# Airbus Service Bulletin A330-27-3222

## Copies (2)

Copies the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist.

- No revision named ("A330-27-3222 R00"), 47 pages: PDF https://openairdocs.org/files/sha256/83/20/832056c339223089965a61fec35e1b37a5d789b071d79e9369dcfb7ac2652d25; text https://openairdocs.org/service-documents/airbus/a330-27-3222/file/832056c33922.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0498; AD 2018-21-07 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- No revision named ("A330-27-3222 R01"), 51 pages: PDF https://openairdocs.org/files/sha256/36/4a/364af936f2cc10695fe55c54e39e668469ac56aa14d04de502049f21b0bfed79; text https://openairdocs.org/service-documents/airbus/a330-27-3222/file/364af936f2cc.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2020-0456, the docket of AD 2020-17-16. Not covered by OpenAirDocs’ CC0 dedication.

## Details

- Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md)
- Type: Service bulletin (Service Bulletin)
- Number: A330-27-3222
- Page: https://openairdocs.org/service-documents/airbus/a330-27-3222

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2018-21-07](https://openairdocs.org/ad/2018-21-07.md), effective Nov 19, 2018: No revision named

## Text (47 pages)

No revision named, the newest copy. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2018-0498; AD 2018-21-07 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

@A330
SERVICE BULLETIN
SUMMARY
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
This summary is for information only and is not approved for modification of the aircraft.
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 27
TITLE: FLIGHT CONTROLS - FCPC - INSTALL FCPC P15/M24 2K2
**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR
 206414S33846
MINOR
 None
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
A new standard of Flight Control Primary Computer (FCPC) has been developed to improve the Angle
Of Attack (AOA) probe monitoring.
This Service Bulletin replaces FCPC standards M23 (hardware LA2K0), P14/M23 (hardware LA2K1)
and P13/M22 (hardware LA2K2) with new FCPC standard P15/M24 (hardware LA2K2).
This Service Bulletin is published to advise all operators of A330 aircraft of the issue of AIRBUS
OPERATIONS SAS Service Bulletin No. LA2K2-27-023 which install new FCPC standard P15/M24
(hardware LA2K2).
To accomplish this Service Bulletin, you have three possibilities, as FCPC upgrade can be done either:
- By replacement of the FCPC(s) on aircraft
- By replacement of associated On Board Replaceable Module (OBRM) set (composed of Part
Number (PN) LA2K2B100DG0100 and PN LA2K2B100DG0200 installed through MOD No.
202680S32364 (Service Bulletin No. A330-27-3205)) on aircraft
- By replacement or reprogramming of OBRM as per AIRBUS OPERATIONS SAS Service Bulletin
No. LA2K2-27-023 on bench.
NOTE
: In case of replacement of M23 (hardware LA2K0) or P14/M23 (hardware LA2K1) by
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 1
5
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### Page 2

@A330
SERVICE BULLETIN
SUMMARY
P15/M24 (hardware LA2K2), only TASK 273222-831-801 001 OPTION 1 - Upgrade by
Replacement of FCPC(s) on Aircraft is possible.
NOTE
: We remind operators that, as described in OIT 999.0020/16, a replacement campaign
of FCPC hardware LA2K0 or LA2K1 (to hardware LA2K2) is on-going. AIRBUS
recommends that operators adhere to this hardware modification campaign as early as
possible.
Accomplishment of this Service Bulletin will improve the AOA probe monitoring.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE
 MANDATORY (1)
 CANCELS INSPECTION SB
 NO
POTENTIAL AD
 YES
 A/C OPERATION AFFECTED
 NO
RELIABILITY AFFECTED
 NO
 PAX COMFORT AFFECTED
 NO
COST SAVING
 NO
 ETOPS AFFECTED
 NO
STRUCTURAL LIFE EXTN
 NO
 VENDOR SB INVOLVED
 YES
NOTE
 (1)
: Service Bulletin must be accomplished.
MATERIAL PRICE INFORMATION
MATERIAL PRICE INFORMATION TABLE
MATERIAL SET
 QTY PER
A/C
PRICE PER
A/C (USD)
MAIN PARTS
Equipment BFEA01
 1
 See SB
 FCPCs
Equipment BFEA02
 1
 See SB
 OBRMs
EFFECTIVITY
This Service Bulletin is applicable to this (these) operator(s) :
12P 18P 34Z 36P 38W 41N 43P 56O 64N 78U 83V 96U 98W
AAL AAR AAW ACA ACI AEA AFL AFR ALD ALK ARA ARG ASL
ASY AVA AZA AZU BEC BEL BER BGH CAL CBJ CCA CEB CES
CHH CPA CRK CRL CSA CSC CSN DAH DAL DGA DLH EDW EIN
ETD EVA EVE F2I FAF FBU FIN FJI FWI GCR GFA GIA GRL
HAL HDA HFY HKC HVN IAW IBE IRA JAI JAV KAC KAL KLM
LAA LNI MAS MAU MEA MLM MNB MOV MSR NMB OBS OHY OMA
ONE PAL PLM QAF QFA QTR RJA RSF RSY RWD RZO SAA SAF
SAI SAS SEY SIA SVA SWR SXD TAE TAM TAP TAR TBA TCX
THA THY TNA TOW TPA TSC U6A UAE UAF VIR VKG VOZ WOW
WRC XAX XLF
CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the
following Service Bulletin(s):
Service Bulletin No. A330-27-3205
A330-27-3207
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 2
5
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### Page 3

@A330
SERVICE BULLETIN
SUMMARY
NOTE
: Service Bulletin No. A330-27-3205 (FLIGHT CONTROLS - FCPC - INTRODUCE NEW
FCPC STD P13M22 2K2) applies MOD No. 202680S32364.
NOTE
: Service Bulletin No.A330-27-3207 (FLIGHT CONTROLS - FLIGHT CONTROL
PRIMARY COMPUTER (FCPC) - INSTALL NEW FCPC M23-2K0 OR P14M23-2K1)
applies MOD No. 203036S32366 and 203034S32365.
NOTE
: Accomplish either Service Bulletin No. A330-27-3205 or Service Bulletin No.
A330-27-3207 as per effectivity specified in these Service Bulletins.
NOTE
: The operator must check the aircraft records to determine which of the above
information is applicable.
REFERENCES / REPERCUSSIONS
TFU
 34.11.00.011
OEB
 None
AOT
 None
SIL
 None
ISI
 22.00.00006
LINE MAINTENANCE AFFECTED
 No
LIFE LIMIT
 None
OTHER
 Operator Information Transmission (OIT) No. 999.0020/16
NATURE OF THE WORK
AIRCRAFT
 NO
EQUIPMENT
 YES
HARD
 YES
SOFT
 NO
OBRM
 YES
MANPOWER
Task 273222-831-801-001: OPTION 1 - Upgrade by Replacement of FCPC(s) on Aircraft
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Task 273222-831-802-001: OPTION 2 - Upgrade by Replacement of FCPC(s) OBRM(s) on
Aircraft
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Task 273222-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPC(s) OBRM(s) in
accordance with VSB on Bench
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours relat ed to Vendor SB; refer to:
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 3
5
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### Page 4

@A330
SERVICE BULLETIN
SUMMARY
Task 273222-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPC(s) OBRM(s) in
accordance with VSB on Bench
Reprogram the OBRMs in accordance with VSB
 AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K2-27-023
APPENDICES
None
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 4
5
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### Page 5

@A330
SERVICE BULLETIN
SUMMARY
**CONF ALL
Z120
FR20
FR1
B
800VU
915VU
A
MODIFICATION OF THE FCPCB
A
2CE1
MODIFICATION OF THE FCPC
MODIFICATION OF THE FCPC
2CE2
2CE3
G_SB_273222_5_SAAA_01_01
Figure A-FSAAA - Sheet 01
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 5
5
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SERVICE BULLETIN
SUMMARY
This Page Intentionally Left Blank
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 6
5
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### Page 7

