# @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



# MANDATORYMANDATORYMANDATORY
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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORYMANDATORYMANDATORY
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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 13472224 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 28283162 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 26242629 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 5

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# @A318/A319/A320/A321 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 17272335 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 31473148 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN DAL 0118 0121 0125 0152 0153 0160 0171 0192 0197 0206 0208 0213 0262 0263 0272 0273 0281 0282 0297 0298 0306 0307 0318 0319 0329 0339 0340 0355 0358 0360 0367 0372 0380 0381 0387 0388 0399 0408 0410 0417 0418 0766 0778 0786 0801 0807 0818 0830 0832 0846 0903 0907 0911 0923 0962 0964 0981 0988 0996 1011 1037 1058 1062 1191 1230 1249 1324 1325 1346 1392 1414 1434 1453 1456 1483 1498 1501 1520 1535 1543 1549 1567 1570 1582 1633 1641 1646 1659 1662 1683 1685 1693 1709 1714 1738 1746 1752 1766 1774 1789 1796 1800 1810 1812 1815 1820 1824 1828 1833 1839 1875 1897 1923 1959 1976 1982 1990 2002 2013 2026 2039 2047 2082 2087 2092 2095 DCS 1053 DKH 2975 3027 3234 3268 3368 DLH 0069 0070 0071 0072 0078 0083 0086 0093 0094 0104 0110 0111 0116 0117 0135 0137 0161 0172 0201 0202 0209 0216 0267 0268 0269 0346 0412 0458 0468 0473 0474 0484 0493 0502 0505 0518 0560 0563 0564 0567 0595 0609 0610 0616 0623 0627 0636 0641 0651 0652 0679 0689 0692 0694 0699 0700 0717 0723 0729 0738 0744 0853 0860 0875 0887 0901 1016 1080 1161 1172 1188 1214 1260 1273 1337 1365 1367 DNV 1630 1805 1808 1841 2093 2179 2241 2751 3065 3179 DQA 2347 DRK 2306 2346 DTR 0444 EAA 0386 0445 EDW 0942 0947 1026 2024 EIN 0926 1023 1094 1242 1394 1443 1983 2001 2191 2206 2217 2250 2256 2272 2294 2364 2374 2399 2409 2411 2432 2486 2542 2583 2635 3054 3102 3129 3169 3318 3345 3377 ETD 0350 1140 1159 1944 1945 1947 1955 2167 3004 3050 ETJ 0325 0428 EVA 3363 EZD 0667 0743 0872 0874 1074 1286 2137 2141 2147 2576 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN FIN 0941 0961 1073 1107 1184 1185 1241 1309 1352 1364 1405 1470 1544 1588 1712 1913 1916 1978 1989 2065 2124 2146 2154 2208 2266 FLI 2186 FPY 0112 0189 0342 FRN 0647 0660 FTZ 1068 1145 2176 G2X 0347 0674 G4I 1157 1795 2507 G8E 0349 0594 2700 2763 GAP 0706 0745 2162 2183 GBB 0067 GCR 2338 GLG 1866 1872 1882 1925 2078 2126 GMI 0970 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN JBU 1123 1156 1173 1235 1240 1257 1270 1280 1302 1327 1398 1446 1452 1506 1528 1546 1557 1610 1650 1705 1739 1784 1785 1849 1861 1898 1904 1915 1917 1927 1948 2006 2020 2031 2042 2063 2075 2099 2125 2132 2136 2149 2150 2159 2160 2177 2201 2215 2231 2246 2259 2280 2284 2286 2307 2314 2336 2352 2368 2384 2386 2415 2447 2449 2461 2489 2491 2504 2520 2535 2577 2580 2640 2647 2671 2710 2725 2755 JSA 2316 2356 2423 2453 2604 JST 1195 1408 2169 2185 2197 2292 2299 2322 2329 2455 2515 2526 2537 2573 2587 2608 2642 2651 2703 2766 2787 JZR 2792 2822 KAC 0181 0182 0195 2046 KCA 0662 KFR 2650 KGL 0663 0668 0787 0852 0954 1060 1293 15542029 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 27763218 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 5

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# @A318/A319/A320/A321 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 28172850 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 20642076 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN SGG 0799 0879 1390 SHJ 0910 SHU 2222 SKU 0179 0406 0447 1400 1523 2119 2129 22142249 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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 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 20172018 2019 2022 20242026 2028 2030 2033 20342035 2036 20372039 2043 2046 20472048 2049 2050 2052 2053 20542056 20572059 2060 2061 2062 20642065 2066 2068 002

