@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

ATA SYSTEM: 28

TITLE: FUEL- MAIN FUEL PUMP SYSTEM - INTRODUCE GROUND FAULT

INTERRUPTERS (GFI) TO CENTER TANK FUEL PUMPS

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 150736J3138

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

The center tank fuel pumps (Pump 1 FIN 37QA / Pump 2 38QA) are supplied by control relays (FIN

35QA / 36QA). These relays are installed in electrical panel 107VU. To protect the pump feeder supply

cable from the electrical panel 107VU and the pump windings against ’earth’ faults, additional earth

leakage protection is required.

Mod. No. 150690J2866 was issued to evaluate the additional earth leakage protection available by

replacing a control relay with Ground Fault Interrupter (GFI). As a result of this mod, an evaluation

Service Bulletin A320-28-1903 was issued to some operators to evaluate the application of Mod. No.

150690J2866.

Additional earth leakage protection was evaluated through installation of a GFI 70QA in electrical panel

107VU instead of control relay FIN 36QA.

This Service Bulletin introduces Mod. No. 150736J3138. This modification introduces GFIs and related

bases into the electrical supply circuits of the center tank fuel pump 1 (FIN 37QA) and pump 2 (FIN

38QA) on A318, A319 and A320 aircraft.

These GFIs have the same ’footprint’ as the existing relay/micro-contactors and physically replace them

on the electrical panel. The new GFI sockets are fool-proofed to prevent incorrectly fitment of a normal

relay/micro-contactor or inappropriate GFI device.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 1

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SERVICE BULLETIN

SUMMARY

These GFIs will replace the existing 3-phase relay/micro-contactors. The function of the GFI is to

electrically isolate the pump if a ground fault condition occurs downstream of the GFI. The GFI gives

additional earth leakage protection to the downstream circuit.

Accomplishment of this Service Bulletin will not change the characteristics of the aircraft.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

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

disruptions.

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 281188A01R00 1 1,680.00 Relay, Base, Placard Set

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 281188A02R00 1 3,360.00 Relay, Base, Placard Set

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 281188A01R00 1 1,680.00 Relay, Base, Placard Set

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 281188A02R00 1 3,360.00 Relay, Base, Placard Set

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 2

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SERVICE BULLETIN

SUMMARY

**CONF 005

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 281188A01R00 1 1,680.00 Relay, Base, Placard Set

**CONF 006

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 281188A02R00 1 3,360.00 Relay, Base, Placard Set

**CONF 007

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 281188A02R00 1 3,360.00 Relay, Base, Placard Set

EFFECTIVITY

**CONF ALL

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

01Z 03X 08U 15T 16T 17W 22V 27V 31V 31X 35U 36V 46U

47Y 52T 53U 53Z 56W 59U 59Z 60X 61T 62X 69X 73W 74T

75T 78T 78X 79W 80X 85T 86W 86Z 87Z 89T 91X 93V 94W

95V 95W 97U 98W 99W AAF AAN AAR AAW ABQ ABY ACA ACI

ADH ADR AEE AFL AFR AGC AHY AIJ AJM ALK AMC AMU ANA

ANZ APJ ART AUA AUH AVA AXM AZA B2V BAB BAL BAW BEC

BEL BER BGF BGH BHP BJN BKP BMA BON BRS BTV C9G CBJ

CCA CCM CEB CEF CES CHB CHH CIB CQH CQN CRK CSA CSC

CSN CSZ CTN CUA CYP D2F DAL DCS DKH DLH DNV DRK EAA

EDW EIN ETD EZD EZY F2I FFT FHE FHY FIN FPY FRN G2X

G4I G8E GAF GAP GFA GIA GIR GLG GMI GOW GSW GWI GWY

HAY HCC HDA HRM HVN I2L I2T IAC IBE IBS IGO IRA ISR

ISS IWD IYE IZM JAG JAV JBU JET JSA JST JZR KAC KFR

KGL KHO KIL KKK KMF KNE KZR LAA LAN LAO LBT LBY LFO

LFX LJB LLM LLP LMJ LMU LZB MAC MAU MDL MEA MHS MJN

MLD MLM MLR MMA MON MSC MSR MXA NIA NKS NLV NLY NMA

NMB NVD O2X OAI OHY ONE ORF OZW PAL PIC PJS PTR PVJ

QAF QTR R1T RBA RBG RFJ RJA RKM RNV ROT RYW RZO SAA

SAS SBI SBN SDM SFJ SFW SGG SHJ SHY SKU SLK SND SNX

SOL STU SUD SVA SVR SVW SWM SWR SYA SYR TAE TAI TAK

TAM TAP TAR TBA TBJ TCW TCX TGW THY TJS TNA TOM TWJ

UAE UAL UDC UEA UKN UNA USA UZB VIM VJC VKG VKH VLE

VLG VLK VOI VRD WAU WGT WHT WTJ WZZ XLF YAP

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 3

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SERVICE BULLETIN

SUMMARY

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

**CONF 002

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 003

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

**CONF 004

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 4

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SERVICE BULLETIN

SUMMARY

**CONF 005

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 006

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF 007

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

APPENDICES

**CONF ALL

None

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 5

7

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@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