@A330
SERVICE BULLETIN
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
T e l:( 3 3 )56 19 33 33 3
Telex : AIRBU 530526F
F a x:( 3 3 )56 19 34 25 1
MANDATORY
 MANDATORY
 MANDATORY
ATA SYSTEM: 27
TITLE: FLIGHT CONTROLS - FCPC - INSTALL FCPC P15/M24 2K2
MODIFICATION No.: 206414S33846
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 embodied before delivery on A330-200 aircraft
Manufacturer Serial Number (MSN) 1771 thru 1785 , 1805 , 1823 , 1835 thru
1847 , 1854 and subsequent, on A330-300 aircraft MSN 1770 and
subsequent and on A330-200F aircraft MSN 1772 and subsequent.
NOTE
: This Service Bulletin is only applicable to aircraft on which MOD
No. 204810S33314 (FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY
COMPUTER (FCPC) - REPLACE FCPC P13 STD BY FCPC MRTT3 STD -
SB ONLY) is not embodied.
(1) Models
330-202 330-203 330-223 330-223F 330-243 330-243F 330-301 330-302
330-303 330-321 330-322 330-323 330-341 330-342 330-343
(2) Effectivity by MSN
0012 0017 0030 0037 0045 0050 0054-0055 0060 0062 0064-0065 0070-0072
0082-0083 0086-0087 0095-0096 0098-0099 0102 0106 0109 0111-0113 0116 0118
0120-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172
0177 0181 0195 0200 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238
0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 1
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@A330
SERVICE BULLETIN
0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293 0295-0296 0300-0301
0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334
0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370
0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401
0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441
0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473
0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513
0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539
0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576
0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607
0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638
0640-0642 0644-0645 0647-0650 0652-0659 0661-0667 0669-0671 0673-0676
0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705
0707-0709 0711-0714 0716-0718 0720-0722 0724-0726 0728-0730 0732-0735
0737-0739 0741-0743 0745-0747 0749-0752 0754-0756 0758-0760 0769-0770
0772-0774 0776-0778 0780-0782 0784-0786 0788-0789 0791-0792 0795-0797 0799
0801-0803 0805-0807 0809-0811 0813-0815 0817-0828 0830-0834 0836 0838-0843
0845 0847 0849-0855 0857-0863 0865-0869 0873-0877 0879 0881-0885 0887-0893
0895-0896 0898-0901 0903-0909 0911 0913-0916 0918-0920 0922-0923 0925-0928
0930-0932 0934-0937 0939-0952 0954 0956-0959 0961-0971 0973-0980 0982-0986
0988-0992 0994-0998 1000-1004 1006-1016 1018-1023 1025-1026 1028-1029
1031-1039 1041-1049 1051-1055 1057-1063 1065-1067 1069-1078 1080-1082
1084-1090 1092-1101 1103-1108 1110 1112 1114-1116 1118 1120 1123-1124
1126-1127 1129-1133 1135-1138 1141 1143 1145-1151 1153 1155-1157 1159-1161
1163-1165 1167-1175 1177-1178 1180-1181 1183-1184 1186-1193 1195-1196
1198-1206 1208-1241 1243-1252 1254-1256 1258-1272 1274-1521 1523-1651
1653-1660 1662-1681 1684-1701 1703-1704 1706 1708-1716 1718-1769 1787 1799
1808 1822 1830 1848
(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
12P
 1787 1848
18P
 1321
34Z
 1491 1542 1554 1651
36P
 1830
38W
 0401
41N
 1676
43P
 1053
56O
 0116 0127
64N
 1751
78U
 0314 0455 0518 0536
83V
 0171
96U
 0396
98W
 0054
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 2
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@A330
SERVICE BULLETIN
OPERATOR
 MSN
AAL
 0315 0323 0333 0337 0342 0370 0375 0380 0388 1011 1022 1041
1069 1076 1095 1100 1415 1417 1441 1455 1480 1502 1512 1526
AAR
 0640 0676 0708 0772 0803 0845 1001 1055 1151 1211 1326 1340
1435 1464 1518
AAW
 1043 1472 1535
ACA
 0277 0279 0284 0344 0400 0408 0412 0419
ACI
 0507 0510
AEA
 0461 0505 0526 0551 0597 0670 0733 0745 0749 0814 0931 0950
0992 1097 1574
AFL
 0963 0973 1014 1045 1047 1058 1065 1072 1077 1103 1232 1247
1264 1270 1284 1299 1301 1323 1328 1345 1356 1371
AFR
 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519
0567 0584 0657
ALD
 0326 0328 0392
ALK
 0303 0306 0311 0313 0456 0627 1564 1583 1604 1650 1669 1687
1689
ARA
 0891 0927
ARG
 0290 0300 0358 0364 0587 0634 1605 1623 1737 1748
ASL
 0885
ASY
 0747 0892 0898 0951 0969 1036 1183
AVA
 1009 1016 1073 1208 1224 1279 1342 1400 1492 1508
AZA
 0272 0339 0825 0831 1123 1135 1218 1225 1252 1283 1308 1313
1327 1354
AZU
 0462 0494 0527 0529 0532
BEC
 0863
BEL
 0030 0037 0045 0082 0095 0229 0249 0324 1085
BER
 0288 0322 0403 0432 0444 0454 0469 0476 0493 0665 0739 0802
0822 0828 0911 0968 1112
BGH
 0255
CAL
 0602 0607 0641 0671 0675 0691 0699 0707 0714 0725 0752 0769
0805 0823 0838 0861 0920 1177 1272 1278 1346 1367 1450 1539
CBJ
 0988 1020 1028 1052 1753 1763
CCA
 0750 0756 0759 0780 0785 0797 0810 0815 0839 0860 0867 0873
0884 0890 0903 0909 0930 0941 0944 0957 1087 1110 1130 1187
1199 1216 1237 1260 1282 1304 1330 1333 1353 1373 1383 1396
1413 1434 1444 1459 1471 1493 1509 1525 1538 1541 1563 1570
1587 1658 1673 1685 1695 1752 1765
CEB
 1420 1445 1495 1527 1552 1602 1712
CES
 0713 0720 0728 0732 0735 0773 0777 0781 0782 0791 0821 0830
0836 0851 0862 0866 0916 0928 0936 0942 1262 1267 1280 1291
1303 1324 1331 1372 1375 1402 1421 1429 1440 1461 1468 1479
1484 1500 1520 1537 1547 1551 1569 1588 1595 1603 1617 1632
1639 1655 1664
CHH
 0875 0881 0906 0982 1159 1168 1178 1190 1255 1325 1438 1532
1558 1573 1591 1614 1634 1656 1663 1677 1686 1703
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 3
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@A330
SERVICE BULLETIN
OPERATOR
 MSN
CPA
 0102 0113 0121 0386 0389 0393 0418 0420 0421 0423 0439 0539
0548 0565 0679 0776 0850 0855 0895 0915 0959 1163 1196 1222
1239 1285 1317 1343 1349 1362 1366 1387 1409 1436 1443 1523
1545 1557 1567 1598 1618 1621
CRK
 1031 1034 1039 1042 1051 1054 1059 1062 1099 1105 1107 1115
1124 1175 1277 1286 1322 1358 1369 1384 1398 1668
CRL
 0285 0320 1359 1376
CSA
 0425
CSC
 1082 1138 1241 1397 1432 1528 1579 1662 1746
CSN
 0649 0652 0656 0664 0818 0840 0879 0889 0908 0935 0937 0954
0958 0964 1096 1116 1129 1202 1220 1233 1244 1297 1309 1335
1392 1425 1430 1494 1519 1536 1575 1593 1625 1636 1645 1699
1714 1760
DAH
 0644 0647 0650 0653 0667 1613 1630 1649
DAL
 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620
0621 0631 0633 0663 0674 0690 0718 0722 0778 0784 0796 0799
0806 0817 0827 0843 0857 0858 0859 0865 1627 1628 1637 1679
1701 1716 1720 1721 1769
DGA
 0240 1735
DLH
 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 0896 0905
0913 0922 0989 1292 1305 1314 1497
EDW
 0291 1193 1711
EIN
 0269 0330 0397 0841 0847 0985 1025 1106 1742 1744
ETD
 0658 0688 0717 0724 0729 0730 0737 0788 0807 0809 0824 0832
0852 0854 0868 0975 0991 1032 1070 1071 1081 1167 1205 1226
1245 1414 1486 1521 1524
EVA
 0655 0661 0678 0693 0755 1254 1268 1274 1684 1690 1767
EVE
 1691
F2I
 0070 0072 0087 0200
FAF
 1808
FBU
 1727
FIN
 0994 1007 1013 1023 1067 1078 1088 1173
FJI
 1394 1416 1465 1692
FWI
 0253 0343 0758 0965 1021 1265
GCR
 0919 1756 1758
GFA
 0276 0281 0286 0287 0334 0340
GIA
 0138 0140 0144 0148 0153 0165 1184 1214 1261 1288 1364 1410
1446 1474 1548 1560 1577 1585 1654 1671 1698 1709 1723 1733
