@A318/A319/A320/A321

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 22

TITLE: AUTO-FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL

STD FAC CAA02 (SHARKLET CAPABILITY AND ROPS FUNCTION)

MODIFICATION No.: 155315P12753

This page transmits Revision No.03 of Service Bulletin No.A320-22-1447

ADDITIONAL WORK

**CONF ALL

No additional work is required by this revision for aircraft modified by any previous issue.

REASON

Revision No. 03 issued to extend the effectivity.

CHANGES

The main changes of this revision are:

- effectivity extended,

- another possibility to connect the PDL added in the "Task 221447-831-801-001 - Modification of the

FAC Software (FINs 1CC1SW1 and 1CC2SW1)",

- minor changes applied.

FRONT MATTER

AUTO-FLIGHT - FLIGHT

AUGMENTATION COMPUTER (FAC) -

INSTALL STD FAC CAA02 (SHARKLET

CAPABILITY AND ROPS FUNCTION)

CONFIGURATION UPDATED R

SUMMARY

REASON/DESCRIPTION/OPERATIONAL

CONSEQUENCES

REASON UPDATED R

GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

CONCURRENT REQUIREMENTS CONCURRENT REQUIREMENTS UPDATED R

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 1

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REVISION TRANSMITTAL SHEET

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Configuration definition

CONF 001 CONFIGURATION DEFINITION UPDATED R

Material Effectivity MATERIAL EFFECTIVITY UPDATED R

CONCURRENT REQUIREMENTS CONCURRENT SB LIST UPDATED R

REASON

Advantages ADVANTAGES UPDATED R

Operational/Maintenance

Consequences

OPERATIONAL/MAINTENANCE CONSEQUENCES

UPDATED

R

DESCRIPTION DESCRIPTION UPDATED R

REFERENCES REFERENCED DOCUMENTATION UPDATED R

PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R

INTERCHANGEABILITY/MIXABILITY INTERCHANGEABILITY/MIXABILITY UPDATED R

SPARES SPARES UPDATED

PART NUMBER UPDATED

PART NUMBER DESCRIPTION UPDATED

R

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Price and Availability PRICE AND AVAILABILITY UPDATED R

ACCOMPLISHMENT INSTRUCTIONS

TASK 221447- 831-801-001-Modification

of the FAC Software (FINs 1CC1SW1 and

1CC2SW1) on Aircraft

TASK SOLUTION UPDATED

CAUTION UPDATED

R

Subtask 221447-470-001-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

NOTE UPDATED

FIN UPDATED

R

Subtask 221447-960-002-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

Subtask 221447-700-001-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

R

TASK 221447- 831-802-001-Modification

of the FAC Software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on

Aircraft

TASK SOLUTION UPDATED

CAUTION UPDATED

R

Subtask 221447-831-002-001 SUBTASK SOLUTION UPDATED R

Subtask 221447-831-003-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

TASK 221447- 831-803-001-Modification

of the FAC Software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on

Bench

TASK SOLUTION UPDATED

CAUTION UPDATED

R

Subtask 221447-831-004-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

LOCATION UPDATED

R

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 2

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REVISION TRANSMITTAL SHEET

Subtask 221447-831-005-001 SUBTASK SOLUTION UPDATED R

Subtask 221447-831-006-001 SUBTASK SOLUTION UPDATED

PANEL UPDATED

LOCATION UPDATED

R

Subtask 221447-831-007-001 SUBTASK SOLUTION UPDATED

NOTE UPDATED

R

FILING INSTRUCTIONS

This Service Bulletin has been generated electronically and is reissued as a complete document.

Replace the complete document.

Put this Revision Transmittal Sheet in front of the Service Bulletin.

HISTORY OF PREVIOUS REVISIONS

Revision No. 01 issued to update the effectivity.

Revision No. 02 issued to extend the effectivity and to add two new possibilities to install the standard

FAC CAA02 in accordance with VSB.

REVISION SEQUENCE

ORIGINAL: Oct 18/13

REVISION No. : 01 - Sep 18/14

REVISION No. : 02 - Dec 02/14

REVISION No. : 03 - Apr 21/15

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 3

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REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 4

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SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

ATA SYSTEM: 22

TITLE: AUTO-FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL

STD FAC CAA02 (SHARKLET CAPABILITY AND ROPS FUNCTION)

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 155315P12753

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

This Service Bulletin has been issued in order to introduce Flight Augmentation Computer (FAC) STD

CAA02 on A318/A319/A320.

This Service Bulletin is published to advise all operators of A318/A319/A320 aircraft of the issue of

THALES AVIONICS Service Bulletin No. C13206A-22-001.

In comparison with FAC CAA01 PN C13206AA01, this new standard introduces the following software

modifications:

- Sharklets capability FAC CAA02 standard introduces software adaptation for A319/A320/CFM/IAE

equipped with Sharklets (weight and Center of Gravity (CG), characteristic speeds).

. Weight and CG computation are adapted to take into account the lower fuel consumption of

Sharklets installations.

. Characteristic speeds: V alpha-Prot, V alpha-Max and V Stall-Warning are adapted to take into

account the Sharklets aerodynamic impact.

Moreover, characteristic speeds are computed using the Flight Management System (FMS) weight. This

minimizes the consequences of a possible weight computation imprecision (no effect on characteristic

speeds displayed on PFD).

- Runway Overrun Prevention System (ROPS) function.

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 1

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SUMMARY

FAC CAA02 includes the software modifications necessary to perform the ROPS function (MOD No.

155269P12511):

- During the approach, FAC computes an estimation of the braking distance of the aircraft on

a dedicated runway. If a runway overrun is detected, ROPS function triggers aural alerts and

Primary Flight Display (PFD) messages requiring either to perform a Go Around or to apply the

maximum braking. On FAC CAA02, this function is activated by a dedicated pin program AB-06C

(MP P12580). This function is compatible with both Terrain Awareness and Warning System

(TAWS) equipment: Enhanced Ground Proximity Warning System (EGPWS) and Traffic, Terrain

and Transponder Collision Avoidance System (T3CAS).

NOTE: For ROPS function, a new Aeronautical Radio Incorporated (ARINC) bus from the

TAWS is acquired by the FAC to know the type of TAWS installed (EGPWS or T3CAS).

- Other improvements:

. Reduction of the Rudder Travel Limitation at high speed. RTLU aims at limiting vertical tail

plane loads.

. Introduction of Stop Rudder Input warning. This audio warning alerts the crew in case of

inadequate and inappropriate use of the rudder pedals in flight. This modification can be

activated by pin program (separate aircraft MOD No. 154473P13357) and requires Flight

Warning Computer (FWC) standard H2F7.

. Computation of a theoretical Trimmable Horizontal Stabilizer (THS) position computation using

the CG position computed from Multifunction Control and Display Unit (MCDU) pilot inputs.

This pseudo THS position is sent to the FWC to trigger the new "Pitch trim MCDU CG

disagree" alert, in case the actual THS position does not correspond to the computed

theoretical position. This function requires FWC standard H2F6.

. Reduction of about 99 percent of a small rudder trim offset (about 0.1 deg) occurring in case of

short power supply cut (Flight Crew Operating Manual (FCOM) temporary Revision No. 356-1).

. Correction of loss of flight plan upon Landing Gear Control and Interface Unit (LGCIU) Nose

wheel failure.

FAC CAA02 includes the software modifications necessary for the introduction of Stop Rudder Input

warning. This audio warning alerts the crew in case of inadequate and inappropriate use of the

rudder pedals in flight. This modification is activated by pin program (separate aircraft MOD No.

154473P13357) Service Bulletin No. A320-22-1280 and requires Flight Warning Computer (FWC)

standard H2F7 as minimum standard.

NOTE: The activation of this function is mandated by European Aviation Safety Agency (EASA).

The operational consequences of this Service Bulletin are impacts on Flight Crew Operating Manual

(FCOM).

For the operational impact, refer to the Modification Operational Impact (MOI) No. 155315.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

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SUMMARY

EVALUATION TABLE

POTENTIAL AD NO A/C OPERATION AFFECTED YES

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

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

disruptions.

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 Media

Equipment BFEA02 1 See SB Media

EFFECTIVITY

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

03X 11S 15S 15T 16T 17R 17S 17W 20Q 26S 27V 29S 31P

31V 31X 32Q 35T 35U 36R 38W 40S 41S 43S 46U 47P 48P

48T 52T 53Z 54S 59Z 61W 62X 66P 69X 73W 74T 76W 79W

80X 83V 85T 85U 86P 86Z 87Q 89T 90Q 91X 94W 95V 95W

98W AAF AAL AAR AAW AAY ABL ABQ ABY ACA ACI ADH ADR

AEE AFL AFR AGY AHY AIB AIC AIJ AJD ALK AMC AMU ANA

ANR ANZ AOJ APJ ART ARU ASL ATR AUA AUH AVA AWC AXM

AZA AZI B2V BAW BEC BEL BER BGF BGH BHP BJN BKP BQB

BRS BSX BTN C2C C8J C9G CAA CBJ CCA CCM CEB CEF CES

CHB CIB CQH CQN CRK CSA CSC CSN CSZ CTN CTV CUA CYP

D2F DAL DAT DCS DKH DLH DNU DNV DQA DRK DTR EAA EDW

EIN ETD ETJ EVA EVE EWG EZY F2I FFT FHY FIN FLI FPY

FRN FTZ G2X G4I G8E GAF GAP GBB GCR GFA GHT GLG GMI

GMR GOW GSW GWI HDA HKE HKJ I2L I2T IAC IAW IBE IBS

IGO IND IRA IRC ISR ISS IYE IZG JAD JAS JAV JBU JJP

JKT JSA JST JZR KAC KAY KFR KGL KKK KMF KNE KZR LAA

LAN LAO LBT LFO LIM LJB LKE LLC LLM LLP LMJ LMU LWA

LZB MAC MAU MEA MJF MJN MLD MLM MLR MMA MON MOV MRJ

MSC MSR MXA MYX NIA NKS NLY NMA NMB NVD NWS OAW OBS

OHY ONE ORF OZW PAL PGT PIA PIC PKZ PTI QAF QDA QTR

R1T RBA RBG RCT RFJ RJA RJD ROT RYW RZO SAA SAI SAS

SBI SDM SFJ SFW SGG SHJ SHU SKU SLK SMX SND SNX SOL

SUD SVA SVR SVW SWM SWR SYA SYR TAE TAI TAM TAP TAR

TBA TBJ TBZ TCW TGW THA THY TJS TNA TTW TVS TXP UAE

UAL UEA UJX UKN ULG UNA USA UZB VAR VIM VIP VIV VJC

VKG VLE VLG VNL VOI VRD VRE VVC WAU WGT WHT WOW WRC

WZZ

CONCURRENT REQUIREMENTS

Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the

following Service Bulletin:

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 3

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SERVICE BULLETIN

SUMMARY

Service Bulletin No. A320-22-1406

NOTE: Service Bulletin No. A320-22-1406 (AUTO FLIGHT - FLIGHT AUGMENTATION

COMPUTER (FAC) - INTRODUCE FAC CAA01) applies MOD No. 39468P11175.

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD YES

SOFT YES

OBRM NO

MANPOWER

Task 221447-831-801-001: Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

on Aircraft

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

Task 221447-831-802-001: Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with VSB on Aircraft

TOTAL MANHOURS 1.75

ELAPSED TIME (HOURS) 1.75

Additional manhours related to Vendor SB; refer to:

Modify the FAC software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with VSB on aircraft

THALES AVIONICS Service Bulletin

No. C13206A-22-001

Task 221447-831-803-001: Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with VSB on Bench

TOTAL MANHOURS 2.75

ELAPSED TIME (HOURS) 2.75

Additional manhours related to Vendor SB; refer to:

Modify the FAC Software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on Bench

THALES AVIONICS Service Bulletin

No. C13206A-22-001

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 4

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SERVICE BULLETIN

SUMMARY

APPENDICES

None

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 5

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SERVICE BULLETIN

SUMMARY

**CONF ALL

A A

A

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

ON AIRCRAFT CONFIGURATION (SEE FIG. A−FSCAA).

1CCMD1

N_SB_221447_5_SBAA_01_00

Figure A-FSBAA - Sheet 01

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

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SERVICE BULLETIN

SUMMARY

**CONF ALL

FR1

FR24A

Z210

A

B

C

B

A

C

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

ON AIRCRAFT CONFIGURATION (SEE FIG. A−FSBAA).

1CCMD1

N_SB_221447_5_SCAA_01_00

Figure A-FSCAA - Sheet 01

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 7

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SUMMARY

This Page Intentionally Left Blank

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 8

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 22

TITLE: AUTO-FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL

STD FAC CAA02 (SHARKLET CAPABILITY AND ROPS FUNCTION)

MODIFICATION No.: 155315P12753

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: TASK 221447-831-801 001 Modification of the FAC Software (FINs

1CC1SW1 and 1CC2SW1) on Aircraft of this Service Bulletin, is only

applicable to aircraft on which MOD No. 153590P12462 (Service Bulletin No.

A320-22-1405) is embodied.

(1) Models

318-111 318-112 319-111 319-112 319-113 319-114 319-115 319-131

319-132 319-133 320-211 320-212 320-214 320-216 320-231 320-232

320-233

(2) Effectivity by MSN

0029 0045-0046 0049-0057 0059 0064-0073 0076-0078 0081-0088 0093-0094 0096

0099 0104 0110-0113 0115-0119 0121-0127 0135 0137-0138 0140-0142 0148-0150

0152-0154 0157-0162 0164-0169 0171-0176 0178 0181-0183 0185 0189-0190 0192

0194-0195 0197-0203 0205-0214 0216-0220 0224 0229-0235 0237 0239-0244

0248-0249 0251-0256 0259-0270 0272-0277 0279 0281-0282 0284-0285 0287

0289-0298 0300-0303 0306-0309 0311-0312 0314 0316-0325 0328-0333 0339-0343

0345-0347 0350-0351 0353-0362 0366-0368 0370-0373 0376 0378 0380-0383

0386-0388 0390-0391 0393 0395-0396 0398-0410 0413-0424 0426-0432 0435-0436

0438-0439 0441-0442 0444-0445 0447-0452 0454-0457 0459-0460 0462-0466

0469-0470 0472 0475-0476 0479-0480 0482-0483 0485-0487 0489-0492 0496-0497

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 1

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SERVICE BULLETIN

0499-0501 0503-0504 0506-0508 0510-0512 0523 0525 0527-0528 0530-0531

0533-0534 0537 0539-0540 0542-0543 0545-0546 0548-0549 0551 0553-0554 0556

0558-0559 0561-0562 0565-0566 0568-0569 0571-0575 0577-0580 0582 0584-0585

0587-0589 0592 0594 0596 0598 0600 0603 0605 0607-0613 0616-0619 0621-0623

0625 0627 0629-0630 0634-0641 0643-0651 0653-0662 0665 0667 0669-0673 0676

0678-0679 0681-0683 0685-0686 0688-0691 0693-0698 0700-0707 0709 0711-0714

0716-0724 0726-0730 0732-0745 0747-0752 0754-0760 0762-0764 0766-0770

0773-0774 0776 0778-0780 0782-0786 0788 0790-0791 0793-0795 0797-0801

0803-0805 0807 0809 0812-0814 0816-0818 0820-0822 0824-0826 0828-0834

0836-0840 0842-0847 0849-0851 0853-0854 0856-0863 0865-0877 0879-0886

0888-0890 0892-0900 0902-0907 0909-0914 0916-0919 0921-0925 0927-0934

0936-0939 0942-0953 0955 0957-0958 0960 0962 0964-0967 0969 0971-0973

0975-0982 0984-0986 0988-0990 0992 0994 0996-1003 1005 1007 1009-1011

1013-1014 1016 1018-1020 1022 1025-1026 1028-1041 1043 1046-1059 1061-1079

1081-1093 1095-1097 1099-1112 1114-1132 1134-1143 1145-1152 1154-1160

1162-1173 1175-1184 1187 1189-1194 1196-1198 1200-1201 1203 1205-1206

1208-1213 1215-1217 1221-1226 1228-1232 1234-1237 1239-1240 1242-1249

1251-1259 1261-1272 1274-1275 1277 1279-1292 1294-1298 1300-1306 1308-1332

1334-1355 1357-1365 1367-1373 1375-1398 1400-1402 1404-1407 1409-1411

1413-1416 1418-1420 1422-1424 1426-1427 1429-1430 1432 1434-1435 1437

1439-1441 1443-1446 1448-1450 1452-1454 1456-1457 1459-1461 1463 1466-1471

1473-1475 1477-1480 1482-1486 1488-1491 1493-1495 1497-1498 1500-1502

1504-1510 1512-1516 1518 1520 1522-1524 1526-1530 1532-1535 1537-1538

1540-1553 1555-1571 1573-1586 1588-1595 1597-1601 1603-1606 1608-1610

1612-1613 1615-1618 1620-1622 1624-1628 1630-1631 1633-1635 1637 1639-1641

1643-1650 1652-1657 1659 1661-1665 1667-1669 1671-1674 1677-1680 1682-1689

1692-1694 1696-1700 1702-1703 1705-1706 1708-1710 1712 1714-1715 1717-1719

1721-1723 1725 1727-1728 1730-1733 1735-1747 1749-1762 1764-1767 1769-1771

1773-1775 1777-1782 1784-1787 1789-1793 1795-1797 1799-1806 1808-1810 1812

1814-1816 1818-1821 1823-1829 1831-1835 1837-1842 1844-1847 1849 1851-1858

1860-1868 1870-1877 1879-1880 1882-1886 1888-1904 1906-1918 1920 1922-1925

1927 1929 1931 1933-1938 1940 1942-1945 1947-1949 1951-1952 1954-1955

1957-1959 1961-1965 1968-1969 1971 1973 1975-1976 1979-1983 1986-1987

1989-1990 1993 1996-2004 2006-2016 2018-2020 2022-2024 2026-2040 2042-2044

2046-2050 2052-2054 2056-2059 2061-2063 2065-2066 2068-2075 2077-2079

2081-2104 2106 2108-2109 2112-2114 2116 2118-2127 2129-2189 2191-2207

2209-2210 2212-2215 2217 2219 2221-2225 2227-2233 2235-2246 2248-2254

2256-2260 2262-2266 2268-2269 2271-2275 2277-2289 2291-2302 2304 2306-2308

2310-2314 2316-2319 2321-2322 2325-2329 2331-2336 2338-2341 2343-2350

2352-2356 2358-2362 2364-2380 2382-2409 2411-2423 2425-2461 2463-2471

2473-2475 2477-2479 2481-2487 2489-2499 2501-2520 2522-2529 2531-2535

2537-2542 2544-2548 2550-2552 2554-2562 2564-2589 2591-2598 2600-2609

2611-2652 2654-2681 2683-2686 2688-2706 2708-2712 2714-2721 2723-2725

2727-2729 2731-2735 2737-2740 2742-2755 2757-2758 2760-2766 2768-2792

2794-2798 2800-2808 2810-2822 2824-2861 2863-2867 2869-2881 2883-2894

2896-2902 2904-2911 2913-2915 2917-2918 2920-2926 2928-2932 2934-2935

2937-2956 2958-2964 2966-2970 2972-2973 2975-2995 2997-2998 3000 3002-3004

3006-3012 3014 3016-3021 3023-3029 3031-3033 3035-3037 3039-3050 3052-3061

3063-3066 3068-3069 3071-3074 3076-3080 3082-3091 3093-3097 3099-3105

3107-3109 3111 3113-3119 3121-3125 3127-3129 3131-3145 3147-3162 3164-3190

3192-3197 3199-3206 3208-3211 3213 3215 3218-3221 3223-3228 3230-3232 3234

3236-3240 3242-3246 3248 3250 3252-3253 3255-3261 3263-3264 3266 3268-3273

3275-3282 3284-3289 3291-3293 3295-3296 3298-3301 3303-3306 3308-3314

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 2

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3316-3321 3323-3325 3327-3328 3330-3333 3335-3338 3341-3349 3351-3354

