# @A318/A319/A320/A321 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONICCOMMON INSTALLATION-GENERALLUGS INSPECTION ON 10VU SLEEVES MODIFICATION No.: None This page transmits Revision No.02 of Service Bulletin No.A320-92-1087 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 02 issued to update the effectivity. CHANGES The main changes of this revision are: - update the effectivity, - delete Config. 02, - modify the Accomplishment Timescale Table, - update the flow chart, - update the Paragraph Inspection. FRONT MATTER ELECTRIC AND ELECTRONIC COMMON INSTALLATION-GENERAL-LUGS INSPECTION ON 10VU SLEEVES CONFIGURATION UPDATED R
SUMMARY GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE UPDATED CONFIGURATION UPDATED R
MATERIAL PRICE INFORMATION TABLE DELETED FOR APPLICABLE MSN D

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
EFFECTIVITY OPERATOR LIST UPDATED R MANPOWER MANPOWER UPDATED CONFIGURATION UPDATED R MANPOWER DELETED FOR APPLICABLE MSN D APPENDICES APPENDICES UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONFIGURATION LIST UPDATED R CONF 001 CONFIGURATION DEFINITION UPDATED CONFIGURATION DESCRIPTION UPDATED R Configuration definition CONFIGURATION DELETED D DESCRIPTION DESCRIPTION UPDATED R COMPLIANCE Accomplishment Timescale ACCOMPLISHMENT TIMESCALE UPDATED CONFIGURATION UPDATED R MANPOWER MANPOWER UPDATED CONFIGURATION UPDATED R MANPOWER DELETED FOR APPLICABLE MSN D WEIGHT AND BALANCE Minor editorial or document structure change R REFERENCES REFERENCED DOCUMENTATION UPDATED CONFIGURATION UPDATED R REFERENCED DOCUMENTATION DELETED FOR APPLICABLE MSN D MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED R Price and Availability PRICE AND AVAILABILITY UPDATED MATERIAL SET UPDATED R LIST OF MATERIALS - OPERATOR SUPPLIED Consumable Materials CONSUMABLE MATERIALS UPDATED R Consumable CMLA01 CONSUMABLE MATERIAL SET UPDATED CONSUMABLE UPDATED R Components Component COMPA01 PART MATERIAL SET UPDATED QUANTITY UPDATED ITEM NUMBER UPDATED PART NUMBER UPDATED KEYWORD UPDATED R

TOOLING Tools TOOLS UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 921087- 832-801-001-Inspection TASK SOLUTION UPDATED NOTE UPDATED CAUTION UPDATED CONFIGURATION UPDATED R

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 2 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Task associated data - 001 CONFIGURATION UPDATED R Task associated data - 002 TASK ASSOCIATED DATA DELETED FOR APPLICABLE MSN D Subtask 921087-910-001-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R

Subtask 921087-839-001-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED R GENERAL TOPIC CONTENT DELETED FOR APPLICABLE MSN D Subtask 921087-941-001-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED NOTE UPDATED PANEL UPDATED R

PREPARATION TOPIC CONTENT DELETED FOR APPLICABLE MSN D Subtask 921087-220-001-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED FIGURE REFERENCE UPDATED PANEL UPDATED NOTE UPDATED REFERENCES UPDATED R

PROCEDURE TOPIC CONTENT DELETED FOR APPLICABLE MSN D TEST TOPIC CONTENT DELETED FOR APPLICABLE MSN D Subtask 921087-942-001-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED R CLOSE-UP TOPIC CONTENT DELETED FOR APPLICABLE MSN D TASK 921087- 833-801-001-Repair TASK SOLUTION UPDATED NOTE UPDATED CONFIGURATION UPDATED CAUTION UPDATED R

Task associated data - 001 CONFIGURATION UPDATED R Task associated data - 002 TASK ASSOCIATED DATA DELETED FOR APPLICABLE MSN D Subtask 921087-910-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED MATERIAL LIST UPDATED REFERENCED DOCUMENTATION UPDATED R

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 3 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 921087-839-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED R GENERAL TOPIC CONTENT DELETED FOR APPLICABLE MSN D Subtask 921087-941-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED REFERENCED DOCUMENTATION UPDATED NOTE UPDATED PANEL UPDATED R

Subtask 921087-010-001-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED FIGURE REFERENCE UPDATED R

PREPARATION TOPIC CONTENT DELETED FOR APPLICABLE MSN D Subtask 921087-320-001-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED LOCATION UPDATED ZONE UPDATED QUANTITY UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED NOTE UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

Subtask 921087-320-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED NOTE UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

Subtask 921087-320-003-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED NOTE UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

Subtask 921087-320-004-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED QUANTITY UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED NOTE UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED R

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 4 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
PROCEDURE TOPIC CONTENT DELETED FOR APPLICABLE MSN D Subtask 921087-941-003-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R

Subtask 921087-700-002-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED NOTE UPDATED R
TEST TOPIC CONTENT DELETED FOR APPLICABLE MSN D Subtask 921087-410-001-002 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED CONSUMABLE UPDATED REFERENCED DOCUMENTATION UPDATED MATERIAL LIST UPDATED REFERENCES UPDATED FIGURE REFERENCE UPDATED R

Subtask 921087-942-003-001 SUBTASK SOLUTION UPDATED CONFIGURATION UPDATED REFERENCED DOCUMENTATION UPDATED PANEL UPDATED REFERENCES UPDATED R

CLOSE-UP TOPIC CONTENT DELETED FOR APPLICABLE MSN D Fig. A-FFAAA FIGURE SOLUTION ADDED N Fig. A-FFAAA Sheet 01 SHEET ADDED N Fig. A-FBB FIGURE DELETED FOR APPLICABLE MSN D Fig. A-FBOAA FIGURE SOLUTION UPDATED CONFIGURATION UPDATED R Fig. A-FBOAB FIGURE SOLUTION DELETED FOR APPLICABLE MSN D Fig. A-FRAAA FIGURE SOLUTION ADDED N Fig. A-FRAAA Sheet 01 SHEET ADDED N Fig. A-FRAAA Sheet 02 SHEET ADDED N APPENDIX APPENDIX DELETED D FILING 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 add operators AZA, IBE and VLE.

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 5 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REVISION TRANSMITTAL SHEET REVISION SEQUENCE ORIGINAL: Mar 28/11 REVISION No. : 01 - May 17/11 REVISION No. : 02 - Nov 25/14

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 6 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. ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONICCOMMON INSTALLATION-GENERALLUGS INSPECTION ON 10VU SLEEVES **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES During an unscheduled maintenance operation which allowed the replacement of an after titanium panel in the cockpit, the 10VU rack was removed for access. Cracks have been detected on 10VU rack side on lugs 1, 3 and 4. The root cause of these findings is under investigation. This Service bulletin details the 10VU rack lugs detailed inspection and the associated repair in case of finding. Accomplishment of this Service Bulletin will limit the risk to have all lugs broken and will contribute to ensure the structural integrity of 10VU rack. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational disruptions.

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPA01 1 See SB Fittings, splice, shims Component COMPA02 1 See SB Fasteners EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

03X 15S 15T 26S 29S 31P 31V 32Q 35U 36R 38W 40S 41S 46U 47P 48P 52T 53Z 59Z 69X 73W 74T 80X 85T 86Z 87Q 90Q 91X 92Q 94W 95W 98W AAF AAR AAY ABL ABQ ABY ACA ACI AEE AFL AFR AGY AHY AIB AIC AIJ AJD ALK AMC AMU ANA ANR ANZ ARR ART ARU ASL ATR AUA AUH AVA AWC AWM AWW AXM AZA AZI B2V BAW BEL BER BGH BHP BIE BKP BQB BRS BSX BTN C9G CBJ CCA CEB CEF CES CIB CQH CQN CSA CSC CSN CSZ CTN CTV CYP D2F DAL DCS DKH DLH DNU DNV DQA DRK DTR EAA EDW EIN ETD ETJ EZD EZY F2I FFT FHY FIN FLI FPY FRN FTZ G2X G4I GAP GBB GCR GHT GLG GMI GMR GWI GZQ HAY HDA HFY HKE HKJ HRM HVN I2L I2T IBE IBS IND IRA IRC ISS IZG JAV JBU JSA JST KAC KFR KGL KHV KKK KMF KZR LAN LBT LFO LKE LLC LLM LLP LMJ LMU LWA LZB M2I MAU MEA MLD MLM MLR MMA MML MON MOV MRJ MSC MSR MXA MYX NAS NKS NLY NMA NVD NVR NWS OAW OHY ORF OZW PIA PIC PTI PTR QAF QTR R1T RBA RCT RFJ RJA RJD ROT RYW RZO SAA SAI SAS SBI SDM SFW SGG SHJ SHU SKU SLK SMX SND SNX SOL SVR SVW SWM SWR SYR TAE TAI TAM TAP TAR TBJ TBZ TCW TCX TGW THY TNA TVS TWJ TXP TYR UAL UEA UJX ULG USA VAR VIM VIV VJC VKG VLE VLG VOI VRD VRE VVC WGT WHT WOW WRC CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 2 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY
HARD NO SOFT NO OBRM NO MANPOWER Task 921087-832-801-001: Inspection TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Task 921087-833-801-001: Repair TOTAL MANHOURS 84.00 ELAPSED TIME (HOURS) 45.00 APPENDICES None

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 3 5

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

**CONF ALL



### A

B B



## A

C FWD VIEW LOOKING AFT AREA TO BE INSPECTED AND POSSIBLE CRACK



### C LUG 1 LUG 3 LUG 4

LUG 2

AREA TO BE INSPECTED AND POSSIBLE CRACK ON THE LH AND RH SIDE OF THE LUG 

## B

N_SB_921087_5_SAAA_01_01 Figure A-FSAAA - Sheet 01

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 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 ATA SYSTEM: 92 

### TITLE: ELECTRIC AND ELECTRONICCOMMON INSTALLATION-GENERALLUGS INSPECTION ON 10VU SLEEVES 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 only applicable to aircraft on which Mod. No. 35869P9460 (ELECTRIC AND ELECTRONIC COMMON INSTALLATION - REINFORCE MAIN INSTRUMENT PANEL STRUCTURE) is not embodied. (1) Models 318-111 318-112 319-111 319-112 319-113 319-114 319-115 319-131 319-132 319-133 320-211 320-212 320-214 320-216 320-231 320-232 320-233 321-111 321-112 321-131 321-211 321-212 321-213 321-231 321-232 (2) Effectivity by MSN 0029 0045-0047 0049-0057 0059 0064-0078 0080-0088 0090 0093-0096 0099 0104 0110-0119 0121-0127 0135 0137-0138 0140-0142 0147-0150 0152-0154 0157-0162 0164-0169 0171-0176 0178 0181-0183 0185 0189-0190 0192 0194-0195 0197-0203 0205-0214 0216-0220 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 0350-0351 0353-0362 0364 0366-0368 0370-0373 0375-0376 0378 0380-0383 0385-0388 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 DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

0633-0707 0709 0711-0752 0754-0771 0773-0788 0790-0955 0957-1043 1045-1097 1099-1112 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 1993-2016 2018-2024 2026-2050 2052-2110 2112-2217 2219-2275 2277-2423 2425-2499 2501-2721 2723-2998 (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 14942910 26S 0368 0424 29S 0291 0292 31P 0229 31V 0164 0293 0332 0420 0436 0605 0932 0943 1048 32Q 1283 35U 0088 0199 0240 0241 0264 36R 1305 38W 1194 40S 1973 41S 0630 46U 2906 2952 2982 47P 0619 48P 2192 52T 1599 53Z 1468 59Z 1556 69X 0219 0449 0588 1998 73W 0087 74T 2165 80X 2748 85T 0190 0234 86Z 0406 87Q 0052 90Q 0594 91X 2837 92Q 0279 0395 94W 1818 95W 2949 98W 0441 AAF 0639 18462870
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 2 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN AAR 0802 1174 1356 1511 2041 2110 222622472290 23972459 2840 AAY 1229 1255 1262 1288 1292 1318 134722242319 2387 ABL 1227 1636 1670 1734 1970 2045 28082943 ABQ 1467 ABY 2764 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 1719 1726 1742 1748 1772 1783 1811 1853 1864 1874 1940 2018 2145 ACI 2152 AEE 2468 2828 AFL 2052 2069 2072 2091 21062116 2133 21442233 2330 2337 2342 2875 2903 2912 2920 294729572965 AFR 0115 0214 0237 0239 0285 0287 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 AGY 0322 0351 AHY 0331 24872516 2588 26852788 28462853 2865 2991 AIB 0138 AIC 0045 0046 0047 0049 0050 0051 0056 0057 0074 0075 0080 0090 0095 0096 0396 0398 0416 0423 0431 0432 0451 0469 0486 0490 0492 0499 2593 26242629 2907 AIJ 0169 0707 1132 1162 1179 1244 1259 1308 1322 1747 1780 2048 2227 2539 AJD 0879 1422 ALK 2345 25642584 AMC 2113 2122 2189 2291 2332 2382 26652768 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 0671 0726 ANZ 2085 2090 2112 2130 21482153 2173 225722972445 2533 2594 2663 ARR 0913 ART 0142 0244 0311 0333 0359 0426 0533 0662 0936 1873 ARU 0573 0582 ASL 1140 1159 22772296 233525872621 2645 ATR 0314 0393