GRL
 0230
HAL
 1104 1114 1171 1217 1259 1295 1302 1310 1316 1389 1399 1404
1422 1469 1488 1496 1511 1530 1565 1606 1615 1672 1732
HDA
 0012 0017 0071 0083 0099 0106 0109 0118 0155 0234 0244 0405
0479 0512 0581 0669 0673 1457 1503
HFY
 0211 0262 1008
HKC
 1320
HVN
 0275 0366 0943 0946 0962 1019 1256 1266
IAW
 1339
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 4
5
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@A330
SERVICE BULLETIN
OPERATOR
 MSN
IBE
 1377 1385 1405 1426 1437 1490 1507 1515 1694 1700 1710 1719
1728 1736 1740 1747 1755 1761
IRA
 1540 1586
JAI
 0888 0923 0947 0956 1351 1361 1370 1391
JAV
 0409
KAC
 1626 1643 1653 1678 1681
KAL
 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350
0351 0368 0428 0484 0490 0550 1133 1155 1200 1203 1393 1556
1576 1590 1611 1638 1647
KLM
 0682 0686 0703 0738 0770 0801 0925 1161 1287 1294 1300 1381
1580
LAA
 1412 1424 1505 1543
LNI
 1675 1680 1693
MAS
 1136 1148 1164 1180 1209 1219 1229 1234 1243 1281 1318 1336
1337 1347 1388 1395 1431 1470 1489
MAU
 0883 1057
MEA
 0926 0984 0995 0998 1725
MLM
 0451
MNB
 1332
MOV
 0535
MSR
 0600 0610 0666 0683 0696 0709 0726 1143 1230 1238 1246
NMB
 1451 1466
OBS
 0833
OHY
 0098 0143 0316 0345 0353 0362 0404 0437 0625 0632
OMA
 1038 1044 1049 1063 1093 1120 1227 1572 1582 1599
ONE
 1506 1608 1657
PAL
 1449 1456 1460 1463 1467 1475 1482 1504 1510 1531 1546 1553
1559 1566 1568
PLM
 0261 0265
QAF
 0487 0605
QFA
 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695
0705 0712 0842 0853 0887 0940 0945 0976 1061 1094 1169 1174
1198 1251 1258 1365
QTR
 0441 0473 0489 0511 0521 0571 0623 0637 0638 0659 0680 0711
0721 0734 0743 0746 0760 0789 0792 0813 0820 0826 0849 0893
0907 0918 1350 1386 1406 1578 1584 1594 1688 1708
RJA
 0979 1002
RSF
 0980 0996 1235 1379 1478 1516
RSY
 0096 0120
RWD
 1741 1759
RZO
 0970
SAA
 1191 1210 1223 1236 1249 1271 1745 1754 1757
SAF
 1667 1762 1799 1822
SAI
 0055 0086 0811 0819 0834 0900
SAS
 0496 0497 0515 0568 1660 1665 1697 1715
SEY
 0751
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 5
5
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@A330
SERVICE BULLETIN
OPERATOR
 MSN
SIA
 0978 0983 0986 0997 1006 1010 1012 1015 1132 1149 1156 1382
1401 1427 1447 1453 1477 1485 1517 1544 1562 1597 1609 1633
1648 1666
SVA
 1108 1127 1137 1141 1147 1153 1189 1192 1454 1462 1473 1513
1724 1726 1729 1731 1734 1738 1739 1743 1749 1764 1766
SWR
 1000 1018 1026 1029 1084 1089 1101 1145 1181 1188 1276 1290
1355 1403
SXD
 0530 0555 0573 0612 0616 0684
TAE
 0348
TAM
 0232 0238 0247 0259 0361 0466 0472 0700
TAP
 0181 0195 0223 0305 0308 0312 0317 0365 0372 0477 0486 0877
0899 0904 0914 0934
TAR
 1631 1641
TBA
 1730
TCX
 0254 0266 0301 0398 0948 0967
THA
 0050 0060 0062 0112 0122 0209 0224 0231 0346 0990 1003 1035
1037 1060 1074 1086 1090 1263 1269 1289 1338 1348 1374 1408
THY
 0463 0504 0697 0704 0742 0754 0774 0869 0874 0876 0882 0901
0932 0939 0949 0961 0977 1004 1092 1118 1150 1160 1170 1172
1204 1212 1213 1221 1228 1240 1298 1307 1311 1344 1418 1442
1458 1476 1483 1487 1499 1501 1514 1529 1550 1571 1592 1616
1620 1622 1629 1635 1640 1642 1644 1696 1704 1706 1713 1718
1722 1750 1768
TNA
 1146 1157 1357 1378
TOW
 1033 1046 1248 1275 1312 1334 1363 1390 1419 1439 1498 1555
1601 1610
TPA
 1368 1380 1428 1448 1534
TSC
 0111 0132 0177 0248 0250 0251 0271 0369 0407 0427 0480 0795
0966 0971
U6A
 0064 0065
UAE
 0283 0293 0295 0382 0384 0452 0491 0509 0525
UAF
 1080 1186 1250
VIR
 1195 1201 1206 1215 1231 1296 1315 1329 1341 1352
VKG
 0309 0349 0356 0357
VOZ
 1293 1306 1319 1407 1452 1561
WOW
 1098 1607 1624
WRC
 0296
XAX
 0654 0662 0692 0716 0741 0786 0952 0974 1048 1066 1075 1126
1131 1165 1411 1423 1433 1481 1533 1549 1581 1589 1596 1600
1612 1619 1646 1659 1670 1674
XLF
 0501 0635 1360
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 6
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@A330
SERVICE BULLETIN
(4) Configuration by MSN
MSN
 CONFIGURATION
0012 0017 0030 0037 0045 0050 0054 0055 0060 0062 0064
0065 0070 0071 0072 0082 0083 0086 0087 0095 0096 0098
0099 0102 0106 0109 0111 0112 0113 0116 0118 0120 0121
0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162
0165 0171 0172 0177 0181 0195 0200 0206 0209 0211 0219
0222 0223 0224 0226 0229 0230 0231 0232 0234 0238 0240
0241 0244 0247 0248 0249 0250 0251 0253 0254 0255 0256
0258 0259 0261 0262 0265 0266 0267 0269 0271 0272 0275
0276 0277 0279 0281 0283 0284 0285 0286 0287 0288 0290
0291 0293 0295 0296 0300 0301 0303 0305 0306 0308 0309
0311 0312 0313 0314 0315 0316 0317 0320 0322 0323 0324
0326 0328 0330 0333 0334 0337 0338 0339 0340 0342 0343
0344 0345 0346 0348 0349 0350 0351 0353 0356 0357 0358
0361 0362 0364 0365 0366 0368 0369 0370 0372 0375 0380
0382 0384 0386 0388 0389 0392 0393 0396 0397 0398 0400
0401 0403 0404 0405 0407 0408 0409 0412 0418 0419 0420
0421 0422 0423 0425 0427 0428 0432 0437 0439 0441 0443
0444 0448 0451 0452 0454 0455 0456 0458 0461 0462 0463
0465 0466 0469 0472 0473 0476 0477 0479 0480 0481 0484
0486 0487 0489 0490 0491 0493 0494 0496 0497 0498 0500
0501 0502 0503 0504 0505 0506 0507 0508 0509 0510 0511
0512 0513 0515 0516 0518 0519 0521 0522 0524 0525 0526
0527 0529 0530 0532 0533 0535 0536 0539 0542 0548 0549
0550 0551 0552 0553 0555 0558 0564 0565 0567 0568 0570
0571 0573 0574 0576 0578 0579 0581 0584 0587 0588 0591
0593 0595 0597 0600 0602 0603 0605 0607 0609 0610 0612
0614 0616 0618 0620 0621 0623 0625 0627 0629 0631 0632
0633 0634 0635 0636 0637 0638 0640 0641 0642 0644 0645
0647 0648 0649 0650 0652 0653 0654 0655 0656 0657 0658
0659 0661 0662 0663 0664 0665 0666 0667 0669 0670 0671
0673 0674 0675 0676 0678 0679 0680 0682 0683 0684 0686
0687 0688 0690 0691 0692 0693 0695 0696 0697 0699 0700
0701 0703 0704 0705 0707 0708 0709 0711 0712 0713 0714
0716 0717 0718 0720 0721 0722 0724 0725 0726 0728 0729
0730 0732 0733 0734 0735 0737 0738 0739 0741 0742 0743
0745 0746 0747 0749 0750 0751 0752 0754 0755 0756 0758
0759 0760 0769 0770 0772 0773 0774 0776 0777 0778 0780
0781 0782 0784 0785 0786 0788 0789 0791 0792 0795 0796
0797 0799 0801 0802 0803 0805 0806 0807 0809 0810 0811
0813 0814 0815 0817 0818 0819 0820 0821 0822 0823 0824
0825 0826 0827 0828 0830 0831 0832 0833 0834 0836 0838
0839 0840 0841 0842 0843 0845 0847 0849 0850 0851 0852
0853 0854 0855 0857 0858 0859 0860 0861 0862 0863 0865
0866 0867 0868 0869 0873 0874 0875 0876 0877 0879 0881
0882 0883 0884 0885 0887 0888 0889 0890 0891 0892 0893
0895 0896 0898 0899 0900 0901 0903 0904 0905 0906 0907
0908 0909 0911 0913 0914 0915 0916 0918 0919 0920 0922
0923 0925 0926 0927 0928 0930 0931 0932 0934 0935 0936
0937 0939 0940 0941 0942 0943 0944 0945 0946 0947 0948
001
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 7
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@A330
SERVICE BULLETIN
MSN
 CONFIGURATION
0949 0950 0951 0952 0954 0956 0957 0958 0959 0961 0962
0963 0964 0965 0966 0967 0968 0969 0970 0971 0973 0974
0975 0976 0977 0978 0979 0980 0982 0983 0984 0985 0986
0988 0989 0990 0991 0992 0994 0995 0996 0997 0998 1000
1001 1002 1003 1004 1006 1007 1008 1009 1010 1011 1012
1013 1014 1015 1016 1018 1019 1020 1021 1022 1023 1025
1026 1028 1029 1031 1032 1033 1034 1035 1036 1037 1038
1039 1041 1042 1043 1044 1045 1046 1047 1048 1049 1051
