@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

ATA SYSTEM: 32

TITLE: LANDING GEAR - ALTERNATE BRAKING WITH ANTI-SKID - INSTALL

A NEW MODIFIED BRAKE DISTRIBUTION DUAL VALVE

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 155579P12900

NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the

mass, balance, structural strength, reliability, operational characteristics affecting the

airworthiness of the product. All other changes are major changes.

REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES

One operator experienced a dual loss of braking: loss of normal braking (failure detection on normal

braking circuit) and loss of alternate braking. The aircraft was stopped with full reversers and Parking

Brake.

The Brake Dual Distribution Valve (BDDV) cover was found filled with ice, thus preventing to command

the alternate braking with the pedals.

Investigation performed on the BDDV revealed that the cover seal was damaged and did not ensure the

sealing efficiency.

Breathing and/or water projection introduce water in the cover.

Due to low temperature reached in flight, the water is freezing and blocks the BDDV rocker arm

movement.

This Service Bulletin is published to advise all operators of A320 family aircraft of the issue of

MESSIER-BUGATTI-DOWTY Service Bulletin No. A25434-32-3374.

This Service Bulletin aims at shortening the drain tube to a length of 80 ± 5 mm (3.15 ± 0.20 in.) and

removing the end plug.

Accomplishment of this Service Bulletin will avoid the freezing of the water by ensuring the continuous

draining of the water.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 1

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SERVICE BULLETIN

SUMMARY

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 YES

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

disruptions.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 321415D01R00 1 26.00 Bolts, Washers, Nuts

Equipment BFEA01 1 See SB BDDV

Equipment BFEA02 1 See SB BDDV

EFFECTIVITY

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

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

53Z 59Z 66X 69X 73W 74T 85T 86W 86Z 92Q 94W 98W AAF

AAR AAY ABL ABQ ACA ACI AFL AFR AGY AHY AIB AIC AIJ

AJD ALK AMC AMU ANA ANR ANZ AOL ARR ART ARU ASL ATR

AUA AVA AWM AWW AXM AZA AZI AZW B2V BAW BEL BER BGH

BIE BKP BQB BRS BTN C9G CCA CES CIB CQH CQN CSC CSN

CTN CTV CYP DAL DCS DLH DNV DQA DTR EAA EDW EIN ETD

ETJ EZD F2I FFT FHY FIN FPY FRN FTZ G2X G4I G8E GAP

GBB GHT GLG GMI GMR GWI GZQ HAY HDA HFY HRM HVN I2L

I2T IBE IBS IND IRA IRM ISS IZG JAV JBU JSA JST KAC

KGL KHV KKK KMF KNE KZR LAN LBT LFO LLC LLM LLP LMJ

LMU MAU MEA MLD MLR MMA MML MON MRJ MSC MSR MXA MYX

NLV NMA NVD NVR NWS OAW OHY OZW PIA PIC PTI PTR QAF

QTR R1T RBA RCT RFJ RJD RYW RZO SAI SAS SBI SDM SFW

SGG SHJ SHU SKU SLK SND SNX SOL SVR SWM SWR SYR TAE

TAI TAM TAP TAR TBJ TBZ TCW TCX THY TNA TVS TXP UAL

UJX ULG USA VIV VKG VLE VLG VLK VOI VRE VVC WGT WHT

WRC WZZ

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 2

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SERVICE BULLETIN

SUMMARY

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT YES

HARD NO

SOFT NO

OBRM NO

MANPOWER

Task 321415-831-801-001: Modification of the BDDV (FIN 2577GM) as per VSB on Aircraft

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

Additional manhours related to Vendor SB; refer to:

Modify the BDDV (FIN 2577GM) and the Drain Hose in

accordance with VSB on Aircraft

MESSIER-BUGATTI-DOWTY

Service Bulletin No.

A25434-32-3374

Task 321415-831-802-001: Modification of the BDDV (FIN 2577GM) as per VSB in Shop

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 5.25

Additional manhours related to Vendor SB; refer to:

Modify the BDDV (FIN 2577GM) and the Drain Hose in

accordance with VSB on Bench

MESSIER-BUGATTI-DOWTY

Service Bulletin No.

A25434-32-3374

Task 321415-831-803-001: Modification by Replacement of the BDDV (FIN 2577GM) on Aircraft

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 5.25

APPENDICES

None

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF ALL

Z744

A

FR47

FR46

BEFORE AFTER

A

B C

B C

NOTE:

AREA OF MODIFICATION

BRAKE DISTRIBUTION

DUAL VALVE

2577GM

BRAKE DISTRIBUTION

DUAL VALVE

2577GM

N_SB_321415_6_SAAA_01_00

Figure A-GSAAA - Sheet 01

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 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: 32

TITLE: LANDING GEAR - ALTERNATE BRAKING WITH ANTI-SKID - INSTALL

A NEW MODIFIED BRAKE DISTRIBUTION DUAL VALVE

MODIFICATION No.: 155579P12900

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

NOTE: This modification is applicable by Service Bulletin only.

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

26925P4576 (INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM) is

not embodied.

(1) Models

319-111 319-112 319-113 319-114 319-115 319-131 319-132 319-133

320-211 320-212 320-214 320-231 320-232 320-233 321-111 321-112

321-131 321-211 321-212 321-213 321-231 321-232

(2) Effectivity by MSN

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

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

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

0197-0203 0205-0214 0216-0220 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 0380-0388 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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 1