3356-3359 3361-3366 3368 3370 3373-3381 3383-3386 3388-3389 3391-3396 3398

3400 3402-3404 3406-3418 3420-3428 3430-3433 3435-3437 3439-3440 3442-3457

3460-3461 3463-3468 3470 3472-3492 3494-3497 3499-3503 3505-3506 3508

3510-3511 3513-3521 3524 3526 3528-3538 3540-3545 3547-3551 3553-3556

3558-3565 3567-3572 3574 3576-3582 3586 3588-3591 3594-3599 3601 3603-3605

3607-3611 3613-3618 3620-3622 3624 3626-3628 3630-3632 3634 3638 3640-3641

3643-3644 3646-3652 3654 3656-3664 3666-3668 3670-3672 3674-3677 3679-3680

3683-3687 3689-3707 3709-3711 3713-3716 3718-3721 3723-3724 3726-3729

3731-3736 3739 3741-3748 3750-3751 3753-3760 3762-3763 3765 3767-3783

3785-3791 3793-3795 3797-3805 3807-3813 3815 3817-3819 3821-3829 3831-3846

3848-3857 3859-3861 3863 3865-3866 3868 3870-3877 3880 3882-3883 3885-3892

3894-3898 3900-3915 3917-3919 3921-3923 3925 3927 3929 3931-3933 3935 3937

3939 3941-3943 3945-3947 3949-3950 3952-3954 3956-3959 3961-3963 3965

3967-3968 3970-3972 3974-3976 3978-3980 3982-3986 3988 3990-3992 3994-3995

3997-4001 4003-4004 4006-4008 4010-4015 4017-4021 4023-4024 4026-4030

4032-4040 4042-4043 4046 4048-4049 4051-4053 4055-4057 4059-4061 4063-4066

4068-4072 4075-4077 4079-4081 4083-4084 4086-4090 4092-4095 4097-4098

4100-4102 4104-4106 4108-4111 4113-4115 4117-4122 4124-4130 4132-4133 4135

4137 4139-4141 4143-4147 4149-4154 4156-4172 4174-4179 4181-4183 4185-4188

4190-4193 4195-4197 4199-4208 4210-4212 4214-4216 4218-4220 4222-4223

4225-4229 4231-4250 4252-4265 4267-4270 4272-4273 4275-4276 4278-4279

4281-4282 4284-4291 4293-4298 4300-4310 4312-4314 4316-4317 4319-4329

4331-4333 4335-4337 4339-4340 4342-4351 4353-4357 4359 4361-4368 4370-4373

4375-4376 4378-4381 4383-4386 4388-4405 4407-4415 4417-4419 4421-4429

4431-4460 4462-4466 4468-4471 4473-4493 4495-4499 4501-4529 4531-4533

4535-4537 4539-4541 4543-4544 4546-4559 4561-4569 4571-4576 4578-4584

4586-4589 4591-4606 4608-4610 4612-4616 4618-4625 4627-4637 4639-4642

4644-4647 4649-4653 4655-4661 4663-4668 4670-4671 4673-4681 4683-4697

4699-4702 4704-4705 4707-4709 4711-4718 4720-4727 4729-4730 4732-4736

4738-4745 4747-4752 4754-4760 4762-4770 4772-4778 4780-4782 4784-4787

4789-4791 4793-4810 4812-4818 4820-4823 4825 4827-4829 4831-4833 4835-4837

4839-4842 4844-4846 4848-4849 4851-4855 4857-4862 4864-4872 4874-4880

4882-4884 4886-4892 4894-4897 4899-4900 4902-4915 4917-4922 4924 4926-4931

4933-4934 4936-4939 4941-4944 4946-4948 4950-4956 4958-4959 4961 4963-4965

4967-4970 4972-4975 4977-4993 4995-5008 5010-5024 5026-5027 5029-5034

5036-5037 5039-5043 5045-5048 5050-5053 5055-5058 5060-5064 5066-5073

5075-5076 5078-5082 5084-5086 5088-5098 5100-5117 5119-5123 5125 5127-5132

5134-5153 5155-5159 5161-5163 5165-5168 5170-5172 5174-5176 5178-5179

5181-5185 5187-5191 5193-5196 5198 5200-5204 5206-5209 5211-5226 5228-5232

5234 5236 5238-5240 5242-5243 5245-5246 5248-5250 5252-5253 5255-5256

5258-5264 5266-5268 5270 5272-5274 5276-5278 5280-5281 5283-5284 5286

5288-5291 5293-5294 5296 5298-5299 5301-5302 5304-5305 5307-5308 5310-5313

5315-5316 5318-5320 5322-5326 5329-5331 5333-5335 5337-5339 5341-5342

5344-5345 5347-5349 5351-5353 5355-5356 5358-5367 5369-5373 5375-5376

5378-5381 5383-5384 5386-5387 5389-5391 5393-5401 5403 5405-5408 5410-5412

5414-5417 5419-5421 5423-5426 5428-5431 5433-5434 5436-5437 5439-5443

5445-5446 5448-5449 5451-5455 5457-5458 5460-5461 5463-5464 5466-5468

5471-5474 5476-5480 5482-5484 5486-5489 5491-5494 5496-5499 5501-5503

5505-5508 5510-5512 5514-5518 5520-5522 5524-5527 5529-5533 5535-5537

5539-5542 5544-5545 5547-5548 5550-5554 5556-5557 5559-5566 5568-5572 5574

5576-5581 5583 5585-5587 5589-5593 5595-5602 5604-5605 5607-5632 5634-5635

5637-5643 5645-5646 5648-5654 5656-5658 5660-5662 5664-5666 5668-5669

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 3

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5671-5673 5675-5680 5682-5683 5685-5688 5690-5695 5697-5698 5700-5704