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 3 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN AUA 0552 0570 0581 0768 0776 0797 0920 0935 1137 1150 1189 1387 1458 1478 1504 1553 1678 1735 1931 19372009 2131 2174 2262 2416 249425472652 AUH 2403 AVA 1612 16342066 2328 2333 2358 2367237723942523 2544 2552 2575 2662 AWC 2791 AWM 0765 AWW 0557 05972273 AXM 2425 2612 2633 2656 2683 2699 2760 2816 2842 2881 2885 2926 2944 2989 AZA 0434 0477 0488 0494 0495 0513 0514 0515 0516 0524 0526 0532 0576 0583 0586 0593 0599 0819 0848 0940 0951 0959 1138 1168 1217 1220 1448 1457 1473 1480 1489 1722 1740 1745 1770 1779 2033 205720742083 20862101 21272869 2932 AZI 0527 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 1482 1509 1510 1513 1529 1537 1558 1574 1590 1594 1604 1606 1661 1665 1687 1689 1690 1696 1708 1711 1754 1760 1782 1814 1829 1834 1871 1883 1892 1899 1902 1907 1910 1958 19872038 2040 20982188 2190 21942305 2320 2323 2324 2351 2363 2389 2429 2441 2466 25362653 269426972720 2799 2981 BEL 0644 1086 1102 1160 1336 1388 1441 1493 1797 1838 1885 1963 2196 2230 2392 2400 2700 2763 2810 2925 BER 1629 1717 1769 1775 1961 1966 1988 19942003 2005 2619 BGH 1087 28442863 BHP 2968 BIE 0519 0827 0891 BKP 2254 2310 2366 24172509 2531 2600 26342648 2660 2664 2783 2874 BQB 1703 BRS 2263 BSX 0648 0650 BTN 1541 1551 C9G 2128 CBJ 2557 2561 2611 26442733 2849 2891 2985 CCA 0876 0921 1296 2000 20072015 2172 2202 2205 22372269 2285 2293 229824542499 25082525 2532 2545 2551 2559 2614 2643 2805 2819 2839 28472890 CEB 2556 25862625 2638 27862790 2821 2831 2852 2876 2994 CEF 2801

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 4 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN 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 1542 1601 1603 1639 1906 1911 1964 1981 2022 20342036 2049 2056 2068 2219 2221 2235 2239 22442309 2315 24372451 24782493 2498 2543 2549 2562 2591 260626272693 27572825 2882 2895 CIB 0774 0809 0884 0894 0905 0957 0971 1381 1402 1416 1437 1607 1968 CQH 0978 1686 1852 1920 2939 CQN 0696 0698 0704 0705 CSA 2719 27582789 CSC 0540 0550 0551 0556 0591 0878 0902 0915 0919 1007 1013 2313 2348 23962431 2510 253425972639 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 23542361 2371 2408 2426 2435 2484 2505 25062511 2519 2521 2530 2541 2546 25542555 2558 2574 2579 263726672680 2689 2701 27082713 27142741 2743 2759 2767 2770 2772 2796 2809 2815 282428342855 2861 2877 2899 2901 29152936 2940 29482950 2960 2969 2971 2986 CSZ 2672 26842841 2905 2909 2935 2973 2980 CTN 0767 0833 1009 1029 1237 1252 CTV 0839 0892 1635 2598 2692 CYP 0256 21082275 23342343 2359 D2F 1439 1450 2496 2502 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 DLH 0069 0070 0071 0072 0078 0083 0086 0093 0094 0104 0110 0111 0116 0137 0161 0172 0201 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 DNU 0444 DNV 1630 1805 1808 1841 2093 2179 2241 2751 DQA 2347 DRK 2306 2346 DTR 0113 0114 DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 5 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN EAA 0386 EDW 0942 0947 1026 20242134 EIN 0926 1023 1094 1242 1394 1443 1983 2001 2191 2206 2217 2250 2256 2272 2294236423742399 2409 2411 2432 2486 2542 2583 2635 ETD 0350 1944 1945 1947 19552167 ETJ 0295 0325 0373 0428 0445 EZD 0667 0743 0872 0874 1074 1286 21372141 21472576 2826 2956 EZY 2037 2043 2050 2053 2062 2120 2170 2181 21842245 2265 2271 2289 2300 2353 2360 2370 2385 23982402 2412 2420 2427 2450 2463 2471 24772481 2492 2495 2503 2512 251425272528 2538 2565 25782605 2636 264626772681 2691 2702 2709 2715 2727 2729 27352742 274427542765 2769 27772779 2782 2795 2803 2812 281828272829 28542860 28662873 28842923 2946 2959 F2I 0085 0148 0168 0203 0220 0230 0243 0249 0251 0270 0294 0301 0391 0422 0460 0497 0724 0758 0976 0999 1010 FFT 1515 1579 1583 1615 1684 1759 1781 1786 1803 1806 1860 1943 1980 19972010 2012 2019 2030 2103 2198 2209 2236 2240 2253 2258 2260 22872318 23252406 24482483 2518 2695 2806 2836 2857 FHY 0580 0771 0855 25242804 FIN 0941 0961 1073 1107 1184 1185 1241 1309 1352 1364 1405 1470 1544 1588 1712 1913 1916 1978 1989 2065 21242146 2154 2208 2266 FLI 2186 FPY 0112 0189 0342 FRN 0647 0660 FTZ 1068 11452176 2268 2281 G2X 0347 0653 0674 G4I 1157 17952507 GAP 0706 07452162 2183 GBB 0067 0076 GCR 2338 2475 GHT 0438 GLG 1866 1872 1882 1925 20782126 GMI 0684 0970 0995 GMR 1407 GWI 0117 0135 0147 0162 0200 0202 0209 0216 0217 0218 0267 0268 0382 0401 0646 0654 0794 1077 1084 1089 1136 1147 1155 1170 1209 127726072628 2632 2813 2833 2976 GZQ 1878 HAY 0714 0716 0730 0888 HDA 0633 0756 0784 0812 0930 0993 1024 1253 1695 1721 1984 2021 2229 22382428 HFY 1004 HKE 2299 2322 2717 HKJ 2706
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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN HRM 0517 0535 0642 0666 HVN 2255 2261 22672974 I2L 0371 0491 0579 0760 0816 I2T 1631 1682 IBE 0158 0173 0176 0207 0224 0266 0274 0323 0356 1021 1027 1154 1362 1530 1572 1655 1674 1681 1716 1793 1809 1836 2115 2220 2225 2242 22642270 2311 235723652381 2391 2472 2488 2563 2599 27362756 2996 IBS 1047 1059 1067 1099 1101 1119 1125 1198 1516 21042143 2248 2807 IND 0343 0357 IRA 0303 0312 0345 0575 08572054 IRC 0354 0414 ISS 0737 0749 1823 1896 2102 IZG 0376 0400 0407 JAV 0029 2061 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 19482006 2020 2031 2042 2063 2075 2099 2125 2132 21362149 2150 2159 2160 21772201 2215 2231 22462259 2280 22842286 230723142336 2352 2368 2384 2386 241524472449 2461 2489 2491 25042520 2535 2577 2580 2640 26472671 2710 27252755 2781 2802 28142832 2848 2871 2880 2900 2945 2970 29772992 JSA 2316 23562423 2453 2604 JST 1195 14082169 2185 21972292 2329 2455 2515 2526 2537 2573 2608 2642 2651 2703 27662787 KAC 0181 0182 0195 2046 KFR 2650 KGL 0663 0668 0787 0852 0954 1060 1293 15542029 2077 KHV 2303 2480 KKK 0604 0614 0675 0761 0808 0823 0968 0974 1124 1390 1438 1451 1503 1624 1730 1950 1953 27472753 KMF 0480 KZR 1042 1204 LAN 1304 1332 1351 1355 1491 1512 1526 1548 1568 1854 1858 1877 1903 2089 2096 2295 23042321 2572 2585 2845 2858 2864 2872 2886 28872892 2894 LBT 0793 0937 1121 1175 1597 17442158 LFO 0659 LKE 2581 26172746 LLC 0415 0990 1715 2987 LLM 1054 1918 1956 1967 1969 1993 2413 2419 2439 LLP 0739 0883 0914 1411 1723 2016 LMJ 1868 LMU 0977 1366 LWA 2878 2954
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 7 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN LZB 2540 2596 M2I 2118 MAU 1592 1936 MEA 1977 2055 MLD 0622 0741 MLM 2592 MLR 1946 2731 MMA 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 2142 2234 2553 2610 2730 2793 MOV 2442 2446 MRJ 0530 1202 1300 1353 MSC 2094 29372966 MSR 0165 0166 0178 0194 0198 0366 0680 0687 0715 0725 2070 2073 2079 2088 MXA 0252 0259 0260 0261 0275 0276 0296 0320 0321 0353 MYX 0566 NAS 1942 19652123 2171 2182 2199 2569 2776 NKS 2433 2470 2473 2476 24852490 2560 25672590 2603 2622 2673 2679 269827042711 2723 27972893 2898 2929 2942 2963 2978 2983 NLY 2529 26682749 28672902 NMA 1697 1732 2676 NVD 0211 0299 0375 0409 0419 0528 0558 0561 0709 0747 1626 1778 NVR 2211 22162410 NWS 1219 1233 1276 1843 2649 29272933 OAW 1886 OHY 0364 0385 0455 0471 0496 0543 0640 0661 0676 0792 0806 0810 0811 0835 0912 0916 0963 1008 2571 2688 ORF 2566 OZW 0429 1922 PIA 2155 2212 2274 PIC 2331 2340 2670 2922 PTI 1263 PTR 0459 0537 QAF 0927 1335 QTR 1487 1566 1648 1656 1773 1895 1928 1957209721072121 2138 2161 22882341 R1T 1908 RBA 2023 2032 2135 2139 2195 RCT 0466 1017 RFJ 0814 RJA 2953 RJD 1618
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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN ROT 2931 2955 RYW 0569 RZO 0795 2011 2390 SAA 2308 23262355 2375 2379 2418 24382469 2501 SAI 0542 0877 14972027 SAS 1183 1383 1587 1619 1642 1675 1798 1807 1817 1848 2817 2850 2856 2883 2888 2911 29582990 SBI 1071 1078 1090 1091 1126 1129 1131 1149 1164 1167 1819 1870 2028 20642076 2279 2369 2373 246424742618 2623 2641 2726 SDM 0427 0525 0649 1130 1200 1379 1488 1560 1578 1654 1657 1679 1743 1753 1761 1767 1851 1863 1876 1890 2151 2163 2465 2497 2879 2913 2930 2964 SFW 0734 0994 1018 SGG 0799 SHJ 0910 SHU 2222 2243 SKU 0447 1400 1523 2119 2129 22142249 2251 2283 2378 2380 2436 2460 2548 SLK 0899 0969 1228 1561 16982058 2252 25172568 2775 SMX 2995 SND 1880 1999 SNX 0289 SOL 0302 SVR 0140 0157 0735 0775 0815 0841 0991 1012 1063 1152 1199 1484 1720 1751 1777 1884 1901 1905 21172166 2175 21872278 2327 2349 27072998 SVW 2921 SWM 0421 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 SYR 0886 0918 1032 1076 1085 1117 TAE 0657 0934 0946 0949 1339 1368 1500 193420842659 TAI 1066 1334 1598 1625 1952 2282 2301 2339 243424442687 2862 2917 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 1771 1801 1802 1804 1825 1826 1827 1831 1832 1835 1837 1855 1857 1888 1891 2014 2044 2372 2393 2467 2513 2661 2734 2737 27842838 2859 2896 2904 2924 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 1668 1713 1718 1756 1765 1799 1816 2178 2792 2822 TAR 0119 0123 0124 0205 0370 0390 0402 0511 0869 0880 0958 0975 1187 1479 1700 TBJ 1485 TBZ 0361 0362 0405 DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 9 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN TCW 1787 1929 1975 21142362 TCX 0677 1006 1238 1250 2060 TGW 2724 2728 THY 1002 1727 1856 1909 19962156 21642395 2401 24042414 2452 2522 2602 2609 2626 2631 2655 27382739 2823 2868 2916 2919 2928 29342941 2984 TNA 0606 0731 0746 0791 0822 2376 2914 TVS 2180 TWJ 2550 TXP 0607 0611 0617 TYR 1385 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 26962762 27742820 2835 UJX 0733 1213 ULG 0308 USA 0053 0054 0055 0064 0065 0066 0077 0081 0082 0099 0317 0448 0538 0555 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 19352193 2302 2312 2405 2422 2430 2458 2482 2570 2595 2613 26152630 2669 2690 VAR 2383 2718 VIM 2732 VIV 2157 2210 2443 2752 2908 VJC 2712 2745 VKG 1881 1887 1889 1921 1932 1954 1960 1972 VLE 1226 DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 10 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