**CONF 001, 003, 005

FR1

FR20

FR24

FR16

FR9

FR15

107VU

A

A

N_SB_281188_5_SAAA_01_01

69QA

Figure A-FSAAA - Sheet 01

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 6

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@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

**CONF 002, 004, 006 thru 007

FR1

FR20

FR24

FR16

FR9

FR15

107VU

A

A

N_SB_281188_5_SAAB_01_01

69QA

70QA

Figure A-FSAAB - Sheet 01

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 7

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 8

7

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

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 28

TITLE: FUEL- MAIN FUEL PUMP SYSTEM - INTRODUCE GROUND FAULT

INTERRUPTERS (GFI) TO CENTER TANK FUEL PUMPS

MODIFICATION No.: 150736J3138

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

This modification is embodied before delivery on A318 aircraft MSN 5294 and subsequent, on

A319 aircraft MSN 5040 and subsequent and on A320 aircraft MSN 4991 and subsequent.

(1) Models

318-111 318-112 318-121 319-111 319-112 319-113 319-114 319-115

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 0039 0042-0059 0061 0063-0078 0080-0090 0093-0097 0099 0102-0104

0109-0127 0135-0155 0157-0162 0164-0176 0178-0179 0181-0183 0185-0187

0189-0192 0194-0195 0197-0224 0227 0229-0237 0239-0270 0272-0279 0281-0287

0289-0303 0306-0312 0314 0316-0337 0339-0343 0345-0362 0365-0373 0375-0384

0386-0390 0392-0396 0398-0411 0413-0432 0435-0436 0438-0457 0459-0466

0469-0472 0475-0476 0478-0480 0482-0483 0485-0487 0489-0492 0496-0497

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

0587-0590 0592 0594 0596 0598 0600-0601 0603 0605 0607-0613 0615-0619

0621-0627 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 0709-0714

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 1

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SERVICE BULLETIN

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

0772-0774 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 1095-1132 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 1463-1464 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 1659-1665

1667-1669 1671-1674 1676-1680 1682-1689 1692-1694 1696-1700 1702-1703

1705-1706 1708-1710 1712 1714-1715 1717-1719 1721-1723 1725 1727-1733

1735-1747 1749-1762 1764-1771 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 1933-1940 1942-1945

1947-1949 1951-1952 1954-1955 1957-1959 1961-1965 1968-1969 1971 1973

1975-1976 1979-1983 1986-1987 1989-1991 1993 1996-2004 2006-2020 2022-2024

2026-2040 2042-2044 2046-2054 2056-2059 2061-2063 2065-2066 2068-2075

2077-2079 2081-2104 2106 2108-2109 2112-2114 2116 2118-2189 2191-2207

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

2256-2260 2262-2266 2268-2269 2271-2289 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 3000-3004 3006-3012 3014

3016-3021 3023-3033 3035-3050 3052-3066 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 3213-3216

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 3316-3321 3323-3325 3327-3328 3330-3333

3335-3338 3341-3349 3351-3354 3356-3359 3361-3366 3368 3370-3371 3373-3381

3383-3386 3388-3396 3398 3400 3402-3404 3406-3418 3420-3428 3430-3433

3435-3440 3442-3457 3460-3461 3463-3470 3472-3492 3494-3497 3499-3503

3505-3506 3508-3511 3513-3521 3524 3526 3528-3538 3540-3545 3547-3551

3553-3556 3558-3565 3567-3572 3574 3576-3582 3585-3586 3588-3591 3594-3599

3601-3611 3613-3618 3620-3622 3624 3626-3628 3630-3632 3634-3635 3638

3640-3644 3646-3652 3654 3656-3664 3666-3668 3670-3672 3674-3677 3679-3680

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 2

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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 4319-4333

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 4977-4990 4992 4995 4998 5005 5018 5023

(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

01Z 1589

03X 2421

08U 4151

15T 0764 1494 2910 3164

16T 4024 4679

17W 3046

22V 4353

27V 3826

31V 0164 0332 0368

31X 2192 4319

35U 0088

36V 0136

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

47Y 0394

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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OPERATOR MSN

52T 1599

53U 3316 3748 3812 3895 3905 3950 4190 4193

53Z 1468

56W 0247 0257 0327 0336

59U 2706 3073

59Z 1556

60X 4650 4878

61T 0407

62X 3402

69X 0219 0588

73W 0087

74T 2165 4228 4768

75T 4732

78T 1306 1725

78X 0739

79W 3751

80X 2748

85T 0234

86W 0384

86Z 0169 1429 1706 1750 1918 1969 1993

87Z 2210 2998

89T 3356

91X 2837

93V 3932

94W 1998

95V 3379

95W 2949

97U 4842

98W 0039 0042 0103 0120

99W 3038

AAF 0244 0639 1846 2870 3852 4268 4589 4675

AAN 0430 0527

AAR 2397 2459 2808 2840 2943 3244 3437 3483 3496 3641 3873

AAW 3224 3236 3615 3657 4004 4203 4330 4489 4521

ABQ 3364 3385 3388 3403 3974

ABY 2349 2712 2930 2964 3044 3218 3444 3476 3626 3802 3840 3925

4061 4243 4310 4468 4524 4539 4568 4806 4848 4890 4958

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 1853 1864 1874 1940 2018 2145