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SERVICE BULLETIN

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

0633-0707 0709 0711-0752 0754-0788 0790-0955 0957-1043 1045-1112 1114-1185

1187-1217 1219-1277 1279-1332 1334-1373 1375-1463 1465-1598 1600-1659

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 2026-2034 2036

2038-2042 2044-2049 2052 2054-2058 2060-2061 2063-2070 2072-2080 2082-2099

2101-2108 2110 2112-2118 2121-2128 2130-2169 2171-2175 2177-2180 2182-2183

2185 2187-2188 2190-2195 2197-2212 2215-2217 2219-2223 2225-2227 2229

2231-2244 2246-2248 2250 2252-2256 2258-2264 2266-2267 2269-2270 2272-2275

2278 2280 2282 2284-2288 2290 2293-2295 2298 2301-2305 2307 2309-2316 2318

2320-2321 2323-2325 2327 2330-2331 2334 2336-2337 2339-2343 2345 2347-2349

2351-2352 2356-2357 2359 2363-2365 2368-2369 2371-2374 2381 2384 2386

2388-2391 2393 2397 2399 2405 2407-2411 2415-2416 2421-2422 2425-2426

2428-2430 2432 2435 2437 2447 2449 2451 2454 2458-2459 2461-2462 2464 2466

2472 2474 2478-2480 2482 2486 2488-2489 2491 2493-2494 2498-2499 2504-2505

2507-2510 2517 2520-2521 2525 2530 2532 2534-2536 2542-2543 2545 2547 2549

2551 2559 2562-2563 2568 2570 2574 2577 2579-2580 2583 2589 2591 2595 2597

2599 2606 2613-2615 2618 2627 2630 2635 2639-2641 2643 2647 2652 2667 2669

2671 2682 2690 2710 2725 2755 2775 2781 2802 2805 2814-2815 2819 2832 2839

2847-2848 2871 2880 2890 2900-2901 2940 2945 2948 2969-2970 2977 2992 3020

3029 3039 3072 3091 3104 3106 3119 3144 3150 3190 3195 3200 3226 3228 3250

3258 3263 3269 3287 3311 3342 3348

(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

26S 0368 0424

29P 0648 0650

29S 0291 0292

31P 0229

31V 0164 0332 0420 0436 0605 0932 0943 1048

31X 2192

32Q 1283

35U 0088 0199 0240 0241 0264

36R 1305

38W 1194

53Z 1468

59Z 1556

66X 1098

69X 0219 0449 0588

73W 0087

74T 2165

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

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SERVICE BULLETIN

OPERATOR MSN

85T 0190 0234

86W 0384

86Z 0168 0460 0497

92Q 0279 0395

94W 1818

98W 0441

AAF 0639 1846

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

AAY 1229 1255 1262 1288 1292 1318 1347

ABL 1227 1636 1670 1734 1970 2045

ABQ 1467

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

AFL 2052 2069 2072 2091 2106 2116 2133 2144 2233 2330 2337 2342

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 2140

AGY 0322 0351

AHY 0331

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

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

AJD 1422

ALK 2345

AMC 2113 2122

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 0445 0671 0726

ANZ 2085 2090 2112 2130 2148 2153 2173

AOL 0400

ARR 0913 1439 1450

ART 0142 0244 0311 0333 0359 0426 0533 0662 0936 1873

ARU 0573 0582

ASL 1140 1159

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

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SERVICE BULLETIN

OPERATOR MSN

ATR 0314 0373 0393

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

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

2262 2416 2494 2547 2652

AVA 1612 1634 2066

AWM 0765

AWW 0557 0597

AXM 2425

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

AZI 0527

AZW 0630 1973

B2V 0185

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

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

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

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

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

2188 2190 2194 2305 2320 2323 2324 2351 2363 2389 2429 2466

2536

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

BER 1629 1717 1775 1961 1966 1988 1994 2003 2005

BGH 1087

BIE 0519 0827 0891

BKP 2254 2310 2509

BQB 1703

BRS 2263

BTN 1541 1551

C9G 0772 1727

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

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

2805 2819 2839 2847 2890 3195 3200 3226 3250

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 2274 2309 2315 2437 2451 2478 2493 2498 2543 2549

2562 2591 2606 2627

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

1968

CQH 0978 1686 1769 1852 1920

CQN 0696 0698 0704 0705

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

2348 2510 2534 2597 2639

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SERVICE BULLETIN

OPERATOR MSN

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

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

2067 2080 2200 2203 2232 2273 2371 2408 2426 2435 2505 2521

2530 2574 2579 2667 2815 2901 2940 2948 2969 3020 3144 3258

3269 3311 3342

CTN 0767 0833 1009 1029 1237 1252

CTV 0839 0892 1635

CYP 0256 2108 2275 2334 2343 2359

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

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

0116 0135 0137 0161 0172 0201 0202 0216 0267 0269 0346 0412

0458 0468 0473 0474 0484 0493 0502 0505 0518 0560 0563 0564

0567 0595 0609 0610 0616 0623 0627 0636 0641 0651 0652 0679

0689 0692 0694 0699 0700 0717 0723 0729 0738 0744 0853 0860

0875 0887 0901 1016 1080 1161 1172 1188 1214 1260 1273 1337

1365 1367

DNV 1630 1805 1808 1841 2093 2179 2241

DQA 2347

DTR 0113 0114 0444

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 0325 0428

EZD 0667 0743 0872 0874 1074 1286 2137 2141 2147

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

FHY 0580 0771 0855

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

FPY 0112 0189 0342

FRN 0647 0660

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SERVICE BULLETIN

OPERATOR MSN

FTZ 1068 1145

G2X 0347 0653 0674

G4I 1157 1795 2507

G8E 0594

GAP 0706 0745 2162 2183

GBB 0067

GHT 0438

GLG 1866 1872 1882 1925 2078 2126

GMI 0684 0970 0995

GMR 1407 2128

GWI 0117 0147 0162 0200 0209 0217 0218 0268 0382 0401 0646 0654

0794 1077 1084 1089 1136 1147 1155 1170 1209 1277

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

HRM 0293 0517 0535 0642 0666

HVN 0619 2255 2261 2267

I2L 0371 0491 0525 0579 0760 0816

I2T 1631 1682

IBE 0158 0173 0176 0207 0224 0266 0274 0323 0356 1021 1027 1047

1154 1362 1572 1655 1674 1681 1716 1793 1809 1836 2115 2220

2225 2242 2264 2270 2311 2357 2365 2381 2391 2472 2488 2563

2599

IBS 1059 1067 1099 1101 1119 1125 1198 1516 1530 2104 2143 2248

IND 0343 0357

IRA 0303 0312 0345 0575 0857 2054

IRM 0354 0414

ISS 0737 0749 1823 1896 2102

IZG 0376 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 3029 3039 3072 3091 3119 3150

3190 3228 3263 3287 3348

JSA 2316 2356

JST 1195 1408 2169 2185 2197

KAC 0181 0182 0195 2046

KGL 0663 0668 0787 0852 0954 1060 1293 1554 2029 2077

KHV 2303 2480

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

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SERVICE BULLETIN

OPERATOR MSN

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

1503 1624 1730 1950 1953

KMF 0480

KNE 1942 1965 2123 2171 2182 2199

KZR 1042 1204

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

1903 2089 2096 2295 2304 2321

LBT 0793 0937 1121 1175 1597 1744 2158

LFO 0659

LLC 0415 0990 1715

LLM 1054 1918 1956 1967 1969 1993

LLP 0739 0883 0914 1411 2016

LMJ 1868

LMU 0977 1366

MAU 1592 1936

MEA 1977 2055

MLD 0622 0741

MLR 1946 3106

MMA 0295 0316 0973 1180 1247 1791

MML 1706 1750

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

1433 1571 1605 1637 1707 1763 1794 1941 2105 2142 2234

MRJ 0530 1202 1300 1353

MSC 2094

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

NLV 1998

NMA 1697 1732

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

NVR 2211 2216 2410

NWS 1219 1233 1276 1843

OAW 1886

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

0811 0835 0912 0916 0963 1008 1482 1509

OZW 0429 1922

PIA 2155 2212

PIC 2331 2340

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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

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SERVICE BULLETIN

OPERATOR MSN

RCT 0466 1017

RFJ 0814

RJD 1618

RYW 0569

RZO 0795 2011 2390

SAI 0542 0877 1497 2027

SAS 1183 1383 1587 1619 1642 1675 1798 1807 1817 1848

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

2028 2064 2076 2369 2373 2464 2474 2618 2641

SDM 0427 0649 1130 1200 1379 1488 1560 1578 1654 1657 1679 1743

1753 1761 1767 1851 1863 1876 1890 2151 2163

SFW 0734 0994 1018

SGG 0799 0879

SHJ 0910

SHU 2222 2243

SKU 0179 0406 0447 1400 1523

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

SND 1880 1999

SNX 0289

SOL 0302

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

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

2327 2349

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

TAI 1066 1334 1598 1625 1952 2282 2301 2339

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

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

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

1187 1479 1700

TBJ 1485

TBZ 0361 0362 0405

TCW 1787 1929 1975 2114

TCX 0677 1006 1238 1250 2060

THY 1002 1856 1909 1996 2156 2164

TNA 0538 0555 0606 0731 0746 0791 0822

TVS 2180

TXP 0607 0611 0617

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SERVICE BULLETIN

OPERATOR MSN

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

UJX 0733 1213

ULG 0308

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

2482 2570 2595 2613 2615 2630 2669 2690

VIV 2157 2210

VKG 1881 1887 1889 1921 1932 1954 1960 1972

VLE 1226

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

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

2479 2589

VLK 0422

VOI 2204

VRE 1429

VVC 1306 1454 1564 1725 1757 1867

WGT 1212

WHT 0548 1256 1723 2118

WRC 0235 0645 0781 1869 2462 2682

WZZ 1834 1892 1902

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0029 0045 0046 0047 0049 0050 0051 0052 0053 0054 0055

0056 0057 0059 0064 0065 0066 0067 0068 0069 0070 0071

0072 0073 0074 0075 0076 0077 0078 0080 0081 0082 0083

0084 0085 0086 0087 0088 0090 0093 0094 0095 0096 0099

0104 0110 0111 0112 0113 0114 0115 0116 0117 0118 0119

0121 0122 0123 0124 0125 0126 0127 0135 0137 0138 0140

0141 0142 0147 0148 0149 0150 0152 0153 0154 0157 0158

0159 0160 0161 0162 0164 0165 0166 0167 0168 0171 0172

0173 0174 0175 0176 0178 0179 0181 0182 0183 0185 0189

0190 0192 0194 0195 0197 0198 0199 0200 0201 0202 0203

0205 0206 0207 0208 0209 0210 0211 0212 0213 0214 0216

0217 0218 0219 0220 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 0384 0385 0386 0387 0388 0390 0391 0393