5706-5708 5710-5714 5716-5719 5721-5727 5729-5732 5734-5735 5737-5742

5744-5746 5748-5750 5752-5754 5756-5757 5759-5762 5764-5766 5768-5769

5771-5773 5775-5778 5780-5782 5784-5786 5788-5789 5791-5794 5796-5799

5801-5802 5804-5807 5809-5819 5821-5824 5826-5833 5835 5837 5839-5841 5844

5846-5848 5850-5853 5855-5859 5861-5864 5866-5871 5873-5875 5877-5880 5882

5885-5889 5891-5894 5896-5898 5900-5903 5905-5908 5910-5912 5914-5915

5917-5918 5920-5921 5924-5928 5930-5931 5933-5934 5937 5940-5945 5948 5951

5953-5954 5956-5957 5959 5962-5964 5967-5968 5970-5971 5973-5974 5976-5979

5981-5982 5985-5986 5988-5990 5993 5996-5997 5999 6001 6003-6004 6007-6008

6011-6012 6014-6015 6017-6019 6022-6023 6028-6030 6032 6034 6037 6039 6041

6043-6045 6047-6048 6052 6058 6060-6062 6064 6068-6069 6071-6073 6075-6079

6081-6082 6084 6086 6088 6090-6091 6093 6095-6096 6098-6099 6102 6105-6107

6109 6111

(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

11S 4211

15S 1589

15T 0764 1494 2910 3164 3261

16T 4024 4679

17R 5768

17S 3333

17W 3046

20Q 4842

26S 0368

27V 3826

29S 0291 0292

31P 0229

31V 0082 0099 0164 0293 0332 0420 0436 0605 0885 0932 0943 1048

31X 4319

32Q 1283

35T 5040

35U 0088 0199 0240 0241 0264

36R 1305

38W 1194

40S 1973

41S 0630

43S 4650

46U 2906 2952 2982 3275 3296 3332 3674 3734 3986 4053 5218 5900

6032

47P 0619

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 4

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SERVICE BULLETIN

OPERATOR MSN

48P 2192

48T 2281

52T 1599

53Z 1468

54S 5261

59Z 1556

61W 0112

62X 3402

66P 0424

69X 0212 0219 0300 0328 0449 0588

73W 0087

74T 2165 4228 4768 5182

76W 0140 0157

79W 3751

80X 2748

83V 0938

85T 0190 0234

85U 5792

86P 0913

86Z 0409 0419 1706 1750

87Q 0052

89T 3356

90Q 0594

91X 2837

94W 1818

95V 3379

95W 2949 4199

98W 0441

AAF 0639 2870 3136 3242 3289 3852 4268 4589 4675 6012

AAL 5678 5698 5704 5745 5753 5761 5781 5786 5788 5789 5798 5810

5827

AAR 2397 2459 3244 3437 3483 3496 3641 3873

AAW 3224 3236 3615 3657 4004 4521 5414 5448

AAY 1229 1255 1262 1288 1292 1318 1347 1530 1540 2224 2265 2271

2319 2387

ABL 2808 2840 2943

ABQ 1467 3974 5891 5943

ABY 2764 3802 3840 3925 4061 4243 4310 4468 4524 4806 4848 4890

4958 5017 5206 5276 5307 5423 5452 5502 5576 5718 5772 5889

5903

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 5

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@A318/A319/A320/A321

SERVICE BULLETIN

OPERATOR MSN

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 1673 1719

1742 1787 1853 1864 1874 1940 1975 2018 2145

ACI 2152 3547

ADH 3328

ADR 4282 4301

AEE 2275 2359 2468 2828 3033 3066 3074 3162 3316 3365 3392 3423

3439 3478 3484 3519 3526 3709 3714 3745 3748 3753 3773 3785

3812 3829 3850 3990 4065 4094 4165

AFL 2052 2069 2072 2091 2106 2116 2133 2144 2233 2875 2920 2947

3052 3063 3157 3373 3410 3511 3545 3574 3627 3631 3640 3644

3699 3711 3778 3786 3789 3794 3823 3835 3923 3942 3954 3998

4133 4160 4453 4498 4579 4625 4649 4656 4684 4692 4712 4835

5421 5536 5565 5572 5578 5580 5585 5614 5873 5921 5967 5970

5974 5982 5989 6017 6022 6043 6044 6060 6071 6090

AFR 0115 0214 0237 0239 0285 0287 0598 0600 0608 0618 0625 0637

0985 0998 1000 1020 1025 1036 1151 1169 1176 1190 1201 1216

1267 1271 1344 1404 1415 1444 1449 1471 1502 1505 1524 1616

1622 1640 1645 1677 1699 1733 1879 1894 1900 1924 1938 1949

2035 2059 2071 2081 2100 2109 2140 2317 2344 2350 2456 2582

2601 2686 2705 2716 2721 2750 2918 2938 2951 2961 2967 2972

3008 3009 3420 3470 3777 3795 3825 3859 4063 4084 4105 4137

4139 4241 4267 4295 4298 4335 4402 4601 4604 4664 4714 4747

4800 4820 4908 5084 5129 5719 5802 5869

AGY 0322

AHY 0331 2487 2516 2588 2685 2788 2846 2853 2865 2991 3006

AIB 0138

AIC 0045 0046 0049 0050 0051 0056 0057 0398 0416 0423 0431 0432

0486 0490 0499 2593 2624 2629 2907 3271 3288 3300 3305 3344

3551 3620 3687 3822 3874 3918 3970 4020 4029 4052 4089 4121

4164 4201 4212 4236 4237

AIJ 0169 0707 1132 1162 1179 1244 1259 1308 1322 1780 2048 2227

2539 3021 3123 3149 3160 3286 3304 3312 3374 3508 3514 3667

3690 4235 4304 4411 4730 4733 4924 4933 5163 5221 5358 5372

5653 5665 5867 5878 5933

AJD 0879 1422

ALK 2345 2584 4694 4869 4915 5086

AMC 2113 2122 2189 2291 2332 2382 2665 2768 3056 3068

AMU 0805 0928 1758 1790 1912 1962 4197

ANA 0167 0383 0413 0482 0501 0507 0531 0534 0549 0554 0658 0669

0685

ANR 0445 0671 0726

ANZ 2085 2090 2112 2130 2148 2153 2173 2257 2297 2445 2533 2594

2663 4553 4584 4884 4926 5629 5682 5847 5962 5993

AOJ 4503

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 6

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SERVICE BULLETIN

OPERATOR MSN

APJ 4887 4936 5015 5166 5304 5384 5440 5540 5640 5724 5874 6004

6107

ART 0142 0244 0333 0359 0533 0662 0888 0936 1823 1873

ARU 0573 0582

ASL 1140 1159 2277 2296 2335 2587 2621 2645 3252 3317

ATR 0314 0393

AUA 0768 0776 0797 1137 1150 1189 1385 1387 1478 1504 1553 1678

1735 1931 1937 2009 2131 2174 2262 2416 2494 2547 2652

AUH 2403

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

2575 2662 3408 3467 3518 3647 3664 3691 3961 3980 3988 3992

4001 4011 4026 4046 4051 4100 4167 4175 4200 4281 4284 4345

4381 4487 4567 4599 4763 4789 4821 4862 4939 5057 5119 5195

5243 5360 5398 5454 5477 5622 5632 5840 5944

AWC 2564 2791 4701

AXM 0667 0743 0872 0874 1074 1286 2137 2141 2147 2425 2576 2612

2633 2656 2683 2699 2760 2816 2826 2842 2881 2885 2926 2944

2956 2989 3000 3018 3064 3117 3140 3154 3173 3182 3194 3201

3223 3232 3277 3291 3299 3327 3338 3353 3370 3394 3404 3427

3448 3477 3486 3489 3505 3521 3536 3549 3568 3576 3582 3610

3628 3648 3679 3701 3715 3729 3765 3776 3813 3875 3963 3997

4019 4035 4070 4079 4088 4098 4126 4147 4263 4278 4293 4302

4333 4346 4361 4367 4386 4390 4404 4426 4458 4462 4477 4486

4533 4557 4571 4582 4793 4797 4807 4882 4889 4917 4964 4969

4979 4980 4989 5098 5137 5149 5153 5165 5200 5215 5272 5283

5325 5344 5347 5353 5359 5397 5420 5428 5430 5431 5468 5505

5547 5593 5619 5627 5657 5703 5706 5762 5812 5824 5839 5846

5851 5863 5866 5888 5897 5905 5908 5914 5918 5959 6015 6034

6048 6064 6075 6084 6088 6096 6105

AZA 0951 1138 1168 1217 1448 1457 1473 1480 1489 1722 1740 1745

1770 1779 2033 2057 2074 2083 2086 2101 2127 2869 2932 3076

3079 3080 3115 3138 3161 3213 3295 3343 3362 3563 3598 3609

3643 3666 3695 3732 3815 3831 3846 3885 3906 3921 3956 3976

3978 4075 4108 4119 4143 4152 4195 4249 4520 4523 4536 4759

4764 4859 4875 4910 5018 5130 5294 5383 5424

AZI 0527

B2V 0185

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

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

1440 1445 1466 1482 1509 1510 1513 1529 1537 1558 1574 1590

1594 1604 1606 1613 1661 1663 1665 1687 1689 1696 1708 1754

1760 1782 1814 1829 1834 1871 1883 1892 1899 1902 1907 1910

1958 1987 2038 2040 2098 2188 2194 2389 2429 2441 2466 2694

2697 2720 2981 3049 3301 3314 3351 3468 3499 3550 3607 3649

3697 3703 3721 3726 3912 4007 4039 4185 4238 4265 4306 4464

4551 4725 4791 4975 5634 5784 5856 5948 5985 6028 6091

BEC 3199

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

2196 2230 2392 2400 2700 2763 2810 2925 3255 3790 3895 4275

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 7

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SERVICE BULLETIN

OPERATOR MSN

BER 1717 1769 1775 1852 1889 1961 2003 2619 3055 3093 3121 3178

3202 3412 3415 3464 3482 3502 3515 3516 3532 3689 3728 3865

3945 4013 4101 4161 4269 4291 4329 4433 4510 4565 4606 4743

4988 5191 5246 5522

BGF 3188

BGH 1087 2844 2863 3139

BHP 2968 3245 3422 3604 4033 4187 4294 4631

BJN 3617 4956

BKP 2254 2273 2310 2366 2417 2509 2531 2600 2634 2648 2660 2664

2783 3421 3424 3454 3694 3759 3911

BQB 1703

BRS 2263

BSX 0648 0650

BTN 1541 1551

C2C 5088 5907

C8J 5545

C9G 1747 1846

CAA 0279

CBJ 2557 2561 2611 2644 2733 2849 2891 2985 3285 3520 3548 3561

3578 3580 3638 3768 3842 3849 3851 3914 3958 3982 4042 4388

4410 4412 4428 4440 4471 4483 4505 4513 4522 4529 4540 4580

4602 4677 5008 5072 5114 5185 5216 5331 5471 5630 5656 5722

5848 5997 6041

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 3215 3221 3226 3250 3337

3461 3506 3601 4317 4348 4473 4566 4593 4775 4803 4829 4895

4900 4963 4985 4997 5014 5032 5091 5174 5352 5386 5419 5568

5600 5664 5690 5771

CCM 3882 3952 5887 5906

CEB 2556 2586 2625 2638 2786 2790 2821 2831 2852 2876 2994 3048

3272 3762 3767 4447 4508 4537 4574 4852 4861 4870 4927 4993

5045 5067 5250 5320 5381 5442 5498 5669 5687 5917 5934

CEF 2801 3085

CES 0665 0754 0838 0854 0897 0909 0925 0939 0967 0984 0986 1028

1030 1041 1070 1072 1093 1108 1285 1303 1312 1316 1330 1345

1357 1361 1377 1386 1532 1542 1601 1639 1906 1911 1964 1981

2022 2034 2036 2049 2056 2068 2219 2221 2235 2239 2244 2437

2451 2478 2493 2498 2562 2591 2606 2627 2693 2757 2825 3168

3170 3186 3197 3481 3559 3611 3613 3650 3677 3692 3716 3775

3793 3797 3870 3904 3929 3937 3965 4027 4037 4043 4111 4144

4186 4220 4239 4240 4252 4297 4309 4340 4342 4355 4423 4627

4659 4685 4702 4709 4711 4718 4722 4723 4729 4748 4765 4769

4776 4799 4831 4844 4857 4877 4886 4903 4938 4946 4967 4987

5047 5048 5053 5063 5135 5136 5144 5156 5242 5267 5273 5326

5330 5338 5363 5376 5380 5412 5439 5461 5508 5516 5524 5527

5623 5628 5668 5691 5700 5710 5711 5726 5735 5759 5823 5826

5852 5864 5886 5920 5942 5973 6052 6062 6111

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 8

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SERVICE BULLETIN

OPERATOR MSN

CHB 4262 4452 4482 4569 4644 4686 4687 4995 5105 5626 5679 5740

5912 6023 6076

CIB 0774 0809 0884 0894 0905 0957 0971 1381 1402 1416 1437 1968

CQH 0978 1920 2939 3014 3023 3747 3819 4072 4093 4168 4244 4331

4366 4373 4375 4499 4586 4738 4750 4760 4809 4816 4909 4978

4983 5022 5051 5108 5378 5403 5434 5446 5466 5562 5778 5816

5911 6073

CQN 0696 0698 0704 0705 3836 3876 3901 3903 3941 5645 5713

CRK 5147 5189 5416 5514 5544 6003

CSA 2719 2758 2789 3031 3043 3060 3094 3097 3406 3436 3452 3660

3892 4258 4713

CSC 0540 0551 0556 0902 0919 1013 2313 2348 2396 2431 2510 2534

2597 2639 3114 3116 3124 3158 3167 3196 3210 3386 3449 3591

3680 3962 4018 4068 4288 4326 4378 4424 4525 4575 4619 4642

4660 4707 4905 4911 5041 5121 5141 5208 5286 5389 5609 5646

5650 5765 5868 5896 5910 5937 5953 5964 5977 6008 6030

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

1039 1057 1971 1986 2004 2008 2200 2203 2232 2354 2361 2371

2408 2426 2435 2484 2505 2506 2511 2519 2541 2546 2554 2555

2558 2574 2579 2637 2667 2680 2689 2701 2708 2714 2743 2770

2772 2796 2815 2824 2834 2855 2861 2877 2899 2901 2915 2940

2948 2950 2960 2969 2986 3020 3144 3258 3269 3311 3342 3828

3860 3890 3910 3959 3983 3999 4003 4017 4036 4038 4071 4140

4172 4205 4225 4232 4248 4260 4279 4290 4322 4325 4350 4362

4365 4370 4396 4456 4507 4550 4613 4671 4696 4751 4782 4794

4808 4836 4854 4864 4880 4883 4912 4919 4928 4982 5061 5151

5168 5170 5183 5202 5214 5225 5268 5288 5410 5480 5484 5503

5506 5561 5564 5579 5602 5611 5671 5693 5730 5750 5756 5797

5817 5832 5837 5875 5930 5945 5976 6018 6078 6106

CSZ 2672 2684 2841 2905 2909 2935 2973 2980 3131 3132 3153 3206

3366 3383 3435 3440 3456 3528 3599 3696 3698 3756 3848 3855

3887 3898 3935 3971 4010 4028 4159 4176 4208 4214 4226 4300

4359 4407 4409 4435 4474 4514 4531 4620 4633 4666 4726 4845

4866 4876 4897 4920 4929 4977 4986 5002 5082 5110 5176 5369

5521 5550 5589 5639 5731 5766 5986 6019

CTN 0767 0833 1009 1029 1237 1252

CTV 0839 0892 1635 2598 2692 3147 3148 3861 4961 5351 5379 5394

5399 5415 5511 5541 5551 5556 5560 5571 5574 5597 5777 5830

CUA 5023

CYP 0256 2108 2334 2343

D2F 2496 2502

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 9

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SERVICE BULLETIN

OPERATOR MSN

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

DAT 0311 0395 0426 0525 0999

DCS 1053 3243

DKH 2975 3027 3234 3268 3368 3485 3596 3605 3967 3984 4064 4102

4154 4276 4401 4429 4573 4587 4652 4833 4840 4981 5013 5070

5071 5131 5226 5329 5339 5455 5491 5737

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

0116 0137 0172 0346 0609 0610 0616 0623 0627 0636 0641 0651

0679 0689 0694 0700 0717 0723 0729 0738 0744 0853 0860 0875

1337 1365 1367 4097 4120 4141 4153 4182 4191 4261 4289 4324

4332 4363 4398 4449 4455 4511 4796 4841 5122 5181 5203 5239

5284 5293 5425 5441 5487 5694 5741 5769 5831

DNU 0406 0444

DNV 1630 1805 1808 1841 2093 2179 2241 2751 3065 3179

DQA 2347

DRK 2306 2346 3950

DTR 0113

EAA 0386

EDW 0942 0947 1026 2024 2134

EIN 1242 1394 1443 1983 2001 2191 2206 2217 2250 2256 2272 2294

2364 2374 2399 2409 2411 2432 2486 2542 2583 2635 3054 3102

3129 3169 3318 3345 3377 3501 3755 3781 3857 4572 4634 4678

4715

ETD 0350 1944 1945 1947 1955 2167 3004 3050 3676 3693 3713 3902

4066 4077 4124 4934 5095 5348 5407 5714 5791 5821 5882 5924

ETJ 0295 0325 0373 0428

EVA 3363 3886

EVE 5642

EWG 5497 5525 5557 5601 5635 5658

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 10

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SERVICE BULLETIN

OPERATOR MSN

EZY 2037 2043 2050 2053 2062 2120 2170 2181 2184 2245 2289 2300

2353 2360 2370 2385 2398 2402 2412 2427 2450 2463 2471 2477

2481 2492 2495 2503 2512 2514 2527 2528 2538 2565 2578 2605

2636 2646 2677 2681 2691 2702 2709 2715 2727 2729 2735 2742

2744 2754 2765 2769 2777 2779 2782 2795 2803 2812 2818 2827

2829 2854 2860 2866 2873 2884 2923 2946 2959 3003 3036 3041

3053 3059 3061 3082 3084 3088 3090 3118 3122 3134 3137 3176

3184 3411 3413 3426 3432 3442 3466 3537 3544 3555 3569 3571

3608 3634 3675 3683 3702 3720 3735 3742 3746 3754 3763 3774

3788 3799 3805 3808 3810 3824 3843 3844 3845 3854 3871 3888

3909 3913 3922 3946 3953 3975 3979 3991 4006 4012 4014 4034

4040 4048 4056 4069 4076 4080 4087 4125 4129 4132 4157 4179

4196 4219 4233 4234 4250 4286 4313 4327 4380 4385 4418 4425

4427 4437 4444 4451 4554 4556 4588 4591 4624 4635 4636 4640

4646 4667 4676 4680 4693 4705 4708 4717 4721 4740 4744 4749

4778 4781 4785 4787 4837 5019 5020 5046 5052 5056 5064 5104

5111 5113 5116 5138 5146 5150 5187 5201 5224 5236 5249 5289

5318 5319 5542 5592 5638 5688 5702 5739 5757 5785 5927 5981

6011 6047 6095

F2I 0085 0148 0168 0203 0220 0230 0243 0249 0251 0270 0294 0301

0391 0422 0427 0460 0496 0497 0724 0758 0799 0976 1010 1068

FFT 1515 1579 1583 1615 1684 1759 1781 1786 1803 1806 1860 1943

1980 1997 2010 2012 2019 2030 2103 2198 2209 2236 2240 2253

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

2857 3205 3389 3431 4127 4204 4253 4254 4272 4307 4562 4641

4668 4688 4704 4727 4745 5526 5661

FHY 0580 2524 2804 3025 4207 4658 5096

FIN 1073 1107 1184 1309 1352 1364 1405 1470 1544 1588 1712 1913

1916 1989 2065 2124 2146 2154 2266

FLI 2186 3905 5079

FPY 0189 0342

FRN 0647 0660

FTZ 1145 2176 2268

G2X 0347 0653 3125

G4I 1157 1795 2507

G8E 0714 0716 0730 2420

GAF 3897 4060

GAP 0706 0745 2162 2183 3087 3187 3273 4777 4984 5007 5012 5103

5310

GBB 0067

GCR 2338 2475 4600 4739 4825 5006 5117 5760 5799 5835 5850 5853

5894 5928 5971

GFA 4030 4059 4083 4146 4158 4188 4218 4255 4502 4541 4780 4827

4860 4865 5171 5175

GHT 0438

GLG 1866 1872 1882 1925 2078 2126 4379 4547

GMI 3019 3407 3533 3560 4663 4691 5085

GMR 1407

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 11

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SERVICE BULLETIN

OPERATOR MSN

GOW 3306 3597 3616 3798 3827 3900 3915 4399 4438 5016 5112 5232

5463 5552 5675 5809 5811 5990 6072

GSW 3589 3818

GWI 0117 0135 0161 0162 0200 0201 0202 0209 0216 0217 0218 0267

0268 0269 0382 0401 0646 0654 0794 1016 1077 1084 1089 1136

1147 1155 1170 1172 1209 1277 2607 2628 2632 2813 2833 2976

3011 3128 3172 3193 3352 3358 3375 3500 3534 3839 3841 4166

4227 4256 4285 4998 5043 5457 5467 5535 5569 5941 5978

HDA 0756 0784 0812 0930 1253 1721 2229 2238 2428 4023 4247 5024

5030 5362 5429

HKE 2299 2322 2717 4970 5260 5264 5266 5341

HKJ 2706 3073 4878

I2L 0371 0491 0579 0760 0816

I2T 1631 1682

IAC 0096 0396 0451 0469 0492

IAW 5115 5290 5464

IBE 0158 0173 0176 0207 0224 0266 0274 0323 0356 1154 1362 1655

1674 1694 1793 1809 2225 2242 2264 2311 2365 2391 2889 3078

3209 3320 3380 3443 3651 3744 5486 5570 5692

IBS 1047 1059 1067 1099 1101 1119 1125 1198 1439 1450 1516 2104

2143 2248 2807 5501 5590 5729 5815

IGO 3357 3414 3453 3457 3497 3541 3618 3782 3863 3943 4008 4113

4156 4216 4312 4328 4384 4481 4488 4506 4518 4535 4552 4603

4609 4614 4630 4637 4752 4757 4762 4812 4813 4818 4868 4888

4918 4947 4954 4965 4973 5027 5036 5073 5076 5080 5090 5092

5094 5120 5155 5188 5190 5194 5228 5230 5231 5259 5262 5291

5298 5313 5335 5365 5375 5411 5426 5437 5449 5460 5473 5476

5507 5537 5577 5641 5676 5683 5712 5727 5744 5807 5829 5893

5898

IND 0343 0357

IRA 0303 0312 0345 0575 0857 2054

IRC 0354 0414

ISR 4354 4413

ISS 0737 0749 2102

IYE 4653 4690

IZG 0376 0400 0407

JAD 0459 0537 3246

JAS 5478

JAV 0029 2061

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 12

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SERVICE BULLETIN

OPERATOR MSN

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 3381 3416 3451 3479 3488 3517 3554