ACI 2152

ADH 3138 3161 3328 3343 3502 3515 3532

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 4

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@A318/A319/A320/A321

SERVICE BULLETIN

OPERATOR MSN

ADR 0043 0191 0444 4282 4301

AEE 1727 1880 2468 3033 3066 3074 3162 3365 3392 3423 3439 3478

3526 3709 3714 3745 3753 3773 3785 3829 3850 3990 4065 4094

4165

AFL 2052 2069 2072 2091 2093 2106 2116 2133 2144 2151 2163 2179

2222 2233 2243 2875 2920 2947 3052 3063 3157 3281 3298 3336

3373 3410 3511 3545 3574 3627 3631 3640 3644 3699 3711 3778

3786 3789 3794 3823 3835 3838 3923 3942 3954 3998 4133 4160

4453 4498 4579 4625 4649 4656 4684 4692 4712 4835

AFR 0044 0061 0063 0102 0115 0144 0145 0155 0186 0187 0214 0227

0236 0237 0239 0270 0278 0285 0286 0287 0337 0352 0377 0491

0598 0600 0608 0618 0625 0637 0938 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 1873 1879 1885 1894 1900 1924 1938 1949 2035 2059 2071

2081 2100 2109 2140 2213 2228 2317 2344 2350 2456 2582 2601

2686 2705 2716 2721 2750 2918 2938 2951 2961 2967 2972 3008

3009 3065 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

AGC 0190 0279 0395

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

AIJ 0707 1132 1162 1179 1244 1259 1308 1322 1747 1780 2048 2189

2227 2539 3021 3123 3149 3160 3286 3304 3312 3374 3508 3514

3667 3690 4235 4304 4411 4730 4733 4924 4933

AJM 0624 0626

ALK 2345 2564 2584 2908 4694 4869 4915

AMC 2113 2122 2142 2186 2291 2332 2382 2665 2768 3056 3068

AMU 0805 0928 1758 1790 1893 1912 1962

ANA 0139 0151 0167 0170 0212 0245 0300 0328 0365 0383 0413 0482

0501 0507 0531 0534 0549 0554 0658 0669 0685 2061 3099 3147

3148 3189

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

2663 4553 4584 4884 4926

APJ 4887 4936

ART 0142 0310 0311 0333 0359 0426 0724

AUA 0768 0776 0797 1137 1150 1189 1385 1387 1478 2131 2174 2262

2416 2494 2547 2652

AUH 2403

AVA 1612 1618 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 4567 4599 4763 4789 4821 4862 4939

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 5

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SERVICE BULLETIN

OPERATOR MSN

AXM 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 3261 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 4557 4571 4582 4793 4797 4807 4882 4889 4917 4964

4969 4979 4980 4989

AZA 0951 0999 1138 1168 1217 1448 1457 1473 1480 1489 1722 1740

1745 1770 1779 2033 2057 2074 2083 2086 2101 2127 2869 2932

2995 3076 3079 3080 3115 3178 3213 3295 3362 3412 3464 3482

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

B2V 0185

BAB 2700 2763 3861 4055 4600

BAL 2335 3492

BAW 0109 1082 1115 1118 1142 1193 1197 1222 1225 1232 1236 1239

1258 1261 1279 1295 1329 1338 1380 1384 1423 1440 1445 1466

1510 1513 1529 1537 1558 1574 1590 1594 1604 1606 1661 1665

1687 1689 1696 1708 1754 1760 1782 1814 1829 1871 1883 1899

1907 1910 1958 2038 2040 3301 3314 3351 3468 3499 3550 3607

3649 3697 3703 3721 3726 3912 4007 4039 4185 4238 4265 4306

4464 4551 4725 4791 4975

BEC 3199

BEL 0644 1086 1102 1160 1336 1388 1441 1493 2196 2230 3255 3790

4275

BER 1504 1553 1797 1838 1931 2009 2619 3093 3121 3242 3289 3415

3447 3516 3661 3689 3700 3704 3728 3865 3872 3945 3995 4013

4101 4128 4161 4269 4291 4329 4433 4463 4478 4510 4565 4606

4674 4743 4988

BGF 3188

BGH 0221 0294 0349 1087 3139

BHP 2968 3055 3202 3245 3422 3604 4033 4187 4294 4631

BJN 3617 4956

BKP 2254 2310 2509 2648 2660 3421 3424 3454 3694 3759 3911

BMA 1014 1177 1418 1424 1922 1987 2098 2188 2194 2389 2429 2441

2466 2694 2697 2720 2981 3049

BON 3142

BRS 2263

BTV 0168 0441 0449 0460 0461 0710 1676

C9G 0246 0772 2277

CBJ 4388 4428

CCA 0876 0921 1296 1679 1753 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