OPERATOR MSN VLG 0992 1171 1208 1210 1221 1349 1372 1396 1430 1461 1540 1550 1694 1736 1749 1862 1914 1933 1979 2168 22072223 2388 2407 2479 2589 2620 2658 26782761 278527942798 2843 2889 2897 2962 2988 VOI 2204 26572666 2771 2780 2979 2997 VRD 2616 26742740 2773 27782800 2811 2830 2851 2993 VRE 1429 2213 2228 VVC 1306 1454 1564 1725 1757 1867 WGT 1212 WHT 0548 12562440 2675 WOW 2457 WRC 0235 0645 0781 1869 2462 2682

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 11 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (4) Configuration by MSN MSN CONFIGURATION 0029 0045 0046 0047 0049 0050 0051 0052 0053 0054 0055 0056 0057 0059 0064 0065 0066 0067 0068 0069 0070 0071 0072 0073 0074 0075 0076 0077 0078 0080 0081 0082 0083 0084 0085 0086 0087 0088 0090 0093 0094 0095 0096 0099 0104 0110 0111 0112 0113 0114 0115 0116 0117 0118 0119 0121 0122 0123 0124 0125 0126 0127 0135 0137 0138 0140 0141 0142 0147 0148 0149 0150 0152 0153 0154 0157 0158 0159 0160 0161 0162 0164 0165 0166 0167 0168 0169 0171 0172 0173 0174 0175 0176 0178 0181 0182 0183 0185 0189 0190 0192 0194 0195 0197 0198 0199 0200 0201 0202 0203 0205 0206 0207 0208 0209 0210 0211 0212 0213 0214 0216 0217 0218 0219 0220 0224 0229 0230 0231 0232 0233 0234 0235 0237 0239 0240 0241 0242 0243 0244 0248 0249 0251 0252 0253 0254 0255 0256 0259 0260 0261 0262 0263 0264 0265 0266 0267 0268 0269 0270 0272 0273 0274 0275 0276 0277 0279 0281 0282 0284 0285 0287 0289 0290 0291 0292 0293 0294 0295 0296 0297 0298 0299 0300 0301 0302 0303 0306 0307 0308 0309 0311 0312 0314 0316 0317 0318 0319 0320 0321 0322 0323 0324 0325 0328 0329 0330 0331 0332 0333 0339 0340 0341 0342 0343 0345 0346 0347 0350 0351 0353 0354 0355 0356 0357 0358 0359 0360 0361 0362 0364 0366 0367 0368 0370 0371 0372 0373 0375 0376 0378 0380 0381 0382 0383 0385 0386 0387 0388 0390 0391 0393 0395 0396 0398 0399 0400 0401 0402 0403 0404 0405 0406 0407 0408 0409 0410 0412 0413 0414 0415 0416 0417 0418 0419 0420 0421 0422 0423 0424 0426 0427 0428 0429 0430 0431 0432 0434 0435 0436 0438 0439 0441 0442 0444 0445 0447 0448 0449 0450 0451 0452 0454 0455 0456 0457 0458 0459 0460 0462 0463 0464 0465 0466 0468 0469 0470 0471 0472 0473 0474 0475 0476 0477 0479 0480 0482 0483 0484 0485 0486 0487 0488 0489 0490 0491 0492 0493 0494 0495 0496 0497 0498 0499 0500 0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511 0512 0513 0514 0515 0516 0517 0518 0519 0520 0521 0522 0523 0524 0525 0526 0527 0528 0529 0530 0531 0532 0533 0534 0535 0537 0538 0539 0540 0541 0542 0543 0544 0545 0546 0548 0549 0550 0551 0552 0553 0554 0555 0556 0557 0558 0559 0560 0561 0562 0563 0564 0565 0566 0567 0568 0569 0570 0571 0572 0573 0574 0575 0576 0577 0578 0579 0580 0581 0582 0583 0584 0585 0586 0587 0588 0589 0591 0592 0593 0594 0595 0596 0597 0598 0599 0600 0603 0604 0605 0606 0607 0608 0609 0610 0611 0612 0613 0614 0616 0617 0618 0619 0620 0621 0622 0623 0625 0627 0629 0630 0631 0633 0634 0635 0636 0637 0638 0639 0640 0641 0642 0643 0644 0645 0646 0647 0648 0649 0650 0651 0652 0653 0654 0655 0656 0657 0658 0659 0660 0661 0662 0663 0664 0665 0666 0667 0668 0669 0670 0671 0672 0673 0674 0675 0676 0677 0678 0679 0680 0681 0682 0683 0684 0685 0686 0687 0688 0689 0690 0691 0692 0693 0694 0695 0696 0697 0698 0699 0700 0701 0702 0703 0704 001

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 12 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 0705 0706 0707 0709 0711 0712 0713 0714 0715 0716 0717 0718 0719 0720 0721 0722 0723 0724 0725 0726 0727 0728 0729 0730 0731 0732 0733 0734 0735 0736 0737 0738 0739 0740 0741 0742 0743 0744 0745 0746 0747 0748 0749 0750 0751 0752 0754 0755 0756 0757 0758 0759 0760 0761 0762 0763 0764 0765 0766 0767 0768 0769 0770 0771 0773 0774 0775 0776 0777 0778 0779 0780 0781 0782 0783 0784 0785 0786 0787 0788 0790 0791 0792 0793 0794 0795 0796 0797 0798 0799 0800 0801 0802 0803 0804 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830 0831 0832 0833 0834 0835 0836 0837 0838 0839 0840 0841 0842 0843 0844 0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0855 0856 0857 0858 0859 0860 0861 0862 0863 0864 0865 0866 0867 0868 0869 0870 0871 0872 0873 0874 0875 0876 0877 0878 0879 0880 0881 0882 0883 0884 0885 0886 0887 0888 0889 0890 0891 0892 0893 0894 0895 0896 0897 0898 0899 0900 0901 0902 0903 0904 0905 0906 0907 0908 0909 0910 0911 0912 0913 0914 0915 0916 0917 0918 0919 0920 0921 0922 0923 0924 0925 0926 0927 0928 0929 0930 0931 0932 0933 0934 0935 0936 0937 0938 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948 0949 0950 0951 0952 0953 0954 0955 0957 0958 0959 0960 0961 0962 0963 0964 0965 0966 0967 0968 0969 0970 0971 0972 0973 0974 0975 0976 0977 0978 0979 0980 0981 0982 0983 0984 0985 0986 0987 0988 0989 0990 0991 0992 0993 0994 0995 0996 0997 0998 0999 1000 1001 1002 1003 1004 1005 1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016 1017 1018 1019 1020 1021 1022 1023 1024 1025 1026 1027 1028 1029 1030 1031 1032 1033 1034 1035 1036 1037 1038 1039 1040 1041 1042 1043 1045 1046 1047 1048 1049 1050 1051 1052 1053 1054 1055 1056 1057 1058 1059 1060 1061 1062 1063 1064 1065 1066 1067 1068 1069 1070 1071 1072 1073 1074 1075 1076 1077 1078 1079 1080 1081 1082 1083 1084 1085 1086 1087 1088 1089 1090 1091 1092 1093 1094 1095 1096 1097 1099 1100 1101 1102 1103 1104 1105 1106 1107 1108 1109 1110 1111 1112 1114 1115 1116 1117 1118 1119 1120 1121 1122 1123 1124 1125 1126 1127 1128 1129 1130 1131 1132 1133 1134 1135 1136 1137 1138 1139 1140 1141 1142 1143 1144 1145 1146 1147 1148 1149 1150 1151 1152 1153 1154 1155 1156 1157 1158 1159 1160 1161 1162 1163 1164 1165 1166 1167 1168 1169 1170 1171 1172 1173 1174 1175 1176 1177 1178 1179 1180 1181 1182 1183 1184 1185 1187 1188 1189 1190 1191 1192 1193 1194 1195 1196 1197 1198 1199 1200 1201 1202 1203 1204 1205 1206 1207 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217 1219 1220 1221 1222 1223 1224 1225 1226 1227 1228 1229 1230 1231 1232 1233 1234 1235 1236 1237 1238 1239 1240 1241 1242 1243 1244 1245 1246 1247 1248 1249 1250 1251 1252 1253 1254 1255 1256 1257 1258 1259 1260 1261 1262 1263 1264 1265 1266 1267 1268 1269 1270 1271 1272 1273 1274 1275 1276 001

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 1277 1279 1280 1281 1282 1283 1284 1285 1286 1287 1288 1289 1290 1291 1292 1293 1294 1295 1296 1297 1298 1299 1300 1301 1302 1303 1304 1305 1306 1307 1308 1309 1310 1311 1312 1313 1314 1315 1316 1317 1318 1319 1320 1321 1322 1323 1324 1325 1326 1327 1328 1329 1330 1331 1332 1334 1335 1336 1337 1338 1339 1340 1341 1342 1343 1344 1345 1346 1347 1348 1349 1350 1351 1352 1353 1354 1355 1356 1357 1358 1359 1360 1361 1362 1363 1364 1365 1366 1367 1368 1369 1370 1371 1372 1373 1375 1376 1377 1378 1379 1380 1381 1382 1383 1384 1385 1386 1387 1388 1389 1390 1391 1392 1393 1394 1395 1396 1397 1398 1399 1400 1401 1402 1403 1404 1405 1406 1407 1408 1409 1410 1411 1412 1413 1414 1415 1416 1417 1418 1419 1420 1421 1422 1423 1424 1425 1426 1427 1428 1429 1430 1431 1432 1433 1434 1435 1436 1437 1438 1439 1440 1441 1442 1443 1444 1445 1446 1447 1448 1449 1450 1451 1452 1453 1454 1455 1456 1457 1458 1459 1460 1461 1462 1463 1465 1466 1467 1468 1469 1470 1471 1472 1473 1474 1475 1476 1477 1478 1479 1480 1481 1482 1483 1484 1485 1486 1487 1488 1489 1490 1491 1492 1493 1494 1495 1496 1497 1498 1499 1500 1501 1502 1503 1504 1505 1506 1507 1508 1509 1510 1511 1512 1513 1514 1515 1516 1517 1518 1519 1520 1521 1522 1523 1524 1525 1526 1527 1528 1529 1530 1531 1532 1533 1534 1535 1536 1537 1538 1539 1540 1541 1542 1543 1544 1545 1546 1547 1548 1549 1550 1551 1552 1553 1554 1555 1556 1557 1558 1559 1560 1561 1562 1563 1564 1565 1566 1567 1568 1569 1570 1571 1572 1573 1574 1575 1576 1577 1578 1579 1580 1581 1582 1583 1584 1585 1586 1587 1588 1589 1590 1591 1592 1593 1594 1595 1596 1597 1598 1599 1600 1601 1602 1603 1604 1605 1606 1607 1608 1609 1610 1611 1612 1613 1614 1615 1616 1617 1618 1619 1620 1621 1622 1623 1624 1625 1626 1627 1628 1629 1630 1631 1632 1633 1634 1635 1636 1637 1638 1639 1640 1641 1642 1643 1644 1645 1646 1647 1648 1649 1650 1651 1652 1653 1654 1655 1656 1657 1658 1659 1661 1662 1663 1664 1665 1666 1667 1668 1669 1670 1671 1672 1673 1674 1675 1677 1678 1679 1680 1681 1682 1683 1684 1685 1686 1687 1688 1689 1690 1691 1692 1693 1694 1695 1696 1697 1698 1699 1700 1701 1702 1703 1704 1705 1706 1707 1708 1709 1710 1711 1712 1713 1714 1715 1716 1717 1718 1719 1720 1721 1722 1723 1724 1725 1726 1727 1728 1730 1731 1732 1733 1734 1735 1736 1737 1738 1739 1740 1741 1742 1743 1744 1745 1746 1747 1748 1749 1750 1751 1752 1753 1754 1755 1756 1757 1758 1759 1760 1761 1762 1763 1764 1765 1766 1767 1769 1770 1771 1772 1773 1774 1775 1776 1777 1778 1779 1780 1781 1782 1783 1784 1785 1786 1787 1788 1789 1790 1791 1792 1793 1794 1795 1796 1797 1798 1799 1800 1801 1802 1803 1804 1805 1806 1807 1808 1809 1810 1811 1812 1814 1815 1816 1817 1818 1819 1820 1821 1823 1824 1825 1826 1827 1828 1829 1831 1832 1833 1834 1835 1836 1837 1838 1839 1840 1841 1842 1843 1844 1845 1846 1847 1848 001