3572 3622 3659 3707 3724 3760 3800 3811 4578 4612 4647 4904

5060 5142 5148 5302 5312 5349 5417 5677 5723 5782

JJP 5093 5145 5161 5245 5274 5281 5355 5492 5499 5520 5598 5618

5649 5695 5701 5717 5732 5796

JKT 5685 5725 5738

JSA 2316 2356 2423 2453 2604 4443 4515 4772 4786 4872 4914 5305

5323 5390 5433 5472 5708 5813

JST 2169 2185 2197 2292 2329 2455 2515 2526 2537 2573 2608 2642

2651 2703 2766 2787 3474 3495 3668 3783 3917 4177 4178 4229

4245 4257 4303 4343 4356 4434 4460 4466 4495 4497 4527 4899

4922 5039 5211 5270 5311 5334 5482 5489 5532 5566 5631 5775

5780 5814 5858 5871

JZR 3919 3939 4162 5033 5625 5833

KAC 0181 0182 0195 2046 3957

KAY 4470 5963

KFR 2650

KGL 2029 2077

KKK 1124 1390 1624 1730 2747 2753

KMF 0480

KNE 1942 1965 2123 2171 2182 2199 2569 2776 3218 3238 3256 3361

3396 3425 3475 3530 3787 3809 3817 3868 3889 3894 3933 4055

4735 5716

KZR 3141 3614 5401 5613 5734 5870 5968 6029 6037

LAA 4405 4450 4490 4526 5373 5405 5494

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

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

2886 2892 2894 3264 3280 3319 3330 3535 3556 3663 3671 3770

3772 3779 4383 4400 4439 4476 4509 4516 4543 4546 4549 4563

4576 4597 4598 4605 4657 4697 4758 4767 4815 4839 4871 4892

4896 4921 4943 4972 5005 5097 5125 5178 5213 5229 5234 5263

5316 5324 5364 5408 5443 5453 5483 5493 5548 5554 5583 5586

5654 5666 5686 5707 5748 5764 5801 5818 5859

LAO 4596 4639 5356 5396

LBT 0793 0937 1121 1175 1597 1744 2158 3089 3480 3487 4623

LFO 0659

LIM 0828

LJB 3985

LKE 2581 2617 2746 3240 5100 5172 5220

LLC 0415 0990 1715 2987 4203 4489

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 13

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SERVICE BULLETIN

OPERATOR MSN

LLM 1054 1918 1969 1993 2413 2419 2439

LLP 0739 0883 0914 1007 1411 1723 2016 2118

LMJ 1868

LMU 0977 1561

LWA 2878 2954

LZB 2540 2596 3028 3309 3564 3780

MAC 4539 4568 5143

MAU 1592 1936

MEA 3736 3804 3837 4296 4339 4632 5000 5152 5162 5253 5746

MJF 4353

MJN 3723 4117 4795

MLD 0622 0741

MLM 2550 3932 4622

MLR 1893 2731

MMA 0316 0973 1180 1247 1791

MON 1081 1320 1413 1571 1605 1637 2142 5581

MOV 2442 2446 3364 3403

MRJ 0530 1300 1353

MSC 2094 2937 2966 3282 3323 3626

MSR 0165 0166 0178 0194 0198 0351 0366 2070 2073 2079 2088

MXA 0252 0259 0260 0261 0275 0276 0296 0320 0321 0353

MYX 0566 1896

NIA 2874 3183 3219

NKS 2433 2470 2473 2485 2490 2560 2567 2603 2622 2673 2679 2698

2704 2711 2723 2797 2893 2898 2929 2942 2963 2978 2983 3007

3017 3026 3165 3393 3395 4206 4264 4321 4431 4548 4592 4595

4902 4951 4996 5029 5042 5132 5159 5370 5387 5458 5517 5624

5672 5804 5861 5880 5954 5999 6082

NLY 2529 2668 2749 2867 2902 3447 3661 4231 4316 4368 4581 4594

5648

NMA 1697 1732 2676

NMB 3346 3586 5366 5400

NVD 0211 0528 0558 0561 0709 0747 1005 1626 1778 1998

NWS 2649

OAW 1886

OBS 3758

OHY 0455 0543 0640 0661 0676 0912 0916 2571 2688

ONE 4222 4287 4336 4891 4913 4941 4942 5193 5278 5299 5754 5841

ORF 2566 4992

OZW 0429 1922

PAL 3310 3455 3553 3579 3652 3731 5081 5140 5315 5371

PGT 5879 5902

PIA 2155 2212 2274

PIC 2331 2340 2670 2922 3012 3621 4459

PKZ 6069

PTI 1263

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 14

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SERVICE BULLETIN

OPERATOR MSN

QAF 0927 1335 3994 4114 4170 5255

QDA 6061 6102

QTR 1566 1648 1656 1773 1895 1957 2097 2121 2138 2161 2288 2341

4110 4130 4183 4436 4479 4496 4615 4700 4754 4784 4802 4810

4858 4930 4968 5010 5078 5127 5217 5361 5395

R1T 1908

RBA 2023 2032 2135 2139 2195 3071

RBG 3152

RCT 0466

RFJ 0814

RJA 2953 3428 3685 3803 3832 4670 4817 4853 5128

RJD 1618 5277

ROT 2931 2955 3220 3225

RYW 0569 5367

RZO 0795 2011 2390 3891

SAA 2308 2326 2355 2375 2379 2418 2438 2469 2501 4990 5011 5637

5680 5956 6007

SAI 0542 0877 1497 2027 3105 3270

SAS 1183 1383 2817 2850 2856 2883 2888 2911 2958 2990 3086 3159

3192 3227 3231 3292 3335

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

2028 2279 2369 2373 2464 2474 2618 2623 2641 3446 3473 3490

3494 3866 3880 4032 4150 5001 5026 5031 5106 5134 5167 5559

5607

SDM 0649 1130 1200 1379 1488 1560 1578 1654 1657 1679 1743 1753

1761 1767 1851 1863 1876 1890 2151 2163 2465 2497 2879 2913

2930 2964 3044

SFJ 4555 4720 5102 5393 5512 5652 5773 5862 5931

SFW 0734 0994 1018

SGG 0076

SHJ 0910

SHU 2222 2243 3108 3281 3298 3336 3838

SKU 0447 1400 1523 2119 2129 2214 2249 2251 2283 2378 2380 2436

2460 2548 3171 3331

SLK 0899 0969 1228 1698 2058 2252 2517 2568 2775 3104 3570 3821

4118 4215 4259 4457 5050 5089 5296 5531 5794

SMX 2995

SND 1880 1999

SNX 0289

SOL 0302

SUD 3040

SVA 4015 4057 4081 4090 4092 4104 4115 4122 4135 4273 4314 4337

4349 4357 4364 4376 4391 4392 4393 4394 4397 4408 4414 4419

4432 4442 4454 4484 4501 4517 4519 4564 4823 4955 5223

SVR 0735 1063 1152 1484 1603 1751 1777 1884 1901 2166 2175 2187

2278 2327 2349 2998 3099 3107 3189 3385 3388 3433 3472 3834

SVW 2592 2921 3100 3133 3542 3856 5445

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 15

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SERVICE BULLETIN

OPERATOR MSN

SWM 0421 0430 0476

SWR 0545 0553 0559 0562 0574 0577 0578 0585 0596 0603 0612 0621

0635 0643 0673 0681 0701 0703 0713 0727 0782 1762 1951 4618

4673 5037 5069 5518

SYA 3853 3872

SYR 0886 0918 1032 1076 1085 1117

TAE 0657 0934 0946 0949 1339 1368 1500 1934 2084 2659

TAI 1066 1334 1598 1625 1952 2282 2301 2339 2434 2444 2917 3042

3057 3103 3113 3248 3276 3378 3418 3510 3538 3581 4906 4944

5068 5219 5238 5280 5333 5406 6068 6099

TAM 1092 1096 1103 1139 1143 1158 1215 1246 1251 1376 1459 1486

1518 1575 1580 1591 1593 1595 1608 1628 1652 1672 1692 1771

1801 1802 1804 1825 1826 1827 1831 1832 1835 1837 1855 1857

1888 1891 2014 2044 2372 2393 2467 2513 2661 2734 2737 2784

2838 2859 2887 2896 2904 2924 3002 3032 3035 3047 3058 3111

3156 3180 3211 3266 3278 3284 3313 3325 3391 3540 3565 3588

3594 3595 3630 3658 3662 3710 3727 3733 3750 3908 3972 4000

4163 4171 4192 4320 4389 4441 4446 4465 4544 4734 4756 4773

4953 4974 5066 5101 5107 5109 5184 5209 5222 5240 5342 5345

5591 5621 5643 5749 5752

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

1667 1668 1718 1756 1765 1799 1816 2178 2792 2822 3769 3883

4021 4095 4106 4145

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

1187 1479 1700 3096 4344 4689 5204 5474 5610

TBA 4766 4801 4846 5157 5256 5451 5529 5563 5855

TBJ 1485

TBZ 0361 0362 0405

TCW 1929 2114 2362

TGW 2724 2728 3757 3801 4181 4210 4421 4445 4469 4491 4493 4532

4561 4608 4645 4879 4931 5496 5596 5605 5662 5697 5721 5805

5915

THA 5198 5248 5258 5301 5436 5553 5806 5828 5857 5892 5951 5979

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

2522 2602 2609 2626 2631 2655 2738 2739 2928 2934 2941 2984

3010 3142 3185 3208 3239 3257 3259 3303 3308 3341 3558 3567

3603 3654 3718 3719 3896 3931 3949 4629 4665 4695 4755 4774

4790

TJS 3513 3632 4169

TNA 0791 0822 2376 2914 3577 5055

TTW 4804 4874

TVS 2180 4699

TXP 0607 0611 0617

UAE 4822

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 16

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SERVICE BULLETIN

OPERATOR MSN

UAL 0435 0439 0442 0450 0452 0454 0456 0457 0462 0463 0464 0465

0470 0472 0475 0479 0483 0485 0487 0489 0500 0503 0504 0506

0508 0510 0512 0523 0539 0568 0571 0587 0589 0592 0613 0638

0655 0678 0683 0686 0690 0702 0748 0751 0759 0780 0783 0788

0798 0804 0820 0824 0825 0826 0834 0836 0842 0843 0847 0850

0851 0858 0862 0865 0867 0871 0873 0882 0893 0898 0944 0948

0952 0955 0965 0980 0989 1001 1022 1031 1104 1105 1128 1146

1163 1192 1211 1243 1248 1266 1272 1282 1290 1291 1321 1341

1343 1359 1363 1401 1409 1420 1426 1427 1432 1435 1460 1469

1474 1475 1477 1495 1507 1508 1514 1522 1533 1538 1545 1555

1559 1569 1573 1581 1584 1585 1586 1600 1609 1617 1620 1627

1647 1649 1653 1664 1669 1671 1680 1688 1702 1728 1731 1737

1741 1755 1821 1840 1842 1845 1847 1865

UEA 2654 2696 2762 2774 2820 2835 3024 3706 4347 5003 5252 5957

UJX 0733 1213

UKN 3260

ULG 0308

UNA 4583 4732

USA 0053 0054 0055 0064 0065 0066 0077 0081 0317 0448 0565 0584

0762 0770 0803 0844 0856 0861 0863 0866 0868 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

1406 1410 1419 1463 1490 1527 1534 1547 1552 1563 1565 1576

1621 1643 1644 1710 1764 1792 1844 1935 2193 2302 2312 2405

2422 2430 2458 2482 2570 2595 2613 2615 2630 2669 2690 4086

4149 4202 4242

UZB 4371 4395 4417 4485 4492 4528 4651 4724 4770 4952

VAR 2383 2718

VIM 2732 4270 4305 5158

VIP 4151

VIV 2157 2210 2443 2752 2908 3743

VJC 2712 2745 3646 3739 3791 4049 4190 4193 4415 4475 4504 4512

4907 5742 5822

VKG 1954

VLE 1226

VLG 0992 1171 1208 1210 1221 1349 1372 1396 1430 1461 1550 1736

1749 1862 1914 1933 1979 2168 2207 2223 2388 2407 2479 2589

2620 2658 2678 2761 2785 2794 2798 2843 2897 2962 2988 3083

3095 3109 3145 3151 3174 3203 3237 3293 3321 3376 3400 3444

3476 3492 3529 3700 3704 3833 3907 3995 4128 4463 4478 4661

4674 4681 4742 4849 4855 4937 5479 5530 5533 5587 5599 5612

5616 5620 5673 5877 5885 5925 5940 6039 6045 6079 6081

VNL 5844 5901 5926

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 17

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SERVICE BULLETIN

OPERATOR MSN

VOI 2204 2657 2666 2771 2780 2979 2997 3045 3069 3077 3175 3253

3279 3450 3463 3491 3524 3543 3590 3624 3672 3705 4403 4422

4741 4798 4828 4832 4950 5062 5207 5212 5308 5322 5337 5391

5488 5510 5595 5651 5776 5793 5819 5988 5996 6014 6109

VRD 2616 2674 2740 2773 2778 2800 2811 2830 2851 2993 3016 3037

3101 3135 3155 3181 3204 3230 3324 3347 3349 3359 3398 3417

3445 3460 3465 3503 3656 3670 3684 3686 4448 4480 4558 4559

4610 4616 4655 4805 4814 4851 4867 4894 4948 4959 4991 4999

5004 5034 5058 5179 5515

VRE 1429 2213 2228

VVC 1306 1370 1454 1564 1686 1725 1757 1867

WAU 3531 3741

WGT 1212

WHT 0548 1256 2440 2675

WOW 2457

WRC 0235 0645

WZZ 3127 3143 3166 3177 3354 3384 3409 3430 3562 3771 3807 3877

3927 3947 3968 4109 4174 4223 4246 4308 4323 4351 4372 4621

4628 4683 4716 4736 5021 5075 5123 5139 5196 5539 5604 5608

5615 5617 5660 6001 6058 6077 6086 6093 6098

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 18

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0029 0045 0046 0049 0050 0051 0052 0053 0054 0055 0056

0057 0059 0064 0065 0066 0067 0068 0069 0070 0071 0072

0073 0076 0077 0078 0081 0082 0083 0084 0085 0086 0087

0088 0093 0094 0096 0099 0104 0110 0111 0112 0113 0115

0116 0117 0118 0119 0121 0122 0123 0124 0125 0126 0127

0135 0137 0138 0140 0141 0142 0148 0149 0150 0152 0153

0154 0157 0158 0159 0160 0161 0162 0164 0165 0166 0167

0168 0169 0171 0172 0173 0174 0175 0176 0178 0181 0182

0183 0185 0189 0190 0192 0194 0195 0197 0198 0199 0200

0201 0202 0203 0205 0206 0207 0208 0209 0210 0211 0212

0213 0214 0216 0217 0218 0219 0220 0224 0229 0230 0231

0232 0233 0234 0235 0237 0239 0240 0241 0242 0243 0244

0248 0249 0251 0252 0253 0254 0255 0256 0259 0260 0261

0262 0263 0264 0265 0266 0267 0268 0269 0270 0272 0273

0274 0275 0276 0277 0279 0281 0282 0284 0285 0287 0289

0290 0291 0292 0293 0294 0295 0296 0297 0298 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 0366 0367 0368 0370 0371 0372 0373 0376 0378 0380

0381 0382 0383 0386 0387 0388 0390 0391 0393 0395 0396

0398 0399 0400 0401 0402 0403 0404 0405 0406 0407 0408

0409 0410 0413 0414 0415 0416 0417 0418 0419 0420 0421

0422 0423 0424 0426 0427 0428 0429 0430 0431 0432 0435

0436 0438 0439 0441 0442 0444 0445 0447 0448 0449 0450

0451 0452 0454 0455 0456 0457 0459 0460 0462 0463 0464

0465 0466 0469 0470 0472 0475 0476 0479 0480 0482 0483

0485 0486 0487 0489 0490 0491 0492 0496 0497 0499 0500

0501 0503 0504 0506 0507 0508 0510 0511 0512 0523 0525

0527 0528 0530 0531 0533 0534 0537 0539 0540 0542 0543

0545 0546 0548 0549 0551 0553 0554 0556 0558 0559 0561

0562 0565 0566 0568 0569 0571 0572 0573 0574 0575 0577

0578 0579 0580 0582 0584 0585 0587 0588 0589 0592 0594

0596 0598 0600 0603 0605 0607 0608 0609 0610 0611 0612

0613 0616 0617 0618 0619 0621 0622 0623 0625 0627 0629

0630 0634 0635 0636 0637 0638 0639 0640 0641 0643 0644

0645 0646 0647 0648 0649 0650 0651 0653 0654 0655 0656

0657 0658 0659 0660 0661 0662 0665 0667 0669 0670 0671

0672 0673 0676 0678 0679 0681 0682 0683 0685 0686 0688

0689 0690 0691 0693 0694 0695 0696 0697 0698 0700 0701

0702 0703 0704 0705 0706 0707 0709 0711 0712 0713 0714

0716 0717 0718 0719 0720 0721 0722 0723 0724 0726 0727

0728 0729 0730 0732 0733 0734 0735 0736 0737 0738 0739

0740 0741 0742 0743 0744 0745 0747 0748 0749 0750 0751

0752 0754 0755 0756 0757 0758 0759 0760 0762 0763 0764

0766 0767 0768 0769 0770 0773 0774 0776 0778 0779 0780

0782 0783 0784 0785 0786 0788 0790 0791 0793 0794 0795

0797 0798 0799 0800 0801 0803 0804 0805 0807 0809 0812

001

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 19

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

SERVICE BULLETIN

MSN CONFIGURATION

0813 0814 0816 0817 0818 0820 0821 0822 0824 0825 0826

0828 0829 0830 0831 0832 0833 0834 0836 0837 0838 0839

0840 0842 0843 0844 0845 0846 0847 0849 0850 0851 0853

0854 0856 0857 0858 0859 0860 0861 0862 0863 0865 0866

0867 0868 0869 0870 0871 0872 0873 0874 0875 0876 0877

0879 0880 0881 0882 0883 0884 0885 0886 0888 0889 0890

0892 0893 0894 0895 0896 0897 0898 0899 0900 0902 0903

0904 0905 0906 0907 0909 0910 0911 0912 0913 0914 0916

0917 0918 0919 0921 0922 0923 0924 0925 0927 0928 0929

0930 0931 0932 0933 0934 0936 0937 0938 0939 0942 0943

0944 0945 0946 0947 0948 0949 0950 0951 0952 0953 0955

0957 0958 0960 0962 0964 0965 0966 0967 0969 0971 0972

0973 0975 0976 0977 0978 0979 0980 0981 0982 0984 0985

0986 0988 0989 0990 0992 0994 0996 0997 0998 0999 1000

1001 1002 1003 1005 1007 1009 1010 1011 1013 1014 1016

1018 1019 1020 1022 1025 1026 1028 1029 1030 1031 1032

1033 1034 1035 1036 1037 1038 1039 1040 1041 1043 1046

1047 1048 1049 1050 1051 1052 1053 1054 1055 1056 1057

1058 1059 1061 1062 1063 1064 1065 1066 1067 1068 1069

1070 1071 1072 1073 1074 1075 1076 1077 1078 1079 1081

1082 1083 1084 1085 1086 1087 1088 1089 1090 1091 1092

1093 1095 1096 1097 1099 1100 1101 1102 1103 1104 1105

1106 1107 1108 1109 1110 1111 1112 1114 1115 1116 1117

1118 1119 1120 1121 1122 1123 1124 1125 1126 1127 1128

1129 1130 1131 1132 1134 1135 1136 1137 1138 1139 1140

1141 1142 1143 1145 1146 1147 1148 1149 1150 1151 1152

1154 1155 1156 1157 1158 1159 1160 1162 1163 1164 1165

1166 1167 1168 1169 1170 1171 1172 1173 1175 1176 1177

1178 1179 1180 1181 1182 1183 1184 1187 1189 1190 1191

1192 1193 1194 1196 1197 1198 1200 1201 1203 1205 1206

1208 1209 1210 1211 1212 1213 1215 1216 1217 1221 1222

1223 1224 1225 1226 1228 1229 1230 1231 1232 1234 1235

1236 1237 1239 1240 1242 1243 1244 1245 1246 1247 1248

1249 1251 1252 1253 1254 1255 1256 1257 1258 1259 1261

1262 1263 1264 1265 1266 1267 1268 1269 1270 1271 1272

1274 1275 1277 1279 1280 1281 1282 1283 1284 1285 1286

1287 1288 1289 1290 1291 1292 1294 1295 1296 1297 1298

1300 1301 1302 1303 1304 1305 1306 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 1357

1358 1359 1360 1361 1362 1363 1364 1365 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 1400 1401 1402 1404 1405

