@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 ELECTRONIC COMMON 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

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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

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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

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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

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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

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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

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

This summary is for information only and is not approved for modification of the aircraft.

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON 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

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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

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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

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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

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 92

TITLE: ELECTRIC AND ELECTRONIC COMMON 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

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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 1494 2910

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 1846 2870

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 2

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SERVICE BULLETIN

OPERATOR MSN

AAR 0802 1174 1356 1511 2041 2110 2226 2247 2290 2397 2459 2840

AAY 1229 1255 1262 1288 1292 1318 1347 2224 2319 2387

ABL 1227 1636 1670 1734 1970 2045 2808 2943

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 2106 2116 2133 2144 2233 2330 2337 2342

2875 2903 2912 2920 2947 2957 2965

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 2487 2516 2588 2685 2788 2846 2853 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 2624 2629 2907

AIJ 0169 0707 1132 1162 1179 1244 1259 1308 1322 1747 1780 2048

2227 2539

AJD 0879 1422

ALK 2345 2564 2584

AMC 2113 2122 2189 2291 2332 2382 2665 2768

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 2148 2153 2173 2257 2297 2445 2533 2594

2663

ARR 0913

ART 0142 0244 0311 0333 0359 0426 0533 0662 0936 1873

ARU 0573 0582

ASL 1140 1159 2277 2296 2335 2587 2621 2645

ATR 0314 0393

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 3

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SERVICE BULLETIN

OPERATOR MSN

AUA 0552 0570 0581 0768 0776 0797 0920 0935 1137 1150 1189 1387

1458 1478 1504 1553 1678 1735 1931 1937 2009 2131 2174 2262

2416 2494 2547 2652

AUH 2403

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

2575 2662

AWC 2791

AWM 0765

AWW 0557 0597 2273

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 2057 2074 2083 2086 2101 2127 2869 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 1987 2038 2040 2098 2188 2190 2194 2305 2320 2323 2324

2351 2363 2389 2429 2441 2466 2536 2653 2694 2697 2720 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 1994 2003 2005 2619

BGH 1087 2844 2863

BHP 2968

BIE 0519 0827 0891

BKP 2254 2310 2366 2417 2509 2531 2600 2634 2648 2660 2664 2783

2874

BQB 1703

BRS 2263

BSX 0648 0650

BTN 1541 1551

C9G 2128

CBJ 2557 2561 2611 2644 2733 2849 2891 2985

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

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

2805 2819 2839 2847 2890

CEB 2556 2586 2625 2638 2786 2790 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

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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 2034 2036 2049 2056 2068 2219 2221 2235

2239 2244 2309 2315 2437 2451 2478 2493 2498 2543 2549 2562

2591 2606 2627 2693 2757 2825 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 2758 2789

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

2348 2396 2431 2510 2534 2597 2639

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 2354 2361 2371 2408 2426 2435 2484

2505 2506 2511 2519 2521 2530 2541 2546 2554 2555 2558 2574

2579 2637 2667 2680 2689 2701 2708 2713 2714 2741 2743 2759

2767 2770 2772 2796 2809 2815 2824 2834 2855 2861 2877 2899

2901 2915 2936 2940 2948 2950 2960 2969 2971 2986

CSZ 2672 2684 2841 2905 2909 2935 2973 2980

CTN 0767 0833 1009 1029 1237 1252

CTV 0839 0892 1635 2598 2692

CYP 0256 2108 2275 2334 2343 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

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SERVICE BULLETIN

OPERATOR MSN

EAA 0386

EDW 0942 0947 1026 2024 2134

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

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

2635

ETD 0350 1944 1945 1947 1955 2167

ETJ 0295 0325 0373 0428 0445

EZD 0667 0743 0872 0874 1074 1286 2137 2141 2147 2576 2826 2956

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

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

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

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

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

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

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 1997 2010 2012 2019 2030 2103 2198 2209 2236 2240 2253