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 14 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 1849 1850 1851 1852 1853 1854 1855 1856 1857 1858 1859 1860 1861 1862 1863 1864 1865 1866 1867 1868 1869 1870 1871 1872 1873 1874 1875 1876 1877 1878 1879 1880 1881 1882 1883 1884 1885 1886 1887 1888 1889 1890 1891 1892 1893 1894 1895 1896 1897 1898 1899 1900 1901 1902 1903 1904 1905 1906 1907 1908 1909 1910 1911 1912 1913 1914 1915 1916 1917 1918 1920 1921 1922 1923 1924 1925 1926 1927 1928 1929 1931 1932 1933 1934 1935 1936 1937 1938 1940 1941 1942 1943 1944 1945 1946 1947 1948 1949 1950 1951 1952 1953 1954 1955 1956 1957 1958 1959 1960 1961 1962 1963 1964 1965 1966 1967 1968 1969 1970 1971 1972 1973 1974 1975 1976 1977 1978 1979 1980 1981 1982 1983 1984 1986 1987 1988 1989 1990 1993 1994 1995 1996 1997 1998 1999 2000 2001 2002 2003 20042005 2006 20072008 2009 2010 2011 2012 2013 201420152016 2018 2019 2020 2021 2022 2023 20242026 202720282029 2030 2031 2032 2033 20342035 203620372038 2039 2040 2041 2042 2043 204420452046 20472048 2049 2050 2052 2053 20542055 2056 20572058 2059 2060 2061 2062 2063 2064 2065 2066 206720682069 2070 2071 2072 2073 20742075 2076 2077 2078 2079 2080 2081 2082 2083 20842085 2086 20872088 2089 2090 2091 2092 2093 209420952096 2097 2098 2099 2100 2101 2102 2103 21042105 210621072108 2109 2110 2112 2113 211421152116 211721182119 2120 2121 2122 2123 21242125 212621272128 2129 2130 2131 2132 2133 213421352136 21372138 2139 2140 2141 2142 2143 2144 2145 2146214721482149 2150 2151 2152 2153 21542155 2156 21572158 2159 2160 2161 2162 2163 2164 2165 2166 216721682169 2170 2171 2172 2173 21742175 2176 2177 2178 2179 2180 2181 2182 2183 21842185 2186 21872188 2189 2190 2191 2192 2193 219421952196 2197 2198 2199 2200 2201 2202 2203 22042205 220622072208 2209 2210 2211 2212 2213 22142215 2216 22172219 2220 2221 2222 2223 22242225 222622272228 2229 2230 2231 2232 2233 223422352236 22372238 2239 2240 2241 2242 2243 2244 2245 2246224722482249 2250 2251 2252 2253 22542255 2256 22572258 2259 2260 2261 2262 2263 2264 2265 2266 226722682269 2270 2271 2272 2273 22742275 22772278 2279 2280 2281 2282 2283 228422852286 2287 2288 2289 2290 2291 2292 2293 22942295 229622972298 2299 2300 2301 2302 2303 23042305 2306 23072308 2309 2310 2311 2312 2313 231423152316 231723182319 2320 2321 2322 2323 23242325 232623272328 2329 2330 2331 2332 2333 233423352336 23372338 2339 2340 2341 2342 2343 2344 2345 2346234723482349 2350 2351 2352 2353 23542355 2356 23572358 2359 2360 2361 2362 2363 2364 2365 2366 236723682369 2370 2371 2372 2373 23742375 2376 2377 2378 2379 2380 2381 2382 2383 23842385 2386 23872388 2389 2390 2391 2392 2393 239423952396 2397 2398 2399 2400 2401 2402 2403 24042405 240624072408 2409 2410 2411 2412 2413 24142415 2416 24172418 2419 2420 2421 001

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 15 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 2422 2423 2425 242624272428 2429 2430 2431 2432 2433 243424352436 24372438 2439 2440 2441 2442 2443 2444 2445 2446244724482449 2450 2451 2452 2453 24542455 2456 24572458 2459 2460 2461 2462 2463 2464 2465 2466 246724682469 2470 2471 2472 2473 24742475 2476 2477 2478 2479 2480 2481 2482 2483 24842485 2486 24872488 2489 2490 2491 2492 2493 249424952496 2497 2498 2499 2501 2502 2503 25042505 2506 25072508 2509 2510 2511 2512 2513 251425152516 251725182519 2520 2521 2522 2523 25242525 252625272528 2529 2530 2531 2532 2533 253425352536 25372538 2539 2540 2541 2542 2543 2544 2545 2546254725482549 2550 2551 2552 2553 25542555 2556 25572558 2559 2560 2561 2562 2563 2564 2565 2566 256725682569 2570 2571 2572 2573 25742575 2576 2577 2578 2579 2580 2581 2582 2583 25842585 2586 25872588 2589 2590 2591 2592 2593 259425952596 2597 2598 2599 2600 2601 2602 2603 26042605 260626072608 2609 2610 2611 2612 2613 26142615 2616 26172618 2619 2620 2621 2622 2623 262426252626 262726282629 2630 2631 2632 2633 26342635 263626372638 2639 2640 2641 2642 2643 264426452646 26472648 2649 2650 2651 2652 2653 2654 2655 2656265726582659 2660 2661 2662 2663 26642665 2666 26672668 2669 2670 2671 2672 2673 2674 2675 2676 267726782679 2680 2681 2682 2683 26842685 2686 2687 2688 2689 2690 2691 2692 2693 26942695 2696 26972698 2699 2700 2701 2702 2703 270427052706 2707 2708 2709 2710 2711 2712 2713 27142715 271627172718 2719 2720 2721 2723 272427252726 272727282729 2730 2731 2732 2733 27342735 273627372738 2739 2740 2741 2742 2743 274427452746 27472748 2749 2750 2751 2752 2753 2754 2755 2756275727582759 2760 2761 2762 2763 27642765 2766 27672768 2769 2770 2771 2772 2773 2774 2775 2776 277727782779 2780 2781 2782 2783 27842785 2786 2787 2788 2789 2790 2791 2792 2793 27942795 2796 27972798 2799 2800 2801 2802 2803 280428052806 2807 2808 2809 2810 2811 2812 2813 28142815 281628172818 2819 2820 2821 2822 2823 28242825 2826 28272828 2829 2830 2831 2832 2833 283428352836 283728382839 2840 2841 2842 2843 28442845 284628472848 2849 2850 2851 2852 2853 285428552856 28572858 2859 2860 2861 2862 2863 2864 2865 2866286728682869 2870 2871 2872 2873 28742875 2876 28772878 2879 2880 2881 2882 2883 2884 2885 2886 288728882889 2890 2891 2892 2893 28942895 2896 2897 2898 2899 2900 2901 2902 2903 29042905 2906 29072908 2909 2910 2911 2912 2913 291429152916 2917 2918 2919 2920 2921 2922 2923 29242925 292629272928 2929 2930 2931 2932 2933 29342935 2936 29372938 2939 2940 2941 2942 2943 294429452946 294729482949 2950 2951 2952 2953 29542955 295629572958 2959 2960 2961 2962 2963 296429652966 29672968 2969 2970 2971 2972 2973 2974 2975 2976297729782979 2980 2981 2982 2983 29842985 001

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 16 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

MSN CONFIGURATION 2986 29872988 2989 2990 2991 2992 2993 2994 2995 2996 29972998 001 (5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Component COMPA01 1 Component COMPA02 1 Consumable CMLA01 As required B. CONCURRENT REQUIREMENTS None C. REASON (1) History During an unscheduled maintenance operation which allowed the replacement of an after titanium panel in the cockpit, the 10VU rack was removed for access. Cracks have been detected on 10VU rack side on lugs 1, 3 and 4. The root cause of these findings is under investigation. (2) Objective/Action This Service bulletin details the 10VU rack lugs detailed inspection and the associated repair in case of finding. (3) Advantages Accomplishment of this Service Bulletin will limit the risk to have all lugs broken and will contribute to ensure the structural integrity of 10VU rack. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 921087-832-801-001: Inspection (1) Do a detailed inspection of the lugs of the 10VU rack. DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 17 5

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# @A318/A319/A320/A321 SERVICE BULLETIN Task 921087-833-801-001: Repair (1) Depending on the result of the inspection, do the repair of the lug 1 of the 10VU rack. (2) Depending on the result of the inspection, do the repair of the lug 2 of the 10VU rack. (3) Depending on the result of the inspection, do the repair of the lug 3 of the 10VU rack. (4) Depending on the result of the inspection, do the repair of the lug 4 of the 10VU rack. E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. (2) Accomplishment Timescale This Service Bulletin has been classified Recommended. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to change this classification to Mandatory. It is anticipated that the AD will confirm the thresholds and/or intervals given but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1, Config. 001 - Do a Detailed Inspection of the Lugs 1, 2, 3 and 4 of the 10VU Rack Compliance time Condition Action Threshold (whichever occurs first) Grace Period (whichever occurs first) Repetitive interval (whichever occurs first)

All aircraft Do a detailed inspection of the lugs of the 10VU rack in accordance with TASK 921087-832-801-001 30000 FC or 60000 FH from Entry Into Service Next adequate maintenance check and not later than 24 months after this Service Bulletin receipt None

Report to Airbus Before next flight None None And No crack found on the lugs Repeat the detailed inspection of the 4 lugs in accordance TASK 921087-832-801-001 None None 20000 FC or 40000 FH

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 18 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Table 1, Config. 001 - Do a Detailed Inspection of the Lugs 1, 2, 3 and 4 of the 10VU Rack Compliance time Condition Action Threshold (whichever occurs first) Grace Period (whichever occurs first) Repetitive interval (whichever occurs first) Repair the damaged lug in accordance with TASK 921087-833-801-001 2 Years or 5000 FC or 10000 FH None None
And Report to Airbus Before next flight None None And one single damaged lug Repeat the detailed inspection of the 4 lugs in accordance TASK 921087-832-801-001 None None 20000 FC or 40000 FH Repair the damaged lugs in accordance with TASK 921087-833-801-001 Before next flight None None
And Report to Airbus Before next flight None None And Crack found on the lugs

Several damaged lugs Repeat the detailed inspection of the 4 lugs in accordance TASK 921087-832-801-001 None None 20000 FC or 40000 FH
F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 921087-832-801-001: Inspection Get Access 0.50 On Aircraft
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 19 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Task 921087-832-801-001: Inspection Do a detailed inspection of the lugs of the 10VU rack. 0.50 Close-Up 0.50 TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 Task 921087-833-801-001: Repair Get Access 24.00 On Bench Depending on the result of the inspection, do the repair of the lug 1 of the 10VU rack. 8.00 Depending on the result of the inspection, do the repair of the lug 2 of the 10VU rack. 7.00 Depending on the result of the inspection, do the repair of the lug 3 of the 10VU rack. 7.00 Depending on the result of the inspection, do the repair of the lug 4 of the 10VU rack. 8.00 Tests 6.00 Close-Up 24.00 TOTAL MANHOURS 84.00 ELAPSED TIME (HOURS) 45.00 NOTE: The minimum manhours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional manhours can apply. H. WEIGHT AND BALANCE The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator’s items. For the definition of (MEW) and operator’s items refer to the Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) 1-00-07. NOTE: for the installation of 1 fitting in replacement of the lug 1 or 4 : - Manufacturers Empty Weight +0.0475 KG (+0.1047 LB) - Effect on Balance +0.195 KGM (+1.410 LB.FT) NOTE: for the installation of 1 fitting in replacement of the lug 2 or 3 : - Manufacturers Empty Weight +0.0966 KG (+0.2129 LB) - Effect on Balance +0.396 KGM (+2.864 LB.FT) NOTE: Depending on the fitting installation you are going to do, the Manufacturers Empty Weight and the Effect on Balance correspond to the sum of the value of each new fittings. For the installation of the 4 fittings : DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 20 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Manufacturers Empty Weight +0.288 KG (+0.6349 LB) Effect on Balance +1.181 KGM (+8.542 LB.FT ) I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52 06-41-53 12-34-24 20-21-11 20-28-00 21-20-00 21-26-00 22-81-12 22-96-00 22-97-00 24-38-51 24-41-00 25-11-51 25-13-14 25-13-41 31-10-00 31-21-21 31-50-00 31-60-00 31-63-22 32-31-11 32-44-21 33-12-13 33-13-00 33-14-00 34-15-21 34-21-22 34-21-25 34-21-26 34-22-24 34-22-25 34-34-22 34-35-22 34-57-22 34-57-25 46-21-21 52-10-00 52-41-00 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 20-52-10 20-55-00 Non Destructive Test Manual (NTM) 51-10-08 51-90-00 Repair Instruction R92512003 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-00 51-24-00 51-42-00 51-43-00 51-44-00 51-47-00 51-70-20 51-75-12 Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) 1-00-07 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 21 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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# @A318/A319/A320/A321 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: Component COMPA01 AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 4012 For ordering by E-mail: ifd.spares@airbus.com AIRBUS Material, Logistics and Suppliers do not stock standard hardware as competitive multiple suppliers ensure access to minimum prices. AIRBUS recommends Customers with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to B/E Aerospace. The address is: Component COMPA02 B/E AEROSPACE INC CONSUMABLES MANAGEMENT 10000 NW 15TH Terrace Miami FL 33172 USA Tel EMEA: +49 (0) 40 822 285 31500 Tel US: +1 305 925 2600 Tel ASIA: +1 310 900 1300 Fax EMEA: +49 (0) 40 822 285 31010 Fax US: +1 305 507 7191 Fax ASIA: +1 310 819 1200 SITA: MIAMMCR E-Mail: AOGdesk_CMG@beaerospace.com internet: www.beconsumables.com or, alternatively any other source on the open market (2) Price and Availability