1052 1053 1054 1055 1057 1058 1059 1060 1061 1062 1063
1065 1066 1067 1069 1070 1071 1072 1073 1074 1075 1076
1077 1078 1080 1081 1082 1084 1085 1086 1087 1088 1089
1090 1092 1093 1094 1095 1096 1097 1098 1099 1100 1101
1103 1104 1105 1106 1107 1108 1110 1112 1114 1115 1116
1118 1120 1123 1124 1126 1127 1129 1130 1131 1132 1133
1135 1136 1137 1138 1141 1143 1145 1146 1147 1148 1149
1150 1151 1153 1155 1156 1157 1159 1160 1161 1163 1164
1165 1167 1168 1169 1170 1171 1172 1173 1174 1175 1177
1178 1180 1181 1183 1184 1186 1187 1188 1189 1190 1191
1192 1193 1195 1196 1198 1199 1200 1201 1202 1203 1204
1205 1206 1208 1209 1210 1211 1212 1213 1214 1215 1216
1217 1218 1219 1220 1221 1222 1223 1224 1225 1226 1227
1228 1229 1230 1231 1232 1233 1234 1235 1236 1237 1238
1239 1240 1241 1243 1244 1245 1246 1247 1248 1249 1250
1251 1252 1254 1255 1256 1258 1259 1260 1261 1262 1263
1264 1265 1266 1267 1268 1269 1270 1271 1272 1274 1275
1276 1277 1278 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 1333 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 1374
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 1464 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 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
001
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 8
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@A330
SERVICE BULLETIN
MSN
 CONFIGURATION
1563 1564 1565 1566 1567 1568 1569 1570 1571 1572 1573
1574 1575 1576 1577 1578 1579 1580 1581 1582 1583 1584
1585 1586 1587 1588 1589 1590 1591 1592 1593 1594 1595
1596 1597 1598 1599 1600 1601 1602 1603 1604 1605 1606
1607 1608 1609 1610 1611 1612 1613 1614 1615 1616 1617
1618 1619 1620 1621 1622 1623 1624 1625 1626 1627 1628
1629 1630 1631 1632 1633 1634 1635 1636 1637 1638 1639
1640 1641 1642 1643 1644 1645 1646 1647 1648 1649 1650
1651 1653 1654 1655 1656 1657 1658 1659 1660 1662 1663
1664 1665 1666 1667 1668 1669 1670 1671 1672 1673 1674
1675 1676 1677 1678 1679 1680 1681 1684 1685 1686 1687
1688 1689 1690 1691 1692 1693 1694 1695 1696 1697 1698
1699 1700 1701 1703 1704 1706 1708 1709 1710 1711 1712
1713 1714 1715 1716 1718 1719 1720 1721 1722 1723 1724
1725 1726 1727 1728 1729 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 1768
1769 1787 1799 1808 1822 1830 1848
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
Equipment BFEA01
 1
 (1)
Equipment BFEA02
 1
 (2)
Reidentified part set REIDA01
 1
 (3)
NOTE
 (1)
: Equipment BFEA01 is applicable for TASK 273222-831-801 001
OPTION 1 - Upgrade by Replacement of FCPC(s) on Aircraft .
NOTE
 (2)
: Equipment BFEA02 is applicable for TASK 273222-831-802 001
OPTION 2 - Upgrade by Replacement of FCPC(s) OBRM(s) on Aircraft .
NOTE
 (3)
: Reidentified part set REIDA01 is applicable for TASK 273222-831-803
001 OPTION 3 - Upgrade by Reprogramming of FCPC(s) OBRM(s) in
accordance with VSB on Bench .
B. CONCURRENT REQUIREMENTS
Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of
the following Service Bulletin(s):
Service Bulletin No. A330-27-3205
A330-27-3207
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 9
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SERVICE BULLETIN
NOTE
: Service Bulletin No. A330-27-3205 (FLIGHT CONTROLS - FCPC -
INTRODUCE NEW FCPC STD P13M22 2K2) applies MOD No.
202680S32364.
NOTE
: Service Bulletin No.A330-27-3207 (FLIGHT CONTROLS - FLIGHT CONTROL
PRIMARY COMPUTER (FCPC) - INSTALL NEW FCPC M23-2K0 OR
P14M23-2K1) applies MOD No. 203036S32366 and 203034S32365.
NOTE
: Accomplish either Service Bulletin No. A330-27-3205 or Service Bulletin No.
A330-27-3207 as per effectivity specified in these Service Bulletins.
NOTE
: The operator must check the aircraft records to determine which of the above
information is applicable.
C. REASON
(1) History
A new standard of Flight Control Primary Computer (FCPC) has been developed to
improve the Angle Of Attack (AOA) probe monitoring.
(2) Objective/Action
This Service Bulletin replaces FCPC standards M23 (hardware LA2K0), P14/M23
(hardware LA2K1) and P13/M22 (hardware LA2K2) with new FCPC standard P15/M24
(hardware LA2K2).
This Service Bulletin is published to advise all operators of A330 aircraft of the issue of
AIRBUS OPERATIONS SAS Service Bulletin No. LA2K2-27-023 which install new FCPC
standard P15/M24 (hardware LA2K2).
To accomplish this Service Bulletin, you have three possibilities, as FCPC upgrade can
be done either:
- By replacement of the FCPC(s) on aircraft
- By replacement of associated On Board Replaceable Module (OBRM) set
(composed of Part Number (PN) LA2K2B100DG0100 and PN LA2K2B100DG0200
installed through MOD No. 202680S32364 (Service Bulletin No. A330-27-3205)) on
aircraft
- By replacement or reprogramming of OBRM as per AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K2-27-023 on bench.
NOTE
: In case of replacement of M23 (hardware LA2K0) or P14/M23 (hardware
LA2K1) by P15/M24 (hardware LA2K2), only TASK 273222-831-801 001
OPTION 1 - Upgrade by Replacement of FCPC(s) on Aircraft is possible.
NOTE
: We remind operators that, as described in OIT 999.0020/16, a
replacement campaign of FCPC hardware LA2K0 or LA2K1 (to hardware
LA2K2) is on-going. AIRBUS recommends that operators adhere to this
hardware modification campaign as early as possible.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 10
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SERVICE BULLETIN
(3) Advantages
Accomplishment of this Service Bulletin will improve the AOA probe monitoring.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
NOTE
: To accomplish this Service Bulletin, you have 3 options but, in case of
replacement of M23 (hardware LA2K0) or P14/M23 (hardware LA2K1) by
P15/M24 (hardware LA2K2), only TASK 273222-831-801 001 OPTION 1 -
Upgrade by Replacement of FCPC(s) on Aircraft is possible.
To accomplish this Service Bulletin it is necessary to :
Task 273222-831-801-001: OPTION 1 - Upgrade by Replacement of FCPC(s) on Aircraft
(1) Replace the FCPC(s)
Task 273222-831-802-001: OPTION 2 - Upgrade by Replacement of FCPC(s) OBRM(s) on
Aircraft
(1) Replace the OBRMs
Task 273222-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPC(s) OBRM(s) in
accordance with VSB on Bench
(1) Remove the OBRMs
(2) Reprogram the OBRMs in accordance with VSB
(3) Install the OBRMs
E. COMPLIANCE
(1) Classification
MANDATORY: Service Bulletin must be accomplished.
(2) Accomplishment Timescale
This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness
Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued
to confirm this classification. The accomplishment timescale, which has not yet been
defined, will be given in the AD.
F. APPROVAL
The technical content of this document is approved under the authority of Design
Organisation Approval No. EASA.21J.031.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 11
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SERVICE BULLETIN
If an aircraft listed in the effectivity has a modification or repair embodied that is not of
AIRBUS origin, and which affects the content of this Service Bulletin, the operator is
responsible for obtaining approval by its airworthiness authority for any adaptation necessary
before incorporation of the Service Bulletin.
G. MANPOWER
The manpower estimates given in this Service Bulletin are based on the direct labor cost to
