320−54−1022

DATE OF INSPECTION :

RETURN TO :

AIRBUS

CUSTOMER SERVICES ENGINEERING − SEES2

WING FIX STRUCTURE − ENGINE PYLON

INSPECTION METHOD :

1 ROND POINT MAURICE BELLONTE

31707 BLAGNAC CEDEX

FRANCE

FAX +33 (0)5 61 93 36 14 DETAILED

YES NO

INSPECTION

LOWER SPAR

MEDIUM

LOWER

SPAR

MEDIUM

SPAR

FWD

FWD

CRACK OR DEFORMATION

RIB11

RIB11

FOUND ON MEDIUM SPAR

YES NO

CRACK OR DEFORMATION

FOUND ON LOWER SPAR

UPPER AREA

LH PYLON

RH PYLON YES NO

LH PYLON SHOWN 

(RH PYLON IDENTICAL)

LH PYLON SHOWN 

(RH PYLON IDENTICAL)

LH

UPPER

AREA

PYLON YES NO LOWER

AREA

YES NO RH

UPPER

AREA

PYLON YES NO LOWER

AREA SPAR

E−mail: structure.sbinspectionresult@airbus.com

N_SB_541022_5_RBAA_01_02

Figure A-FRBAA - Sheet 01

Inspection Report - Lower and Medium Spars

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 59

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This Page Intentionally Left Blank

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 60

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Appendix 01 - Elapsed Time Assumption of the Inspection of the Corner Fittings

**CONF ALL

This chart is only a proposal. Operators may determine that another way to do the work is more

suitable for them.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 1

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Appendix 01 - Elapsed Time Assumption of the Inspection of the Corner Fittings

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320−54−1022

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

8.00

4.00

STEPS

2.00 1.00

0

CLOSE−UP 2.00 1.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

PER

2

2

:

:

SB ELAPSED TIME

(HOURS)

1 2 3 4

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

ON PYLON LH

INSPECTION OF THE

ON PYLON RH

INSPECTION OF THE

CORNER FITTINGS

CORNER FITTINGS

2.00 2.00 1

2.00 2.00 1

N_SB_541022_5_ACAA_01_02

Figure A-FACAA - Sheet 01

Elapsed Time Assumption of the Inspection of the Corner Fittings

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 2

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Appendix 02 - Elapsed Time Assumption of the Inspection of the Lower and Medium Spars

**CONF ALL

This chart is only a proposal. Operators may determine that another way to do the work is more

suitable for them.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 1

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Appendix 02 - Elapsed Time Assumption of the Inspection of the Lower and Medium Spars

**CONF 001

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320−54−1022

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

8.00

4.00

STEPS

2.00 1.00

LOWER AND MEDIUM SPAR

2.00 2.00

CLOSE−UP 2.00 1.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

PER

2

1

2

LOWER AND MEDIUM SPAR

2.00 2.00 1

:

:

SB ELAPSED TIME

(HOURS)

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

0 1 2 3 4

DETAIL INSPECTION OF THE

OF THE LH PYLON

OF THE RH PYLON

DETAIL INSPECTION OF THE

N_SB_541022_5_ADAA_01_01

Figure A-FADAA - Sheet 01

Elapsed Time Assumption of the Inspection of the Lower and Medium Spars for aircraft with IAE

engines

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 2

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Appendix 02 - Elapsed Time Assumption of the Inspection of the Lower and Medium Spars

**CONF 002

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320−54−1022

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

12.00

6.00

STEPS

4.00 2.00

LOWER AND MEDIUM SPAR

2.00 2.00

CLOSE−UP 4.00 2.00

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL.

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM.

01

02

NOTE:

PER

2

1

2

LOWER AND MEDIUM SPAR

2.00 2.00 1

:

:

SB ELAPSED TIME

(HOURS)

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART.

0 1 2 3 4 5 6

DETAIL INSPECTION OF THE

OF THE LH PYLON

OF THE RH PYLON

DETAIL INSPECTION OF THE

N_SB_541022_5_ADAB_01_00

Figure A-FADAB - Sheet 01

Elapsed Time Assumption of the Inspection of the Lower and Medium Spars for aircraft with CFM

engines

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 3

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REPORTING SHEET

TITLE: NACELLES/PYLONS - GENERAL - INSPECTION OF FORWARD

CORNER FITTING OF PYLON AFT SECONDARY STRUCTURE.

MODIFICATION No.: None

Please complete the appropriate item (A or B):

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

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

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

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

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

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

Or : Intermediate revision YES/NO

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

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

the next feasible revision, this will result in

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

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

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

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

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

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

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 1

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QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022

REVISION No.: 03 - Apr 15/14 Page: 1

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