Component COMPA01 No Airbus kit will be provided. Operator supplied airbus part required to accomplish this Service Bulletin are to be purchased by a spares purchase order. Component COMPA02
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 23 5

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# @A318/A319/A320/A321 SERVICE BULLETIN No AIRBUS kit will be provided. Operator supplied standard hardware parts required to accomplish this Service Bulletin are to be supplied from the Operator’s stock. B. INDUSTRY SUPPORT INFORMATION AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials NOTE: To accomplish this Service Bulletin it is necessary to use the expendable parts listed in the subsequent referenced AMM tasks: - AMM Task 33-12-13-400-001 - AMM Task 33-12-13-400-002 Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTESSynthetic Ester Base GreaseGeneral Purpose Clay 03HBB1 As required Wash Primer - Structure 04CMA2 As required Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required Polysulfide Sealant - General Purpose Brushable 06AAA1 As required Non Aqueous Cleaner-General 08BAA9 As required (2) Components Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES R9251200420200 1 Fitting R9251200420300 1 Fitting R9251200520000 2 Fitting R9251200620000 2 Splice

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 24 5

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# @A318/A319/A320/A321 SERVICE BULLETIN Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 12 NAS1726-4E 6 Nut 13 NAS1726-5E 2 Nut HL10VF6-3 20 Bolt HL10VF6-4 54 Bolt HL10VF6-5 2 Bolt HL10VF6-6 6 Bolt HL70-6 82 Collar NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING (1) Tooling - Price and Availability None (2) Tools To accomplish this Service Bulletin it is necessary to use the tools listed in the subsequent referenced AMM tasks:
- AMM Task 32-31-11-400-001 - AMM Task 34-21-22-000-001 - AMM Task 34-21-25-000-001 - AMM Task 34-21-26-000-001 - AMM Task 34-22-24-000-001 - AMM Task 34-22-25-000-001 - AMM Task 52-10-00-010-001

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 25 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (3) Special Tools None

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 26 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 921087-832-801-001 - Inspection WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. NOTE: The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words "refer to" are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words "in accordance with" are used then the given procedure must be followed. 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: 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. 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.

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 27 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Task Associated Data Zone 210 Access Door 811 Manpower TOTAL MANHOURS 1.50 ELAPSED TIME (HOURS) 1.50 A. GENERAL (1) Subtask 921087-910-001-001 - Standard Practices Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 Consumable Material List (CML) (a) For the specification of the materials (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML). (b) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (2) Subtask 921087-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 921087-941-001-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills AIRFRAME

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 28 5

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References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 52-41-00-010-002 NOTE: The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic systems depressurized - Access to the cockpit and cabin is available - All circuit breakers are in closed position - All controls in NORM, AUTO or OFF position (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-869-002. (b) Put an access platform in position at door 811. (c) Open the avionics compartment door 811, refer toAMM Task 52-41-00-010-002. C. PROCEDURE (1) Subtask 921087-220-001-001 - Do a detailed inspection of the lugs of the 10VU rack. Work Zones and Access Panels Zone Access/Work location 210 Access Door 811 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

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# @A318/A319/A320/A321 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTESNon Aqueous CleanerGeneral 08BAA9 As required
References Fig. A-FFAAA Flow chart Sheet01 Fig. A-FBAAA Area to be inspected Sheet 01 Fig. A-FRAAA Inspection report Sheet01 Sheet02 (a) At the threshold given in the PLANNING INFORMATION paragraph E.(2): Do a detailed inspection of the 4 lugs of the 10VU Refer to Fig. A-FBAAA Refer to Fig. A-FFAAA NOTE: Clean the area to be inspected with: Non Aqueous Cleaner-General 08BAA9 As required

1 If no crack is found:
a Report to AIRBUS, refer to Fig. A-FRAAA

. And Repeat the detailed inspection of the 4 lugs at the interval given in the PLANNING INFORMATION paragraph E.(2) in accordance with TASK 921087-832-801 001 Inspection 2 If crack is found
a One single damaged lug: <1> Repair the damaged lug in accordance with TASK 921087-833-801 001 Repair at the threshold given in the PLANNING INFORMATION paragraph E.(2). And Report to Airbus, refer to Fig. A-FRAAA And
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 30 5

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# @A318/A319/A320/A321 SERVICE BULLETIN Repeat the detailed inspection of the 4 lugs at the interval given in the PLANNING INFORMATION paragraph E.(2) in accordance with TASK 921087-832-801 001 Inspection b Several damaged lugs: <1> Repair the damaged lugs in accordance with TASK 921087-833-801 001 Repair before next flight And Report to Airbus, refer to Fig. A-FRAAA And Repeat the detailed inspection of the 4 lugs at the interval given in the PLANNING INFORMATION paragraph E.(2) in accordance with TASK 921087-832-801 001 Inspection D. TEST None E. CLOSE-UP (1) Subtask 921087-942-001-001 - Close-up Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the avionics compartment door 811, refer toAMM Task 52-41-00-410-002. (c) Remove the access platform(s). (d) Put the aircraft back to its initial configuration.

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# @A318/A319/A320/A321 SERVICE BULLETIN Task 921087-833-801-001 - Repair 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 include procedures given in other documents or in other sections of the Service Bulletin. When the words "refer to" are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words "in accordance with" are used then the given procedure must be followed. 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. Task Associated Data Zone 210 Modified FIN 10VU 130VU 131VU 301VU 400VU 401VU 402VU 403VU 500VU

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# @A318/A319/A320/A321 SERVICE BULLETIN
Manpower TOTAL MANHOURS 84.00 ELAPSED TIME (HOURS) 45.00 A. GENERAL (1) Subtask 921087-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 06-31-53, Page Block 001 06-41-52, Page Block 001 06-41-53, Page Block 001 Task 20-21-11-911-001 20-28-00, Page Block 201 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-23-00 51-24-00 51-42-00 51-43-00 51-44-00 51-47-00 51-70-20 51-75-12 (a) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to Consumable Material List (CML). (b) Apply general repair requirements in accordance with SRM 51-70-20. (c) For the Frame (FR) identification, refer toAMM 06-31-53, Page Block 001. (d) For the identification of zones, refer toAMM 06-20-00, Page Block 001. (e) For the identification of access panels, refer toAMM 06-41-52, Page Block 001 and AMM 06-41-53, Page Block 001. (f) Tag the part that you must remove and retain to make the subsequent installation easier. (g) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (h) Put blanking caps on the disconnected electrical connectors. (i) Remove and install fasteners in accordance with SRM 51-42-00. (j) Apply fastener spacing and margin data in accordance with SRM 51-47-00. DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 34 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (k) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00. (l) Do the coating application in accordance with SRM 51-23-00. (m) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-001. (n) Do the repair of paint coating in accordance with SRM 51-75-12. (o) For the electrical bonding, refer to ESPM 20-51-20 and AMM 20-28-00, Page Block 201. (p) Obtain alternative and substitute fastener data in accordance with SRM 51-43-00. (2) Subtask 921087-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 921087-941-002-001 - Job Set-up Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002 Task 24-38-51-000-001 Task 52-41-00-010-002 NOTE: The items given in this note shall be considered as the basic Aircraft configuration before you start a maintenance task: - Aircraft on the ground resting on landing gear (the ground safety locks and the wheel chocks are in position on the landing gear) - Engine shut down, thrust reversers closed and locked - Aircraft in clean configuration - Parking brake applied - Aircraft electrical network de-energized - Hydraulic systems depressurized DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 35 5

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# @A318/A319/A320/A321 SERVICE BULLETIN - Access to the cockpit and cabin is available - All circuit breakers are in closed position - All controls in NORM, AUTO or OFF position (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-869-002. (b) Put an access platform in position at door 811. (c) Open the avionics compartment door 811, refer toAMM Task 52-41-00-010-002. (d) Make sure that the external connector(s) is(are) not connected to the aircraft receptacle(s) EXT PW. (e) Make sure that there is(are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (f) Make sure that the EMER EXIT LT push button switch on 25VU is on OFF position. (g) In the cockpit, on the overhead panel 35VU release BAT push button switches. (h) Put a warning notice on panel 35VU to tell persons not to operate the batteries. (i) Put a warning notice on refuel/defuel panel 800VU to tell persons not to operate the NORMAL BATTERY switch. (j) Put a warning notice in the cockpit to tell persons not to start the APU. (k) Put a warning notice in the cockpit to tell persons not to start the ENG 1, 2. (l) Battery disconnection 1 For job set up, refer to the removal of the batteries, refer to AMM Task 24-38-51-000-001. 2 Turn the knurled nut a quarter turn. 3 Disconnect the connectors. 4 Put blanking caps on the disconnected electrical connectors. (2) Subtask 921087-010-001-001 - Remove/open for access. Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills AIRFRAME

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) Task 21-20-00-010-001 Task 22-81-12-000-001 Task 25-11-51-000-001 Task 25-13-14-000-001 Task 25-13-14-000-004 Task 25-13-41-000-002 Task 31-21-21-000-001 Task 31-63-22-000-001 Task 32-31-11-000-001 Task 32-44-21-000-001 Task 33-12-13-000-001 Task 33-12-13-000-002 Task 34-15-21-000-001 Task 34-21-22-000-001 Task 34-21-25-000-001 Task 34-21-26-000-001 Task 34-22-24-000-001 Task 34-22-25-000-001 Task 34-34-22-000-001 Task 34-35-22-000-001 Task 34-57-22-000-001 Task 34-57-22-000-002 Task 34-57-25-000-001 Task 46-21-21-000-001 Structural Repair Manual (SRM) 51-42-00 Fig. A-FBCAA Removal/installation of the cover assies of the 10VU rack Sheet 01 Fig. A-FBDAA Removal/installation of the panel 130VU Sheet 01 Fig. A-FBEAA Removal/installation of the panel 131VU Sheet 01 Fig. A-FBGAA Removal/installation of the panel 500VU Sheet 01 Fig. A-FBHAA Removal/installation of the panel 301VU Sheet 01 Fig. A-FBIAA Removal/installation of the panel 402VU Sheet 01 Fig. A-FBJAA Removal/installation of the panel assies Sheet 01 Fig. A-FBKAA Removal/installation of the air conditioning system Sheet 01
Fig. A-FBLAA Removal/installation of the panel 401VU Sheet 01 Fig. A-FBMAA Removal/installation of the panel 403VU Sheet 01

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Fig. A-FBNAA Removal/installation of the panel 400VU Sheet 01 Fig. A-FBOAA Removal/installation of the 10VU rack Sheet 01 Sheet 02 Fig. A-FBPAA Removal/installation of the equipment 1FR Sheet 01

