# @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 5

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

# @A318/A319/A320/A321
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 5

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

# @A318/A319/A320/A321
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 5

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

# @A318/A319/A320/A321
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 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 ATA SYSTEM: 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 5

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

# @A318/A319/A320/A321
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 REVISION No.: 00 - Sep 02/14 Page: 2 5

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

# @A318/A319/A320/A321
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 REVISION No.: 00 - Sep 02/14 Page: 3 5

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

# @A318/A319/A320/A321
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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 4 5

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

# @A318/A319/A320/A321
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 DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 5 5

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

# @A318/A319/A320/A321
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 REVISION No.: 00 - Sep 02/14 Page: 6 5

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

# @A318/A319/A320/A321
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 REVISION No.: 00 - Sep 02/14 Page: 7 5

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

# @A318/A319/A320/A321
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 DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 8 5

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

# @A318/A319/A320/A321
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 REVISION No.: 00 - Sep 02/14 Page: 9 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN
(4) Configuration by MSN MSN CONFIGURATION 0029 0045 0046 0047 0049 0050 0051 0052 0053 0054 0055 0056 0057 0059 0064 0065 0066 0067 0068 0069 0070 0071 0072 0073 0074 0075 0076 0077 0078 0080 0081 0082 0083 0084 0085 0086 0087 0088 0090 0093 0094 0095 0096 0099 0104 0110 0111 0112 0113 0114 0115 0116 0117 0118 0119 0121 0122 0123 0124 0125 0126 0127 0135 0137 0138 0140 0141 0142 0147 0148 0149 0150 0152 0153 0154 0157 0158 0159 0160 0161 0162 0164 0165 0166 0167 0168 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 REVISION No.: 00 - Sep 02/14 Page: 10 5

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

# @A318/A319/A320/A321
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 5

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

# @A318/A319/A320/A321
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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 12 5

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

# @A318/A319/A320/A321
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 5

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

# @A318/A319/A320/A321
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 5

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

# @A318/A319/A320/A321
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 REVISION No.: 00 - Sep 02/14 Page: 15 5

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

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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 16 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 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 DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 17 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN
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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 18 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 19 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 20 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: 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.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 21 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN
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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 22 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN
(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 DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 23 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN
(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 thisService Bulletin, it is necessary to use the tools defined in MESSIERBUGATTI-DOWTY Service Bulletin A25434-32-3374. (3) Special Tools None

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 24 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 25 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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.

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 26 5

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

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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 27 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 28 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN
(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 DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 29 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN
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 DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 30 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 34 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

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

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

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

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 46 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

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

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

# @A318/A319/A320/A321
SERVICE BULLETIN

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 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

**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 5

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

# @A318/A319/A320/A321
SERVICE BULLETIN

**CONF ALL



## AFTER

12
4

2 (1) 

## 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 5

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

# @A318/A319/A320/A321
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 5

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

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

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

DATE: Sep 02/14 SERVICE BULLETIN No.: A320-32-1415 REVISION No.: 00 - Sep 02/14 Page: 1 5

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