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 6

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SERVICE BULLETIN

OPERATOR MSN

CCM 1068 1145 3882 3952

CEB 2419 2439 2556 2586 2625 2638 2786 2790 2821 2831 2852 2876

2994 3048 3272 3433 3472 3487 3646 3762 3767 4447 4508 4537

4574 4852 4861 4870 4927

CEF 2801 3085

CES 0665 0754 0828 0838 0854 0883 0897 0909 0914 0925 0939 0967

0984 0986 1005 1028 1030 1041 1070 1072 1093 1108 1285 1303

1312 1316 1330 1345 1357 1361 1377 1386 1532 1541 1542 1551

1601 1603 1639 1778 1786 1906 1911 1964 1981 2022 2034 2036

2049 2056 2068 2155 2171 2182 2199 2212 2219 2221 2235 2239

2244 2274 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

CHB 4482

CHH 2557 2561 2581 2611 2617 2644 2733 2746 2849 2891 2985 3285

3520 3548 3561 3578 3580 3638 3768 3842 3849 3851 3914 3958

3982 4042 4262 4410 4412 4440 4452 4471 4483 4505 4513 4522

4529 4540 4569 4580 4602 4644 4677 4686 4687 4739 4825 4995

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

CQH 0978 1286 1372 1686 1769 1852 1920 2939 3014 3023 3747 3819

4072 4093 4168 4244 4331 4366 4373 4375 4499 4586 4738 4750

4760 4809 4816 4909 4978 4983

CQN 0696 0698 0704 0705 3836 3876 3901 3941

CRK 4970

CSA 1439 1450 2719 2758 2789 3031 3043 3060 3094 3097 3406 3436

3452 3660 3892 4258 4713

CSC 0540 0551 0556 0573 0582 0874 0902 0912 0919 1007 1013 1500

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

CSN 0709 0712 0718 0720 0722 0849 0859 0881 0895 0900 0950 0966

1035 1039 1057 1971 1986 2004 2008 2200 2203 2232 2273 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 3903 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

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

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 7

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SERVICE BULLETIN

OPERATOR MSN

CTN 0258 0767 0833 1009 1029 1237 1252

CUA 5023

CYP 0256 1729 1768 2108 2275 2334 2343 2359 2383 2718 4197

D2F 0211 0243 0251 0326 0411 0478 0946 1963 2747 2753

DAL 0118 0121 0125 0152 0153 0160 0171 0192 0197 0206 0208 0213

0262 0263 0272 0273 0281 0282 0297 0298 0306 0307 0318 0319

0329 0339 0340 0355 0358 0360 0367 0372 0380 0381 0387 0388

0399 0408 0410 0417 0418 0766 0778 0786 0801 0807 0818 0830

0832 0846 0903 0907 0911 0923 0962 0964 0981 0988 0996 1011

1037 1058 1062 1191 1230 1249 1324 1325 1346 1392 1414 1434

1453 1456 1483 1498 1501 1520 1535 1543 1549 1567 1570 1582

1633 1641 1646 1659 1662 1683 1685 1693 1709 1714 1738 1746

1752 1766 1774 1789 1796 1800 1810 1812 1815 1820 1824 1828

1833 1839 1875 1897 1923 1959 1976 1982 1990 2002 2013 2026

2039 2047 2082 2087 2092 2095

DCS 1053 3243 3513 3632

DKH 2879 2913 2975 3027 3234 3268 3368 3485 3596 3605 3967 3984

4064 4102 4154 4276 4401 4429 4573 4587 4652 4833 4840 4981

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

0116 0117 0135 0137 0147 0161 0162 0172 0200 0201 0202 0209

0216 0217 0218 0267 0268 0269 0346 0382 0401 0609 0610 0616

0623 0627 0636 0641 0646 0651 0654 0679 0689 0694 0700 0717

0723 0729 0738 0744 0794 0853 0860 0875 1016 1172 1337 1365

1367 4097 4120 4141 4153 4182 4191 4261 4289 4324 4332 4363

4398 4449 4455 4511 4796 4841

DNV 1630 1805

DRK 2306 2346

EAA 0325 0386 0445

EDW 0942 0947 1026

EIN 1242 1394 1443 1467 2191 2206 2217 2250 2256 2272 2294 2364

2374 2399 2409 2411 2432 2486 2542 2583 2635 2810 3129 3136

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

EZD 0667 0743 0872 1074 2137 2141 2147 3621 4533

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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SERVICE BULLETIN