NOTE: Depending on aircraft configuration these parts or equipment can be installed or not. (a) Remove the captain and first officer seat (FINs 3MS and 4MS), refer to AMM Task 25-11-51-000-001. (b) Remove the panel (FIN 211LW), refer toAMM Task 25-13-41-000-002. (c) Remove the panels assies. Refer to Fig. A-FBJAA 1 Remove : 10 Screw Item (22) Retain 1 LH panel assy Item (90) Retain 1 LH panel assy Item (20) Retain 1 RH panel assy Item (21) Retain 1 RH panel assy Item (91) Retain (d) Remove the foot rests (captain and first officer), refer to AMM Task 25-13-14-000-001 or AMM Task 25-13-14-000-004. (e) Remove the panel assies. Refer to Fig. A-FBCAA 1 LH panel assy Item (24) Retain 1 Panel assy Item (25) Retain 1 RH panel assy Item (26) Retain (f) Remove the main instrument panel lights (FINs 36LE and 37LE), refer to AMM Task 33-12-13-000-001. (g) Remove the main instrument panel lights FIN 38LE, refer to AMM Task 33-12-13-000-002.
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 38 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (h) Remove the Paravisual Indicating (PVI) (FIN 1FW), refer to AMM Task 34-34-22-000-001. (i) Remove the Head-Up Display (HUD) Optical Head Unit (OHU) (FIN 3FH), refer to AMM Task 34-35-22-000-001. (j) Remove the Angle Of Attack (AOA) indicators (FINs 17FN1 and 17FN2), refer to AMM Task 34-15-21-000-001. (k) Remove the panel assy (FIN 131VU). Refer to Fig. A-FBEAA In accordance with SRM 51-42-00 1 Remove : 3 Screw Item (28) Retain 3 Washer Item (29) Retain FIN 131VU 1 Panel assy Item (30) Retain Depending on the aircraft configuration remove also : 2 Screw Item (27) Retain 2 Washer Item (29) Retain 2 Disconnect the connector 2111VCA from below of the panel assy (FIN 131VU). (l) Remove the panel assy (FIN 130VU). Refer to Fig. A-FBDAA In accordance with SRM 51-42-00 1 Remove : 3 Screw Item (28) Retain 3 Washer Item (29) Retain FIN 130VU 1 Panel assy Item (31) Retain Depending on the aircraft configuration remove also : 2 Screw Item (27) Retain

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# @A318/A319/A320/A321 SERVICE BULLETIN
2 Washer Item (29) Retain 2 Disconnect the connector 2112VCA from below of the panel assy (FIN 130VU). (m) Remove the panel assy (FIN 301VU). Refer to Fig. A-FBHAA In accordance with SRM 51-42-00 1 Remove : 4 Screw Item (32) Retain 4 Washer Item (33) Retain FIN 301VU 1 Panel assy Item (35) Retain 2 Disconnect the connectors 2101VCA and 2103VCA from the rear of the panel assy (FIN 301VU). (n) Remove the display units (FINs2WT1, 2WT2, 3WT1, 3WT2, 4WT1 and 4WT2), refer toAMM Task 31-63-22-000-001. (o) Remove the VOR/DME RMI (FIN 11FN), refer toAMM Task 34-57-22-000-001. (p) Remove the standby horizon indicator (FIN 7FN), refer to AMM Task 34-22-24-000-001. (q) Remove the standby altimeter (FIN 3FN), refer toAMM Task 34-21-22-000-001. (r) Remove the standby airspeed indicator (FIN 9FN), refer to AMM Task 34-21-26-000-001. (s) Remove the ADF RMI (FIN 13FN), refer toAMM Task 34-57-25-000-001. (t) Remove the metric altimeter (FIN 15FN), refer toAMM Task 34-21-25-000-001. (u) Remove the VOR/ADF/DME RMI (FIN 21FN), refer to AMM Task 34-57-22-000-002). (v) Remove the Integrated Stanby Instrument System (ISIS) indicator (FIN 22FN), refer toAMM Task 34-22-25-000-001. (w) Remove the panel assy (FIN 403VU). Refer to Fig. A-FBMAA In accordance with SRM 51-42-00

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# @A318/A319/A320/A321 SERVICE BULLETIN

1 Remove : 2 Screw Item (39) Retain 2 Washer Item (40) Retain FIN 403VU 1 Panel assy Item (41) Retain 2 Disconnect the connectors 2105VCA and 2109VCA from the rear of the panel assy (FIN 403VU). (x) Remove the Datalink Control and Display Unit (DCDU) (FINs 2TX1 and 2TX2), refer toAMM Task 46-21-21-000-001. (y) Remove the equipment (FIN 1FR). Refer to Fig. A-FBPAA 1 Remove : 1 Clamp Item (6) Retain FIN 1FR 1 Equipment Item (92) Retain (z) Remove the panel assy (FIN 401VU). Refer to Fig. A-FBLAA In accordance with SRM 51-42-00 1 Remove : 7 Screw Item (32) Retain 7 Washer Item (33) Retain FIN 401VU 1 Panel assy Item (42) Retain 2 Disconnect the connector 2TX1A from the rear of the panel assy (FIN 401VU) (if existing on aircraft). (aa) Remove the Flight Control Unit (FCU) (FIN 2CA), refer to AMM Task 22-81-12-000-001. (ab) Remove the panel assy (FIN 402VU). Refer to Fig. A-FBIAA In accordance with SRM 51-42-00
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# @A318/A319/A320/A321 SERVICE BULLETIN

1 Remove : 4 Screw Item (36) Retain 4 Washer Item (37) Retain FIN 402VU 1 Panel assy Item (38) Retain 2 Disconnect the connectors 2100VCA and 2102VCA from the rear of the panel assy (402VU). (ac) Remove the clock (FIN 2FS), refer toAMM Task 31-21-21-000-001. (ad) Remove the brake yellow pressure triple indicator (FIN 60GG), refer to AMM Task 32-44-21-000-001. (ae) Remove the landing gear normal control lever (FIN 6GA), refer to AMM Task 32-31-11-000-001. (af) Remove the panel assy (FIN 400VU). Refer to Fig. A-FBNAA In accordance with SRM 51-42-00 1 Remove : 7 Screw Item (32) Retain 7 Washer Item (33) Retain FIN 400VU 1 Panel assy Item (43) Retain 2 Disconnect the connector 2TX2A from the rear of the panel assy (FIN 400VU) (if existing on aircraft). (ag) Remove the panel assy (FIN 500VU). Refer to Fig. A-FBGAA In accordance with SRM 51-42-00 1 Remove : 4 Screw Item (32) Retain 4 Washer Item (33) Retain FIN 500VU 1 Panel assy Item (34) Retain
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2 Disconnect the connectors 2104VCA and 2108VCA from the rear of the panel assy (500VU). (ah) To permit the removal of the 10VU rack, disconnect the air conditioning hoses. Refer to Fig. A-FBKAA Refer to AMM Task 21-20-00-010-001 1 Remove : 4 clamp Item (5) Retain and disconnect the 4 hoses. (ai) Remove all the routing from the 10VU rack. 1 Before removing the routing from their 10VU rack, identify the position and the routing number for each clamp and fastener (by photos or placards). 2 Remove the routing from the 10VU rack to permit its removal and repair on bench. (aj) WARNING: BE CAREFUL DURING THE REMOVAL OF THE 10VU RACK. YOU CAN CAUSE DAMAGE TO EQUIPMENT OR INJURY TO PERSONS. Remove the 10VU rack. Refer to Fig. A-FBOAA In accordance with SRM 51-42-00 2 Screw Item (46) Retain 2 Washer Item (47) Retain 6 Nut Item (12) Discard 2 Nut Item (13) Discard 1 Axle Item (48) Retain 1 Axle Item (49) Retain 2 Axle Item (50) Retain 2 Axle Item (51) Retain 1 Axle Item (52) Retain DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 43 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
1 Axle Item (53) Retain FIN 10VU 1 Rack Item (54) Retain C. PROCEDURE (1) Subtask 921087-320-001-001 - Depending on the result of the inspection, do the repair of the lug 1 of the 10VU rack. Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Manhours 8.00 Minimum number of person 1 Subtask elapsed time 8.00 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES R9251200520000 1 Fitting R9251200620000 1 Splice Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES HL10VF6-4 20 Bolt HL10VF6-5 1 Bolt HL10VF6-6 3 Bolt HL70-6 24 Collar Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Wash Primer - Structure 04CMA2 As required Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001 20-28-00, Page Block 201
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 44 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Elec. Std. Practices Manual (ESPM) 20-51-20 Non Destructive Test Manual (NTM) 51-10-08 51-90-00 Repair Instruction R92512003 Structural Repair Manual (SRM) 51-23-00 51-24-00 51-42-00 51-43-00 51-44-00 51-47-00 51-70-20 51-75-12 Fig. A-FBAAA Area to be inspected Sheet 01 (a) On bench, do the repair of the lug 1 of the 10VU rack following the repair instruction. Refer to Repair Instruction R92512003 Refer to Fig. A-FBAAA(for location of the lugs) Refer to NTM 51-10-08 (for HFEC) Refer to NTM 51-90-00 (for DVI) Refer to AMM Task 20-21-11-911-001 and AMM 20-28-00, Page Block 201 Refer to ESPM 20-51-20 In accordance SRM 51-23-00, SRM 51-42-00, SRM 51-43-00, SRM 51-44-00, SRM 51-47-00, SRM 51-70-20 and SRM 51-75-12 1 Install : 1 Lateral fitting R9251200520000 1 Lateral splice R9251200620000 20 Bolt HL10VF6-4 1 Bolt HL10VF6-5 3 Bolt HL10VF6-6 24 Collar HL70-6 NOTE: On the cut out area and drilling parts only: Wash Primer - Structure 04CMA2 As required

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 45 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required

NOTE: Apply: Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
to interfaces of structure and new parts in accordance with SRM 51-24-00 NOTE: Apply on the fasteners (wet assembly): Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
(2) Subtask 921087-320-002-001 - Depending on the result of the inspection, do the repair of the lug 2 of the 10VU rack. Manpower Resources Manhours 7.00 Minimum number of person 1 Subtask elapsed time 7.00 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES R9251200420200 1 Fitting Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES HL10VF6-3 10 Bolt HL10VF6-4 7 Bolt HL70-6 17 Collar Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Wash Primer - Structure 04CMA2 As required Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required

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# @A318/A319/A320/A321 SERVICE BULLETIN

ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001 20-28-00, Page Block 201 Elec. Std. Practices Manual (ESPM) 20-51-20 Non Destructive Test Manual (NTM) 51-10-08 51-90-00 Repair Instruction R92512003 Structural Repair Manual (SRM) 51-23-00 51-24-00 51-42-00 51-43-00 51-44-00 51-47-00 51-70-20 51-75-12 Fig. A-FBAAA Area to be inspected Sheet 01 (a) On bench, do the repair of the lug 2 of the 10VU rack following the repair instruction. Refer to Repair Instruction R92512003 Refer to Fig. A-FBAAA(for location of the lugs) Refer to NTM 51-10-08 (for HFEC) Refer to NTM 51-90-00 (for DVI) Refer to AMM Task 20-21-11-911-001 and AMM 20-28-00, Page Block 201 Refer to ESPM 20-51-20 In accordance SRM 51-23-00, SRM 51-42-00, SRM 51-43-00, SRM 51-44-00, SRM 51-47-00, SRM 51-70-20 and SRM 51-75-12 1 Install : 1 LH central fitting R9251200420200 10 Bolt HL10VF6-3 7 Bolt HL10VF6-4 17 Collar HL70-6

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 47 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
NOTE: On the cut out area and drilling parts only: Wash Primer - Structure 04CMA2 As required
Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required

NOTE: Apply: Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
to interfaces of structure and new parts in accordance with SRM 51-24-00 NOTE: Apply on the fasteners (wet assembly): Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
(3) Subtask 921087-320-003-001 - Depending on the result of the inspection, do the repair of the lug 3 of the 10VU rack. Manpower Resources Manhours 7.00 Minimum number of person 1 Subtask elapsed time 7.00 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES R9251200420300 1 Fitting Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES HL10VF6-3 10 Bolt HL10VF6-4 7 Bolt HL70-6 17 Collar

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 48 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Wash Primer - Structure 04CMA2 As required Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001 20-28-00, Page Block 201 Elec. Std. Practices Manual (ESPM) 20-51-20 Non Destructive Test Manual (NTM) 51-10-08 51-90-00 Repair Instruction R92512003 Structural Repair Manual (SRM) 51-23-00 51-24-00 51-42-00 51-43-00 51-44-00 51-47-00 51-70-20 51-75-12 Fig. A-FBAAA Area to be inspected Sheet 01 (a) On bench, do the repair of the lug 3 of the 10VU rack following the repair instruction. Refer to Repair Instruction R92512003 Refer to Fig. A-FBAAA(for location of the lugs) Refer to NTM 51-10-08 (for HFEC) Refer to NTM 51-90-00 (for DVI) Refer to AMM Task 20-21-11-911-001 and AMM 20-28-00, Page Block 201 Refer to ESPM 20-51-20 In accordance SRM 51-23-00, SRM 51-42-00, SRM 51-43-00, SRM 51-44-00, SRM 51-47-00, SRM 51-70-20 and SRM 51-75-12 1 Install : 1 RH central fitting R9251200420300 10 Bolt HL10VF6-3
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 49 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

7 Bolt HL10VF6-4 17 Collar HL70-6 NOTE: On the cut out area and drilling parts only: Wash Primer - Structure 04CMA2 As required
Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required