1406 1407 1409 1410 1411 1413 1414 1415 1416 1418 1419

1420 1422 1423 1424 1426 1427 1429 1430 1432 1434 1435

1437 1439 1440 1441 1443 1444 1445 1446 1448 1449 1450

1452 1453 1454 1456 1457 1459 1460 1461 1463 1466 1467

1468 1469 1470 1471 1473 1474 1475 1477 1478 1479 1480

001

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 20

5

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

SERVICE BULLETIN

MSN CONFIGURATION

1482 1483 1484 1485 1486 1488 1489 1490 1491 1493 1494

1495 1497 1498 1500 1501 1502 1504 1505 1506 1507 1508

1509 1510 1512 1513 1514 1515 1516 1518 1520 1522 1523

1524 1526 1527 1528 1529 1530 1532 1533 1534 1535 1537

1538 1540 1541 1542 1543 1544 1545 1546 1547 1548 1549

1550 1551 1552 1553 1555 1556 1557 1558 1559 1560 1561

1562 1563 1564 1565 1566 1567 1568 1569 1570 1571 1573

1574 1575 1576 1577 1578 1579 1580 1581 1582 1583 1584

1585 1586 1588 1589 1590 1591 1592 1593 1594 1595 1597

1598 1599 1600 1601 1603 1604 1605 1606 1608 1609 1610

1612 1613 1615 1616 1617 1618 1620 1621 1622 1624 1625

1626 1627 1628 1630 1631 1633 1634 1635 1637 1639 1640

1641 1643 1644 1645 1646 1647 1648 1649 1650 1652 1653

1654 1655 1656 1657 1659 1661 1662 1663 1664 1665 1667

1668 1669 1671 1672 1673 1674 1677 1678 1679 1680 1682

1683 1684 1685 1686 1687 1688 1689 1692 1693 1694 1696

1697 1698 1699 1700 1702 1703 1705 1706 1708 1709 1710

1712 1714 1715 1717 1718 1719 1721 1722 1723 1725 1727

1728 1730 1731 1732 1733 1735 1736 1737 1738 1739 1740

1741 1742 1743 1744 1745 1746 1747 1749 1750 1751 1752

1753 1754 1755 1756 1757 1758 1759 1760 1761 1762 1764

1765 1766 1767 1769 1770 1771 1773 1774 1775 1777 1778

1779 1780 1781 1782 1784 1785 1786 1787 1789 1790 1791

1792 1793 1795 1796 1797 1799 1800 1801 1802 1803 1804

1805 1806 1808 1809 1810 1812 1814 1815 1816 1818 1819

1820 1821 1823 1824 1825 1826 1827 1828 1829 1831 1832

1833 1834 1835 1837 1838 1839 1840 1841 1842 1844 1845

1846 1847 1849 1851 1852 1853 1854 1855 1856 1857 1858

1860 1861 1862 1863 1864 1865 1866 1867 1868 1870 1871

1872 1873 1874 1875 1876 1877 1879 1880 1882 1883 1884

1885 1886 1888 1889 1890 1891 1892 1893 1894 1895 1896

1897 1898 1899 1900 1901 1902 1903 1904 1906 1907 1908

1909 1910 1911 1912 1913 1914 1915 1916 1917 1918 1920

1922 1923 1924 1925 1927 1929 1931 1933 1934 1935 1936

1937 1938 1940 1942 1943 1944 1945 1947 1948 1949 1951

1952 1954 1955 1957 1958 1959 1961 1962 1963 1964 1965

1968 1969 1971 1973 1975 1976 1979 1980 1981 1982 1983

1986 1987 1989 1990 1993 1996 1997 1998 1999 2000 2001

2002 2003 2004 2006 2007 2008 2009 2010 2011 2012 2013

2014 2015 2016 2018 2019 2020 2022 2023 2024 2026 2027

2028 2029 2030 2031 2032 2033 2034 2035 2036 2037 2038

2039 2040 2042 2043 2044 2046 2047 2048 2049 2050 2052

2053 2054 2056 2057 2058 2059 2061 2062 2063 2065 2066

2068 2069 2070 2071 2072 2073 2074 2075 2077 2078 2079

2081 2082 2083 2084 2085 2086 2087 2088 2089 2090 2091

2092 2093 2094 2095 2096 2097 2098 2099 2100 2101 2102

2103 2104 2106 2108 2109 2112 2113 2114 2116 2118 2119

2120 2121 2122 2123 2124 2125 2126 2127 2129 2130 2131

2132 2133 2134 2135 2136 2137 2138 2139 2140 2141 2142

2143 2144 2145 2146 2147 2148 2149 2150 2151 2152 2153

2154 2155 2156 2157 2158 2159 2160 2161 2162 2163 2164

001

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 21

5

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

SERVICE BULLETIN

MSN CONFIGURATION

2165 2166 2167 2168 2169 2170 2171 2172 2173 2174 2175

2176 2177 2178 2179 2180 2181 2182 2183 2184 2185 2186

2187 2188 2189 2191 2192 2193 2194 2195 2196 2197 2198

2199 2200 2201 2202 2203 2204 2205 2206 2207 2209 2210

2212 2213 2214 2215 2217 2219 2221 2222 2223 2224 2225

2227 2228 2229 2230 2231 2232 2233 2235 2236 2237 2238

2239 2240 2241 2242 2243 2244 2245 2246 2248 2249 2250

2251 2252 2253 2254 2256 2257 2258 2259 2260 2262 2263

2264 2265 2266 2268 2269 2271 2272 2273 2274 2275 2277

2278 2279 2280 2281 2282 2283 2284 2285 2286 2287 2288

2289 2291 2292 2293 2294 2295 2296 2297 2298 2299 2300

2301 2302 2304 2306 2307 2308 2310 2311 2312 2313 2314

2316 2317 2318 2319 2321 2322 2325 2326 2327 2328 2329

2331 2332 2333 2334 2335 2336 2338 2339 2340 2341 2343

2344 2345 2346 2347 2348 2349 2350 2352 2353 2354 2355

2356 2358 2359 2360 2361 2362 2364 2365 2366 2367 2368

2369 2370 2371 2372 2373 2374 2375 2376 2377 2378 2379

2380 2382 2383 2384 2385 2386 2387 2388 2389 2390 2391

2392 2393 2394 2395 2396 2397 2398 2399 2400 2401 2402

2403 2404 2405 2406 2407 2408 2409 2411 2412 2413 2414

2415 2416 2417 2418 2419 2420 2421 2422 2423 2425 2426

2427 2428 2429 2430 2431 2432 2433 2434 2435 2436 2437

2438 2439 2440 2441 2442 2443 2444 2445 2446 2447 2448

2449 2450 2451 2452 2453 2454 2455 2456 2457 2458 2459

2460 2461 2463 2464 2465 2466 2467 2468 2469 2470 2471

2473 2474 2475 2477 2478 2479 2481 2482 2483 2484 2485

2486 2487 2489 2490 2491 2492 2493 2494 2495 2496 2497

2498 2499 2501 2502 2503 2504 2505 2506 2507 2508 2509

2510 2511 2512 2513 2514 2515 2516 2517 2518 2519 2520

2522 2523 2524 2525 2526 2527 2528 2529 2531 2532 2533

2534 2535 2537 2538 2539 2540 2541 2542 2544 2545 2546

2547 2548 2550 2551 2552 2554 2555 2556 2557 2558 2559

2560 2561 2562 2564 2565 2566 2567 2568 2569 2570 2571

2572 2573 2574 2575 2576 2577 2578 2579 2580 2581 2582

2583 2584 2585 2586 2587 2588 2589 2591 2592 2593 2594

2595 2596 2597 2598 2600 2601 2602 2603 2604 2605 2606

2607 2608 2609 2611 2612 2613 2614 2615 2616 2617 2618

2619 2620 2621 2622 2623 2624 2625 2626 2627 2628 2629

2630 2631 2632 2633 2634 2635 2636 2637 2638 2639 2640

2641 2642 2643 2644 2645 2646 2647 2648 2649 2650 2651

2652 2654 2655 2656 2657 2658 2659 2660 2661 2662 2663

2664 2665 2666 2667 2668 2669 2670 2671 2672 2673 2674

2675 2676 2677 2678 2679 2680 2681 2683 2684 2685 2686

2688 2689 2690 2691 2692 2693 2694 2695 2696 2697 2698

2699 2700 2701 2702 2703 2704 2705 2706 2708 2709 2710

2711 2712 2714 2715 2716 2717 2718 2719 2720 2721 2723

2724 2725 2727 2728 2729 2731 2732 2733 2734 2735 2737

2738 2739 2740 2742 2743 2744 2745 2746 2747 2748 2749

2750 2751 2752 2753 2754 2755 2757 2758 2760 2761 2762

2763 2764 2765 2766 2768 2769 2770 2771 2772 2773 2774

2775 2776 2777 2778 2779 2780 2781 2782 2783 2784 2785

001

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 22

5

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

SERVICE BULLETIN

MSN CONFIGURATION

2786 2787 2788 2789 2790 2791 2792 2794 2795 2796 2797

2798 2800 2801 2802 2803 2804 2805 2806 2807 2808 2810

2811 2812 2813 2814 2815 2816 2817 2818 2819 2820 2821

2822 2824 2825 2826 2827 2828 2829 2830 2831 2832 2833

2834 2835 2836 2837 2838 2839 2840 2841 2842 2843 2844

2845 2846 2847 2848 2849 2850 2851 2852 2853 2854 2855

2856 2857 2858 2859 2860 2861 2863 2864 2865 2866 2867

2869 2870 2871 2872 2873 2874 2875 2876 2877 2878 2879

2880 2881 2883 2884 2885 2886 2887 2888 2889 2890 2891

2892 2893 2894 2896 2897 2898 2899 2900 2901 2902 2904

2905 2906 2907 2908 2909 2910 2911 2913 2914 2915 2917

2918 2920 2921 2922 2923 2924 2925 2926 2928 2929 2930

2931 2932 2934 2935 2937 2938 2939 2940 2941 2942 2943

2944 2945 2946 2947 2948 2949 2950 2951 2952 2953 2954

2955 2956 2958 2959 2960 2961 2962 2963 2964 2966 2967

2968 2969 2970 2972 2973 2975 2976 2977 2978 2979 2980

2981 2982 2983 2984 2985 2986 2987 2988 2989 2990 2991

2992 2993 2994 2995 2997 2998 3000 3002 3003 3004 3006

3007 3008 3009 3010 3011 3012 3014 3016 3017 3018 3019

3020 3021 3023 3024 3025 3026 3027 3028 3029 3031 3032

3033 3035 3036 3037 3039 3040 3041 3042 3043 3044 3045

3046 3047 3048 3049 3050 3052 3053 3054 3055 3056 3057

3058 3059 3060 3061 3063 3064 3065 3066 3068 3069 3071

3072 3073 3074 3076 3077 3078 3079 3080 3082 3083 3084

3085 3086 3087 3088 3089 3090 3091 3093 3094 3095 3096

3097 3099 3100 3101 3102 3103 3104 3105 3107 3108 3109

3111 3113 3114 3115 3116 3117 3118 3119 3121 3122 3123

3124 3125 3127 3128 3129 3131 3132 3133 3134 3135 3136

3137 3138 3139 3140 3141 3142 3143 3144 3145 3147 3148

3149 3150 3151 3152 3153 3154 3155 3156 3157 3158 3159

3160 3161 3162 3164 3165 3166 3167 3168 3169 3170 3171

3172 3173 3174 3175 3176 3177 3178 3179 3180 3181 3182

3183 3184 3185 3186 3187 3188 3189 3190 3192 3193 3194

3195 3196 3197 3199 3200 3201 3202 3203 3204 3205 3206

3208 3209 3210 3211 3213 3215 3218 3219 3220 3221 3223

3224 3225 3226 3227 3228 3230 3231 3232 3234 3236 3237

3238 3239 3240 3242 3243 3244 3245 3246 3248 3250 3252

3253 3255 3256 3257 3258 3259 3260 3261 3263 3264 3266

3268 3269 3270 3271 3272 3273 3275 3276 3277 3278 3279

3280 3281 3282 3284 3285 3286 3287 3288 3289 3291 3292

3293 3295 3296 3298 3299 3300 3301 3303 3304 3305 3306

3308 3309 3310 3311 3312 3313 3314 3316 3317 3318 3319

3320 3321 3323 3324 3325 3327 3328 3330 3331 3332 3333

3335 3336 3337 3338 3341 3342 3343 3344 3345 3346 3347

3348 3349 3351 3352 3353 3354 3356 3357 3358 3359 3361

3362 3363 3364 3365 3366 3368 3370 3373 3374 3375 3376

3377 3378 3379 3380 3381 3383 3384 3385 3386 3388 3389

3391 3392 3393 3394 3395 3396 3398 3400 3402 3403 3404

3406 3407 3408 3409 3410 3411 3412 3413 3414 3415 3416

3417 3418 3420 3421 3422 3423 3424 3425 3426 3427 3428

3430 3431 3432 3433 3435 3436 3437 3439 3440 3442 3443

001

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 23

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

SERVICE BULLETIN

MSN CONFIGURATION

3444 3445 3446 3447 3448 3449 3450 3451 3452 3453 3454

3455 3456 3457 3460 3461 3463 3464 3465 3466 3467 3468

3470 3472 3473 3474 3475 3476 3477 3478 3479 3480 3481

3482 3483 3484 3485 3486 3487 3488 3489 3490 3491 3492

3494 3495 3496 3497 3499 3500 3501 3502 3503 3505 3506

3508 3510 3511 3513 3514 3515 3516 3517 3518 3519 3520

3521 3524 3526 3528 3529 3530 3531 3532 3533 3534 3535

3536 3537 3538 3540 3541 3542 3543 3544 3545 3547 3548

3549 3550 3551 3553 3554 3555 3556 3558 3559 3560 3561

3562 3563 3564 3565 3567 3568 3569 3570 3571 3572 3574

3576 3577 3578 3579 3580 3581 3582 3586 3588 3589 3590

3591 3594 3595 3596 3597 3598 3599 3601 3603 3604 3605

3607 3608 3609 3610 3611 3613 3614 3615 3616 3617 3618

3620 3621 3622 3624 3626 3627 3628 3630 3631 3632 3634

3638 3640 3641 3643 3644 3646 3647 3648 3649 3650 3651

3652 3654 3656 3657 3658 3659 3660 3661 3662 3663 3664

3666 3667 3668 3670 3671 3672 3674 3675 3676 3677 3679

3680 3683 3684 3685 3686 3687 3689 3690 3691 3692 3693

3694 3695 3696 3697 3698 3699 3700 3701 3702 3703 3704

3705 3706 3707 3709 3710 3711 3713 3714 3715 3716 3718

3719 3720 3721 3723 3724 3726 3727 3728 3729 3731 3732

3733 3734 3735 3736 3739 3741 3742 3743 3744 3745 3746

3747 3748 3750 3751 3753 3754 3755 3756 3757 3758 3759

3760 3762 3763 3765 3767 3768 3769 3770 3771 3772 3773

3774 3775 3776 3777 3778 3779 3780 3781 3782 3783 3785

3786 3787 3788 3789 3790 3791 3793 3794 3795 3797 3798

3799 3800 3801 3802 3803 3804 3805 3807 3808 3809 3810

3811 3812 3813 3815 3817 3818 3819 3821 3822 3823 3824

3825 3826 3827 3828 3829 3831 3832 3833 3834 3835 3836

3837 3838 3839 3840 3841 3842 3843 3844 3845 3846 3848

3849 3850 3851 3852 3853 3854 3855 3856 3857 3859 3860

3861 3863 3865 3866 3868 3870 3871 3872 3873 3874 3875

3876 3877 3880 3882 3883 3885 3886 3887 3888 3889 3890

3891 3892 3894 3895 3896 3897 3898 3900 3901 3902 3903

3904 3905 3906 3907 3908 3909 3910 3911 3912 3913 3914

3915 3917 3918 3919 3921 3922 3923 3925 3927 3929 3931

3932 3933 3935 3937 3939 3941 3942 3943 3945 3946 3947

3949 3950 3952 3953 3954 3956 3957 3958 3959 3961 3962

3963 3965 3967 3968 3970 3971 3972 3974 3975 3976 3978

3979 3980 3982 3983 3984 3985 3986 3988 3990 3991 3992

3994 3995 3997 3998 3999 4000 4001 4003 4004 4006 4007

4008 4010 4011 4012 4013 4014 4015 4017 4018 4019 4020

4021 4023 4024 4026 4027 4028 4029 4030 4032 4033 4034

4035 4036 4037 4038 4039 4040 4042 4043 4046 4048 4049

4051 4052 4053 4055 4056 4057 4059 4060 4061 4063 4064

4065 4066 4068 4069 4070 4071 4072 4075 4076 4077 4079

4080 4081 4083 4084 4086 4087 4088 4089 4090 4092 4093

4094 4095 4097 4098 4100 4101 4102 4104 4105 4106 4108

4109 4110 4111 4113 4114 4115 4117 4118 4119 4120 4121

4122 4124 4125 4126 4127 4128 4129 4130 4132 4133 4135

4137 4139 4140 4141 4143 4144 4145 4146 4147 4149 4150

001

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 24

5

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

SERVICE BULLETIN

MSN CONFIGURATION

4151 4152 4153 4154 4156 4157 4158 4159 4160 4161 4162

4163 4164 4165 4166 4167 4168 4169 4170 4171 4172 4174

4175 4176 4177 4178 4179 4181 4182 4183 4185 4186 4187

4188 4190 4191 4192 4193 4195 4196 4197 4199 4200 4201

4202 4203 4204 4205 4206 4207 4208 4210 4211 4212 4214

4215 4216 4218 4219 4220 4222 4223 4225 4226 4227 4228

4229 4231 4232 4233 4234 4235 4236 4237 4238 4239 4240

4241 4242 4243 4244 4245 4246 4247 4248 4249 4250 4252

4253 4254 4255 4256 4257 4258 4259 4260 4261 4262 4263

4264 4265 4267 4268 4269 4270 4272 4273 4275 4276 4278

4279 4281 4282 4284 4285 4286 4287 4288 4289 4290 4291

4293 4294 4295 4296 4297 4298 4300 4301 4302 4303 4304

4305 4306 4307 4308 4309 4310 4312 4313 4314 4316 4317

4319 4320 4321 4322 4323 4324 4325 4326 4327 4328 4329

4331 4332 4333 4335 4336 4337 4339 4340 4342 4343 4344

4345 4346 4347 4348 4349 4350 4351 4353 4354 4355 4356

4357 4359 4361 4362 4363 4364 4365 4366 4367 4368 4370

4371 4372 4373 4375 4376 4378 4379 4380 4381 4383 4384

4385 4386 4388 4389 4390 4391 4392 4393 4394 4395 4396

4397 4398 4399 4400 4401 4402 4403 4404 4405 4407 4408

4409 4410 4411 4412 4413 4414 4415 4417 4418 4419 4421

4422 4423 4424 4425 4426 4427 4428 4429 4431 4432 4433

4434 4435 4436 4437 4438 4439 4440 4441 4442 4443 4444

4445 4446 4447 4448 4449 4450 4451 4452 4453 4454 4455

4456 4457 4458 4459 4460 4462 4463 4464 4465 4466 4468

4469 4470 4471 4473 4474 4475 4476 4477 4478 4479 4480

4481 4482 4483 4484 4485 4486 4487 4488 4489 4490 4491

4492 4493 4495 4496 4497 4498 4499 4501 4502 4503 4504

4505 4506 4507 4508 4509 4510 4511 4512 4513 4514 4515

4516 4517 4518 4519 4520 4521 4522 4523 4524 4525 4526