0395 0396 0398 0399 0400 0401 0402 0403 0404 0405 0406

0407 0408 0409 0410 0412 0413 0414 0415 0416 0417 0418

0419 0420 0421 0422 0423 0424 0426 0427 0428 0429 0430

0431 0432 0434 0435 0436 0438 0439 0441 0442 0444 0445

0447 0448 0449 0450 0451 0452 0454 0455 0456 0457 0458

0459 0460 0462 0463 0464 0465 0466 0468 0469 0470 0471

0472 0473 0474 0475 0476 0477 0479 0480 0482 0483 0484

0485 0486 0487 0488 0489 0490 0491 0492 0493 0494 0495

0496 0497 0498 0499 0500 0501 0502 0503 0504 0505 0506

0507 0508 0509 0510 0511 0512 0513 0514 0515 0516 0517

0518 0519 0520 0521 0522 0523 0524 0525 0526 0527 0528

0529 0530 0531 0532 0533 0534 0535 0537 0538 0539 0540

0541 0542 0543 0544 0545 0546 0548 0549 0550 0551 0552

0553 0554 0555 0556 0557 0558 0559 0560 0561 0562 0563

0564 0565 0566 0567 0568 0569 0570 0571 0572 0573 0574

0575 0576 0577 0578 0579 0580 0581 0582 0583 0584 0585

0586 0587 0588 0589 0591 0592 0593 0594 0595 0596 0597

0598 0599 0600 0603 0604 0605 0606 0607 0608 0609 0610

0611 0612 0613 0614 0616 0617 0618 0619 0620 0621 0622

0623 0625 0627 0629 0630 0631 0633 0634 0635 0636 0637

0638 0639 0640 0641 0642 0643 0644 0645 0646 0647 0648

0649 0650 0651 0652 0653 0654 0655 0656 0657 0658 0659

0660 0661 0662 0663 0664 0665 0666 0667 0668 0669 0670

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

001

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

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SERVICE BULLETIN

MSN CONFIGURATION

0704 0705 0706 0707 0709 0711 0712 0713 0714 0715 0716

0717 0718 0719 0720 0721 0722 0723 0724 0725 0726 0727

0728 0729 0730 0731 0732 0733 0734 0735 0736 0737 0738

0739 0740 0741 0742 0743 0744 0745 0746 0747 0748 0749

0750 0751 0752 0754 0755 0756 0757 0758 0759 0760 0761

0762 0763 0764 0765 0766 0767 0768 0769 0770 0771 0772

0773 0774 0775 0776 0777 0778 0779 0780 0781 0782 0783

0784 0785 0786 0787 0788 0790 0791 0792 0793 0794 0795

0796 0797 0798 0799 0800 0801 0802 0803 0804 0805 0806

0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817

0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828

0829 0830 0831 0832 0833 0834 0835 0836 0837 0838 0839

0840 0841 0842 0843 0844 0845 0846 0847 0848 0849 0850

0851 0852 0853 0854 0855 0856 0857 0858 0859 0860 0861

0862 0863 0864 0865 0866 0867 0868 0869 0870 0871 0872

0873 0874 0875 0876 0877 0878 0879 0880 0881 0882 0883

0884 0885 0886 0887 0888 0889 0890 0891 0892 0893 0894

0895 0896 0897 0898 0899 0900 0901 0902 0903 0904 0905

0906 0907 0908 0909 0910 0911 0912 0913 0914 0915 0916

0917 0918 0919 0920 0921 0922 0923 0924 0925 0926 0927

0928 0929 0930 0931 0932 0933 0934 0935 0936 0937 0938

0939 0940 0941 0942 0943 0944 0945 0946 0947 0948 0949

0950 0951 0952 0953 0954 0955 0957 0958 0959 0960 0961

0962 0963 0964 0965 0966 0967 0968 0969 0970 0971 0972

0973 0974 0975 0976 0977 0978 0979 0980 0981 0982 0983

0984 0985 0986 0987 0988 0989 0990 0991 0992 0993 0994

0995 0996 0997 0998 0999 1000 1001 1002 1003 1004 1005

1006 1007 1008 1009 1010 1011 1012 1013 1014 1015 1016

1017 1018 1019 1020 1021 1022 1023 1024 1025 1026 1027

1028 1029 1030 1031 1032 1033 1034 1035 1036 1037 1038

1039 1040 1041 1042 1043 1045 1046 1047 1048 1049 1050

1051 1052 1053 1054 1055 1056 1057 1058 1059 1060 1061

1062 1063 1064 1065 1066 1067 1068 1069 1070 1071 1072

1073 1074 1075 1076 1077 1078 1079 1080 1081 1082 1083

1084 1085 1086 1087 1088 1089 1090 1091 1092 1093 1094

1095 1096 1097 1098 1099 1100 1101 1102 1103 1104 1105

1106 1107 1108 1109 1110 1111 1112 1114 1115 1116 1117

1118 1119 1120 1121 1122 1123 1124 1125 1126 1127 1128

1129 1130 1131 1132 1133 1134 1135 1136 1137 1138 1139

1140 1141 1142 1143 1144 1145 1146 1147 1148 1149 1150

1151 1152 1153 1154 1155 1156 1157 1158 1159 1160 1161

1162 1163 1164 1165 1166 1167 1168 1169 1170 1171 1172

1173 1174 1175 1176 1177 1178 1179 1180 1181 1182 1183

1184 1185 1187 1188 1189 1190 1191 1192 1193 1194 1195

1196 1197 1198 1199 1200 1201 1202 1203 1204 1205 1206

1207 1208 1209 1210 1211 1212 1213 1214 1215 1216 1217

1219 1220 1221 1222 1223 1224 1225 1226 1227 1228 1229

1230 1231 1232 1233 1234 1235 1236 1237 1238 1239 1240

1241 1242 1243 1244 1245 1246 1247 1248 1249 1250 1251

1252 1253 1254 1255 1256 1257 1258 1259 1260 1261 1262

1263 1264 1265 1266 1267 1268 1269 1270 1271 1272 1273

001

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 11

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SERVICE BULLETIN

MSN CONFIGURATION

1274 1275 1276 1277 1279 1280 1281 1282 1283 1284 1285

1286 1287 1288 1289 1290 1291 1292 1293 1294 1295 1296

1297 1298 1299 1300 1301 1302 1303 1304 1305 1306 1307

1308 1309 1310 1311 1312 1313 1314 1315 1316 1317 1318

1319 1320 1321 1322 1323 1324 1325 1326 1327 1328 1329

1330 1331 1332 1334 1335 1336 1337 1338 1339 1340 1341

1342 1343 1344 1345 1346 1347 1348 1349 1350 1351 1352

1353 1354 1355 1356 1357 1358 1359 1360 1361 1362 1363

1364 1365 1366 1367 1368 1369 1370 1371 1372 1373 1375

1376 1377 1378 1379 1380 1381 1382 1383 1384 1385 1386

1387 1388 1389 1390 1391 1392 1393 1394 1395 1396 1397

1398 1399 1400 1401 1402 1403 1404 1405 1406 1407 1408

1409 1410 1411 1412 1413 1414 1415 1416 1417 1418 1419

1420 1421 1422 1423 1424 1425 1426 1427 1428 1429 1430

1431 1432 1433 1434 1435 1436 1437 1438 1439 1440 1441

1442 1443 1444 1445 1446 1447 1448 1449 1450 1451 1452

1453 1454 1455 1456 1457 1458 1459 1460 1461 1462 1463

1465 1466 1467 1468 1469 1470 1471 1472 1473 1474 1475

1476 1477 1478 1479 1480 1481 1482 1483 1484 1485 1486

1487 1488 1489 1490 1491 1492 1493 1494 1495 1496 1497

1498 1499 1500 1501 1502 1503 1504 1505 1506 1507 1508

1509 1510 1511 1512 1513 1514 1515 1516 1517 1518 1519

1520 1521 1522 1523 1524 1525 1526 1527 1528 1529 1530

1531 1532 1533 1534 1535 1536 1537 1538 1539 1540 1541

1542 1543 1544 1545 1546 1547 1548 1549 1550 1551 1552

1553 1554 1555 1556 1557 1558 1559 1560 1561 1562 1563

1564 1565 1566 1567 1568 1569 1570 1571 1572 1573 1574

1575 1576 1577 1578 1579 1580 1581 1582 1583 1584 1585

1586 1587 1588 1589 1590 1591 1592 1593 1594 1595 1596

1597 1598 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

001

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SERVICE BULLETIN

MSN CONFIGURATION

1847 1848 1849 1850 1851 1852 1853 1854 1855 1856 1857

1858 1859 1860 1861 1862 1863 1864 1865 1866 1867 1868

1869 1870 1871 1872 1873 1874 1875 1876 1877 1878 1879

1880 1881 1882 1883 1884 1885 1886 1887 1888 1889 1890

1891 1892 1893 1894 1895 1896 1897 1898 1899 1900 1901

1902 1903 1904 1905 1906 1907 1908 1909 1910 1911 1912