do the work. These estimates assume that the work will be done by experienced personnel,
and may need to be revised upwards to suit operator’s circumstances. The estimates do not
include the time to prepare, plan or inspect the work. Manufacture and procurement of parts
and tools, drying times for paints, sealants, etc., and general administration work are also not
included.
Task 273222-831-801-001: OPTION 1 - Upgrade by Replacement of FCPC(s) on Aircraft
Get Access
 0.50
On Aircraft
Replace the FCPC(s)
 1.00
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
Task 273222-831-802-001: OPTION 2 - Upgrade by Replacement of FCPC(s) OBRM(s) on
Aircraft
Get Access
 0.50
On Aircraft
Replace the OBRMs
 0.50
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Task 273222-831-803-001: OPTION 3 - Upgrade by Reprogramming of FCPC(s) OBRM(s) in
accordance with VSB on Bench
Get Access
 0.50
On Aircraft
Remove the OBRMs
 0.25
Install the OBRMs
 0.25
Tests
 0.50
Close-Up
 0.50
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours relat ed to Vendor SB; refer to:
Reprogram the OBRMs in accordance with VSB
 AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K2-27-023
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 12
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@A330
SERVICE BULLETIN
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
20-15-00 22-97-00 27-93-34
27-96-00
ATA Common Support Data Dictionary (CSDD),
Chapter 2
Elec. Std. Practices Manual (ESPM)
 20-55-00
Service Bulletin (SB)
 A330-27-3205
A330-27-3207
Vendor Service Bulletin (VSB)
 AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K2-27-023
K. PUBLICATION AFFECTED
Aircraft Wiring List (AWL)
Illustrated Parts Catalog (IPC)
 27-93-08
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
FCPC
 LA2K2B100DG0000
 LA2K2B100DH0000
 03
 NO
 (1) (2)
FCPC
 LA2K01500AF0000
 LA2K2B100DH0000
 03
 NO
 (2) (3)
FCPC
 LA2K1A100DF0000
 LA2K2B100DH0000
 03
 NO
 (2) (4)
OBRM1
 LA2K2B100DG0100
 LA2K2B100DH0100
 03
 NO
 (1)
OBRM2
 LA2K2B100DG0200
 LA2K2B100DH0200
 03
 NO
 (1)
NOTE
: For definitions of interchangeability codes in column INT., refer to ATA
Common Support Data Dictionary (CSDD), Chapter 2.
NOTE
: Only the mixability configuration(s) and condition(s) stated in this Service
Bulletin are approved.
NOTE
 (1)
: Not interchangeable, but one-way interchangeable as a set.
- When the old PN FCPC LA2K2B100DG0000 (and its associated OBRM
PNs LA2K2B100DG0100 and LA2K2B100DG0200) is removed, it may be
replaced:
. By the old PN FCPC LA2K2B100DG0000 (and its associated OBRM
PNs LA2K2B100DG0100 and LA2K2B100DG0200)
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 13
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SERVICE BULLETIN
. By new PN FCPC LA2K2B100DH0000 (and its associated OBRM
PNs LA2K2B100DH0100 and LA2K2B100DH0200) only if the
complete set of old PN is replaced with a set of new PN.
- When the new PN FCPC LA2K2B100DH0000 (and its associated OBRM
PNs LA2K2B100DH0100 and LA2K2B100DH0200) is removed, it must
be replaced by new PN FCPC LA2K2B100DH0000 (and its associated
OBRM PNs LA2K2B100DH0100 and LA2K2B100DH0200).
NOTE
 (2)
: Mixed configuration of FCPC standard P15/M24 (hardware LA2K2) with
P14/M23 (hardware LA2K1) or M23 (hardware LA2K0) or P13/M22 (hardware
LA2K2 is(are) not allowed.
NOTE
 (3)
: Not interchangeable, but one-way interchangeable as a set.
- When the old PN FCPC LA2K01500AF0000 (and its associated OBRM
PNs LA2K01500AF0100 and LA2K01500AF0200) is removed, it may be
replaced:
. By the old PN FCPC LA2K01500AF0000 (and its associated OBRM
PNs LA2K01500AF0100 and LA2K01500AF0200)
. By new PN FCPC LA2K2B100DH0000 (and its associated OBRM
PNs LA2K2B100DH0100 and LA2K2B100DH0200) only if the
complete set of old PN is replaced with a set of new PN.
- When the new PN FCPC LA2K2B100DH0000 (and its associated OBRM
PNs LA2K2B100DH0100 and LA2K2B100DH0200) is removed, it must
be replaced by new PN FCPC LA2K2B100DH0000 (and its associated
OBRM PNs LA2K2B100DH0100 and LA2K2B100DH0200).
NOTE
 (4)
: Not interchangeable, but one-way interchangeable as a set.
- When the old PN FCPC LA2K1A100DF0000 (and its associated OBRM
PNs LA2K1A100DF0100 and LA2K1A100DF0200) is removed, it may be
replaced:
. By the old PN FCPC LA2K1A100DF0000 (and its associated OBRM
PNs LA2K1A100DF0100 and LA2K1A100DF0200)
. By new PN FCPC LA2K2B100DH0000 (and its associated OBRM
PNs LA2K2B100DH0100 and LA2K2B100DH0200) only if the
complete set of old PN is replaced with a set of new PN.
- When the new PN FCPC LA2K2B100DH0000 (and its associated OBRM
PNs LA2K2B100DH0100 and LA2K2B100DH0200) is removed, it must
be replaced by new PN FCPC LA2K2B100DH0000 (and its associated
OBRM PNs LA2K2B100DH0100 and LA2K2B100DH0200).
M. SPARES
FCPC LA2K01500AF0000
FCPC LA2K1A100DF0000
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 14
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SERVICE BULLETIN
FCPC LA2K2B100DG0000
The parts listed here must not be installed anymore on aircraft which have accomplished this
Service Bulletin or which have the equivalent production modification embodied.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 15
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2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Vendor parts are to be procured from
Equipment BFEA01
Equipment BFEA02
AIRBUS OPERATIONS SAS
AVIONICS AND SIMULATION PRODUCTS
VENDOR CODE F6198
EYY - M8621 - 316, route de Bayonne
31060 TOULOUSE Cedex 09 - FRANCE
e mail: systems.support@airbus.com
FAX : 33 (0)5 61 18 04 94
Or Modification of removed equipment should be negotiated directly with AIRBUS
OPERATIONS SAS as per instructions given in Service Bulletin No. LA2K2-27-023
Reidentified part set REIDA01
 AIRBUS OPERATIONS SAS
AVIONICS AND SIMULATION PRODUCTS
VENDOR CODE F6198
EYY - M8621 - 316, route de Bayonne
31060 TOULOUSE Cedex 09 - FRANCE
e mail: systems.support@airbus.com
FAX : 33 (0)5 61 18 04 94
(2) Price and Availability
Equipment BFEA01
No AIRBUS kit will be provided.
Procurement terms for the equipment must be negotiated with the equipment supplier.
Equipment BFEA02
No AIRBUS kit will be provided.
Procurement terms for the equipment must be negotiated with the equipment supplier.
Reidentified part set REIDA01
No AIRBUS kit will be provided.
Refer to AIRBUS OPERATIONS SAS Servic e Bulletin No. LA2K2-27-023 for the
equipment modification sales terms.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 17
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B. INDUSTRY SUPPORT INFORMATION
For equipment BFEA01 and BFEA02, industry support terms for the equipment must be
negotiated with the equipment supplier.
For re-identified part set REIDA01, refer to AIRBUS OPERATIONS SAS Service Bulletin No.
LA2K2-27-023 for the industry support terms of the Vendor Service Bulletin parts and labor.
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit
management department.
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
France
E-mail: monitored.retrofit@airbus.com
C. LIST OF COMPONENTS
No Kit
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
None
(2) Components
None
(3) Equipment
Equipment BFEA01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K2B100DH0000