4527 4528 4529 4531 4532 4533 4535 4536 4537 4539 4540

4541 4543 4544 4546 4547 4548 4549 4550 4551 4552 4553

4554 4555 4556 4557 4558 4559 4561 4562 4563 4564 4565

4566 4567 4568 4569 4571 4572 4573 4574 4575 4576 4578

4579 4580 4581 4582 4583 4584 4586 4587 4588 4589 4591

4592 4593 4594 4595 4596 4597 4598 4599 4600 4601 4602

4603 4604 4605 4606 4608 4609 4610 4612 4613 4614 4615

4616 4618 4619 4620 4621 4622 4623 4624 4625 4627 4628

4629 4630 4631 4632 4633 4634 4635 4636 4637 4639 4640

4641 4642 4644 4645 4646 4647 4649 4650 4651 4652 4653

4655 4656 4657 4658 4659 4660 4661 4663 4664 4665 4666

4667 4668 4670 4671 4673 4674 4675 4676 4677 4678 4679

4680 4681 4683 4684 4685 4686 4687 4688 4689 4690 4691

4692 4693 4694 4695 4696 4697 4699 4700 4701 4702 4704

4705 4707 4708 4709 4711 4712 4713 4714 4715 4716 4717

4718 4720 4721 4722 4723 4724 4725 4726 4727 4729 4730

4732 4733 4734 4735 4736 4738 4739 4740 4741 4742 4743

4744 4745 4747 4748 4749 4750 4751 4752 4754 4755 4756

4757 4758 4759 4760 4762 4763 4764 4765 4766 4767 4768

4769 4770 4772 4773 4774 4775 4776 4777 4778 4780 4781

4782 4784 4785 4786 4787 4789 4790 4791 4793 4794 4795

001

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SERVICE BULLETIN

MSN CONFIGURATION

4796 4797 4798 4799 4800 4801 4802 4803 4804 4805 4806

4807 4808 4809 4810 4812 4813 4814 4815 4816 4817 4818

4820 4821 4822 4823 4825 4827 4828 4829 4831 4832 4833

4835 4836 4837 4839 4840 4841 4842 4844 4845 4846 4848

4849 4851 4852 4853 4854 4855 4857 4858 4859 4860 4861

4862 4864 4865 4866 4867 4868 4869 4870 4871 4872 4874

4875 4876 4877 4878 4879 4880 4882 4883 4884 4886 4887

4888 4889 4890 4891 4892 4894 4895 4896 4897 4899 4900

4902 4903 4904 4905 4906 4907 4908 4909 4910 4911 4912

4913 4914 4915 4917 4918 4919 4920 4921 4922 4924 4926

4927 4928 4929 4930 4931 4933 4934 4936 4937 4938 4939

4941 4942 4943 4944 4946 4947 4948 4950 4951 4952 4953

4954 4955 4956 4958 4959 4961 4963 4964 4965 4967 4968

4969 4970 4972 4973 4974 4975 4977 4978 4979 4980 4981

4982 4983 4984 4985 4986 4987 4988 4989 4990 4991 4992

4993 4995 4996 4997 4998 4999 5000 5001 5002 5003 5004

5005 5006 5007 5008 5010 5011 5012 5013 5014 5015 5016

5017 5018 5019 5020 5021 5022 5023 5024 5026 5027 5029

5030 5031 5032 5033 5034 5036 5037 5039 5040 5041 5042

5043 5045 5046 5047 5048 5050 5051 5052 5053 5055 5056

5057 5058 5060 5061 5062 5063 5064 5066 5067 5068 5069

5070 5071 5072 5073 5075 5076 5078 5079 5080 5081 5082

5084 5085 5086 5088 5089 5090 5091 5092 5093 5094 5095

5096 5097 5098 5100 5101 5102 5103 5104 5105 5106 5107

5108 5109 5110 5111 5112 5113 5114 5115 5116 5117 5119

5120 5121 5122 5123 5125 5127 5128 5129 5130 5131 5132

5134 5135 5136 5137 5138 5139 5140 5141 5142 5143 5144

5145 5146 5147 5148 5149 5150 5151 5152 5153 5155 5156

5157 5158 5159 5161 5162 5163 5165 5166 5167 5168 5170

5171 5172 5174 5175 5176 5178 5179 5181 5182 5183 5184

5185 5187 5188 5189 5190 5191 5193 5194 5195 5196 5198

5200 5201 5202 5203 5204 5206 5207 5208 5209 5211 5212

5213 5214 5215 5216 5217 5218 5219 5220 5221 5222 5223

5224 5225 5226 5228 5229 5230 5231 5232 5234 5236 5238

5239 5240 5242 5243 5245 5246 5248 5249 5250 5252 5253

5255 5256 5258 5259 5260 5261 5262 5263 5264 5266 5267

5268 5270 5272 5273 5274 5276 5277 5278 5280 5281 5283

5284 5286 5288 5289 5290 5291 5293 5294 5296 5298 5299

5301 5302 5304 5305 5307 5308 5310 5311 5312 5313 5315

5316 5318 5319 5320 5322 5323 5324 5325 5326 5329 5330

5331 5333 5334 5335 5337 5338 5339 5341 5342 5344 5345

5347 5348 5349 5351 5352 5353 5355 5356 5358 5359 5360

5361 5362 5363 5364 5365 5366 5367 5369 5370 5371 5372

5373 5375 5376 5378 5379 5380 5381 5383 5384 5386 5387

5389 5390 5391 5393 5394 5395 5396 5397 5398 5399 5400

5401 5403 5405 5406 5407 5408 5410 5411 5412 5414 5415

5416 5417 5419 5420 5421 5423 5424 5425 5426 5428 5429

5430 5431 5433 5434 5436 5437 5439 5440 5441 5442 5443

5445 5446 5448 5449 5451 5452 5453 5454 5455 5457 5458

5460 5461 5463 5464 5466 5467 5468 5471 5472 5473 5474

5476 5477 5478 5479 5480 5482 5483 5484 5486 5487 5488

001

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MSN CONFIGURATION

5489 5491 5492 5493 5494 5496 5497 5498 5499 5501 5502

5503 5505 5506 5507 5508 5510 5511 5512 5514 5515 5516

5517 5518 5520 5521 5522 5524 5525 5526 5527 5529 5530

5531 5532 5533 5535 5536 5537 5539 5540 5541 5542 5544

5545 5547 5548 5550 5551 5552 5553 5554 5556 5557 5559

5560 5561 5562 5563 5564 5565 5566 5568 5569 5570 5571

5572 5574 5576 5577 5578 5579 5580 5581 5583 5585 5586

5587 5589 5590 5591 5592 5593 5595 5596 5597 5598 5599

5600 5601 5602 5604 5605 5607 5608 5609 5610 5611 5612

5613 5614 5615 5616 5617 5618 5619 5620 5621 5622 5623

5624 5625 5626 5627 5628 5629 5630 5631 5632 5634 5635

5637 5638 5639 5640 5641 5642 5643 5645 5646 5648 5649

5650 5651 5652 5653 5654 5656 5657 5658 5660 5661 5662

5664 5665 5666 5668 5669 5671 5672 5673 5675 5676 5677

5678 5679 5680 5682 5683 5685 5686 5687 5688 5690 5691

5692 5693 5694 5695 5697 5698 5700 5701 5702 5703 5704

5706 5707 5708 5710 5711 5712 5713 5714 5716 5717 5718

5719 5721 5722 5723 5724 5725 5726 5727 5729 5730 5731

5732 5734 5735 5737 5738 5739 5740 5741 5742 5744 5745

5746 5748 5749 5750 5752 5753 5754 5756 5757 5759 5760

5761 5762 5764 5765 5766 5768 5769 5771 5772 5773 5775

5776 5777 5778 5780 5781 5782 5784 5785 5786 5788 5789

5791 5792 5793 5794 5796 5797 5798 5799 5801 5802 5804

5805 5806 5807 5809 5810 5811 5812 5813 5814 5815 5816

5817 5818 5819 5821 5822 5823 5824 5826 5827 5828 5829

5830 5831 5832 5833 5835 5837 5839 5840 5841 5844 5846

5847 5848 5850 5851 5852 5853 5855 5856 5857 5858 5859

5861 5862 5863 5864 5866 5867 5868 5869 5870 5871 5873

5874 5875 5877 5878 5879 5880 5882 5885 5886 5887 5888

5889 5891 5892 5893 5894 5896 5897 5898 5900 5901 5902

5903 5905 5906 5907 5908 5910 5911 5912 5914 5915 5917

5918 5920 5921 5924 5925 5926 5927 5928 5930 5931 5933

5934 5937 5940 5941 5942 5943 5944 5945 5948 5951 5953

5954 5956 5957 5959 5962 5963 5964 5967 5968 5970 5971

5973 5974 5976 5977 5978 5979 5981 5982 5985 5986 5988

5989 5990 5993 5996 5997 5999 6001 6003 6004 6007 6008

6011 6012 6014 6015 6017 6018 6019 6022 6023 6028 6029

6030 6032 6034 6037 6039 6041 6043 6044 6045 6047 6048

6052 6058 6060 6061 6062 6064 6068 6069 6071 6072 6073

6075 6076 6077 6078 6079 6081 6082 6084 6086 6088 6090

6091 6093 6095 6096 6098 6099 6102 6105 6106 6107 6109

6111

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.

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(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1 (1)

Equipment BFEA02 1 (2)

NOTE (1): Equipment BFEA01 is applicable to TASK 221447-831-801 001

Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1) on

Aircraft .

NOTE (2): Equipment BFEA02 is applicable to TASK 221447-831-802 001

Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with VSB on Aircraft and TASK 221447-831-803 001

Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1) 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:

Service Bulletin No. A320-22-1406

NOTE: Service Bulletin No. A320-22-1406 (AUTO FLIGHT - FLIGHT

AUGMENTATION COMPUTER (FAC) - INTRODUCE FAC CAA01) applies

MOD No. 39468P11175.

C. REASON

(1) History

This Service Bulletin has been issued in order to introduce Flight Augmentation

Computer (FAC) STD CAA02 on A318/A319/A320.

(2) Objective/Action

This Service Bulletin is published to advise all operators of A318/A319/A320 aircraft of

the issue of THALES AVIONICS Service Bulletin No. C13206A-22-001.

(3) Advantages

In comparison with FAC CAA01 PN C13206AA01, this new standard introduces the

following software modifications:

- Sharklets capability FAC CAA02 standard introduces software adaptation for

A319/A320/CFM/IAE equipped with Sharklets (weight and Center of Gravity (CG),

characteristic speeds).

. Weight and CG computation are adapted to take into account the lower fuel

consumption of Sharklets installations.

. Characteristic speeds: V alpha-Prot, V alpha-Max and V Stall-Warning are

adapted to take into account the Sharklets aerodynamic impact.

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Moreover, characteristic speeds are computed using the Flight Management System

(FMS) weight. This minimizes the consequences of a possible weight computation

imprecision (no effect on characteristic speeds displayed on PFD).

- Runway Overrun Prevention System (ROPS) function.

FAC CAA02 includes the software modifications necessary to perform the ROPS

function (MOD No. 155269P12511):

- During the approach, FAC computes an estimation of the braking distance of the

aircraft on a dedicated runway. If a runway overrun is detected, ROPS function

triggers aural alerts and Primary Flight Display (PFD) messages requiring either to

perform a Go Around or to apply the maximum braking. On FAC CAA02, this

function is activated by a dedicated pin program AB-06C (MP P12580). This

function is compatible with both Terrain Awareness and Warning System (TAWS)

equipment: Enhanced Ground Proximity Warning System (EGPWS) and Traffic,

Terrain and Transponder Collision Avoidance System (T3CAS).

NOTE: For ROPS function, a new Aeronautical Radio Incorporated (ARINC) bus

from the TAWS is acquired by the FAC to know the type of TAWS

installed (EGPWS or T3CAS).

- Other improvements:

. Reduction of the Rudder Travel Limitation at high speed. RTLU aims at limiting

vertical tail plane loads.

. Introduction of Stop Rudder Input warning. This audio warning alerts the crew

in case of inadequate and inappropriate use of the rudder pedals in flight.

This modification can be activated by pin program (separate aircraft MOD No.

154473P13357) and requires Flight Warning Computer (FWC) standard H2F7.

. Computation of a theoretical Trimmable Horizontal Stabilizer (THS) position

computation using the CG position computed from Multifunction Control and

Display Unit (MCDU) pilot inputs. This pseudo THS position is sent to the FWC

to trigger the new "Pitch trim MCDU CG disagree" alert, in case the actual THS

position does not correspond to the computed theoretical position. This function

requires FWC standard H2F6.

. Reduction of about 99 percent of a small rudder trim offset (about 0.1 deg)

occurring in case of short power supply cut (Flight Crew Operating Manual

(FCOM) temporary Revision No. 356-1).

. Correction of loss of flight plan upon Landing Gear Control and Interface Unit

(LGCIU) Nose wheel failure.

FAC CAA02 includes the software modifications necessary for the introduction of Stop

Rudder Input warning. This audio warning alerts the crew in case of inadequate and

inappropriate use of the rudder pedals in flight. This modification is activated by pin

program (separate aircraft MOD No. 154473P13357) Service Bulletin No. A320-22-1280

and requires Flight Warning Computer (FWC) standard H2F7 as minimum standard.

NOTE: The activation of this function is mandated by European Aviation Safety

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Agency (EASA).

(4) Operational/Maintenance Consequences

The operational consequences of this Service Bulletin are impacts on Flight Crew

Operating Manual (FCOM).

For the operational impact, refer to the Modification Operational Impact (MOI) No.

155315.

D. DESCRIPTION

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

- Either Modify the FAC Software (FINs 1CC1SW1 and 1CC2SW1) on

Aircraft as described in TASK 221447-831-801 001 Modification of the

FAC Software (FINs 1CC1SW1 and 1CC2SW1) on Aircraft (only valid

for aircraft on which MOD No. 153590P12462 (Service Bulletin No.

A320-22-1405) is embodied).

- Or Modify them in accordance with VSB on Aircraft as described in TASK

221447-831-802 001 Modification of the FAC Software (FINs 1CC1SW1

and 1CC2SW1) in accordance with VSB on Aircraft

- Or Modify them in accordance with VSB on Bench as described in TASK

221447-831-803 001 Modification of the FAC Software (FINs 1CC1SW1

and 1CC2SW1) in accordance with VSB on Bench

To accomplish this Service Bulletin it is necessary to :

Task 221447-831-801-001: Modification of the FAC Software (FINs 1CC1SW1 and

1CC2SW1) on Aircraft

(1) Upload the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

(2) Replace the disk (FIN 1CCMD1), in the cockpit stowage box

Task 221447-831-802-001: Modification of the FAC Software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on Aircraft

(1) Modify the FAC software (FINs 1CC1SW1 and 1CC2SW1) in accordance with VSB

on aircraft

(2) Replace the disk (FIN 1CCMD1), in the cockpit stowage box

Task 221447-831-803-001: Modification of the FAC Software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on Bench

(1) Remove the two FACs (FINs 1CC1 and 1CC2)

(2) Modify the FAC Software (FINs 1CC1SW1 and 1CC2SW1) in accordance with VSB

on Bench

(3) Install the two modified FACs (FINs 1C1 and 1CC2)

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(4) Replace the disk (FIN 1CCMD1), in the cockpit stowage box

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.

F. APPROVAL

The technical content of this document is approved under the authority of Design

Organization Approval No. EASA.21J.031.

If an aircraft listed in the effectivity has a modification or repair embodied that is not of

AIRBUS origin, and which affects the content of this Service Bulletin, the operator is

responsible for obtaining approval by its airworthiness authority for any adaptation necessary

before incorporation of the Service Bulletin.

G. MANPOWER

The manpower estimates given in this Service Bulletin are based on the direct labor cost to

do the work. These estimates assume that the work will be done by experienced personnel,

and may need to be revised upwards to suit operator’s circumstances. The estimates do not

include the time to prepare, plan or inspect the work. Manufacture and procurement of parts

and tools, drying times for paints, sealants, etc., and general administration work are also not

included.