OPERATOR MSN

EZY 2037 2043 2050 2053 2062 2119 2120 2129 2170 2176 2181 2184

2245 2251 2265 2271 2289 2300 2319 2353 2360 2370 2378 2380

2385 2387 2398 2402 2412 2420 2427 2436 2442 2446 2450 2460

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

2548 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

F2I 0283 0615

FFT 1515 1579 1583 1615 1660 1684 1759 1781 1803 1806 1841 1939

1943 1980 1991 1997 2010 2012 2017 2019 2030 2051 2103 2198

2209 2218 2236 2240 2241 2253 2258 2260 2276 2287 2318 2325

2392 2400 2406 2448 2465 2483 2497 2518 2751 2806 2836 2857

3389 3431 4127 4204 4253 4254 4272 4307 4562 4641 4668 4688

4704 4727 4745

FHE 0888 0936 1171 1210

FHY 0580 2524 4207 4658

FIN 1073 1107 1184 1309 1352 1364 1405 1470 1544 1588 1678 1712

1735 1791 1808 1913 1916 1989 2065 2124 2146 2154 2266

FPY 0112 0342 0438

FRN 0409 0466 0497

G2X 0189

G4I 1157 1795 2507

G8E 0222 0348 1464

GAF 3897 4060

GAP 2162 2183 4415 4475 4504 4512 4777 4907 4984

GFA 1884 1901 3706 4030 4059 4083 4146 4158 4188 4218 4255 4502

4541 4780 4827 4860 4865

GIA 0839 0892 1635 2598 2692

GIR 0630 1973

GLG 1866 1872 1882 1925 2078 2126 4379 4487 4547

GMI 3019 3407 4663 4691

GOW 3256 3306 3597 3616 3798 3827 3900 3915 3933 4399 4438

GSW 0376

GWI 1077 1084 1089 1136 1147 1155 1170 1209 1277 2607 2628 2632

2813 2833 2976 3011 3128 3172 3193 3352 3358 3375 3500 3534

3839 3841 4166 4227 4256 4285 4998

GWY 1564 1860 1867

HAY 2745 3533 3560

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 9

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SERVICE BULLETIN

OPERATOR MSN

HCC 2180 4699

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

HRM 0293

HVN 0590 0594 0601 0605 0607 0611 0617 0619 0648 0650

I2L 0415 0443 0543 0661 1349 1497 1749

I2T 1631 1682

IAC 0045 0046 0047 0048 0049 0050 0051 0056 0057 0058 0074 0075

0080 0089 0090 0095 0096 0097 0308 0314 0396 0398 0416 0423

0431 0432 0451 0469 0486 0490 0492 0499 1668 1718 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

IBE 0223 0274 1047 1059 1067 1099 1119 1154 1180 1208 1229 1247

1255 1262 1288 1292 1318 1347 1362 1516 1530 1540 1655 1674

1694 1736 1793 1809 2225 2242 2248 2264 2311 2347 2365 2391

2776 2807 2843 2897 3054 3078 3102 3179 3209 3320 3380 3443

3651 3744

IBS 0173 0176 0207 0224 0266 0323 1101

IGO 2844 2863 2883 2911 2958 2990 3086 3159 3192 3227 3335 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 4813 4818 4868 4888 4947 4954

4965

IRA 0303 0312 0345 0530 0575 0857 2054

ISR 4354 4413

ISS 0737 0749 1048 1125 1198 1283 1305 1715 1723 1823 1896 1937

1983 2001 2102

IWD 2011 3758 3868 3889 4735

IYE 4653 4690

IZM 1730 2118 2404 2414 2452

JAG 4503

JAV 0029

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

JET 0204 0215 0371 0421 0542 0647 0660 0816 0877 2698 2723 2797

JSA 2156 2164 2316 2356 2395 2401 2423 2453 2457 2604 4443 4515

4772 4786 4872 4914

JST 2169 2185 2197 2292 2299 2322 2329 2338 2455 2475 2515 2526

2537 2573 2587 2600 2608 2642 2651 2703 2717 2766 2787 3474

3495 3547 3668 3743 3783 3917 4177 4178 4229 4245 4257 4303

4343 4356 4434 4460 4466 4495 4497 4527 4899 4922

JZR 2569 2792 2822 3919 3939 4162

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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SERVICE BULLETIN

OPERATOR MSN

KAC 0181 0182 0195 2046 3957

KFR 2366 2376 2413 2443 2496 2502 2522 2531 2576 2621 2634 2645

2650 2664 2670 2676 2731 2817 2856 2874 2922 3012 3089 3105

3270 4961

KGL 2029 2077

KHO 0354 0361 0362 0405

KIL 2214 2224 2249

KKK 1124

KMF 0480

KNE 1886 2123 3238 3361 3396 3425 3475 3530 3787 3817 3894

KZR 2016 2128 2828 2987 3141 3484 3519 3614

LAA 4405 4450 4490 4526

LAN 1304 1332 1351 1355 1491 1512 1526 1548 1568 1626 1854 1858

1877 1903 2089 2096 2295 2304 2321 2572 2585 2845 2858 2864

2872 2886 2887 2892 2894 3264 3280 3319 3330 3371 3390 3438

3469 3509 3535 3556 3585 3602 3606 3635 3642 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

LAO 4596 4639

LBT 0301 0400 0793 0937 1121 1175 1597 1744 3480 4623

LBY 0558 0561 1098

LFO 0659

LFX 3589 3818

LJB 3985

LLM 1054

LLP 1411

LMJ 1868

LMU 0932 0943

LZB 2540 2596 3028 3309 3564 3780

MAC 2166 3809 3833

MAU 1592 1936

MDL 4918 4973

MEA 3736 3804 3837 4296 4339 4632

MHS 1300 1353

MJN 3723 4117 4795

MLD 0249 0622 0741

MLM 2592 3363 4199 4470 4622

MLR 0977

MMA 0113 0114 0295 0316

MON 0379 0389 0392 1081 1370

MSC 2937 2966 3282 3323

MSR 0165 0166 0178 0194 0198 0322 0351 0366 2070 2073 2079 2088

2094

MXA 0252 0259 0260 0261 0275 0276 0291 0292 0296 0320 0321 0347

0353 0357 0369 0373

NIA 3183 3219

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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SERVICE BULLETIN