 3
 FCPC
 LA2K01500AF0000
 03
LA2K1A100DF0000
 03
LA2K2B100DG0000
 03
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.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 18
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Equipment BFEA02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 ITEM
 OLD PART N˚
 INT
 SEE
NOTES
LA2K2B100DH0100
 3
 OBRM1
 LA2K2B100DG0100
 03
LA2K2B100DH0200
 3
 OBRM2
 LA2K2B100DG0200
 03
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
Reidentified part set REIDA01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K2B100DH0100
 OBRM1
 LA2K2B100DG0100
LA2K2B100DH0200
 OBRM2
 LA2K2B100DG0200
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS SAS
Service Bulletin No. LA2K2-27-023.
F. TOOLING
(1) Tooling - Price and Availability
None
(2) Tools
To accomplish TASK 273222-831-803 001 OPTION 3 - Upgrade by Reprogramming of
FCPC(s) OBRM(s) in accordance with VSB on Bench of this Service Bulletin, it is
necessary to use the tools defined in AIRBUS OPERATIONS SAS Service Bulletin No.
LA2K2-27-023.
(3) Special Tools
None
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 19
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3. ACCOMPLISHMENT INSTRUCTIONS
Task 273222-831-801-001 - OPTION 1 - Upgrade by Replacement of FCPC(s) 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 classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. Other paragraphs are recommended and may be deviated
from, done as part of other actions or done with accepted methods different from
those given in the Service Bulletin, as long as the RC paragraphs can be done and
the aircraft can be put back into a serviceable condition.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
For any deviations to the instructions contained herein, contact Airbus for further
instructions and approval.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 21
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NOTE
: To accomplish this Service Bulletin, you have 3 options but, in case of replacement
of M23 (hardware LA2K0) or P14/M23 (hardware LA2K1) by P15/M24 (hardware
LA2K2), only TASK 273222-831-801 001 OPTION 1 - Upgrade by Replacement of
FCPC(s) on Aircraft is possible.
Task Associated Data
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.50
ELAPSED TIME (HOURS)
 2.50
A. GENERAL
(1) Subtask 273222-910-001-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
(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.
(2) Subtask 273222-839-001-001 - 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 273222-941-001-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 22
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configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPC(s) (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
C. PROCEDURE
(1) Subtask 273222-960-001-001 - Replace the FCPC(s)
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 1.00
Minimum number of person
 1
Subtask elapsed time
 1.00
Skills
 ELECTRICAL
Material necessary to do the job
Equipment BFEA01
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K2B100DH0000
 3
 FCPC
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 23
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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 27-93-34-000-801
Task 27-93-34-400-801
(a) Remove, refer to AMM Task 27-93-34-000-801:
FIN 2CE1
1 FCPC LA2K2B100DG0000
or
FIN 2CE1
1 FCPC LA2K01500AF0000
or
FIN 2CE1
1 FCPC LA2K1A100DF0000
and
FIN 2CE2
1 FCPC LA2K2B100DG0000
or
FIN 2CE2
1 FCPC LA2K01500AF0000
or
FIN 2CE2
1 FCPC LA2K1A100DF0000
and
FIN 2CE3
1 FCPC LA2K2B100DG0000
or
FIN 2CE3
1 FCPC LA2K01500AF0000
or
FIN 2CE3
1 FCPC LA2K1A100DF0000
(b) Install, refer to AMM Task 27-93-34-400-801:
FIN 2CE1
1 FCPC LA2K2B100DH0000
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 24
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and
FIN 2CE2
1 FCPC LA2K2B100DH0000
and
FIN 2CE3
1 FCPC LA2K2B100DH0000
D. TEST
(1) Subtask 273222-700-001-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(a) Job Set-up:
1
 Remove the safety clip(s) and/or tag(s) and close/unlock the circuit breaker(s)
as specified after the installation of the FCPC(s) (2CE1, 2CE2 and 2CE3),
refer to AMM Task 27-93-34-400-801.
(b) Procedure:
1
 Do the test procedure as specified after the installation of the FCPC(s) (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
E. CLOSE-UP
(1) Subtask 273222-942-002-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(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 in the installation of the FCPC(s) (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 25
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Task 273222-831-802-001 - OPTION 2 - Upgrade by Replacement of FCPC(s) OBRM(s) 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.
CAUTION
: REFER TO AMM 20-15-00, Page Block 201 FOR ELECTROSTATIC
DISCHARGE PRECAUTIONS.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has a procedure accepted by the local authority
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. Other paragraphs are recommended and may be deviated
from, done as part of other actions or done with accepted methods different from
those given in the Service Bulletin, as long as the RC paragraphs can be done and
the aircraft can be put back into a serviceable condition.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 27
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For any deviations to the instructions contained herein, contact Airbus for further
instructions and approval.
NOTE
: To accomplish this Service Bulletin, you have 3 options but, in case of replacement
of M23 (hardware LA2K0) or P14/M23 (hardware LA2K1) by P15/M24 (hardware
LA2K2), only TASK 273222-831-801 001 OPTION 1 - Upgrade by Replacement of
FCPC(s) on Aircraft is possible.
NOTE
: TASK 273222-831-802 001 OPTION 2 - Upgrade by Replacement of FCPC(s)
OBRM(s) on Aircraft is applicable to the operators fitted with FCPC standard
P13/M22 (hardware LA2K2).
Task Associated Data
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
A. GENERAL
(1) Subtask 273222-910-002-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
(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.
(2) Subtask 273222-839-002-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 28
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B. PREPARATION
(1) Subtask 273222-941-002-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPC(s) (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
NOTE
: The circuit breakers will be managed in SUBTASK 273222-960-002
001 Replace the OBRMs to allow the BITE test of the Electrical
Flight Control System (EFCS).
C. PROCEDURE
(1) Subtask 273222-960-002-001 - Replace the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 29
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Manpower Resources
Manhours
 0.50
Minimum number of person
 1
Subtask elapsed time
 0.50
Skills
 ELECTRICAL
Material necessary to do the job
Equipment BFEA02
ITEM
 NEW PART N˚
 QTY (UM)
 KEYWORD
 SEE
NOTES
LA2K2B100DH0100
 3
 OBRM1
LA2K2B100DH0200
 3
 OBRM2
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 27-93-34-000-801
Task 27-96-00-740-807
(a) Before replacement of the OBRMs:
1