1913 1914 1915 1916 1917 1918 1920 1921 1922 1923 1924

1925 1926 1927 1928 1929 1931 1932 1933 1934 1935 1936

1937 1938 1940 1941 1942 1943 1944 1945 1946 1947 1948

1949 1950 1951 1952 1953 1954 1955 1956 1957 1958 1959

1960 1961 1962 1963 1964 1965 1966 1967 1968 1969 1970

1971 1972 1973 1974 1975 1976 1977 1978 1979 1980 1981

1982 1983 1984 1986 1987 1988 1989 1990 1993 1994 1995

1996 1997 1998 1999 2000 2001 2002 2003 2004 2005 2006

2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 2018

2019 2020 2021 2022 2023 2024 2026 2027 2028 2029 2030

2031 2032 2033 2034 2036 2038 2039 2040 2041 2042 2044

2045 2046 2047 2048 2049 2052 2054 2055 2056 2057 2058

2060 2061 2063 2064 2065 2066 2067 2068 2069 2070 2072

2073 2074 2075 2076 2077 2078 2079 2080 2082 2083 2084

2085 2086 2087 2088 2089 2090 2091 2092 2093 2094 2095

2096 2097 2098 2099 2101 2102 2103 2104 2105 2106 2107

2108 2110 2112 2113 2114 2115 2116 2117 2118 2121 2122

2123 2124 2125 2126 2127 2128 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 2171 2172 2173 2174 2175 2177 2178 2179 2180

2182 2183 2185 2187 2188 2190 2191 2192 2193 2194 2195

2197 2198 2199 2200 2201 2202 2203 2204 2205 2206 2207

2208 2209 2210 2211 2212 2215 2216 2217 2219 2220 2221

2222 2223 2225 2226 2227 2229 2231 2232 2233 2234 2235

2236 2237 2238 2239 2240 2241 2242 2243 2244 2246 2247

2248 2250 2252 2253 2254 2255 2256 2258 2259 2260 2261

2262 2263 2264 2266 2267 2269 2270 2272 2273 2274 2275

2278 2280 2282 2284 2285 2286 2287 2288 2290 2293 2294

2295 2298 2301 2302 2303 2304 2305 2307 2309 2310 2311

2312 2313 2314 2315 2316 2318 2320 2321 2323 2324 2325

2327 2330 2331 2334 2336 2337 2339 2340 2341 2342 2343

2345 2347 2348 2349 2351 2352 2356 2357 2359 2363 2364

2365 2368 2369 2371 2372 2373 2374 2381 2384 2386 2388

2389 2390 2391 2393 2397 2399 2405 2407 2408 2409 2410

2411 2415 2416 2421 2422 2425 2426 2428 2429 2430 2432

2435 2437 2447 2449 2451 2454 2458 2459 2461 2462 2464

2466 2472 2474 2478 2479 2480 2482 2486 2488 2489 2491

2493 2494 2498 2499 2504 2505 2507 2508 2509 2510 2517

2520 2521 2525 2530 2532 2534 2535 2536 2542 2543 2545

2547 2549 2551 2559 2562 2563 2568 2570 2574 2577 2579

2580 2583 2589 2591 2595 2597 2599 2606 2613 2614 2615

2618 2627 2630 2635 2639 2640 2641 2643 2647 2652 2667

2669 2671 2682 2690 2710 2725 2755 2775 2781 2802 2805

001

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 13

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SERVICE BULLETIN

MSN CONFIGURATION

2814 2815 2819 2832 2839 2847 2848 2871 2880 2890 2900

2901 2940 2945 2948 2969 2970 2977 2992 3020 3029 3039

3072 3091 3104 3106 3119 3144 3150 3190 3195 3200 3226

3228 3250 3258 3263 3269 3287 3311 3342 3348

001

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 321415D01R00 1

Equipment BFEA01 1 (1)

Equipment BFEA02 1 (2)

NOTE (1): Equipment BFEA01 is applicable for TASK 321415-831-801 001

Modification of the BDDV (FIN 2577GM) as per VSB on Aircraft and for

TASK 321415-831-802 001 Modification of the BDDV (FIN 2577GM) as

per VSB in Shop .

NOTE (2): Equipment BFEA02 is applicable for TASK 321415-831-803 001

Modification by Replacement of the BDDV (FIN 2577GM) on Aircraft .

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

One operator experienced a dual loss of braking: loss of normal braking (failure

detection on normal braking circuit) and loss of alternate braking. The aircraft was

stopped with full reversers and Parking Brake.

The Brake Dual Distribution Valve (BDDV) cover was found filled with ice, thus

preventing to command the alternate braking with the pedals.

Investigation performed on the BDDV revealed that the cover seal was damaged and did

not ensure the sealing efficiency.

Breathing and/or water projection introduce water in the cover.

Due to low temperature reached in flight, the water is freezing and blocks the BDDV

rocker arm movement.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 14

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SERVICE BULLETIN

(2) Objective/Action

This Service Bulletin is published to advise all operators of A320 family aircraft of the

issue of MESSIER-BUGATTI-DOWTY Service Bulletin No. A25434-32-3374.

This Service Bulletin aims at shortening the drain tube to a length of 80 ± 5 mm (3.15 ±

0.20 in.) and removing the end plug.

(3) Advantages

Accomplishment of this Service Bulletin will avoid the freezing of the water by ensuring

the continuous draining of the water.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

NOTE: To accomplish this Service Bulletin, three possibilities are available:

- Either modify the BDDV (FIN 2577GM) as described in TASK

321415-831-801 001 Modification of the BDDV (FIN 2577GM) as per

VSB on Aircraft .

- Or modify it as described in TASK 321415-831-802 001 Modification of

the BDDV (FIN 2577GM) as per VSB in Shop .

- Or replace it as described in TASK 321415-831-803 001 Modification by

Replacement of the BDDV (FIN 2577GM) on Aircraft .

NOTE: For each possibilities, a check of presence of water and hydraulic fluid in the

drain hose must be done before the modification.

To accomplish this Service Bulletin it is necessary to :

Task 321415-831-801-001: Modification of the BDDV (FIN 2577GM) as per VSB on Aircraft

(1) Remove the Drain Hose Supports for the Emergency Brake Dual Distribution Valve

(2) Do a Check of Presence of Water or Hydraulic Fluid

(3) Modify the BDDV (FIN 2577GM) and the Drain Hose in accordance with VSB on

Aircraft

(4) Install the Hydraulic Pipe Clamp Fasteners

Task 321415-831-802-001: Modification of the BDDV (FIN 2577GM) as per VSB in Shop

(1) Remove the Drain Hose Supports for the Emergency Brake Dual Distribution Valve

(2) Do a Check of Presence of Water or Hydraulic Fluid

(3) Remove the BDDV (FIN 2577GM) and the Drain Hose

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

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(4) Modify the BDDV (FIN 2577GM) and the Drain Hose in accordance with VSB on

Bench

(5) Install the modified BDDV (FIN 2577GM) and the Drain Hose

(6) Install the Hydraulic Pipe Clamp Fasteners

Task 321415-831-803-001: Modification by Replacement of the BDDV (FIN 2577GM) on

Aircraft

(1) Remove the Drain Hose Supports for the Emergency Brake Dual Distribution Valve

(2) Do a Check of Presence of Water or Hydraulic Fluid

(3) Replace the BDDV (FIN 2577GM) and the Drain Hose

(4) Install the Hydraulic Pipe Clamp Fasteners

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available, but must not exceed 24 months from SB

original issue date.