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022 REVISION No.: 03 - Apr 15/14 Page: 14 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 2069 2071 2072 20742076 2078 2081 2082 2083 2086 2087 2091 2092 2093 2095 2100 2101 2103 21042106 2109 2113 21142115 2116 21172119 2120 2122 2123 2124 2126 2127 2129 2131 2133 21342140 2142 2143 21442145 2146 2151 21542155 2158 2162 2163 2165 2166 2170 2171 21742175 2176 2178 2179 2180 2181 2182 2183 21842186 21872189 2191 2196 2198 2199 2206 22072208 2209 2212 2213 2214 22172219 2220 2221 2222 22242225 22272228 2230 2233 2235 2236 22372239 2240 2241 2242 2243 2244 2245 2248 2249 2250 2251 2253 2256 2258 2260 2262 2264 2265 2266 2269 2270 2271 2272 22742278 2279 2283 2285 22872289 2291 2293 22942298 2300 2306 2309 2311 2315 23172318 2319 2325 23272328 2330 2332 2333 23372342 23442346 23472349 2350 2353 235423572358 2360 2361 23642365 23672369 2370 2373 237423772378 2380 2381 2382 2385 23872388 2390 2391 2392 23942398 2399 2400 2402 2406 24072409 2411 2412 2416 2419 2420 2425 2427 2432 2436 24372439 2440 2442 2446 2448 2450 2451 2456 2460 2463 24642465 2471 2472 247424772478 2481 2483 24842486 24872488 2492 2493 24942495 24972498 2499 2503 2506 25072508 2511 2512 25142516 2518 2519 2523 2525 2527 2528 2529 2532 2538 2539 2540 2541 2542 2543 25442545 2546 25472548 2549 2550 2551 2552 25542555 2556 2557 2558 2561 2562 2563 2565 2569 2575 2578 2581 2582 2583 25842586 2588 2591 2592 2593 2596 2599 2601 2605 2606 26072611 2612 2616 26172618 2619 2620 2623 26242625 26272628 2629 2632 2633 2635 2636 26372638 2641 2644 2646 2652 26542656 2658 2662 2665 2668 2672 26742675 26772678 2681 2683 26842685 2686 2691 2693 2695 2696 2699 2700 2702 2705 2706 27072708 2709 2712 2715 2716 2719 2721 2726 27272729 2733 2735 2736 2740 2742 2743 27442745 2746 2748 2749 2750 2751 27542756 27572758 2760 2761 2762 2763 27642765 2768 2769 2770 2773 2774 2776 27772778 2779 2782 2785 2786 2788 2789 2790 2792 27942795 2796 2798 2800 2801 2803 2805 2806 28072810 2811 2812 2816 2818 2819 2820 2821 2822 2824 2825 2826 28272829 2830 2831 28342835 2836 28372839 2841 2842 2843 2846 28472849 2851 2852 2853 28542855 28572860 2861 2865 2866 28672869 2870 2873 2875 2876 28772878 2879 2881 2882 28842885 2889 2890 2891 2895 28972899 2902 2903 2905 29072909 2910 2912 2913 2915 2918 2920 2921 2923 29242925 2926 2930 2932 2935 2937 2938 2939 29442946 29472949 2950 2951 29542956 2957 2959 2960 2961 2962 29642965 2966 29672968 2972 2973 2975 2980 2985 2986 2988 2989 2991 2993 2995 2996 2998 3000 3002 3003 30063008 3009 30143016 30183019 3021 3023 3024 3025 30273028 3031 3035 3036 30373040 3041 3043 3044 3046 30473051 3052 3053 305430553056 3058 3059 3060 3061 3063 306430653068 3070 3073 3076 3078 3079 3080 3082 3083 308430853088 3090 3093 30943095 3096 3097 3098 3099 3100 3101 3102 3109 3111 31173118 3121 3122 002

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022 REVISION No.: 03 - Apr 15/14 Page: 15 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 3129 3131 3132 3133 31343135 313631373138 3139 3140 3145 31473148 3151 3152 3153 31543155 3161 3168 3169 3173 31743176 3179 3180 3181 3182 31843186 3188 3189 31943199 3201 3202 3203 320432063209 3211 3215 3218 3221 3223 322432263232 3234323632373242 3245 3246 3255 3261 3268 3272 32773282 32853289 3291 3293 3299 3318 3320 3321 3323 3327333733383345 3346 3349 3353 3361 3363 3366 33683370 3376 33773380 3383 002