2258 2260 2287 2318 2325 2406 2448 2483 2518 2695 2806 2836

2857

FHY 0580 0771 0855 2524 2804

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

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

2266

FLI 2186

FPY 0112 0189 0342

FRN 0647 0660

FTZ 1068 1145 2176 2268 2281

G2X 0347 0653 0674

G4I 1157 1795 2507

GAP 0706 0745 2162 2183

GBB 0067 0076

GCR 2338 2475

GHT 0438

GLG 1866 1872 1882 1925 2078 2126

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 1277 2607 2628 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 2238 2428

HFY 1004

HKE 2299 2322 2717

HKJ 2706

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 6

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SERVICE BULLETIN

OPERATOR MSN

HRM 0517 0535 0642 0666

HVN 2255 2261 2267 2974

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 2264 2270 2311 2357 2365 2381 2391 2472 2488 2563

2599 2736 2756 2996

IBS 1047 1059 1067 1099 1101 1119 1125 1198 1516 2104 2143 2248

2807

IND 0343 0357

IRA 0303 0312 0345 0575 0857 2054

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 1948 2006 2020 2031 2042 2063

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

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

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

2640 2647 2671 2710 2725 2755 2781 2802 2814 2832 2848 2871

2880 2900 2945 2970 2977 2992

JSA 2316 2356 2423 2453 2604

JST 1195 1408 2169 2185 2197 2292 2329 2455 2515 2526 2537 2573

2608 2642 2651 2703 2766 2787

KAC 0181 0182 0195 2046

KFR 2650

KGL 0663 0668 0787 0852 0954 1060 1293 1554 2029 2077

KHV 2303 2480

KKK 0604 0614 0675 0761 0808 0823 0968 0974 1124 1390 1438 1451

1503 1624 1730 1950 1953 2747 2753

KMF 0480

KZR 1042 1204

LAN 1304 1332 1351 1355 1491 1512 1526 1548 1568 1854 1858 1877

1903 2089 2096 2295 2304 2321 2572 2585 2845 2858 2864 2872

2886 2887 2892 2894

LBT 0793 0937 1121 1175 1597 1744 2158

LFO 0659

LKE 2581 2617 2746

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

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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 2937 2966

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 1965 2123 2171 2182 2199 2569 2776

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

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

2983

NLY 2529 2668 2749 2867 2902

NMA 1697 1732 2676

NVD 0211 0299 0375 0409 0419 0528 0558 0561 0709 0747 1626 1778

NVR 2211 2216 2410

NWS 1219 1233 1276 1843 2649 2927 2933

OAW 1886

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

0811 0835 0912 0916 0963 1008 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 1957 2097 2107 2121 2138

2161 2288 2341

R1T 1908

RBA 2023 2032 2135 2139 2195

RCT 0466 1017

RFJ 0814

RJA 2953

RJD 1618

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 8

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SERVICE BULLETIN

OPERATOR MSN

ROT 2931 2955

RYW 0569

RZO 0795 2011 2390

SAA 2308 2326 2355 2375 2379 2418 2438 2469 2501

SAI 0542 0877 1497 2027

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

2856 2883 2888 2911 2958 2990

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

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

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 2214 2249 2251 2283 2378 2380 2436

2460 2548

SLK 0899 0969 1228 1561 1698 2058 2252 2517 2568 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 2117 2166 2175 2187 2278 2327

2349 2707 2998

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 1934 2084 2659

TAI 1066 1334 1598 1625 1952 2282 2301 2339 2434 2444 2687 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 2784 2838 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

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@A318/A319/A320/A321

SERVICE BULLETIN

OPERATOR MSN

TCW 1787 1929 1975 2114 2362

TCX 0677 1006 1238 1250 2060

TGW 2724 2728

THY 1002 1727 1856 1909 1996 2156 2164 2395 2401 2404 2414 2452

2522 2602 2609 2626 2631 2655 2738 2739 2823 2868 2916 2919

2928 2934 2941 2984

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 2696 2762 2774 2820 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 1935 2193 2302 2312 2405 2422 2430 2458