 On the FLT CTL section of the overhead panel 241VU (212VU), make sure
that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the
OFF and FAULT legends of this (these) pushbutton switch(es) are off).
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the old PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Open, safety/lock and tag this (these) circuit breaker(s) as specified in the
removal of the FCPC(s) (2CE1, 2CE2 and 2CE3), refer to AMM Task
27-93-34-000-801.
(b) Remove the OBRMs from the FCPC(s) (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K2B100DG0100
and
3 OBRM2 LA2K2B100DG0200
NOTE
: Some OBRMs are located behind a flap on the equipment, open it if
necessary.
NOTE
: To remove the OBRM, unlock the two locks located at the lower
and upper extremities of the OBRM.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 30
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(c) Install the OBRMs on the FCPC(s) (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K2B100DH0100
and
3 OBRM2 LA2K2B100DH0200
NOTE
: Re-identification of the FCPC(s) from PN LA2K2B100DG0000 to PN
LA2K2B100DH0000 is automatically performed by replacement of
the OBRMs, nevertheless, the responsible quality inspector can put
his own sticker and his own control seal on the front face to confirm
the replacement of the OBRMs.
D. TEST
(1) Subtask 273222-700-002-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 22-97-00-740-801
Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-802
Task 27-96-00-740-807
(a) Job Set-up:
1
 Remove the safety clip(s) and/or tag(s) and close/unlock this (these) circuit
breaker(s) as specified in the installation of the FCPC(s) (2CE1, 2CE2 and
2CE3), refer to AMM Task 27-93-34-400-801.
(b) Procedure:
1
 After power-up, on the FLT CTL section of the overhead panel 241VU
(212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es)
is (are) pushed (the OFF and FAULT legends of this (these) pushbutton
switch(es) are off).
If a FAULT is present, do a reset with the concerned pushbutton switch.
If FAULT persists, replace the concerned computer, refer to AMM Task
27-93-34-000-801 and AMM Task 27-93-34-400-801.
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the new PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Do the BITE test of the EFCS (SYSTEM TEST), refer to AMM Task
27-96-00-740-802.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 31
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4
 If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III
capability test, refer to AMM Task 22-97-00-740-801.
E. CLOSE-UP
(1) Subtask 273222-942-003-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(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 in the installation of the FCPC(s) (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 32
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Task 273222-831-803-001 - OPTION 3 - Upgrade by Reprogramming of FCPC(s) OBRM(s) in
accordance with VSB on Bench
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.
CAUTION
: REFER TO AMM 20-15-00, Page Block 201 FOR ELECTROSTATIC
DISCHARGE PRECAUTIONS.
NOTE
: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
’refer to’ are used and the operator has a procedure accepted by the local authority
he belongs to, the accepted alternative procedure can be used. When the words ’in
accordance with’ are used then the given procedure must be followed.
NOTE
: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE
: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE
: This Service Bulletin is classified mandatory or expected to be classified mandatory
by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these
accomplishment instructions are Required for Compliance (RC) and must be done
to comply with the AD. Other paragraphs are recommended and may be deviated
from, done as part of other actions or done with accepted methods different from
those given in the Service Bulletin, as long as the RC paragraphs can be done and
the aircraft can be put back into a serviceable condition.
NOTE
: This Service Bulletin contains the instructions for the on-aircraft maintenance
necessary to ensure the continued airworthiness of the aircraft.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 33
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SERVICE BULLETIN
For any deviations to the instructions contained herein, contact Airbus for further
instructions and approval.
NOTE
: To accomplish this Service Bulletin, you have 3 options but, in case of replacement
of M23 (hardware LA2K0) or P14/M23 (hardware LA2K1) by P15/M24 (hardware
LA2K2), only TASK 273222-831-801 001 OPTION 1 - Upgrade by Replacement of
FCPC(s) on Aircraft is possible.
NOTE
: TASK 273222-831-803 001 OPTION 3 - Upgrade by Reprogramming of FCPC(s)
OBRM(s) in accordance with VSB on Bench is applicable to the operators fitted
with FCPC standard P13/M22 (hardware LA2K2).
Task Associated Data
Zone
120
Modified FIN
2CE1 2CE2 2CE3
Access
Door
 811
Manpower
TOTAL MANHOURS
 2.00
ELAPSED TIME (HOURS)
 2.00
Additional manhours related to Vendor SB; refer to:
AIRBUS OPERATIONS SAS Service Bulletin No. LA2K2-27-023
A. GENERAL
(1) Subtask 273222-910-003-001 - Standard Practices
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 06-20-00, Page Block 001
06-31-53, Page Block 001
(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) Tag all the parts you must remove and retain to make the subsequent installation
easier.
(d) Put all the retained hardware in identified plastic bags and attach the bags to the
related unit.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 34
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SERVICE BULLETIN
(2) Subtask 273222-839-003-001 - Administrative
Manpower Resources
Skills
 NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
B. PREPARATION
(1) Subtask 273222-941-004-001 - Job Set-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 12-34-24-860-802
Task 27-93-34-000-801
NOTE
: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety
locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration
- Parking brake applied
- Aircraft electrical network de-energized
- Hydraulic system s depressurized
- Access to the cockpit and cabin is available
- All circuit breakers are in closed position
- All controls in NORM, AUTO or OFF position.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-860-802.
(b) Do the job set-up procedure as specified in the removal of the FCPC(s) (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-000-801.
NOTE
: The circuit breakers will be managed in another SUBTASK
273222-020-001 001 Remove the OBRMs to allow the BITE test of
the EFCS.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 35
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SERVICE BULLETIN
C. PROCEDURE
(1) Subtask 273222-020-001-001 - Remove the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 ELECTRICAL
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-000-801
Task 27-96-00-740-807
(a) Before reprogramming of the OBRMs:
1
 On the FLT CTL section of the overhead panel 241VU (212VU), make sure
that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es) is (are) pushed (the
OFF and FAULT legends of this (these) pushbutton switch(es) are off).