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022 REVISION No.: 03 - Apr 15/14 Page: 16 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 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 20042006 20072008 20142015 2016 2020 2021 2023 20272029 2031 2032 2038 2040 2041 2042 20442045 2055 2058 2063 20672070 2073 2075 2077 2079 2080 20842085 2088 2089 2090 20942096 20972098 2099 2102 2105 21072108 2110 2112 2118 2121 2125 2128 2130 2132 2135 2136 21372138 2139 2141 2147 2148 2149 2150 2152 2153 2156 21572159 2160 2161 2164 21672168 2169 2172 2173 21772185 2188 2190 2192 2193 21942195 21972200 2201 2202 2203 22042205 2210 2211 2215 2216 2223 2226 2229 2231 2232 22342238 2246 2247 2252 2254 2255 22572259 2261 2263 22672268 2273 2275 22772280 2281 2282 22842286 2288 2290 2292 2295 2296 22972299 2301 2302 2303 23042305 23072308 2310 2312 2313 2314 2316 2320 2321 2322 2323 23242326 2329 2331 23342335 2336 2338 2339 2340 2341 2343 2345 2348 2351 2352 2355 2356 2359 2362 2363 2366 2368 2371 2372 2375 2376 2379 2383 23842386 2389 2393 2395 2396 23972401 2403 2404 2405 2408 2410 2413 24142415 24172418 2421 2422 2423 2426 2428 2429 2430 2431 2433 24342435 2438 2441 2443 24442445 24472449 2452 2453 24542455 2457 2458 2459 2461 2462 2466 24672468 2469 2470 2473 2475 2476 2479 2480 2482 2485 2489 2490 2491 2496 2501 2502 25042505 2509 2510 2513 2515 25172520 2521 2522 2524 2526 2530 2531 2533 25342535 2536 25372553 2559 2560 25642566 25672568 2570 2571 2572 2573 25742576 2577 2579 2580 2585 25872589 2590 25942595 25972598 2600 2602 2603 26042608 2609 2610 2613 26142615 2621 2622 2626 2630 2631 26342639 2640 2642 2643 2645 26472648 2649 2650 2651 2653 2655 26572659 2660 2661 2663 2664 2666 2667 2669 2670 2671 2673 2676 2679 2680 2682 2687 2688 2689 2690 2692 269426972698 2701 2703 27042710 2711 2713 271427172718 2720 2723 27242725 2728 2730 2731 2732 273427372738 2739 2741 27472752 2753 2755 2759 2766 27672771 2772 2775 2780 2783 278427872791 2793 2797 001

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022 REVISION No.: 03 - Apr 15/14 Page: 18 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 2799 28042808 2809 2813 2815 28172823 2828 2833 2838 2840 28442845 2850 2856 2858 2859 2862 2863 28642868 2872 28742883 2886 28872888 2892 2893 2894 2896 2898 2901 29042906 2908 2911 29142916 29172919 2922 2927 2928 2929 2933 29342936 2940 2941 2942 2943 2948 2952 2953 2958 2963 2969 2971 29742976 2978 2979 2981 2982 2983 298429872990 29972999 30043005 3007 3010 3011 3012 3013 3015 30173020 3022 30263032 3042 3045 3049 3050 305730673069 3071 3075 30773081 3086 3103 3104 3106 3112 3113 31143116 312431253126 3141 3142 3144 3156 3159 3162 31653175 3183 31853192 3195 3198 3200 320732083219 3231 3239 32443253 32573275 3279 3283 3292 329632973303 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 toTASK 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 5

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# @A318/A319/A320/A321 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 REVISION No.: 03 - Apr 15/14 Page: 25 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 REVISION No.: 03 - Apr 15/14 Page: 26 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022 REVISION No.: 03 - Apr 15/14 Page: 28 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 475476485486 Access Panel 475AL476AR485AL486AR 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
**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 REVISION No.: 03 - Apr 15/14 Page: 31 5

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# @A318/A319/A320/A321 SERVICE BULLETIN - 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN - 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 REVISION No.: 03 - Apr 15/14 Page: 33 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 Sheet01 Sheet02 Sheet03 Fig. A-FFAAA Flow Chart Sheet01 Fig. A-FRAAA Inspection Report - Corner Fittings Sheet01 (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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 Sheet01 Sheet02 Sheet03 Fig. A-FFAAA Flow Chart Sheet01 Fig. A-FRAAA Inspection Report - Corner Fittings Sheet01 (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 REVISION No.: 03 - Apr 15/14 Page: 36 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
**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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Task Associated Data **CONF 001 Zone 470 480 Manpower TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.00 **CONF 002 Zone 470 475476480 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN - 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
**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 Sheet01 Sheet02 Sheet03 Sheet04 Sheet05 Fig. A-FFAAA Flow Chart Sheet01 Fig. A-FRBAA Inspection Report - Lower and Medium Spars Sheet01
(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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (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 Sheet01 Sheet02 Sheet03 Sheet04 Sheet05 Fig. A-FFAAA Flow Chart Sheet01 Fig. A-FRBAA Inspection Report - Lower and Medium Spars Sheet01
(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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
**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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

RIB11

TOP VIEW PYLON AXIS



## C

**NOTE:** INSPECTION AREA ON MEDIUM SPAR UPPER SURFACE BETWEEN RIB11 AND HALF WAY TO RIB12 01 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

RIB11 CORNER FITTING

CORNER FITTING PYLON AXIS

TOP VIEW

**NOTE:** INSPECTION AREA ON LOWER SPAR UPPER SURFACE BETWEEN RIB11 AND HALF WAY TO RIB12 01 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

RIB11 PYLON AXIS

BOTTOM VIEW

**NOTE:** INSPECTION AREA ON LOWER SPAR LOWER SURFACE BETWEEN RIB11 AND HALF WAY TO RIB12 01 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**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

DAMAGE FOUND NO 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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

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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**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 YES NO RH PYLON **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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022 REVISION No.: 03 - Apr 15/14 Page: 60 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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

2.00 1.00 CLOSE−UP

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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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

4.00 2.00 CLOSE−UP

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. 5 0 1 2 3 4 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Jul 07/09 SERVICE BULLETIN No.: A320-54-1022 REVISION No.: 03 - Apr 15/14 Page: 1 5

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