2482 2570 2595 2613 2615 2630 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

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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 2207 2223 2388 2407

2479 2589 2620 2658 2678 2761 2785 2794 2798 2843 2889 2897

2962 2988

VOI 2204 2657 2666 2771 2780 2979 2997

VRD 2616 2674 2740 2773 2778 2800 2811 2830 2851 2993

VRE 1429 2213 2228

VVC 1306 1454 1564 1725 1757 1867

WGT 1212

WHT 0548 1256 2440 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

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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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REVISION No.: 02 - Nov 25/14 Page: 13

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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

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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 2004 2005 2006 2007 2008

2009 2010 2011 2012 2013 2014 2015 2016 2018 2019 2020

2021 2022 2023 2024 2026 2027 2028 2029 2030 2031 2032

2033 2034 2035 2036 2037 2038 2039 2040 2041 2042 2043

2044 2045 2046 2047 2048 2049 2050 2052 2053 2054 2055

2056 2057 2058 2059 2060 2061 2062 2063 2064 2065 2066

2067 2068 2069 2070 2071 2072 2073 2074 2075 2076 2077

2078 2079 2080 2081 2082 2083 2084 2085 2086 2087 2088

2089 2090 2091 2092 2093 2094 2095 2096 2097 2098 2099

2100 2101 2102 2103 2104 2105 2106 2107 2108 2109 2110

2112 2113 2114 2115 2116 2117 2118 2119 2120 2121 2122

2123 2124 2125 2126 2127 2128 2129 2130 2131 2132 2133

2134 2135 2136 2137 2138 2139 2140 2141 2142 2143 2144

2145 2146 2147 2148 2149 2150 2151 2152 2153 2154 2155

2156 2157 2158 2159 2160 2161 2162 2163 2164 2165 2166

2167 2168 2169 2170 2171 2172 2173 2174 2175 2176 2177

2178 2179 2180 2181 2182 2183 2184 2185 2186 2187 2188

2189 2190 2191 2192 2193 2194 2195 2196 2197 2198 2199

2200 2201 2202 2203 2204 2205 2206 2207 2208 2209 2210

2211 2212 2213 2214 2215 2216 2217 2219 2220 2221 2222

2223 2224 2225 2226 2227 2228 2229 2230 2231 2232 2233

2234 2235 2236 2237 2238 2239 2240 2241 2242 2243 2244

2245 2246 2247 2248 2249 2250 2251 2252 2253 2254 2255

2256 2257 2258 2259 2260 2261 2262 2263 2264 2265 2266

2267 2268 2269 2270 2271 2272 2273 2274 2275 2277 2278

2279 2280 2281 2282 2283 2284 2285 2286 2287 2288 2289

2290 2291 2292 2293 2294 2295 2296 2297 2298 2299 2300

2301 2302 2303 2304 2305 2306 2307 2308 2309 2310 2311

2312 2313 2314 2315 2316 2317 2318 2319 2320 2321 2322

2323 2324 2325 2326 2327 2328 2329 2330 2331 2332 2333

2334 2335 2336 2337 2338 2339 2340 2341 2342 2343 2344

2345 2346 2347 2348 2349 2350 2351 2352 2353 2354 2355

2356 2357 2358 2359 2360 2361 2362 2363 2364 2365 2366

2367 2368 2369 2370 2371 2372 2373 2374 2375 2376 2377

2378 2379 2380 2381 2382 2383 2384 2385 2386 2387 2388

2389 2390 2391 2392 2393 2394 2395 2396 2397 2398 2399

2400 2401 2402 2403 2404 2405 2406 2407 2408 2409 2410

2411 2412 2413 2414 2415 2416 2417 2418 2419 2420 2421

001

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SERVICE BULLETIN

MSN CONFIGURATION

2422 2423 2425 2426 2427 2428 2429 2430 2431 2432 2433