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the old PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Open, safety/lock and tag this (these) circuit breaker(s) as specified in the
removal of the FCPC(s) (2CE1, 2CE2 and 2CE3), refer to AMM Task
27-93-34-000-801.
(b) Remove the OBRMs from the FCPC(s) (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K2B100DG0100 Retain
NOTE
: Retained for modification.
and
3 OBRM2 LA2K2B100DG0200 Retain
NOTE
: Retained for modification.
NOTE
: Some OBRMs are located behind a flap on the equipment, open it if
necessary.
NOTE
: To remove the OBRM, unlock the two locks located at the lower
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 36
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and upper extremities of the OBRM.
(2) Subtask 273222-831-001-001 - Reprogram the OBRMs in accordance with VSB
Material necessary to do the job
Reidentified part set REIDA01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K2B100DH0100
 OBRM1
 LA2K2B100DG0100
LA2K2B100DH0200
 OBRM2
 LA2K2B100DG0200
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K2-27-023.
References
Vendor Service Bulletin (VSB)
 AIRBUS OPERATIONS SAS LA2K2-27-023
(a) Reprogram and re-identify the OBRMs in accordance with AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K2-27-023.
(b) After the re-identification:
3 OBRM1 LA2K2B100DG0100
becomes
3 OBRM1 LA2K2B100DH0100
and
3 OBRM2 LA2K2B100DG0200
becomes
3 OBRM2 LA2K2B100DH0200
(3) Subtask 273222-420-001-001 - Install the OBRMs
Work Zones and Access Panels
Zone
 Access/Work location
120
 Access
 Door 811
Work location
 Electrical panel 800VU
Electrical panel 915VU
Manpower Resources
Manhours
 0.25
Minimum number of person
 1
Subtask elapsed time
 0.25
Skills
 ELECTRICAL
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 37
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SERVICE BULLETIN
Material necessary to do the job
Reidentified part set REIDA01
ITEM
 NEW PART N˚
 KEYWORD
 ITEM
 OLD PART N˚
 SEE
NOTES
LA2K2B100DH0100
 OBRM1
LA2K2B100DH0200
 OBRM2
NOTE
: Parts are re-identified in accordance with the AIRBUS OPERATIONS
SAS Service Bulletin No. LA2K2-27-023.
(a) Install the OBRMs on the FCPC(s) (2CE1, 2CE2 and 2CE3):
3 OBRM1 LA2K2B100DH0100
and
3 OBRM2 LA2K2B100DH0200
NOTE
: Re-identification of the FCPC(s) (2CE1, 2CE2 and 2CE3) from
PN LA2K2B100DG0000 to PN LA2K2B100DH0000 is automatically
performed by replacement of the OBRMs, nevertheless, the
responsible quality inspector can put his own sticker and his own
control seal on the front face to confirm the replacement of the
OBRMs.
D. TEST
(1) Subtask 273222-700-003-001 - Testing
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 22-97-00-740-801
Task 27-93-34-000-801
Task 27-93-34-400-801
Task 27-96-00-740-802
Task 27-96-00-740-807
(a) Job Set-up:
1
 Remove the safety clip(s) and/or tag(s) and close/unlock this (these) circuit
breaker(s) as specified in the installation of the FCPC(s) (2CE1, 2CE2 and
2CE3), refer to AMM Task 27-93-34-400-801.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 38
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(b) Procedure:
1
 After power-up, on the FLT CTL section of the overhead panel 241VU
(212VU), make sure that the PRIM 1 (PRIM 2) (PRIM 3) pushbutton switch(es)
is (are) pushed (the OFF and FAULT legends of this (these) pushbutton
switch(es) are off).
If a FAULT is present, do a reset with the concerned pushbutton switch.
If FAULT persists, replace the concerned computer, refer to AMM Task
27-93-34-000-801 and AMM Task 27-93-34-400-801.
2
 Do the BITE test of the EFCS (LRU IDENT), refer to AMM Task
27-96-00-740-807 and make sure that the new PN of the FCPCs (2CE1, 2CE2
and 2CE3) are correct.
NOTE
: Print the LRU IDENTIFICATION page (if the printer is not
available, a visual check is acceptable).
3
 Do the BITE test of the EFCS (SYSTEM TEST), refer to AMM Task
27-96-00-740-802.
4
 If the airline operates the aircraft in CAT 3 conditions, do the LAND CAT III
capability test, refer to AMM Task 22-97-00-740-801.
E. CLOSE-UP
(1) Subtask 273222-942-004-001 - Close-up
Manpower Resources
Skills
 NON SPECIFIC
References
Aircraft Maintenance Manual (AMM)
 Task 27-93-34-400-801
(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 in the installation of the FCPC(s) (2CE1,
2CE2 and 2CE3), refer to AMM Task 27-93-34-400-801.
(c) Put the aircraft back to its initial configuration.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 39
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SERVICE BULLETIN
Service Bulletin REPORTING
TITLE: FLIGHT CONTROLS - FCPC - INSTALL FCPC P15/M24 2K2
MODIFICATION No.: 206414S33846
SB Reporting status
This Service Bulletin will only be incorporated into affected customized Maintenance and Flight
Operations Products if it is duly reported to Airbus.
General information
The SB Reporting policy is published in ISI 00.00.00135. This document provides information regarding:
the SB Reporting means and benefits, the update of customized Maintenance Products and customized
Flight Operations Products.
If this Service Bulletin has an operational impact, refer to paragraph "Flight Operations Products" for
further information on the update of affected Flight Operations Products.
SB Reporting procedure
Standard practice to report SB is to use the online reporting application on AirbusWorld.
Refer to ISI 00.00.00179:
- For complete information on reporting means to Airbus. Question 2 "What are the standard
practices for SB reporting?"
- If this SB requires previous or simultaneous accomplishment of other SBs, Question 3 "What about
the reporting of prerequisite Service Bulletin?"
NOTE:
 ISI 00.00.00179 covers all the frequently asked questions about SB Reporting. It is revised on a
regular basis.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 1
5
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SERVICE BULLETIN
QUALITY PERCEPTION FORM
Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data
that you provide us will be used to analyse areas of difficulties and to take corrective action to further
improve the quality of our Service Bulletins.
We thank you for the time you have taken in completing this form.
(Please rate on a scale of 1 to 4, with 4 being the highest score)
- Quality rating of this SB 4321
- Quality rating of the Accomplishment Instructions 4321
- Quality rating of the Illustrations 4321
- Is this SB easy to understand ? Y/N
If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a
short description of the issue.
Planning Material Instructions
X Effectivity X Kit content X Preparation
X Reason X List of Materials Operator Supplied X Mod/Inspection
X Manpower X Industry support X Test
X References X Re-identification X Close-Up
X Publication X Tooling X Illustrations
Comments:
Operator: Date:
Name/Title:
Please return this form to:
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX FRANCE
Attn : SEM4 Service Bulletins Management
F A X:( 3 3 )56 19 34 25 1
Or via your Resident Customer Support Office.
DATE: Feb 16/17 SERVICE BULLETIN No.: A330-27-3222
REVISION No.: 00 - Feb 16/17 Page: 1
5
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

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