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 date given above but reference should be made to the AD for

confirmation of the mandated accomplishment timescale.

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.

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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 321415-831-801-001: Modification of the BDDV (FIN 2577GM) as per VSB on Aircraft

Get Access 0.50

On Aircraft

Remove the Drain Hose Supports for the Emergency

Brake Dual Distribution Valve

1.00

Do a Check of Presence of Water or Hydraulic Fluid 0.50

Install the Hydraulic Pipe Clamp Fasteners 0.50

Tests 0.25

Close-Up 0.50

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

Additional manhours related to Vendor SB; refer to:

Modify the BDDV (FIN 2577GM) and the Drain Hose in

accordance with VSB on Aircraft

MESSIER-BUGATTI-DOWTY

Service Bulletin No.

A25434-32-3374

Task 321415-831-802-001: Modification of the BDDV (FIN 2577GM) as per VSB in Shop

Get Access 0.50

On Aircraft

Remove the Drain Hose Supports for the Emergency

Brake Dual Distribution Valve

1.00

Do a Check of Presence of Water or Hydraulic Fluid 0.50

Remove the BDDV (FIN 2577GM) and the Drain Hose 1.00

Install the modified BDDV (FIN 2577GM) and the Drain

Hose

1.00

Install the Hydraulic Pipe Clamp Fasteners 0.50

Tests 0.25

Close-Up 0.50

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 5.25

Additional manhours related to Vendor SB; refer to:

Modify the BDDV (FIN 2577GM) and the Drain Hose in

accordance with VSB on Bench

MESSIER-BUGATTI-DOWTY

Service Bulletin No.

A25434-32-3374

Task 321415-831-803-001: Modification by Replacement of the BDDV (FIN 2577GM) on Aircraft

Get Access 0.50

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Task 321415-831-803-001: Modification by Replacement of the BDDV (FIN 2577GM) on Aircraft

On Aircraft

Remove the Drain Hose Supports for the Emergency

Brake Dual Distribution Valve

1.00

Do a Check of Presence of Water or Hydraulic Fluid 0.50

Replace the BDDV (FIN 2577GM) and the Drain Hose 2.00

Install the Hydraulic Pipe Clamp Fasteners 0.50

Tests 0.25

Close-Up 0.50

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 5.25

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 12-34-24

20-21-11 32-12-00 32-43-00

32-43-14

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

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

Vendor Service Bulletin (VSB) MESSIER-BUGATTI-DOWTY

Service Bulletin No.

A25434-32-3374

K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 29-15-03 32-43-03

L. INTERCHANGEABILITY/MIXABILITY

The interchangeability/mixability possibilities are for new or modified parts introduced by the

accomplishment of this Service Bulletin.

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

BDDV A25434005-101A A25434005-1010A 01 Not

Applicable

BDDV A25434005-201A A25434005-2010A 01 Not

Applicable

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DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

BDDV A25434005-301A A25434005-3010A 01 Not

Applicable

BDDV A25434006-101A A25434006-1010A 01 Not

Applicable

BDDV A25434006-3A A25434006-3000A 01 Not

Applicable

BDDV A25434005-301B A25434005-3010B 01 Not

Applicable

BDDV A25434005-401B A25434005-4010B 01 Not

Applicable

BDDV A25434006-101 A25434006-1010 01 Not

Applicable

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

M. SPARES

BDDV A25434005-101A

BDDV A25434005-201A

BDDV A25434005-301A

BDDV A25434005-301B

BDDV A25434005-401B

BDDV A25434006-101

BDDV A25434006-101A

BDDV A25434006-3A

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This Page Intentionally Left Blank

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Customers with aircraft shown in the effectivity of this Service Bulletin should send a

purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:

Kit 321415D01R00 AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 2590

For ordering by E-mail: ifd.spare@airbus.com

Modification of removed equipment should be negotiated directly with MESSIERBUGATTI-DOWTY as per instructions given in Service Bulletin No. A25434-32-3374.

Equipment BFEA01 MESSIER-BUGATTI-DOWTY

Inovel Parc Sud

BP 40

78140 VELIZY-VILLACOUBLAY

FRANCE

Tel: +33(0)1 46 29 81 00

Fax: +33(0)1 46 83 02 00

Or, vendor parts are to be procured from:

Equipment BFEA02 MESSIER-BUGATTI-DOWTY

Inovel Parc Sud

BP 40

78140 VELIZY-VILLACOUBLAY

FRANCE

Tel: +33(0)1 46 29 81 00

Fax: +33(0)1 46 83 02 00

(2) Price and Availability

Kit 321415D01R00

Cost 26.00 USD

Availability 60 calendar days from receipt of order

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

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

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

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

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

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

Equipment BFEA01

Refer to the MESSIER-BUGATTI-DOWTY Service Bulletin No. A25434-32-3374 for the

equipment modification sales terms.

Equipment BFEA02

Procurement terms for the equipment must be negotiated with the equipment supplier.

B. INDUSTRY SUPPORT INFORMATION

For Kit 321415D01R00, AIRBUS will not provide industry support for accomplishment of this

Service Bulletin.

For Equipment BFEA01, refer to the MESSIER-BUGATTI-DOWTY Service Bulletin No.

A25434-32-3374 for the industry support terms of the Vendor Service Bulletin parts and labor.

For Equipment BFEA02, industry support terms for the equipment must be negotiated with

the equipment supplier.

C. LIST OF COMPONENTS

Kit 321415D01R00

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

NOTES

2 NAS1726C3E 1 NUT

4 NAS1149D0332K 1 WASHER

12 NAS6703U19 1 BOLT

NOTE: If you find part numbers of hardware components in the related kit(s) which

you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,

refer to Standards Manual (SM). The SM will give you the correct part number

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

To accomplish this Service Bulletin it is necessary to use the expendable parts listed in

the subsequent referenced AMM Task 32-43-14-400-001.

(2) Components

None

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(3) Equipment

Equipment BFEA01

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

NOTES

A25434005-1010A 3 BDDV A25434005-101A 01

A25434005-2010A 3 BDDV A25434005-201A 01

A25434005-3010A 3 BDDV A25434005-301A 01

A25434005-3010B 3 BDDV A25434005-301B 01

A25434005-4010B 3 BDDV A25434005-401B 01

A25434006-1010 3 BDDV A25434006-101 01

A25434006-1010A 3 BDDV A25434006-101A 01

A25434006-3000A 3 BDDV A25434006-3A 01

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

Equipment BFEA02

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

NOTES

A25434005-1010A 1 BDDV A25434005-101A 01

A25434005-2010A 1 BDDV A25434005-201A 01

A25434005-3010A 1 BDDV A25434005-301A 01

A25434005-3010B 1 BDDV A25434005-301B 01

A25434005-4010B 1 BDDV A25434005-401B 01

A25434006-1010 1 BDDV A25434006-101 01

A25434006-1010A 1 BDDV A25434006-101A 01

A25434006-3000A 1 BDDV A25434006-3A 01

NOTE: For definitions of interchangeability codes in column INT., refer to ATA

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

NOTE: For TASK 321415-831-801 001 Modification of the BDDV (FIN 2577GM) as

per VSB on Aircraft and TASK 321415-831-802 001 Modification of the BDDV

(FIN 2577GM) as per VSB in Shop , parts are re-identified in accordance with

the MESSIER-BUGATTI-DOWTY Service Bulletin No. A25434-32-3374.