OPERATOR MSN

NKS 2433 2470 2473 2485 2490 2560 2567 2603 2622 2673 2679 2704

2711 2893 2898 2929 2942 2963 2978 2983 3007 3017 3026 3165

3393 3395 4206 4264 4321 4431 4548 4592 4595 4902 4951

NLV 2157

NLY 2529 2668 2749 2867 2902 4231 4316 4368 4581 4594

NMA 1697 1732

NMB 3346 3586

NVD 0299 0375 0419

O2X 1183 1383

OAI 1454

OHY 0455 0471 0496 0640 0676 0916 1482 1509 2571 2688

ONE 3001 3030 3062 3214 3216 4222 4287 4336 4891 4913 4941 4942

ORF 2566 4992

OZW 0429

PAL 0706 0745 2878 2925 2954 3087 3107 3108 3187 3205 3273 3310

3455 3553 3579 3652 3731

PIC 0990 4459

PJS 4211

PTR 0459 0537

PVJ 3542

QAF 0927 1335 3994 4114 4170

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

3071 4110 4130 4183 4436 4479 4496 4615 4700 4754 4784 4802

4810 4858 4930 4968

R1T 1908

RBA 2023 2032 2135 2139 2195

RBG 2764 3152 3246

RFJ 0814

RJA 2649 2953 3428 3685 3803 3832 4670 4817 4853

RKM 2158 3907

RNV 0229 0913 3834

ROT 2931 2955 3220 3225

RYW 0569

RZO 0795 2390 2425 3891

SAA 2268 2281 2308 2326 2355 2375 2379 2418 2438 2469 2501 4990

SAS 2850 2888 3231 3292

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

SBN 0428

SDM 0427 0525 0649 1130 1488 1560 1578 1654 1657 1743 1761 1767

1851 1863 1876 1890

SFJ 2620 2658 2695 3025 4555 4720

SFW 0671 0994

SGG 0799 0879 1390

SHJ 0910

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 12

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SERVICE BULLETIN

OPERATOR MSN

SHY 0138 0148 1194

SKU 0179 0406 0447 1400 1523 2283

SLK 0899 0969 1228 1422 1561 1698 2058 2252 2517 2568 2775 3104

3570 3821 4118 4215 4259 4457 4701

SND 1999

SNX 0289

SOL 0302

STU 0420 0436 0446

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

SVR 0140 0157 0203 0220 0735 1063 1152 1484 1751 1777 2175 2187

2278 2327

SVW 2921 3100 3133 3856

SWM 0476

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

0635 0643 0673 0681 0701 0703 0713 0727 0734 0782 1018 1762

1951 2024 2134 4618 4673

SYA 3853

SYR 0886 0918 1032 1076 1085 1117

TAE 0657 0934 2084 2659

TAI 1066 1113 1334 1598 1624 1625 1934 1952 2282 2301 2339 2434

2444 2791 2917 3042 3057 3103 3113 3248 3276 3378 3418 3510

3538 3577 3581 4906 4944

TAK 3171 3331

TAM 0250 0334 0335 0440 0758 0976 1010 1092 1096 1103 1139 1143

1158 1215 1246 1251 1339 1368 1376 1459 1486 1518 1575 1580

1591 1593 1595 1608 1613 1628 1652 1663 1672 1692 1703 1717

1757 1771 1775 1801 1802 1804 1818 1825 1826 1827 1831 1832

1835 1837 1855 1857 1888 1891 2014 2044 2372 2393 2417 2467

2513 2602 2661 2734 2737 2783 2784 2838 2859 2896 2904 2924

3002 3032 3035 3047 3058 3111 3156 3180 3211 3240 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

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 1756 1765 1799 1816 2178 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

TBA 4766 4801 4846

TBJ 1485

TCW 0425 0453 0653 1787 1929 1975 2362

TCX 0424 0716 1942 1961 1965 2003 2114

TGW 2331 2340 2724 2728 3757 3801 4181 4210 4421 4445 4469 4491

4493 4532 4561 4608 4645 4804 4812 4874 4879 4931

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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@A318/A319/A320/A321

SERVICE BULLETIN

OPERATOR MSN

THY 1002 1856 1909 1996 2609 2626 2631 2655 2738 2739 2928 2934

2941 2984 3010 3185 3208 3239 3257 3259 3303 3308 3341 3558

3567 3603 3654 3718 3719 3896 3931 3949 4629 4665 4695 4755

4774 4790

TJS 4169

TNA 0791 0822 2914

TOM 1320 1571 1605 1637

TWJ 2550

UAE 4822

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

UDC 0085 0230 0235 0579 0645 0662 0733 0747 0760

UEA 0949 1263 2654 2696 2762 2774 2820 2835 3024 4347

UKN 3260

UNA 3333 3886 4583

USA 0052 0053 0054 0055 0064 0065 0066 0067 0076 0077 0081 0082

0099 0317 0448 0565 0584 0762 0770 0803 0844 0856 0861 0863

0866 0868 0885 0889 0890 0896 0904 0922 0924 0929 0931 0953

0972 0997 1003 1019 1033 1038 1040 1043 1046 1049 1050 1051

1052 1055 1056 1061 1064 1065 1069 1075 1079 1083 1088 1095

1097 1109 1110 1111 1112 1114 1116 1122 1134 1135 1141 1148

1166 1178 1182 1196 1203 1205 1223 1224 1234 1245 1254 1264

1265 1268 1269 1274 1275 1281 1284 1287 1289 1294 1297 1298

1301 1310 1311 1313 1314 1315 1317 1319 1323 1326 1328 1331

1340 1342 1348 1350 1354 1358 1360 1369 1371 1373 1375 1378

1382 1389 1391 1393 1395 1397 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