NOTE: Apply: Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
to interfaces of structure and new parts in accordance with SRM 51-24-00 NOTE: Apply on the fasteners (wet assembly): Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
(4) Subtask 921087-320-004-001 - Depending on the result of the inspection, do the repair of the lug 4 of the 10VU rack. Manpower Resources Manhours 8.00 Minimum number of person 1 Subtask elapsed time 8.00 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES R9251200520000 1 Fitting R9251200620000 1 Splice Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES HL10VF6-4 20 Bolt HL10VF6-5 1 Bolt
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 50 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES HL10VF6-6 3 Bolt HL70-6 24 Collar Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Wash Primer - Structure 04CMA2 As required Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001 20-28-00, Page Block 201 Elec. Std. Practices Manual (ESPM) 20-51-20 Non Destructive Test Manual (NTM) 51-10-08 51-90-00 Repair Instruction R92512003 Structural Repair Manual (SRM) 51-23-00 51-24-00 51-42-00 51-43-00 51-44-00 51-47-00 51-70-20 51-75-12 Fig. A-FBAAA Area to be inspected Sheet 01 (a) On bench, do the repair of the lug 4 of the 10VU rack following the repair instruction. Refer to Repair Instruction R92512003 Refer to Fig. A-FBAAA(for location of the lugs) Refer to NTM 51-10-08 (for HFEC) Refer to NTM 51-90-00 (for DVI) Refer to AMM Task 20-21-11-911-001 and AMM 20-28-00, Page Block 201 Refer to ESPM 20-51-20 In accordance SRM 51-23-00, SRM 51-42-00, SRM 51-43-00, SRM 51-44-00, SRM 51-47-00, SRM 51-70-20 and SRM 51-75-12

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 51 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

1 Install : 1 Lateral fitting R9251200520000 1 Lateral splice R9251200620000 20 Bolt HL10VF6-4 1 Bolt HL10VF6-5 3 Bolt HL10VF6-6 24 Collar HL70-6 NOTE: On the cut out area and drilling parts only: Wash Primer - Structure 04CMA2 As required
Primer Polyurethane Paint - Corrosion Inhibiting 04EAC2 As required

NOTE: Apply: Polysulfide Sealant - General Purpose Brushable 06AAA1 As required
to interfaces of structure and new parts in accordance with SRM 51-24-00 NOTE: Apply on the fasteners (wet assembly): Polysulfide Sealant - General Purpose Brushable 06AAA1 As required

D. TEST (1) Subtask 921087-941-003-001 - Energize Electrical Network Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 24-38-51-400-001 Task 24-41-00-861-002 (a) Battery re-connection 1 For job set up, refer to the installation of the batteries (Refer to AMM Task 24-38-51-400-001). DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 52 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

2 Remove the blanking cap from the electrical connectors. 3 Make sure that the electrical connectors are clean and in correct condition. 4 Connect the connector on the battery. 5 turn the knurled nut a quarter turn. (b) Remove all the warning notices. (c) Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-002. (2) Subtask 921087-700-002-001 - Testing Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 21-20-00-410-001 Task 21-26-00-710-001 Task 22-96-00-710-001 Task 22-97-00-710-001 Task 25-11-51-400-001 Task 25-13-14-400-004 Task 31-10-00-700-001 Task 31-21-21-400-001 Task 31-50-00-710-001 Task 31-50-00-710-004 Task 31-60-00-710-001 Task 32-31-11-400-001 Task 32-44-21-400-001 Task 33-12-13-400-001 Task 33-12-13-400-002 Task 33-13-00-710-001 Task 33-14-00-710-001 Task 34-15-21-400-001 Task 34-22-24-400-001 Task 34-22-25-400-001 Task 34-34-22-400-001 Task 34-35-22-400-001 Task 34-57-22-400-001 Task 34-57-22-400-002 Task 34-57-25-400-001 Task 46-21-21-400-001 Elec. Std. Practices Manual (ESPM) 20-52-10 NOTE: This test procedure is to be accomplished after the installation of the equipment removed for access, refer to SUBTASK 921087-410-001 002 Install/Close Items Removed/Opened for access. (a) Preliminary tests NOTE: If the aircraft is operated in CAT 3 conditions, you must also do the DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 53 5

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# @A318/A319/A320/A321 SERVICE BULLETIN land CAT 3 capability test, refer toAMM Task 22-97-00-710-001. 1 On each connector which was disconnected :
a Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by this ESPM procedure is given hereafter. 2 Do the operational test of the instrument and panel integral lightning, refer to AMM Task 33-13-00-710-001. 3 Do the operational test of the light, refer toAMM Task 33-14-00-710-001. 4 Do the operational check of the system via MCDU, refer to AMM Task 21-26-00-710-001. 5 Do the operational test of the AFS, refer toAMM Task 22-96-00-710-001. 6 Do the operational test of the EIS, refer toAMM Task 31-60-00-710-001. 7 Do the operational test of the ECAM control panel, refer to AMM Task 31-50-00-710-004. 8 Ground scanning of the central warning system, refer to AMM Task 31-50-00-710-001. (b) Procedures 1 Depending on the removed items for access, do the applicable test procedure as specified after the installation of the :
a Captain and first officer seat (FINs 3MS and 4MS), refer to AMM Task 25-11-51-400-001. b Foot rests (captain and first officer), refer to AMM Task 25-13-14-400-004.
c Main instrument panel lights (FINs 36LE and 37LE), refer to AMM Task 33-12-13-400-001. d Main instrument panel lights (FIN 38LE), refer to AMM Task 33-12-13-400-002.
e PVI (FIN 1FW), refer toAMM Task 34-34-22-400-001. f HUD OHU (FIN 3FH), refer toAMM Task 34-35-22-400-001. g Panel assy (FIN 131VU), refer toAMM Task 31-10-00-700-001. h Panel assy (FIN 130VU), refer toAMM Task 31-10-00-700-001. i Panel assy (FIN 301VU), refer toAMM Task 31-10-00-700-001.

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 54 5

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# @A318/A319/A320/A321 SERVICE BULLETIN j VOR/DME RMI (FIN 11FN), refer toAMM Task 34-57-22-400-001. k Standby horizon indicator (FIN 7FN), refer to AMM Task 34-22-24-400-001. l ADF RMI (FIN 13FN), refer toAMM Task 34-57-25-400-001.
m VOR/ADF/DME RMI (FIN 21FN), refer toAMM Task 34-57-22-400-002.
n ISIS indicator (FIN 22FN), refer toAMM Task 34-22-25-400-001.
o AOA indicators (FIN 17FN1, 17FN2), refer to AMM Task 34-15-21-400-001. p DCDU (FINs2TX1 and 2TX2), refer toAMM Task 46-21-21-400-001. q Panel assy (FIN 403VU), refer toAMM Task 31-10-00-700-001.
r Panel assy (FIN 402VU), refer toAMM Task 31-10-00-700-001.
s Clock (FIN 2FS), refer toAMM Task 31-21-21-400-001. t Brake yellow pressure triple indicator (FIN 60GG), refer to AMM Task 32-44-21-400-001.
u Landing gear normal control lever (FIN 6GA), refer to AMM Task 32-31-11-400-001.
v Panel assy (FIN 500VU), refer toAMM Task 31-10-00-700-001.
w Air conditioning distribution ducts, refer toAMM Task 21-20-00-410-001. E. CLOSE-UP (1) Subtask 921087-410-001-002 - Install/Close Items Removed/Opened for access. Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills AIRFRAME Material necessary to do the job Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 12 NAS1726-4E 6 Nut 13 NAS1726-5E 2 Nut

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 55 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Synthetic Ester Base Grease-General Purpose Clay 03HBB1 As required

References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-001 Task 21-20-00-410-001 Task 22-81-12-400-001 Task 25-11-51-400-001 Task 25-13-14-400-001 Task 25-13-14-400-004 Task 25-13-41-400-002 Task 31-21-21-400-001 Task 31-63-22-400-001 Task 32-31-11-400-001 Task 32-44-21-400-001 Task 33-12-13-400-001 Task 33-12-13-400-002 Task 34-15-21-400-001 Task 34-21-22-400-001 Task 34-21-25-400-001 Task 34-21-26-400-001 Task 34-22-24-400-001 Task 34-22-25-400-001 Task 34-34-22-400-001 Task 34-35-22-400-001 Task 34-57-22-400-001 Task 34-57-22-400-002 Task 34-57-25-400-001 Task 46-21-21-400-001 Task 52-10-00-410-001 Task 52-41-00-410-002 Structural Repair Manual (SRM) 51-42-00 51-43-00 Fig. A-FBCAA Removal/installation of the cover assies of the 10VU rack Sheet 01 Fig. A-FBDAA Removal/installation of the panel 130VU Sheet 01 Fig. A-FBEAA Removal/installation of the panel 131VU Sheet 01 Fig. A-FBGAA Removal/installation of the panel 500VU Sheet 01 Fig. A-FBHAA Removal/installation of the panel 301VU Sheet 01 Fig. A-FBIAA Removal/installation of the panel 402VU Sheet 01

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 56 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

References Fig. A-FBJAA Removal/installation of the panel assies Sheet 01 Fig. A-FBKAA Removal/installation of the air conditioning system Sheet 01
Fig. A-FBLAA Removal/installation of the panel 401VU Sheet 01 Fig. A-FBMAA Removal/installation of the panel 403VU Sheet 01 Fig. A-FBNAA Removal/installation of the panel 400VU Sheet 01 Fig. A-FBOAA Removal/installation of the 10VU rack Sheet 01 Sheet 02 Fig. A-FBPAA Removal/installation of the equipment 1FR Sheet 01
(a) Install the equipments removed for access. NOTE: Depending on aircraft configuration these parts or equipment can be installed or not. 1 WARNING: BE CAREFUL DURING THE INSTALLATION OF THE 10VU RACK. YOU CAN CAUSE DAMAGE TO EQUIPMENT OR INJURY TO PERSONS. Install the 10VU rack. Refer to Fig. A-FBOAA Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00 FIN 10VU 1 Rack Item (54) Retained at removal 2 Screw Item (46) Retained at removal 2 Washer Item (47) Retained at removal 6 Nut NAS1726-4E Item 12 2 Nut NAS1726-5E Item 13

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 57 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
1 Axle Item (48) Retained at removal 1 Axle Item (49) Retained at removal 2 Axle Item (50) Retained at removal 2 Axle Item (51) Retained at removal 1 Axle Item (52) Retained at removal 1 Axle Item (53) Retained at removal Install the axles with : Synthetic EsterBase GreaseGeneral Purpose Clay 03HBB1 As required