F. TOOLING

(1) Tooling - Price and Availability

None

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(2) Tools

NOTE: For TASK 321415-831-801 001 Modification of the BDDV (FIN 2577GM)

as per VSB on Aircraft and TASK 321415-831-802 001 Modification of

the BDDV (FIN 2577GM) as per VSB in Shop and to accomplish this

Service Bulletin, it is necessary to use the tools defined in MESSIERBUGATTI-DOWTY Service Bulletin A25434-32-3374.

(3) Special Tools

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 321415-831-801-001 - Modification of the BDDV (FIN 2577GM) as per VSB on Aircraft

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 mandated or expected to be mandated by an Airworthiness

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

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

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

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

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

back into a serviceable condition.

Task Associated Data

Zone

744

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Modified FIN

2577GM

Access

Door Right MLG

Manpower

TOTAL MANHOURS 3.25

ELAPSED TIME (HOURS) 3.25

Additional manhours related to Vendor SB; refer to:

MESSIER-BUGATTI-DOWTY Service Bulletin No. A25434-32-3374

A. GENERAL

(1) Subtask 321415-910-005-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-40-00

51-42-00

51-43-00

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

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

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

(d) To torque tighten the standard threaded fasteners, refer to AMM 20-21-11, task

911-001.

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

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

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

Part" column.

(g) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(h) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

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(2) Subtask 321415-839-001-001 - 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 321415-941-006-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-802

Task 32-43-14-000-001

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 are closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin available

- All circuit breakers are in closed position

- All controls in NORM, AUTO, OFF position.

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

12-34-24-869-802.

(b) Do the Job Set-up procedure as specified in the removal of the BDDV (FIN

2577GM), refer to AMM Task 32-43-14-000-001.

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C. PROCEDURE

(1) Subtask 321415-020-201-001 - Remove the Drain Hose Supports for the Emergency

Brake Dual Distribution Valve

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Fig. A-GBAAA

Modification of the Brake Dual

Distribution Valve Drain Pipe Supports

Sheet 01

Sheet 02

(a) Remove the Fasteners and P-Clamps, for the Drain Hose, Item (1).

1 As shown in Fig. A-GBAAA Sheet 01, View B, remove:

1 Nut Item (7) Discard

1 Bolt Item (9) Discard

1 Washer Item (8) Discard

1 P-Clamp Item (10) Discard

1 P-Clamp Item (11) Discard

1 Nut Item (2) Discard

1 Bolt Item (5) Discard

1 Washer Item (4) Discard

1 Spacer Item (3) Discard

1 P-Clamp Item (6) Discard

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(2) Subtask 321415-210-001-001 - Do a Check of Presence of Water or Hydraulic Fluid

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-43-14-000-001

Task 32-43-14-200-003

Task 32-43-14-400-001

(a) Drain the contents of the drain hose into a container.

(b) If presence of ice in the cover is expected, do a check for ice:

1 If ice found, remove the ice and do the procedure for corrosion inspection,

refer to AMM Task 32-43-14-200-003.

NOTE: If water found in the cover, it can become ice in flight or in cold

weather conditions. This can cause a problem with the draining

of the Brake Dual Distribution Valve (BDDV)

2 If corrosion found in a not permitted area, replace the BDDV 2577GM,

refer to AMM Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and

"corrosion" must be mentioned as the reason for removal.

(c) If water found in the drain hose, do the procedure for corrosion inspection, refer to

AMM Task 32-43-14-200-003.

1 If corrosion found in a not permitted area, replace the BDDV 2577GM,

refer to AMM Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and

"corrosion" must be mentioned as the reason for removal.

(d) If hydraulic fluid found in the drain hose, replace the BDDV 2577GM, refer to AMM

Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and "hydraulic leakage"

must be mentioned as the reason for removal.

(3) Subtask 321415-831-006-001 - Modify the BDDV (FIN 2577GM) and the Drain Hose

in accordance with VSB on Aircraft

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

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Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

A25434005-1010A 1 BDDV

A25434005-2010A 1 BDDV

A25434005-3010A 1 BDDV

A25434005-3010B 1 BDDV

A25434005-4010B 1 BDDV

A25434006-1010 1 BDDV

A25434006-1010A 1 BDDV

A25434006-3000A 1 BDDV

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

Vendor Service Bulletin (VSB) MESSIER-BUGATTI-DOWTY

A25434-32-3374

(a) Modify the BDDV (FIN 2577GM) as per instruction given in MESSIER-BUGATTIDOWTY Service Bulletin No. A25434-32-3374:

FIN 2577GM

1 BDDV A25434005-101A

Becomes

FIN 2577GM

1 BDDV A25434005-1010A

or

FIN 2577GM

1 BDDV A25434005-201A

Becomes

FIN 2577GM

1 BDDV A25434005-2010A

or

FIN 2577GM

1 BDDV A25434005-301A

Becomes

FIN 2577GM

1 BDDV A25434005-3010A

or

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FIN 2577GM

1 BDDV A25434005-301B

becomes

FIN 2577GM

1 BDDV A25434005-3010B

or

FIN 2577GM

1 BDDV A25434005-401B

Becomes

FIN 2577GM

1 BDDV A25434005-4010B

or

FIN 2577GM

1 BDDV A25434006-101

becomes

FIN 2577GM

1 BDDV A25434006-1010

or

FIN 2577GM

1 BDDV A25434006-101A

Becomes

FIN 2577GM

1 BDDV A25434006-1010A

or

FIN 2577GM

1 BDDV A25434006-3A

Becomes

FIN 2577GM

1 BDDV A25434006-3000A

(4) Subtask 321415-420-201-001 - Install the Hydraulic Pipe Clamp Fasteners

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 31

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 321415D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1726C3E 1 NUT

4 NAS1149D0332K 1 WASHER

12 NAS6703U19 1 BOLT

References

Fig. A-GBAAA

Modification of the Brake Dual

Distribution Valve Drain Pipe Supports

Sheet 01

Sheet 02

(a) Install the new Fasteners.

1 As shown in Fig. A-GBAAA Sheet 02, View C, install:

1 Bolt NAS6703U19 Item 12

1 Washer NAS1149D0332K Item 4

1 Nut NAS1726C3E Item 2

D. TEST

(1) Subtask 321415-700-001-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-43-00-710-001

Task 32-43-14-400-001

(a) Job Set-up:

1 Remove the Safety clip(s) and/or tag(s) and close/unlock this (these) circuit

breaker(s) as specified after the Installation of the Dual Valve Alternate Brake

Distribution, refer to AMM Task 32-43-14-400-001.

(b) Procedure:

1 Do the test procedure as specified after the Installation of the Dual Valve

Alternate Brake Distribution, refer to AMM Task 32-43-14-400-001.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 32

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E. CLOSE-UP

(1) Subtask 321415-942-005-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-12-00-410-001

Task 32-43-14-400-001

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

equipment.

(b) Do the Close-up procedure as specified after the installation of the BDDV (FIN

2577GM), refer to AMM Task 32-43-14-400-001.

(c) Put the aircraft back to its initial configuration.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 33

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This Page Intentionally Left Blank

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 34

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Task 321415-831-802-001 - Modification of the BDDV (FIN 2577GM) as per VSB in Shop

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 mandated or expected to be mandated by an Airworthiness

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

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

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

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

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

back into a serviceable condition.

Task Associated Data

Zone

744

Modified FIN

2577GM

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 35

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Access

Door Right MLG

Manpower

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 5.25

Additional manhours related to Vendor SB; refer to:

MESSIER-BUGATTI-DOWTY Service Bulletin No. A25434-32-3374

A. GENERAL

(1) Subtask 321415-910-006-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-40-00

51-42-00

51-43-00

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

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

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

(d) To torque tighten the standard threaded fasteners, refer to AMM 20-21-11, task

911-001.

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

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

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

Part" column.

(g) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(h) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 36

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(2) Subtask 321415-839-002-001 - 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 321415-941-007-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-802

Task 32-43-14-000-001

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 are closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin available

- All circuit breakers are in closed position

- All controls in NORM, AUTO, OFF position.

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

12-34-24-869-802.