Task 221447-831-801-001: Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

on Aircraft

Get Access 0.50

On Aircraft

Upload the FAC Software (FINs 1CC1SW1 and

1CC2SW1)

0.25

Replace the disk (FIN 1CCMD1), in the cockpit

stowage box

0.25

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

Task 221447-831-802-001: Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with VSB on Aircraft

Get Access 0.50

On Aircraft

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Task 221447-831-802-001: Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with VSB on Aircraft

Replace the disk (FIN 1CCMD1), in the cockpit

stowage box

0.25

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 1.75

ELAPSED TIME (HOURS) 1.75

Additional manhours related to Vendor SB; refer to:

Modify the FAC software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on aircraft

THALES AVIONICS Service Bulletin

No. C13206A-22-001

Task 221447-831-803-001: Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with VSB on Bench

Get Access 0.50

On Aircraft

Remove the two FACs (FINs 1CC1 and 1CC2) 0.50

Install the two modified FACs (FINs 1C1 and 1CC2) 0.50

Replace the disk (FIN 1CCMD1), in the cockpit

stowage box

0.25

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 2.75

ELAPSED TIME (HOURS) 2.75

Additional manhours related to Vendor SB; refer to:

Modify the FAC Software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on Bench

THALES AVIONICS Service Bulletin

No. C13206A-22-001

H. WEIGHT AND BALANCE

Not Changed

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-41-52

12-34-24 22-66-00 22-66-34

24-41-00 29-10-00 29-23-00

29-24-00 31-32-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Flight Crew Operating Manual (FCOM)

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Modification Operational Impact (MOI) 155315

Service Bulletin (SB) A320-22-1406

Vendor Service Bulletin (VSB) THALES AVIONICS Service

Bulletin No. C13206A-22-001

K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL)

Flight Crew Operating Manual (FCOM)

Illustrated Parts Catalog (IPC) 22-67-08

This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in

advance, in case you need your operational documentation to be amended by a revision prior

to Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to:

AIRBUS Customer Services Technical Data

Fax: (33) 5 61 93 28 06

E-mail: sb.reporting@airbus.com

SB Reporting service is accessible on-line through AIRBUSWorld from:

- "My on-line services" section, available on all AIRBUSWorld pages.

- The Maintenance and Engineering Community, in:

. Modify and Upgrade page - Access SB and VSB section.

These amendments will be confirmed by the next normal revision of operational

documentation, once your Service Bulletin accomplishment report has been sent, as usual, to

our Customer Services Aircraft In-Service Data department.

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

Disk-FAC Operational

Program

F1421204 F1422927 03 Not

Applicable

Software-FAC

Operational Pro

G2856AAA01 G2856AAA02 03 NO

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.

M. SPARES

None

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This Page Intentionally Left Blank

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Vendor parts are to be procured from:

Equipment BFEA01 THALES AVIONICS

105, Avenue du General Eisenhower

BP 63647

31036 TOULOUSE CEDEX 1

FRANCE

Tel: (33) 5 61 19 76 95

Fax: (33) 5 61 19 68 20

E-mail: retrofit@fr.thalesgroup.com

Or, modification of removed equipment should be negotiated directly with THALES

AVIONICS as per instructions given in Service Bulletin No. C13206A-22-001:

Equipment BFEA02 THALES AVIONICS

105, Avenue du General Eisenhower

BP 63647

31036 TOULOUSE CEDEX 1

FRANCE

Tel: (33) 5 61 19 76 95

Fax: (33) 5 61 19 68 20

E-mail: retrofit@fr.thalesgroup.com

(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.

Refer to the THALES AVIONICS Service Bulletin No. C13206A-22-001 for the

equipment modification sales terms.

B. INDUSTRY SUPPORT INFORMATION

For Equipment BFEA01, Industry support terms for the equipment must be negotiated with

the equipment supplier.

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For Equipment BFEA02, refer to the THALES AVIONICS Service Bulletin No.

C13206A-22-001 for the industry support terms of the Vendor Service Bulletin parts and

labor.

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

F1422927 1 MEDIA F1421204 03 (1)

G2856AAA02 1 SOFTWARE G2856AAA01 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.

NOTE (1): Operators shall only order media disk FIN 1CCMD1 (PN F1422927)

which contains the FAC Software FINs 1CC1SW1 and 1CC2SW1 (PN

G2856AAA02).

Equipment BFEA02

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

NOTES

F1422927 1 MEDIA F1421204 03 (1)

G2856AAA02 1 SOFTWARE G2856AAA01 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.

NOTE (1): Operators shall only order media disk FIN 1CCMD1 (PN F1422927)

which contains the FAC Software FINs 1CC1SW1 and 1CC2SW1 (PN

G2856AAA02).

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E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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This Page Intentionally Left Blank

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 221447-831-801-001 - Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

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.

Task Associated Data

Zone

210

Modified FIN

1CC1SW1 1CC2SW1 1CCMD1

Access

Door 831 841

Manpower

TOTAL MANHOURS 2.00

ELAPSED TIME (HOURS) 2.00

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A. GENERAL

(1) Subtask 221447-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-52, 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) For the identification of access panels, refer to AMM 06-41-52, Page Block 001.

(2) Subtask 221447-839-001-001 - 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 221447-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

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- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position

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

12-34-24-869-002.

C. PROCEDURE

(1) Subtask 221447-470-001-001 - Upload the FAC Software (FINs 1CC1SW1 and

1CC2SW1)

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831, Door 841

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

G2856AAA02 1 SOFTWARE

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 22-66-00-610-802

Task 24-41-00-861-002

Task 29-10-00-864-003

Task 29-23-00-864-001

Task 29-24-00-864-001

Task 31-32-00-860-001

(a) Do a check of the PN reference of the element(s) (pre-loaded into the related

FAC), included in the "Uploading of the FAC Software", refer to AMM Task

22-66-00-610-802.

NOTE: If the AMM Task 22-66-00-610-802 is not available in the latest

AMM operator’s issue, do these steps:

1 Make sure that the aircraft is in the ground configuration.

2 Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-002.

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3 Make sure that hydraulic systems are depressurized, refer to AMM

Task 29-10-00-864-003, AMM Task 29-23-00-864-001 and AMM Task

29-24-00-864-001.

4 On the overhead panel, on the FLT CTL panels 23VU and 24VU:

- Make sure that the FAC1 and FAC2 pushbutton switches are pushed (in)

(FAULT and OFF legends are off).

5 Make sure that these circuit breakers are closed:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU AUTO FLT/FAC1/28VDC 5CC1 04 B

49VU AUTO FLT/FAC1/26VAC 14CC1 03 B

49VU AUTO FLT/MCDU/1 11CA1 01 B

121VU DATA/LOADER/SPLY 3TD 16 J (1)

121VU DLS&/DLRB/SPLY 5TD 15 J

121VU PDL/PWR/SPLY 14TD 19 K

121VU AUTO FLT/FAC2/28VDC 5CC2 19 M

121VU AUTO FLT/FAC2/26VAC 14CC2 18 M

NOTE (1): If equipped.

6 Check of the PN reference of the related FAC:

a Identify and record the part number of the FAC1 (2).

b Get access to the system/report test menu page, refer to AMM Task

31-32-00-860-001.

c Procedure:

ACTION RESULT

1. Push the line key adjacent to the AFS

indication.

- The AFS menu page comes into view.

2. Push the line key adjacent to the LRU

IDENTIFICATION indication.

- The LRU IDENTIFICATION page comes into

view.

3. Make sure that the FAC PN on the LRU

IDENTIFICATION page is of the C13206XXXX

type.

4. Do a check of the two last alphanumerical

characters of the FAC PN shown on the LRU

IDENTIFICATION page and shown on the LRU

IDENT DISPLAYED on the media disk:

- If the two last alphanumerical characters are

different, continue the procedure.

- If the two last alphanumerical characters are the

same, the software is already uploaded.

No uploading is necessary.

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ACTION RESULT

5. Do a check of the two alphanumerical

characters that follow "C13206" of the FAC PN

shown on the LRU IDENTIFICATION page and

shown on the LRU IDENT DISPLAYED on the

media disk:

- If the two alphanumerical characters are the

same, continue the procedure.

- If one alphanumerical character is different, the

FAC and the media disk are not compatible,

stop the procedure and contact Airbus support.

(b) Do the uploading of the FAC Software, refer to AMM Task 22-66-00-610-802:

FIN 1CC1SW1

1 Software-FAC

Operational Pro

G2856AAA01 Discard

becomes:

FIN 1CC1SW1

1 Software-FAC

Operational Pro

G2856AAA02

and

FIN 1CC2SW1

1 Software-FAC

Operational Pro

G2856AAA01 Discard

becomes:

FIN 1CC2SW1

1 Software-FAC

Operational Pro

G2856AAA02

NOTE: If the AMM Task 22-66-00-610-802 is not available in the latest

AMM operator’s issue, do these steps:

1 If a Portable Data Loader (PDL) is used, install the PDL as follows:

a On the overhead panel, on DATA LOADING panel 52VU:

<1> Loosen the two middle quick-release fasteners of the access cover

and remove it.

<2> Connect the cable to he PORTABLE DATA LOADER (PMAT2000)

or LOADER - DATA, PORTABLE and to the SYSTEMS data loader

connector (2TD).

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b On the center pedestal, on the DATA LOADING panel 117VU (if

available):

<1> Loosen the two middle quick-release fasteners of the access cover

and remove it.

<2> Connect the cable to the PMAT2000 KIT (P2KABF01) or PMAT2000

DATA KIT SECURE (P2KABF02) or LOADER - DATA, PORTABLE

and to the DATA LOADER connector (2147VC).

2 If a PDL is used, start the PDL as follows:

a Start PORTABLE DATA LOADER (PMAT2000) or LOADER - DATA,

PORTABLE, refer to the portable data-loader user-guide.

3 Procedure:

a Uploading of the FAC Software (with MDDU):

NOTE: This procedure is for FAC1. For the FAC2, which is

identical, use the indications between the parentheses.

ACTION RESULT

1. Open the circuit breaker 5CC1(2).

2. On the overhead panel, on the Data Loading

Selector:

- Set the ON/OFF switch to ON.

On the multipurpose disk drive unit:

- The < < MDDU READY > > indication is shown.

Make sure that the circuit breakers 5TD and 3TD

are closed.

On the multipurpose disk drive unit:

The < < MDDU READY > > indication comes into

view.

3. On the overhead panel, on the Data Loading

Selector:

- Push the PREV or NEXT key until you get the

indicator FAC1(2)

- Push the SEL CTL key.

On the display of the Data Loading Selector:

- FAC1(2) SELECTED indication is shown.

4. Put the media disk of the FAC into the disk

drive of the MDDU.

On the display of the Data Loading Selector:

- The READY indication comes into view,

- Then, the WAIT RESPONSE indication is

shown.

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ACTION RESULT

5. Close the circuit breaker 5CC1(2). On the MDDU:

- The TRANS IN PROG indication is shown after

a few seconds (with a maximum of 45 seconds).

NOTE: If "block XXXX" appears "XXXX"

shows the remaining file blocks of

the uploading.

- When all the data are loaded in the computer,

the TRANSF COMPLETE indication is shown.

6. On the MDDU:

- Eject the disk from the disk drive.

On the MDDU:

- The < < MDDU READY > > indication comes

into view.

7. On the overhead panel, on the Data Loading

Selector:

- Push the SEL CTL key.

On the display of the Data Loading Selector:

- FAC1(2) NOT SELECTED indication is shown.

8. On the Data Loading Selector:

- Set the ON/OFF switch to OFF.

9. Open the circuit breaker 5CC1(2).

b Uploading of the FAC Software (with PDL):

NOTE: This procedure is for FAC1. For the FAC2, which is

identical, use the indications between the parentheses.

ACTION RESULT

1. Open the circuit breaker 5CC1(2).

2. On the overhead panel, on the Data Loading

Selector:

- Set the ON/OFF switch to ON.

- Make sure that the circuit breaker 5TD is closed.

- Make sure that the PDL is ready, refer to the

portable data-loader user-guide.

3. On the overhead panel, on the Data Loading

Selector:

- Push the PREV or NEXT key until you get the

indication FAC1(2)

- Push the SEL CTL key.

On the display of the Data Loading Selector:

- FAC1(2) SELECTED indication is shown.

4. Close the circuit breaker 5CC1(2)

5. Upload the FAC software, refer to the portable

data-loader user-guide.

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ACTION RESULT

6. On the Data Loading Selector:

- Set the ON/OFF switch to OFF.

7. Open the circuit breaker 5CC1(2).

c Uploading of the FAC Software (with PDL through ARINC 615) (if

available):

NOTE: This procedure is used to upload software to the FAC

with the PDL (PMAT2000 KIT or equivalent).

NOTE: If the PDL has the digital signature check, two messages

can be triggered by the PDL:

- One if the PDL detects that the software is not

signed, refer to PDL user-guide, this message can

be ignored and has no effect on aircraft software

uploading.

- One if the PDL detects an incorrect or corrupted

signature, refer to PDL user-guide, then the software

uploading will not be possible and another software

has to be used.

For data security reasons, AIRBUS recommends that the

user does a report of the fault to his Aircraft Security

Focal Point.

NOTE: This procedure is for FAC1. For the FAC2, which is

identical, use the indications between the parentheses.

ACTION RESULT

1. Open the circuit breaker 5CC1(2).

2. On the overhead panel, on the Data Loading

Selector:

- Set the ON/OFF switch to ON.

- Make sure that the circuit breaker 5TD and

14TD are closed.

- Make sure that the PDL is ready, refer to the

portable data-loader user-guide.

3. On the overhead panel, on the Data Loading

Selector:

- Push the PREV or NEXT key until you get the

indication FAC1(2)

- Push the SEL CTL key.

On the display of the Data Loading Selector:

- FAC1(2) SELECTED indication is shown.

4. Close the circuit breaker 5CC1(2).

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ACTION RESULT

5. Upload the FAC software, refer to the portable

data-loader user-guide.

6. On the Data Loading Selector:

- Set the ON/OFF switch to OFF.

7. Open the circuit breaker 5CC1(2).

(2) Subtask 221447-960-002-001 - Replace the disk (FIN 1CCMD1), in the cockpit

stowage box

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831, Door 841

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F1422927 1 MEDIA (1)

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

shall be ordered as necessary through the given channel.

NOTE (1): Operators shall only order media disk FIN 1CCMD1 (PN F1422927)

which contains the FAC Software FINs 1CC1SW1 and 1CC2SW1 (PN

G2856AAA02).

References

Fig. A-FBAAA

Disk stowage location.

Sheet 01

Fig. A-FBBAA

Disk stowage location.

Sheet 01

(a) In the cockpit, replace the disk in the stowage box:

Refer to Fig. A-FBAAA and Fig. A-FBBAA

1 Remove:

FIN 1CCMD1

1 Disk-FAC Operational

Program

F1421204 Discard

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2 Install:

FIN 1CCMD1

1 Disk-FAC Operational

Program

F1422927

NOTE: This disk FIN 1CCMD1 contains the software FINs 1CC1SW1

and 1CC2SW1 (PN G2856AAA02).

D. TEST

(1) Subtask 221447-700-001-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-00-610-802

Task 31-32-00-860-001

(a) Procedure:

1 Do two checks of the reference of the software loaded in the FAC included in

the "Uploading of the FAC Software", refer to AMM Task 22-66-00-610-802.

NOTE: If the AMM Task 22-66-00-610-802 is not available in the latest

AMM operator’s issue, do these steps:

a Do the check of the reference of the software loaded in the FAC through

the LRU IDENTIFICATION.

<1> Do the procedure to get access to the SYSTEM REPORT/TEST

Menu Page, refer to AMM Task 31-32-00-860-001.

<2> Procedure:

NOTE: This procedure is for FAC1. For the FAC2,

which is identical, use the indications between the

parentheses.

ACTION RESULT

1. Close the circuit breaker 5CC1(2). Make sure that:

- FAC1(2) is ON

- No ECAM message related to FAC1(2) is shown

- FAULT indication is not shown on the

pushbutton switch 12CC1 (2) on the panels

23VU (24VU).

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ACTION RESULT

2. On the MCDU:

- Push the line key adjacent to the AFS indication.

On the MCDU:

- The AFS menu page comes into view.

3. Push the line key adjacent to the LRU

IDENTIFICATION indication.

On the MCDU:

- The LRU IDENTIFICATION page comes into

view.

4.Make sure that the PN of the FAC shown on the

LRU IDENTIFICATION page is the same as the

PN on the media disk.

5. push the MCDU MENU mode key. - The MCDU MENU page comes into view.

NOTE: A fictive Part Number C13206AA02 is created

to represent the complete computer (hardware

C13206AA00 and software G2856AA02). It is the

one that is indicated to the crew or to the

maintenance team when they perform a LRU

IDENTIFICATION.

b Do the check of the reference of the software loaded in the FAC through

the aircraft Config Report:

ACTION RESULT

1. On the MCDU:

- Push the line key adjacent to the CFDS

indication.

- Push the NEXT key.

- Push the AVIONICS CONFIG REPORT key.

- Push the START key.

- Push the line key adjacent to the FAC.

On the MCDU:

- The CFDS menu page comes into view.

2. Make sure that the PN of the FAC shown is the

same as the PN on the media disk.

2 If a PDL was used, stop the PDL as follows:

a Stop the PORTABLE DATA LOADER (PMAT2000) or LOADER - DATA,

PORTABLE, refer to the portable data-loader user-guide.

3 If a PDL is used, remove the PDL as follows:

a On the overhead panel, on DATA LOADING panel 52VU:

<1> Disconnect the cable from the PORTABLE DATA LOADER

(PMAT2000) or LOADER - DATA, PORTABLE and to the

SYSTEMS data loader connector (2TD).

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<2> Install the access cover and tighten the two middle quick-release

fasteners.

b On the center pedestal, on the DATA LOADING panel 117VU (if

available):

<1> Disconnect the cable from the PMAT2000 KIT (P2KABF01) or

PMAT2000 DATA KIT SECURE (P2KABF02) or LOADER - DATA,

PORTABLE and from the DATA LOADER connector (2147VC).

<2> Install the access cover and tighten the two middle quick-release

fasteners.

4 Close-up:

a Put the aircraft back to its initial configuration.

<1> On the MCDU, push the line key adjacent to the RETURN indication

until the CFDS MENU page comes into view.

<2> On the MCDU, set the BRT knobs to OFF position.

<3> Remove the old media disk (PN F1421204) from stowage box. Then

put the new media disk in the stowage box.

E. CLOSE-UP

(1) Subtask 221447-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

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

equipment.