VIM 2732 2804 3125 4270 4305

VJC 3739 3791 4049

VKG 1889 1954

VKH 0393 0414

VLE 1226

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 14

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@A318/A319/A320/A321

SERVICE BULLETIN

OPERATOR MSN

VLG 0143 0146 0158 0199 0240 0241 0264 0356 0992 1221 1396 1407

1413 1430 1461 1550 1862 1914 1933 1979 2027 2104 2143 2168

2207 2223 2388 2407 2479 2589 2678 2761 2785 2794 2798 2889

2962 2988 3083 3095 3109 3145 3151 3174 3203 3237 3293 3321

3376 3400 3529 4661 4681 4742 4849 4855 4937

VLK 0422 0528 0714 0730 1200 1213 1379

VOI 1140 1159 2204 2296 2657 2666 2771 2780 2979 2997 3045 3069

3077 3175 3252 3253 3279 3317 3450 3463 3491 3524 3543 3590

3624 3672 3705 4403 4422 4741 4798 4828 4832 4950

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

WAU 3531 3741

WGT 1212

WHT 0726 1256 2440 2675

WTJ 0548

WZZ 1834 1892 1902 2752 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

XLF 0343

YAP 0533 0566 0973

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 15

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@A318/A319/A320/A321

SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

0029 0039 0042 0043 0044 0045 0046 0047 0048 0049 0050

0051 0052 0053 0054 0055 0056 0057 0058 0059 0061 0063

0064 0065 0066 0067 0068 0069 0070 0071 0072 0073 0074

0075 0076 0077 0078 0080 0081 0082 0083 0084 0085 0086

0087 0088 0089 0090 0093 0094 0095 0096 0097 0099 0102

0103 0104 0109 0110 0111 0112 0113 0114 0115 0116 0117

0118 0119 0120 0121 0122 0123 0124 0125 0126 0127 0135

0136 0137 0138 0139 0140 0141 0142 0143 0144 0145 0146

0147 0148 0149 0150 0151 0152 0153 0154 0155 0157 0159

0160 0161 0162 0164 0165 0166 0167 0168 0169 0170 0171

0172 0174 0175 0178 0179 0181 0182 0183 0186 0187 0189

0190 0192 0194 0195 0197 0198 0199 0200 0201 0202 0203

0204 0205 0206 0208 0209 0210 0211 0212 0213 0214 0215

0216 0217 0218 0219 0220 0221 0222 0227 0229 0230 0231

0232 0233 0234 0235 0236 0237 0239 0240 0241 0242 0243

0244 0245 0246 0247 0248 0249 0250 0251 0252 0253 0254

0255 0256 0257 0258 0259 0260 0261 0262 0263 0264 0265

0267 0268 0269 0270 0272 0273 0275 0276 0277 0278 0279

0281 0282 0283 0284 0285 0286 0287 0289 0290 0291 0292

0293 0294 0295 0296 0297 0298 0299 0300 0301 0302 0303

0306 0307 0308 0309 0310 0311 0312 0314 0316 0317 0318

0319 0320 0321 0322 0324 0325 0326 0327 0328 0329 0330

0331 0332 0333 0334 0335 0336 0337 0339 0340 0341 0342

0343 0345 0346 0347 0348 0349 0350 0351 0352 0353 0354

0355 0357 0358 0359 0360 0361 0362 0365 0366 0367 0368

0369 0370 0371 0372 0373 0375 0376 0377 0378 0379 0380

0381 0382 0383 0384 0386 0387 0388 0389 0390 0392 0393

0394 0396 0398 0399 0400 0401 0402 0403 0404 0405 0406

0407 0408 0409 0410 0411 0413 0414 0415 0416 0417 0418

0419 0420 0421 0422 0423 0424 0425 0426 0427 0428 0429

0430 0431 0432 0435 0436 0438 0439 0440 0441 0442 0443

0444 0445 0446 0447 0448 0449 0450 0451 0452 0453 0454

0455 0456 0457 0459 0460 0461 0462 0463 0464 0465 0466

0469 0470 0471 0472 0475 0476 0478 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 0590 0592

0594 0596 0598 0600 0601 0603 0605 0607 0608 0609 0610

0611 0612 0613 0615 0616 0617 0618 0619 0621 0622 0623

0624 0625 0626 0627 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

0710 0711 0712 0713 0714 0716 0717 0718 0719 0720 0721

002

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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@A318/A319/A320/A321

SERVICE BULLETIN

MSN CONFIGURATION

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 0751 0752 0754 0756 0757 0758 0759 0760

0762 0763 0764 0766 0767 0768 0769 0770 0772 0773 0774

0776 0778 0779 0780 0782 0783 0784 0785 0786 0788 0791

0793 0794 0795 0797 0798 0799 0800 0801 0803 0804 0805

0807 0809 0812 0813 0814 0816 0817 0818 0820 0822 0824

0825 0826 0828 0829 0830 0831 0832 0833 0834 0836 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 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 0907 0909 0910 0911 0912 0913 0914 0916 0918

0919 0921 0922 0923 0924 0925 0928 0929 0930 0931 0932

0934 0936 0937 0938 0939 0942 0943 0944 0946 0947 0948

0949 0950 0951 0952 0953 0955 0957 0958 0962 0964 0965

0966 0967 0969 0971 0972 0973 0975 0976 0977 0978 0980

0981 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 1035 1036 1037 1038 1039 1040 1041