(b) Do the Job Set-up procedure as specified in the removal of the BDDV (FIN

2577GM), refer to AMM Task 32-43-14-000-001.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 37

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C. PROCEDURE

(1) Subtask 321415-020-202-001 - Remove the Drain Hose Supports for the Emergency

Brake Dual Distribution Valve

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Fig. A-GBAAA

Modification of the Brake Dual

Distribution Valve Drain Pipe Supports

Sheet 01

Sheet 02

(a) Remove the Fasteners and P-Clamps, for the Drain Hose, Item (1).

1 As shown in Fig. A-GBAAA Sheet 01, View B, remove:

1 Nut Item (7) Discard

1 Bolt Item (9) Discard

1 Washer Item (8) Discard

1 P-Clamp Item (10) Discard

1 P-Clamp Item (11) Discard

1 Nut Item (2) Discard

1 Bolt Item (5) Discard

1 Washer Item (4) Discard

1 Spacer Item (3) Discard

1 P-Clamp Item (6) Discard

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 38

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(2) Subtask 321415-210-002-001 - Do a Check of Presence of Water or Hydraulic Fluid

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-43-14-000-001

Task 32-43-14-200-003

Task 32-43-14-400-001

(a) Drain the contents of the drain hose into a container.

(b) If presence of ice in the cover is expected, do a check for ice:

1 If ice found, remove the ice and do the procedure for corrosion inspection,

refer to AMM Task 32-43-14-200-003.

NOTE: If water found in the cover, it can become ice in flight or in cold

weather conditions. This can cause a problem with the draining

of the Brake Dual Distribution Valve (BDDV)

2 If corrosion found in a not permitted area, replace the BDDV 2577GM,

refer to AMM Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and

"corrosion" must be mentioned as the reason for removal.

(c) If water found in the drain hose, do the procedure for corrosion inspection, refer to

AMM Task 32-43-14-200-003.

1 If corrosion found in a not permitted area, replace the BDDV 2577GM,

refer to AMM Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and

"corrosion" must be mentioned as the reason for removal.

(d) If hydraulic fluid found in the drain hose, replace the BDDV 2577GM, refer to AMM

Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and "hydraulic leakage"

must be mentioned as the reason for removal.

(3) Subtask 321415-831-007-001 - Remove the BDDV (FIN 2577GM) and the Drain Hose

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 39

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 32-43-14-000-001

(a) Remove the BDDV (FIN 2577GM):

Refer to AMM Task 32-43-14-000-001

FIN 2577GM

1 BDDV A25434005-101A

or

FIN 2577GM

1 BDDV A25434005-201A

or

FIN 2577GM

1 BDDV A25434005-301A

or

FIN 2577GM

1 BDDV A25434005-301B

or

FIN 2577GM

1 BDDV A25434005-401B

or

FIN 2577GM

1 BDDV A25434006-101

or

FIN 2577GM

1 BDDV A25434006-101A

or

FIN 2577GM

1 BDDV A25434006-3A

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 40

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(4) Subtask 321415-831-003-001 - Modify the BDDV (FIN 2577GM) and the Drain Hose

in accordance with VSB on Bench

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

A25434005-1010A 1 BDDV

A25434005-2010A 1 BDDV

A25434005-3010A 1 BDDV

A25434005-3010B 1 BDDV

A25434005-4010B 1 BDDV

A25434006-1010 1 BDDV

A25434006-1010A 1 BDDV

A25434006-3000A 1 BDDV

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

Vendor Service Bulletin (VSB) MESSIER-BUGATTI-DOWTY

A25434-32-3374

(a) Modify the BDDV (FIN 2577GM) as per instruction given in MESSIER-BUGATTIDOWTY Service Bulletin No. A25434-32-3374:

FIN 2577GM

1 BDDV A25434005-101A

Becomes

FIN 2577GM

1 BDDV A25434005-1010A

or

FIN 2577GM

1 BDDV A25434005-201A

Becomes

FIN 2577GM

1 BDDV A25434005-2010A

or

FIN 2577GM

1 BDDV A25434005-301A

Becomes

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 41

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FIN 2577GM

1 BDDV A25434005-3010A

or

FIN 2577GM

1 BDDV A25434005-301B

becomes

FIN 2577GM

1 BDDV A25434005-3010B

or

FIN 2577GM

1 BDDV A25434005-401B

Becomes

FIN 2577GM

1 BDDV A25434005-4010B

or

FIN 2577GM

1 BDDV A25434006-101

becomes

FIN 2577GM

1 BDDV A25434006-1010

or

FIN 2577GM

1 BDDV A25434006-101A

Becomes

FIN 2577GM

1 BDDV A25434006-1010A

or

FIN 2577GM

1 BDDV A25434006-3A

Becomes

FIN 2577GM

1 BDDV A25434006-3000A

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 42

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(5) Subtask 321415-400-001-001 - Install the modified BDDV (FIN 2577GM) and the

Drain Hose

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

A25434005-1010A 1 BDDV

A25434005-2010A 1 BDDV

A25434005-3010A 1 BDDV

A25434005-3010B 1 BDDV

A25434005-4010B 1 BDDV

A25434006-1010 1 BDDV

A25434006-1010A 1 BDDV

A25434006-3000A 1 BDDV

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

Aircraft Maintenance Manual (AMM) Task 32-43-14-400-001

(a) Install the BDDV (FIN 2577GM):

Refer to AMM Task 32-43-14-400-001

FIN 2577GM

1 BDDV A25434005-1010A

or

FIN 2577GM

1 BDDV A25434005-2010A

or

FIN 2577GM

1 BDDV A25434005-3010A

or

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 43

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FIN 2577GM

1 BDDV A25434005-3010B

or

FIN 2577GM

1 BDDV A25434005-4010B

or

FIN 2577GM

1 BDDV A25434006-1010

or

FIN 2577GM

1 BDDV A25434006-1010A

or

FIN 2577GM

1 BDDV A25434006-3000A

(6) Subtask 321415-420-202-001 - Install the Hydraulic Pipe Clamp Fasteners

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 321415D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1726C3E 1 NUT

4 NAS1149D0332K 1 WASHER

12 NAS6703U19 1 BOLT

References

Fig. A-GBAAA

Modification of the Brake Dual

Distribution Valve Drain Pipe Supports

Sheet 01

Sheet 02

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 44

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(a) Install the new Fasteners.

1 As shown in Fig. A-GBAAA Sheet 02, View C, install:

1 Bolt NAS6703U19 Item 12

1 Washer NAS1149D0332K Item 4

1 Nut NAS1726C3E Item 2

D. TEST

(1) Subtask 321415-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-43-00-710-001

Task 32-43-14-400-001

(a) Job Set-up:

1 Remove the Safety clip(s) and/or tag(s) and close/unlock this (these) circuit

breaker(s) as specified after the Installation of the Dual Valve Alternate Brake

Distribution, refer to AMM Task 32-43-14-400-001.

(b) Procedure:

1 Do the test procedure as specified after the Installation of the Dual Valve

Alternate Brake Distribution, refer to AMM Task 32-43-14-400-001.

E. CLOSE-UP

(1) Subtask 321415-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-12-00-410-001

Task 32-43-14-400-001

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

equipment.

(b) Do the Close-up procedure as specified after the installation of the BDDV (FIN

2577GM), refer to AMM Task 32-43-14-400-001.

(c) Put the aircraft back to its initial configuration.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 45

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This Page Intentionally Left Blank

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 46

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Task 321415-831-803-001 - Modification by Replacement of the BDDV (FIN 2577GM) on

Aircraft

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 mandated or expected to be mandated by an Airworthiness

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

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

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

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

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

back into a serviceable condition.

Task Associated Data

Zone

744

Modified FIN

2577GM

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 47

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Access

Door Right MLG

Manpower

TOTAL MANHOURS 5.25

ELAPSED TIME (HOURS) 5.25

A. GENERAL

(1) Subtask 321415-910-007-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

Task 20-21-11-911-001

Structural Repair Manual (SRM) 51-40-00

51-42-00

51-43-00

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

(b) For the Frame (FR) identification, refer to AMM 06-31-53, Page Block 001.