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

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Task 221447-831-802-001 - Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

in accordance with 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.

Task Associated Data

Zone

210

Modified FIN

1CC1SW1 1CC2SW1 1CCMD1

Access

Door 831 841

Manpower

TOTAL MANHOURS 1.75

ELAPSED TIME (HOURS) 1.75

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Additional manhours related to Vendor SB; refer to:

THALES AVIONICS Service Bulletin No. C13206A-22-001

A. GENERAL

(1) Subtask 221447-910-002-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-52, Page Block 001

(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) For the identification of access panels, refer to AMM 06-41-52, Page Block 001.

(2) Subtask 221447-839-002-001 - 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 221447-941-002-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

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- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position

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

12-34-24-869-002.

C. PROCEDURE

(1) Subtask 221447-831-002-001 - Modify the FAC software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on aircraft

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831, Door 841

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

G2856AAA02 1 SOFTWARE

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 22-66-00-610-802

Task 24-41-00-861-002

Task 29-10-00-864-003

Task 29-23-00-864-001

Task 29-24-00-864-001

Task 31-32-00-860-001

Vendor Service Bulletin (VSB) THALES AVIONICS C13206A-22-001

(a) Do a check of the PN reference of the element(s) (pre-loaded into the related

FAC), included in the "Uploading of the FAC Software", refer to AMM Task

22-66-00-610-802.

NOTE: If the AMM Task 22-66-00-610-802 is not available in the latest

AMM operator’s issue, do these steps:

1 Make sure that the aircraft is in the ground configuration.

2 Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-002.

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3 Make sure that hydraulic systems are depressurized, refer to AMM

Task 29-10-00-864-003, AMM Task 29-23-00-864-001 and AMM Task

29-24-00-864-001.

4 On the overhead panel, on the FLT CTL panels 23VU and 24VU:

- Make sure that the FAC1 and FAC2 pushbutton switches are pushed (in)

(FAULT and OFF legends are off).

5 Make sure that these circuit breakers are closed:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU AUTO FLT/FAC1/28VDC 5CC1 04 B

49VU AUTO FLT/FAC1/26VAC 14CC1 03 B

49VU AUTO FLT/MCDU/1 11CA1 01 B

121VU DATA/LOADER/SPLY 3TD 16 J (1)

121VU DLS&/DLRB/SPLY 5TD 15 J

121VU PDL/PWR/SPLY 14TD 19 K

121VU AUTO FLT/FAC2/28VDC 5CC2 19 M

121VU AUTO FLT/FAC2/26VAC 14CC2 18 M

NOTE (1): If equipped.

6 Check of the PN reference of the related FAC:

a Identify and record the part number of the FAC1 (2).

b Get access to the system/report test menu page, refer to AMM Task

31-32-00-860-001.

c Procedure:

ACTION RESULT

1. Push the line key adjacent to the AFS

indication.

- The AFS menu page comes into view.

2. Push the line key adjacent to the LRU

IDENTIFICATION indication.

- The LRU IDENTIFICATION page comes into

view.

3. Make sure that the FAC PN on the LRU

IDENTIFICATION page is of the C13206XXXX

type.

4. Do a check of the two last alphanumerical

characters of the FAC PN shown on the LRU

IDENTIFICATION page and shown on the LRU

IDENT DISPLAYED on the media disk:

- If the two last alphanumerical characters are

different, continue the procedure.

- If the two last alphanumerical characters are the

same, the software is already uploaded.

No uploading is necessary.

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ACTION RESULT

5. Do a check of the two alphanumerical

characters that follow "C13206" of the FAC PN

shown on the LRU IDENTIFICATION page and

shown on the LRU IDENT DISPLAYED on the

media disk:

- If the two alphanumerical characters are the

same, continue the procedure.

- If one alphanumerical character is different, the

FAC and the media disk are not compatible,

stop the procedure and contact Airbus support.

(b) Do the Reprogramming of the FAC Software (FINs 1CC1SW1 and 1CC2SW1) as

per instructions given in THALES AVIONICS Service Bulletin No. C13206A-22-001.

FIN 1CC1SW1

1 Software-FAC

Operational Pro

G2856AAA01 Discard

becomes

FIN 1CC1SW1

1 Software-FAC

Operational Pro

G2856AAA02

and

FIN 1CC2SW1

1 Software-FAC

Operational Pro

G2856AAA01 Discard

becomes

FIN 1CC2SW1

1 Software-FAC

Operational Pro

G2856AAA02

(2) Subtask 221447-831-003-001 - Replace the disk (FIN 1CCMD1), in the cockpit

stowage box

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831, Door 841

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

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Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F1422927 1 MEDIA (1)

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

shall be ordered as necessary through the given channel.

NOTE (1): Operators shall only order media disk FIN 1CCMD1 (PN F1422927)

which contains the FAC Software FINs 1CC1SW1 and 1CC2SW1 (PN

G2856AAA02).

References

Fig. A-FBAAA

Disk stowage location.

Sheet 01

Fig. A-FBBAA

Disk stowage location.

Sheet 01

(a) In the cockpit, replace the disk in the stowage box:

Refer to Fig. A-FBAAA and Fig. A-FBBAA

1 Remove:

FIN 1CCMD1

1 Disk-FAC Operational

Program

F1421204 Discard

2 Install:

FIN 1CCMD1

1 Disk-FAC Operational

Program

F1422927

NOTE: This disk FIN 1CCMD1 contains the software FINs 1CC1SW1

and 1CC2SW1 (PN G2856AAA02).

D. TEST

(1) Subtask 221447-700-002-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-00-610-802

Task 31-32-00-860-001

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(a) Procedure:

1 Do two checks of the reference of the software loaded in the FAC included in

the "Uploading of the FAC Software", refer to AMM Task 22-66-00-610-802.

NOTE: If the AMM Task 22-66-00-610-802 is not available in the latest

AMM operator’s issue, do these steps:

a Do the check of the reference of the software loaded in the FAC through

the LRU IDENTIFICATION.

<1> Do the procedure to get access to the SYSTEM REPORT/TEST

Menu Page, refer to AMM Task 31-32-00-860-001.

<2> Procedure:

NOTE: This procedure is for FAC1. For the FAC2,

which is identical, use the indications between the

parentheses.

ACTION RESULT

1. Close the circuit breaker 5CC1(2). Make sure that:

- FAC1(2) is ON

- No ECAM message related to FAC1(2) is shown

- FAULT indication is not shown on the

pushbutton switch 12CC1 (2) on the panels

23VU (24VU).

2. On the MCDU:

- Push the line key adjacent to the AFS indication.

On the MCDU:

- The AFS menu page comes into view.

3. Push the line key adjacent to the LRU

IDENTIFICATION indication.

On the MCDU:

- The LRU IDENTIFICATION page comes into

view.

4. Make sure that the PN of the FAC shown on

the LRU IDENTIFICATION page is the same as

the PN on the media disk.

5. Push the MCDU MENU mode key. - The MCDU MENU page comes into view.

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b Do the check of the reference of the software loaded in the FAC through

the aircraft Config Report:

ACTION RESULT

1. On the MCDU:

- Push the line key adjacent to the CFDS

indication.

- Push the NEXT key.

- Push the AVIONICS CONFIG REPORT key.

- Push the START key.

- Push the line key adjacent to the FAC.

On the MCDU:

- The CFDS menu page comes into view.

2. Make sure that the PN of the FAC shown is the

same as the PN on the media disk.

E. CLOSE-UP

(1) Subtask 221447-942-003-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

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

equipment.

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

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Task 221447-831-803-001 - Modification of the FAC Software (FINs 1CC1SW1 and 1CC2SW1)

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.

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.

Task Associated Data

Zone

120 210

Modified FIN

1CC1 1CC1SW1 1CC2 1CC2SW1 1CCMD1

Access

Door 824 831 841

Manpower

TOTAL MANHOURS 2.75

ELAPSED TIME (HOURS) 2.75

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Additional manhours related to Vendor SB; refer to:

THALES AVIONICS Service Bulletin No. C13206A-22-001

A. GENERAL

(1) Subtask 221447-910-003-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-41-52, 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) For the identification of access panels, refer to AMM 06-41-52, Page Block 001.

(2) Subtask 221447-839-003-001 - 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 221447-941-003-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002

Task 22-66-34-000-002

NOTE: The items given in this note shall be considered as the basic Aircraft

configuration before you start a maintenance task:

- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)

- Engine shut down, thrust reversers closed and locked

- Aircraft in clean configuration

- Parking brake applied

- Aircraft electrical network de-energized

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

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- Hydraulic systems depressurized

- Access to the cockpit and cabin is available

- All circuit breakers are in closed position

- All controls in NORM, AUTO or OFF position

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

12-34-24-869-002.

(b) Do the Job Set up procedure as specified in the removal of the two FACs (FINs

1CC1 and 1CC2), refer to AMM Task 22-66-34-000-002.

C. PROCEDURE

(1) Subtask 221447-831-004-001 - Remove the two FACs (FINs 1CC1 and 1CC2)

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 824

Work location Electrical panel 80VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-000-002

(a) Remove the two FACs (FINs 1CC1 and 1CC2), refer to AMM Task

22-66-34-000-002.

(2) Subtask 221447-831-005-001 - Modify the FAC Software (FINs 1CC1SW1 and

1CC2SW1) in accordance with VSB on Bench

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

G2856AAA02 1 SOFTWARE

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

shall be ordered as necessary through the given channel.

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References

Aircraft Maintenance Manual (AMM) Task 22-66-00-610-802

Task 24-41-00-861-002

Task 29-10-00-864-003

Task 29-23-00-864-001

Task 29-24-00-864-001

Task 31-32-00-860-001

Vendor Service Bulletin (VSB) THALES AVIONICS C13206A-22-001

(a) Do a check of the PN reference of the element(s) (pre-loaded into the related

FAC), included in the "Uploading of the FAC Software", refer to AMM Task

22-66-00-610-802.

NOTE: If the AMM Task 22-66-00-610-802 is not available in the latest

AMM operator’s issue, do these steps:

1 Make sure that the aircraft is in the ground configuration.

2 Energize the aircraft electrical circuits, refer to AMM Task 24-41-00-861-002.

3 Make sure that hydraulic systems are depressurized, refer to AMM

Task 29-10-00-864-003, AMM Task 29-23-00-864-001 and AMM Task

29-24-00-864-001.

4 On the overhead panel, on the FLT CTL panels 23VU and 24VU:

- Make sure that the FAC1 and FAC2 pushbutton switches are pushed (in)

(FAULT and OFF legends are off).

5 Make sure that these circuit breakers are closed:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

49VU AUTO FLT/FAC1/28VDC 5CC1 04 B

49VU AUTO FLT/FAC1/26VAC 14CC1 03 B

49VU AUTO FLT/MCDU/1 11CA1 01 B

121VU DATA/LOADER/SPLY 3TD 16 J (1)

121VU DLS&/DLRB/SPLY 5TD 15 J

121VU PDL/PWR/SPLY 14TD 19 K

121VU AUTO FLT/FAC2/28VDC 5CC2 19 M

121VU AUTO FLT/FAC2/26VAC 14CC2 18 M

NOTE (1): If equipped.

6 Check of the PN reference of the related FAC:

a Identify and record the part number of the FAC1 (2).

b Get access to the system/report test menu page, refer to AMM Task

31-32-00-860-001.

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c Procedure:

ACTION RESULT

1. Push the line key adjacent to the AFS

indication.

- The AFS menu page comes into view.

2. Push the line key adjacent to the LRU

IDENTIFICATION indication.

- The LRU IDENTIFICATION page comes into

view.

3. Make sure that the FAC PN on the LRU

IDENTIFICATION page is of the C13206XXXX

type.

4. Do a check of the two last alphanumerical

characters of the FAC PN shown on the LRU

IDENTIFICATION page and shown on the LRU

IDENT DISPLAYED on the media disk:

- If the two last alphanumerical characters are

different, continue the procedure.

- If the two last alphanumerical characters are the

same, the software is already uploaded.

No uploading is necessary.

5. Do a check of the two alphanumerical

characters that follow "C13206" of the FAC PN

shown on the LRU IDENTIFICATION page and

shown on the LRU IDENT DISPLAYED on the

media disk:

- If the two alphanumerical characters are the

same, continue the procedure.

- If one alphanumerical character is different, the

FAC and the media disk are not compatible,

stop the procedure and contact Airbus support.

(b) Do the Reprogramming of the FAC Software (FINs 1CC1SW1 and 1CC2SW1) as

per instructions given in THALES AVIONICS Service Bulletin No. C13206A-22-001.

FIN 1CC1SW1

1 Software-FAC

Operational Pro

G2856AAA01 Discard

becomes

FIN 1CC1SW1

1 Software-FAC

Operational Pro

G2856AAA02

and

FIN 1CC2SW1

1 Software-FAC

Operational Pro

G2856AAA01 Discard

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becomes

FIN 1CC2SW1

1 Software-FAC

Operational Pro

G2856AAA02

(3) Subtask 221447-831-006-001 - Install the two modified FACs (FINs 1C1 and 1CC2)

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 824

Work location Electrical panel 80VU

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002

(a) Install the two modified FACs (FINs 1CC1 and 1CC2), refer to AMM Task

22-66-34-400-002.

(4) Subtask 221447-831-007-001 - Replace the disk (FIN 1CCMD1), in the cockpit

stowage box

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831, Door 841

Manpower Resources

Manhours 0.25

Minimum number of person 1

Subtask elapsed time 0.25

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA02

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F1422927 1 MEDIA (1)

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

shall be ordered as necessary through the given channel.

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NOTE (1): Operators shall only order media disk FIN 1CCMD1 (PN F1422927)

which contains the FAC Software FINs 1CC1SW1 and 1CC2SW1 (PN

G2856AAA02).

References

Fig. A-FBAAA

Disk stowage location.

Sheet 01

Fig. A-FBBAA

Disk stowage location.

Sheet 01

(a) In the cockpit, replace the disk in the stowage box:

Refer to Fig. A-FBAAA and Fig. A-FBBAA

1 Remove:

FIN 1CCMD1

1 Disk-FAC Operational

Program

F1421204 Discard

2 Install:

FIN 1CCMD1

1 Disk-FAC Operational

Program

F1422927

NOTE: This disk FIN 1CCMD1 contains the software FINs 1CC1SW1

and 1CC2SW1 (PN G2856AAA02).

D. TEST

(1) Subtask 221447-700-003-001 - Testing

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-00-610-802

Task 22-66-34-400-002

Task 31-32-00-860-001

(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 FAC, refer to AMM Task

22-66-34-400-002.

(b) Procedure:

1 Do the test procedure as specified after the installation of the two FACs (FINs

1CC1 and 1CC2), refer to AMM Task 22-66-34-400-002.

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2 Do two checks of the reference of the software loaded in the FAC included in

the "Uploading of the FAC Software", refer to AMM Task 22-66-00-610-802.

NOTE: If the AMM Task 22-66-00-610-802 is not available in the latest

AMM operator’s issue, do these steps:

a Do the check of the reference of the software loaded in the FAC through

the LRU IDENTIFICATION.

<1> Do the procedure to get access to the SYSTEM REPORT/TEST

Menu Page, refer to AMM Task 31-32-00-860-001.

<2> Procedure:

NOTE: This procedure is for FAC1. For the FAC2,

which is identical, use the indications between the

parentheses.

ACTION RESULT

1. Close the circuit breaker 5CC1(2). Make sure that:

- FAC1(2) is ON

- No ECAM message related to FAC1(2) is shown

- FAULT indication is not shown on the

pushbutton switch 12CC1 (2) on the panels

23VU (24VU).

2. On the MCDU:

- Push the line key adjacent to the AFS indication.

On the MCDU:

- The AFS menu page comes into view.

3. Push the line key adjacent to the LRU

IDENTIFICATION indication.

On the MCDU:

- The LRU IDENTIFICATION page comes into

view.

4. Make sure that the PN of the FAC shown on

the LRU IDENTIFICATION page is the same as

the PN on the media disk.

5. Push the MCDU MENU mode key. - The MCDU MENU page comes into view.

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b Do the check of the reference of the software loaded in the FAC through

the aircraft Config Report:

ACTION RESULT

1. On the MCDU:

- Push the line key adjacent to the CFDS

indication.

- Push the NEXT key.

- Push the AVIONICS CONFIG REPORT key.

- Push the START key.

- Push the line key adjacent to the FAC.

On the MCDU:

- The CFDS menu page comes into view.

2. Make sure that the PN of the FAC shown is the

same as the PN on the media disk.

E. CLOSE-UP

(1) Subtask 221447-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-400-002

(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 two FACs (FINs

1CC1 and 1CC2), refer to AMM Task 22-66-34-400-002.

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

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**CONF ALL

FR1

FR24A

Z210

A

B

C

B

A

C

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

ON AIRCRAFT CONFIGURATION (SEE FIG. A−FBBAA).

1CCMD1

N_SB_221447_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Disk stowage location.

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 68

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SERVICE BULLETIN

**CONF ALL

A A

A

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

ON AIRCRAFT CONFIGURATION (SEE FIG. A−FBAAA).

1CCMD1

N_SB_221447_5_BBAA_01_01

Figure A-FBBAA - Sheet 01

Disk stowage location.

DATE: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 69

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SERVICE BULLETIN

REPORTING SHEET

TITLE: AUTO-FLIGHT - FLIGHT AUGMENTATION COMPUTER (FAC) - INSTALL

STD FAC CAA02 (SHARKLET CAPABILITY AND ROPS FUNCTION)

MODIFICATION No.: 155315P12753

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: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

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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: Oct 18/13 SERVICE BULLETIN No.: A320-22-1447

REVISION No.: 03 - Apr 21/15 Page: 1

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