Torque the threaded fasteners : - Items (51), (50), (49), (48) between 0.82 m.daN (72.5 in.lb) Min. to 1.06 m.daN (94 in.lb) Max.. - Items (52), (53) between 1.38 m.daN (122 in.lb) Min. to 1.79 m.daN (158 in.lb) Max.. 2 Install the routing on the 10VU rack in accordance with the identification of the position of the routing and the hardware done during the removal (photos or placards). 3 Install the air conditioning hoses on the 10VU rack. Refer to Fig. A-FBKAA Refer to AMM Task 21-20-00-410-001
a Put in position on the 10VU rack the 4 hoses. b Install : 4 clamp Item (5) Retained at removal 4 Install the panel assy (FIN 500VU). Refer to Fig. A-FBGAA
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 58 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connectors 2104VCA and 2108VCA on the rear of the panel assy (FIN 500VU). b Install : FIN 500VU 1 Panel assy Item (34) Retained at removal 4 Screw Item (32) Retained at removal 4 Washer Item (33) Retained at removal 5 Install the panel assy (FIN 400VU). Refer to Fig. A-FBNAA Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connector 2TX2A on the rear of the panel assy (FIN 400VU) (if existing on aircraft). b Install : FIN 400VU 1 Panel assy Item (43) Retained at removal 7 Screw Item (32) Retained at removal 7 Washer Item (33) Retained at removal 6 Install the landing gear normal control lever (FIN 6GA), refer to AMM Task 32-31-11-400-001. 7 Install the brake yellow pressure triple indicator (FIN 60GG), refer to AMM Task 32-44-21-400-001. 8 Install the clock (FIN 2FS), refer toAMM Task 31-21-21-400-001. 9 Install the panel assy (FIN 402VU). Refer to Fig. A-FBIAA
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 59 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connectors 2100VCA and 2102VCA on the rear of the panel assy (FIN 402VU). b Install : FIN 402VU 1 Panel assy Item (38) Retained at removal 4 Screw Item (36) Retained at removal 4 Washer Item (37) Retained at removal 10 Install the FCU (FIN 2CA), refer toAMM Task 22-81-12-400-001. 11 Install the panel assy (FIN 401VU). Refer to Fig. A-FBLAA Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connector 2TX1A on the rear of the panel assy (401VU) (if existing on aircraft). b Install : FIN 401VU 1 Panel assy Item (42) Retained at removal 7 Screw Item (32) Retained at removal 7 Washer Item (33) Retained at removal 12 Install the equipment (1FR). Refer to Fig. A-FBPAA
a Install : FIN 1FR 1 Equipment Item (92) Retained at removal
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 60 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
1 Clamp Item (6) Retained at removal 13 Install the DCDU (FINs 2TX1 and 2TX2), refer to AMM Task 46-21-21-400-001. 14 Install the panel assy (FIN 403VU). Refer to Fig. A-FBMAA Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connectors 2105VCA and 2109VCA on the rear of the panel assy (FIN 403VU). b Install : 2 Screw Item (39) Retained at removal 2 Washer Item (40) Retained at removal FIN 403VU 1 Panel assy Item (41) Retained at removal 15 Install the ISIS indicator (FIN 22FN), refer toAMM Task 34-22-25-400-001. 16 Install the VOR/ADF/DME RMI (FIN 21FN), refer to AMM Task 34-57-22-400-002. 17 Install the metric altimeter (FIN 15FN), refer toAMM Task 34-21-25-400-001. 18 Install the ADF RMI (FIN 13FN), refer toAMM Task 34-57-25-400-001. 19 Install the standby airspeed indicator (FIN 9FN), refer to AMM Task 34-21-26-400-001. 20 Install the standby altimeter (FIN 3FN), refer toAMM Task 34-21-22-400-001. 21 Install the standby horizon indicator (FIN 7FN), refer to AMM Task 34-22-24-400-001. 22 Install the VOR/DME RMI (FIN 11FN), refer toAMM Task 34-57-22-400-001. 23 Install the display units (FINs 2WT1, 2WT2, 3WT1, 3WT2, 4WT1 and 4WT2), refer toAMM Task 31-63-22-400-001. 24 Install the panel assy (FIN301VU). Refer to Fig. A-FBHAA DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 61 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connectors 2101VCA and 2103VCA on the rear of the panel assy (301VU). b Install : FIN 301VU 1 Panel assy Item (35) Retained at removal 4 Screw Item (32) Retained at removal 4 Washer Item (33) Retained at removal 25 Install the panel assy (FIN 130VU). Refer to Fig. A-FBDAA Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connector 2112VCA from below of the panel assy (FIN 130VU). b Install : FIN 130VU 1 Panel assy Item (31) Retained at removal 3 Screw Item (28) Retained at removal 3 Washer Item (29) Retained at removal Depending on the aircraft configuration install also : 2 Screw Item (27) Retained at removal 2 Washer Item (29) Retained at removal 26 Install the panel assy (FIN 131VU). Refer to Fig. A-FBEAA
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 62 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
Refer to AMM Task 20-21-11-911-001 In accordance with SRM 51-42-00 and SRM 51-43-00
a Connect the connector 2111VCA from below of the panel assy (FIN 131VU). b Install : FIN 131VU 1 Panel assy Item (30) Retained at removal 3 Screw Item (28) Retained at removal 3 Washer Item (29) Retained at removal Depending on the aircraft configuration install also : 2 Screw Item (27) Retained at removal 2 Washer Item (29) Retained at removal 27 Install the AOA indicators (FIN 17FN1, 17FN2), refer to AMM Task 34-15-21-400-001. 28 Install the HUD OHU (FIN 3FH), refer toAMM Task 34-35-22-400-001. 29 Install the PVI (FIN 1FW), refer toAMM Task 34-34-22-400-001. 30 Install the main instrument panel lights (FIN 38LE), refer to AMM Task 33-12-13-400-002. 31 Install the main instrument panel lights (FINs 36LE and 37LE), refer to AMM Task 33-12-13-400-001. 32 Install the panel assies. Refer to Fig. A-FBCAA 1 LH panel assy Item (24) Retained at removal 1 Panel assy Item (25) Retained at removal 1 RH panel assy Item (26) Retained at removal

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 63 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

33 Install the foot rests (captain and first officer), refer to AMM Task 25-13-14-400-001 or AMM Task 25-13-14-400-004. 34 Install the panels assies. Refer to Fig. A-FBJAA
a Install : 10 Screw Item (22) Retained at removal 1 LH panel assy Item (90) Retained at removal 1 LH panel assy Item (20) Retained at removal 1 RH panel assy Item (21) Retained at removal 1 RH panel assy Item (91) Retained at removal 35 Install the panel (FIN 211LW), refer toAMM Task 25-13-41-400-002. 36 Install the captain and first officer seat (FINs 3MS and 4MS), refer to AMM Task 25-11-51-400-001. (2) Subtask 921087-942-003-001 - Close-up Work Zones and Access Panels Zone Access/Work location 210 Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 52-41-00-410-002 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the avionics compartment door 811, refer toAMM Task 52-41-00-410-002. (c) Remove the access platform(s). (d) Put the aircraft back to its initial configuration.

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 64 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL



### A

B B



## A

B
C FWD

VIEW LOOKING AFT AREA TO BE INSPECTED AND POSSIBLE CRACK

AREA TO BE INSPECTED AND POSSIBLE CRACK ON THE 

### C LUG 1 LUG 3 LUG 4

LUG 2

NOTE: THE INSPECTION OF THE FOUR 10VU LUGS MUST BE DONE THROUGH THE AVIONICS COMPARTMENT (ACCESS DOOR 811). LH AND RH SIDE OF THE LUG

N_SB_921087_5_BAAA_01_01 Figure A-FBAAA - Sheet 01 Area to be inspected
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 65 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL
DO A DETAILED INSPECTION OF THE 10VU LUGS 1, 2, 3 AND 4 AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.(2) IN

NO CRACK FOUND

REPEAT THE INSPECTION IN ACCORDANCE

WITH TASK 921087

−832

−801

−001 AT THE REPORT TO AIRBUS ACCORDANCE WITH TASK 921087

−832

−801

−001

INTERVAL GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.(2)

QUESTION
ACTION FINDING YES

REPAIR THE DAMAGED LUG IN ACCORDANCE WITH TASK 921087

−833

−801

− 001 AT THE THRESHOLD GIVEN IN THE REPAIR THE DAMAGED LUGS IN ACCORDANCE WITH TASK 921087

−833

−

REPORT TO AIRBUS ONE SINGLE DAMAGED LUG SEVERAL DAMAGED LUGS

801

−001 BEFORE NEXT FLIGHT PLANNING INFORMATION PARAGRAPH E.(2)

REPEAT THE INSPECTION IN ACCORDANCE

WITH TASK 921087

−832

−801

−001 AT THE INTERVAL GIVEN IN THE PLANNING

INFORMATION PARAGRAPH E.(2)

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 OR

N_SB_921087_5_FAAA_01_01 Figure A-FFAAA - Sheet 01 Flow chart
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 66 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

N_SB_921087_5_BJAA_01_00 

### A B B

LH SIDE RH SIDE

LH SIDE SHOWN RH SIDE SYMMETRICAL (20) (21) LH SIDE RH SIDE (90) (91)

(22)

(22) 

## A

B LH SIDE SHOWN RH SIDE SYMMETRICAL

Figure A-FBJAA - Sheet 01 Removal/installation of the panel assies
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 67 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

NOTE: PANELS REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION N_SB_921087_5_BCAA_01_00 

### A



## A

(24) (25) (26)

Figure A-FBCAA - Sheet 01 Removal/installation of the cover assies of the 10VU rack
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 68 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION 

### A



## A

2x (27) (29)

(28) (29) 2x (30) DISCONNECT THE CONNECTOR 2111VCA FROM BELOW

(28) (29)

N_SB_921087_5_BEAA_01_01 Figure A-FBEAA - Sheet 01 Removal/installation of the panel 131VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 69 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION 

### A

(31)

(28) (29) 2x 2x (27) (29) DISCONNECT THE CONNECTOR 2112VCA FROM BELOW

(28) (29)



## A

N_SB_921087_5_BDAA_01_01 Figure A-FBDAA - Sheet 01 Removal/installation of the panel 130VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 70 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION 

### A

4x DISCONNECT THE CONNECTOR 2101VCA

DISCONNECT THE CONNECTOR 2103VCA
(32) (33) (35)



## A

N_SB_921087_5_BHAA_01_01 Figure A-FBHAA - Sheet 01 Removal/installation of the panel 301VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 71 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL



### A

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION DISCONNECT THE CONNECTOR 2105VCA

(41)

(39) (40) DISCONNECT THE CONNECTOR 2109VCA



## A 2x

N_SB_921087_5_BMAA_01_02 Figure A-FBMAA - Sheet 01 Removal/installation of the panel 403VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 72 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL



### A

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION 

## A

N_SB_921087_5_BPAA_01_00 

## B (6)
(92) 

### B

Figure A-FBPAA - Sheet 01 Removal/installation of the equipment 1FR
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 73 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL



### A

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION DISCONNECT THE CONNECTOR 2TX1A (42)

(32) (33) 7x



## A

N_SB_921087_5_BLAA_01_02 Figure A-FBLAA - Sheet 01 Removal/installation of the panel 401VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 74 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION 4x

DISCONNECT THE CONNECTOR 2102VCA DISCONNECT THE CONNECTOR 2100VCA 

### A

(38) (36) (37)



## A

N_SB_921087_5_BIAA_01_01 Figure A-FBIAA - Sheet 01 Removal/installation of the panel 402VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 75 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION DISCONNECT THE CONNECTOR 2TX2A (32) (33)



## A A (43)

7x

N_SB_921087_5_BNAA_01_02 Figure A-FBNAA - Sheet 01 Removal/installation of the panel 400VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 76 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

NOTE: PANEL REPRESENTATION MAY DIFFER, DEPENDING ON THE AIRCRAFT CONFIGURATION 

### A

4x 

## A (34)

(32) (33) DISCONNECT THE CONNECTOR 2108VCA DISCONNECT THE CONNECTOR 2104VCA

N_SB_921087_5_BGAA_01_01 Figure A-FBGAA - Sheet 01 Removal/installation of the panel 500VU
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 77 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL

Z210 

### A

FR1 FR4 

## A

N_SB_921087_5_BKAA_01_01 HOSES TO BE DISCONNECTED FROM THE 10VU RACK 

### C

HOSES TO BE DISCONNECTED FROM THE 10VU RACK (5)



## C (5)



## B B

Figure A-FBKAA - Sheet 01 Removal/installation ofthe air conditioning system
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 78 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL



### A

NOTE: INSTALL THE AXLES WITH MAT. No. 04

−004B N_SB_921087_5_BOAA_01_00 

## A B B

(54) (53) (13) 13 (51) (12) 12

(51) (12) 12 (52) (13) 13 (50) (12) 12 (49) (12) 12 (48) (12) 12 (50) (12) 12

Figure A-FBOAA - Sheet 01 Removal/installation of the 10VU rack
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 79 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL FR3

FR3 

### C D



## B LH SIDE SHOWN RH SIDE SYMMETRICAL

VIEW LOOKING FORWARD



## D TOP VIEW AFTER ADJUSTMENT OF THE CLEVIS TORQUE THE BOLTS (IF NECESSARY) (46) (47) FWD

FWD N_SB_921087_5_BOAA_02_01 STRIPPING DIA. 14mm (0.551 in.) ON THE VISIBLE FACE



## C

Figure A-FBOAA - Sheet 02 Removal/installation of the 10VU rack
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 80 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

**CONF ALL



### A

B B



## A

C FWD VIEW LOOKING AFT AREA TO BE INSPECTED AND POSSIBLE CRACK



### C LUG 1 LUG 3 LUG 4

LUG 2

AREA TO BE INSPECTED AND POSSIBLE CRACK ON THE LH AND RH SIDE OF THE LUG 

## B

N_SB_921087_5_RAAA_01_00 Figure A-FRAAA - Sheet 01 Inspection report
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 81 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

−92

−1087

DATE OF INSPECTION : RETURN TO : AIRBUS CUSTOMER SERVICES ENGINEERING

−SEEA5 ELECTRICAL POWER & LIGHTING SYSTEMS

INSPECTION METHOD : 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 44 25 DETAILED INSPECTION

10VU PART

NUMBER CRACK LENGTH IN MM LUG 1

QUESTION TO THE OPERATOR: DID THE OPERATOR INSTALL (THANKS TO AN STC) AN ADDITIONNAL EQUIPMENT ATTACHED ON THE 10VU LIKE FOR INSTANCE THE ONBOARD INFORMATION TERMINAL (OIT)

IF LUGS HAVE BEEN REPLACED THE REMOVED PART SHOULD BE SENT TO AIRBUS FOR INVESTIGATION NOTE: LUG 2 LUG 3 LUG 4

N_SB_921087_5_RAAA_02_00 Figure A-FRAAA - Sheet 02 Inspection report
DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 82 5

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# @A318/A319/A320/A321 SERVICE BULLETIN REPORTING SHEET 

### TITLE: ELECTRIC AND ELECTRONICCOMMON INSTALLATION-GENERALLUGS INSPECTION ON 10VU SLEEVES 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: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 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: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087 REVISION No.: 02 - Nov 25/14 Page: 1 5

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