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

(d) To torque tighten the standard threaded fasteners, refer to AMM 20-21-11, task

911-001.

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

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

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

Part" column.

(g) If the length of any fastener specified in this Service Bulletin does not meet

installation standards given in SRM Chapter 51, then a fastener of the same

specification, or an approved substitute, with a length which meets the installation

standards given in SRM Chapter 51 may be used. In addition, washers may be

installed for fastener grip length in accordance with SRM Chapter 51.

(h) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(2) Subtask 321415-839-003-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 48

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B. PREPARATION

(1) Subtask 321415-941-008-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-802

Task 32-43-14-000-001

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 are closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin available

- All circuit breakers are in closed position

- All controls in NORM, AUTO, OFF position.

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

12-34-24-869-802.

(b) Do the Job Set-up procedure as specified in the removal of the BDDV (FIN

2577GM), refer to AMM Task 32-43-14-000-001.

C. PROCEDURE

(1) Subtask 321415-020-203-001 - Remove the Drain Hose Supports for the Emergency

Brake Dual Distribution Valve

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 49

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Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills AIRFRAME

References

Fig. A-GBAAA

Modification of the Brake Dual

Distribution Valve Drain Pipe Supports

Sheet 01

Sheet 02

(a) Remove the Fasteners and P-Clamps, for the Drain Hose, Item (1).

1 As shown in Fig. A-GBAAA Sheet 01, View B, remove:

1 Nut Item (7) Discard

1 Bolt Item (9) Discard

1 Washer Item (8) Discard

1 P-Clamp Item (10) Discard

1 P-Clamp Item (11) Discard

1 Nut Item (2) Discard

1 Bolt Item (5) Discard

1 Washer Item (4) Discard

1 Spacer Item (3) Discard

1 P-Clamp Item (6) Discard

(2) Subtask 321415-210-003-001 - Do a Check of Presence of Water or Hydraulic Fluid

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 50

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References

Aircraft Maintenance Manual (AMM) Task 32-43-14-000-001

Task 32-43-14-200-003

Task 32-43-14-400-001

(a) Drain the contents of the drain hose into a container.

(b) If presence of ice in the cover is expected, do a check for ice:

1 If ice found, remove the ice and do the procedure for corrosion inspection,

refer to AMM Task 32-43-14-200-003.

NOTE: If water found in the cover, it can become ice in flight or in cold

weather conditions. This can cause a problem with the draining

of the Brake Dual Distribution Valve (BDDV)

2 If corrosion found in a not permitted area, replace the BDDV 2577GM,

refer to AMM Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and

"corrosion" must be mentioned as the reason for removal.

(c) If water found in the drain hose, do the procedure for corrosion inspection, refer to

AMM Task 32-43-14-200-003.

1 If corrosion found in a not permitted area, replace the BDDV 2577GM,

refer to AMM Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and

"corrosion" must be mentioned as the reason for removal.

(d) If hydraulic fluid found in the drain hose, replace the BDDV 2577GM, refer to AMM

Task 32-43-14-000-001 and AMM Task 32-43-14-400-001 and "hydraulic leakage"

must be mentioned as the reason for removal.

(3) Subtask 321415-831-008-001 - Replace the BDDV (FIN 2577GM) and the Drain Hose

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

Manpower Resources

Manhours 2.00

Minimum number of person 1

Subtask elapsed time 2.00

Skills AIRFRAME

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

A25434005-1010A 1 BDDV

A25434005-2010A 1 BDDV

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 51

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

A25434005-3010A 1 BDDV

A25434005-3010B 1 BDDV

A25434005-4010B 1 BDDV

A25434006-1010 1 BDDV

A25434006-1010A 1 BDDV

A25434006-3000A 1 BDDV

NOTE: The above list of components is not an AIRBUS Kit, the required parts

shall be ordered as necessary through the given channel.

References

Aircraft Maintenance Manual (AMM) Task 32-43-14-000-001

Task 32-43-14-400-001

(a) Remove the BDDV (FIN 2577GM):

Refer to AMM Task 32-43-14-000-001

FIN 2577GM

1 BDDV A25434005-101A

or

FIN 2577GM

1 BDDV A25434005-201A

or

FIN 2577GM

1 BDDV A25434005-301A

or

FIN 2577GM

1 BDDV A25434005-301B

or

FIN 2577GM

1 BDDV A25434005-401B

or

FIN 2577GM

1 BDDV A25434006-101

or

FIN 2577GM

1 BDDV A25434006-101A

or

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 52

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FIN 2577GM

1 BDDV A25434006-3A

(b) Install the BDDV (FIN 2577GM):

Refer to AMM Task 32-43-14-400-001

FIN 2577GM

1 BDDV A25434005-1010A

or

FIN 2577GM

1 BDDV A25434005-2010A

or

FIN 2577GM

1 BDDV A25434005-3010A

or

FIN 2577GM

1 BDDV A25434005-3010B

or

FIN 2577GM

1 BDDV A25434005-4010B

or

FIN 2577GM

1 BDDV A25434006-1010

or

FIN 2577GM

1 BDDV A25434006-1010A

or

FIN 2577GM

1 BDDV A25434006-3000A

(4) Subtask 321415-420-203-001 - Install the Hydraulic Pipe Clamp Fasteners

Work Zones and Access Panels

Zone Access/Work location

744 Access Door Right MLG

Work location from Frame 46 to Frame 47

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 53

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Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills AIRFRAME

Material necessary to do the job

Kit 321415D01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 NAS1726C3E 1 NUT

4 NAS1149D0332K 1 WASHER

12 NAS6703U19 1 BOLT

References

Fig. A-GBAAA

Modification of the Brake Dual

Distribution Valve Drain Pipe Supports

Sheet 01

Sheet 02

(a) Install the new Fasteners.

1 As shown in Fig. A-GBAAA Sheet 02, View C, install:

1 Bolt NAS6703U19 Item 12

1 Washer NAS1149D0332K Item 4

1 Nut NAS1726C3E Item 2

D. TEST

(1) Subtask 321415-700-003-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-43-00-710-001

Task 32-43-14-400-001

(a) Job Set-up:

1 Remove the Safety clip(s) and/or tag(s) and close/unlock this (these) circuit

breaker(s) as specified after the Installation of the Dual Valve Alternate Brake

Distribution, refer to AMM Task 32-43-14-400-001.

(b) Procedure:

1 Do the test procedure as specified after the Installation of the Dual Valve

Alternate Brake Distribution, refer to AMM Task 32-43-14-400-001.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 54

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E. CLOSE-UP

(1) Subtask 321415-942-004-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 32-12-00-410-001

Task 32-43-14-400-001

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

equipment.

(b) Do the Close-up procedure as specified after the installation of the BDDV (FIN

2577GM), refer to AMM Task 32-43-14-400-001.

(c) Put the aircraft back to its initial configuration.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 55

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**CONF ALL

Z744

A

FR47

FR46

BEFORE

(1)

(6)

(3)

(2)

(9)

(8) (10)

(11)

(7)

(5)

(4)

END PLUG

A

B C

B

BRAKE DISTRIBUTION

DUAL VALVE

2577GM

N_SB_321415_6_BAAA_01_01

Figure A-GBAAA - Sheet 01

Modification of the Brake Dual Distribution Valve Drain Pipe Supports

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 56

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**CONF ALL

AFTER

12

4

(1) 2

C

BRAKE DISTRIBUTION

DUAL VALVE

2577GM

N_SB_321415_6_BAAA_02_00

Figure A-GBAAA - Sheet 02

Modification of the Brake Dual Distribution Valve Drain Pipe Supports

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 57

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SERVICE BULLETIN

REPORTING SHEET

TITLE: LANDING GEAR - ALTERNATE BRAKING WITH ANTI-SKID - INSTALL

A NEW MODIFIED BRAKE DISTRIBUTION DUAL VALVE

MODIFICATION No.: 155579P12900

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: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 1

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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: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415

REVISION No.: 00 - Sep 02/14 Page: 1

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