2434 2435 2436 2437 2438 2439 2440 2441 2442 2443 2444

2445 2446 2447 2448 2449 2450 2451 2452 2453 2454 2455

2456 2457 2458 2459 2460 2461 2462 2463 2464 2465 2466

2467 2468 2469 2470 2471 2472 2473 2474 2475 2476 2477

2478 2479 2480 2481 2482 2483 2484 2485 2486 2487 2488

2489 2490 2491 2492 2493 2494 2495 2496 2497 2498 2499

2501 2502 2503 2504 2505 2506 2507 2508 2509 2510 2511

2512 2513 2514 2515 2516 2517 2518 2519 2520 2521 2522

2523 2524 2525 2526 2527 2528 2529 2530 2531 2532 2533

2534 2535 2536 2537 2538 2539 2540 2541 2542 2543 2544

2545 2546 2547 2548 2549 2550 2551 2552 2553 2554 2555

2556 2557 2558 2559 2560 2561 2562 2563 2564 2565 2566

2567 2568 2569 2570 2571 2572 2573 2574 2575 2576 2577

2578 2579 2580 2581 2582 2583 2584 2585 2586 2587 2588

2589 2590 2591 2592 2593 2594 2595 2596 2597 2598 2599

2600 2601 2602 2603 2604 2605 2606 2607 2608 2609 2610

2611 2612 2613 2614 2615 2616 2617 2618 2619 2620 2621

2622 2623 2624 2625 2626 2627 2628 2629 2630 2631 2632

2633 2634 2635 2636 2637 2638 2639 2640 2641 2642 2643

2644 2645 2646 2647 2648 2649 2650 2651 2652 2653 2654

2655 2656 2657 2658 2659 2660 2661 2662 2663 2664 2665

2666 2667 2668 2669 2670 2671 2672 2673 2674 2675 2676

2677 2678 2679 2680 2681 2682 2683 2684 2685 2686 2687

2688 2689 2690 2691 2692 2693 2694 2695 2696 2697 2698

2699 2700 2701 2702 2703 2704 2705 2706 2707 2708 2709

2710 2711 2712 2713 2714 2715 2716 2717 2718 2719 2720

2721 2723 2724 2725 2726 2727 2728 2729 2730 2731 2732

2733 2734 2735 2736 2737 2738 2739 2740 2741 2742 2743

2744 2745 2746 2747 2748 2749 2750 2751 2752 2753 2754

2755 2756 2757 2758 2759 2760 2761 2762 2763 2764 2765

2766 2767 2768 2769 2770 2771 2772 2773 2774 2775 2776

2777 2778 2779 2780 2781 2782 2783 2784 2785 2786 2787

2788 2789 2790 2791 2792 2793 2794 2795 2796 2797 2798

2799 2800 2801 2802 2803 2804 2805 2806 2807 2808 2809

2810 2811 2812 2813 2814 2815 2816 2817 2818 2819 2820

2821 2822 2823 2824 2825 2826 2827 2828 2829 2830 2831

2832 2833 2834 2835 2836 2837 2838 2839 2840 2841 2842

2843 2844 2845 2846 2847 2848 2849 2850 2851 2852 2853

2854 2855 2856 2857 2858 2859 2860 2861 2862 2863 2864

2865 2866 2867 2868 2869 2870 2871 2872 2873 2874 2875

2876 2877 2878 2879 2880 2881 2882 2883 2884 2885 2886

2887 2888 2889 2890 2891 2892 2893 2894 2895 2896 2897

2898 2899 2900 2901 2902 2903 2904 2905 2906 2907 2908

2909 2910 2911 2912 2913 2914 2915 2916 2917 2918 2919

2920 2921 2922 2923 2924 2925 2926 2927 2928 2929 2930

2931 2932 2933 2934 2935 2936 2937 2938 2939 2940 2941

2942 2943 2944 2945 2946 2947 2948 2949 2950 2951 2952

2953 2954 2955 2956 2957 2958 2959 2960 2961 2962 2963

2964 2965 2966 2967 2968 2969 2970 2971 2972 2973 2974

2975 2976 2977 2978 2979 2980 2981 2982 2983 2984 2985

001

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 16

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SERVICE BULLETIN

MSN CONFIGURATION

2986 2987 2988 2989 2990 2991 2992 2993 2994 2995 2996

2997 2998

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

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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

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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

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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

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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

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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

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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

NOTES

Synthetic Ester Base GreaseGeneral Purpose Clay03HBB1 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

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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

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(3) Special Tools

None

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

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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

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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

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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 to AMM 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

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

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Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Non Aqueous CleanerGeneral08BAA9 As required

References

Fig. A-FFAAA

Flow chart

Sheet 01

Fig. A-FBAAA

Area to be inspected

Sheet 01

Fig. A-FRAAA

Inspection report

Sheet 01

Sheet 02

(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

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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 to AMM 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

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This Page Intentionally Left Blank

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

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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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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 to AMM 06-31-53, Page Block 001.

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

(e) For the identification of access panels, refer to AMM 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.

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(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

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- 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 to AMM 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

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

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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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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 to AMM 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.

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(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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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 to AMM Task 31-63-22-000-001.

(o) Remove the VOR/DME RMI (FIN 11FN), refer to AMM 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 to AMM 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 to AMM Task 34-57-25-000-001.

(t) Remove the metric altimeter (FIN 15FN), refer to AMM 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

to AMM 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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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 to AMM 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

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 41

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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 to AMM 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

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

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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

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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

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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

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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

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 46

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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

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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

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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

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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

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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

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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

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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

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land CAT 3 capability test, refer to AMM 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 to AMM 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 to AMM Task 22-96-00-710-001.

6 Do the operational test of the EIS, refer to AMM 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 to AMM Task 34-34-22-400-001.

f HUD OHU (FIN 3FH), refer to AMM Task 34-35-22-400-001.

g Panel assy (FIN 131VU), refer to AMM Task 31-10-00-700-001.

h Panel assy (FIN 130VU), refer to AMM Task 31-10-00-700-001.

i Panel assy (FIN 301VU), refer to AMM Task 31-10-00-700-001.

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

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j VOR/DME RMI (FIN 11FN), refer to AMM 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 to AMM Task 34-57-25-400-001.

m VOR/ADF/DME RMI (FIN 21FN), refer to AMM Task 34-57-22-400-002.

n ISIS indicator (FIN 22FN), refer to AMM Task 34-22-25-400-001.

o AOA indicators (FIN 17FN1, 17FN2), refer to AMM Task

34-15-21-400-001.

p DCDU (FINs 2TX1 and 2TX2), refer to AMM Task 46-21-21-400-001.

q Panel assy (FIN 403VU), refer to AMM Task 31-10-00-700-001.

r Panel assy (FIN 402VU), refer to AMM Task 31-10-00-700-001.

s Clock (FIN 2FS), refer to AMM 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 to AMM Task 31-10-00-700-001.

w Air conditioning distribution ducts, refer to AMM 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

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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

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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

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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 Ester

Base 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

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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 to AMM 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

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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 to AMM 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

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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 to AMM 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 to AMM Task 34-21-25-400-001.

18 Install the ADF RMI (FIN 13FN), refer to AMM 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 to AMM 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 to AMM Task 34-57-22-400-001.

23 Install the display units (FINs 2WT1, 2WT2, 3WT1, 3WT2, 4WT1 and 4WT2),

refer to AMM 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

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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

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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 to AMM Task 34-35-22-400-001.

29 Install the PVI (FIN 1FW), refer to AMM 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

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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 to AMM 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 to AMM 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

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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

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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

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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

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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

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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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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

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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

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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

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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

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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

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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

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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

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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

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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 of the air conditioning system

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 78

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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

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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

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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

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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

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@A318/A319/A320/A321

SERVICE BULLETIN

REPORTING SHEET

TITLE: ELECTRIC AND ELECTRONIC COMMON 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

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

SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Mar 28/11 SERVICE BULLETIN No.: A320-92-1087

REVISION No.: 02 - Nov 25/14 Page: 1

5

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