1043 1046 1048 1049 1050 1051 1052 1053 1054 1055 1056

1057 1058 1061 1062 1063 1064 1065 1066 1068 1069 1070

1071 1072 1073 1074 1075 1076 1077 1078 1079 1081 1082

1083 1084 1085 1086 1088 1089 1090 1091 1092 1093 1095

1096 1097 1098 1102 1103 1104 1105 1107 1108 1109 1110

1111 1112 1113 1114 1115 1116 1117 1118 1121 1122 1123

1124 1125 1126 1128 1129 1130 1131 1132 1134 1135 1136

1138 1139 1140 1141 1142 1143 1145 1146 1147 1148 1149

1151 1152 1155 1156 1157 1158 1159 1160 1162 1163 1164

1166 1167 1168 1169 1170 1171 1172 1173 1175 1176 1177

1178 1179 1182 1183 1184 1187 1189 1190 1191 1192 1193

1194 1196 1197 1198 1200 1201 1203 1205 1209 1210 1211

1212 1213 1215 1216 1217 1221 1222 1223 1224 1225 1226

1228 1230 1232 1234 1235 1236 1237 1239 1240 1242 1243

1244 1245 1246 1248 1249 1251 1252 1253 1254 1256 1257

1258 1259 1261 1263 1264 1265 1266 1267 1268 1269 1270

1271 1272 1274 1275 1277 1279 1280 1281 1282 1283 1284

1285 1286 1287 1289 1290 1291 1294 1295 1296 1297 1298

1300 1301 1302 1303 1304 1305 1306 1308 1309 1310 1311

1312 1313 1314 1315 1316 1317 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

1348 1349 1350 1351 1352 1353 1354 1355 1357 1358 1359

1360 1361 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

002

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SERVICE BULLETIN

MSN CONFIGURATION

1441 1443 1444 1445 1446 1448 1449 1450 1452 1453 1456

1457 1459 1460 1461 1463 1464 1466 1467 1468 1469 1470

1471 1473 1474 1475 1477 1478 1480 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 1518 1520 1522 1523 1524 1526 1527 1528 1529

1532 1533 1534 1535 1537 1538 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 1656 1657 1659 1660 1661 1662

1663 1664 1665 1668 1669 1671 1672 1673 1676 1677 1678

1679 1680 1682 1683 1684 1685 1686 1687 1688 1689 1692

1693 1696 1697 1698 1699 1700 1702 1703 1705 1706 1708

1709 1710 1712 1714 1715 1717 1718 1719 1721 1722 1723

1725 1727 1728 1729 1730 1731 1732 1733 1735 1737 1738

1739 1740 1741 1742 1743 1744 1745 1746 1747 1749 1750

1751 1752 1753 1754 1755 1757 1758 1759 1760 1761 1762

1764 1766 1767 1768 1769 1770 1771 1773 1774 1775 1777

1778 1779 1780 1781 1782 1784 1785 1786 1787 1789 1790

1791 1792 1795 1796 1797 1800 1801 1802 1803 1804 1805

1806 1808 1809 1810 1812 1814 1815 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 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 1939

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 1991 1993 1996 1997 1998 1999 2000 2001 2002

2003 2004 2006 2007 2008 2009 2010 2011 2012 2013 2014

2015 2016 2017 2018 2019 2020 2022 2023 2024 2026 2027

2028 2029 2030 2031 2032 2033 2034 2035 2036 2037 2038

2039 2040 2042 2043 2044 2047 2048 2049 2050 2051 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 2106 2108 2109 2112 2113 2114 2116 2118 2119 2120

2121 2122 2123 2124 2125 2126 2127 2128 2129 2130 2131

2132 2133 2134 2135 2136 2137 2138 2139 2140 2141 2142

002

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@A318/A319/A320/A321

SERVICE BULLETIN

MSN CONFIGURATION

2144 2145 2146 2147 2148 2149 2150 2151 2152 2153 2154

2155 2156 2157 2158 2159 2160 2161 2162 2163 2164 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 2214

2215 2217 2218 2219 2221 2222 2223 2224 2227 2229 2230

2231 2232 2233 2235 2236 2237 2238 2239 2240 2241 2243

2244 2245 2249 2250 2251 2252 2253 2254 2256 2257 2258

2260 2262 2263 2265 2266 2268 2269 2271 2272 2273 2274

2275 2276 2277 2278 2281 2282 2283 2285 2287 2288 2289

2291 2292 2293 2294 2295 2296 2297 2298 2299 2300 2301

2302 2304 2306 2308 2310 2312 2313 2316 2317 2318 2319

2321 2322 2325 2326 2327 2328 2329 2331 2332 2333 2334

2335 2338 2339 2340 2341 2343 2344 2345 2346 2348 2349

2350 2353 2354 2355 2356 2358 2359 2360 2361 2362 2364

2366 2367 2369 2370 2371 2372 2373 2374 2375 2376 2377

2378 2379 2380 2382 2383 2385 2387 2388 2389 2390 2392

2393 2394 2395 2396 2397 2398 2399 2400 2401 2402 2404

2405 2406 2407 2408 2409 2411 2412 2413 2414 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 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 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 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 2777 2778 2779 2780 2781

2782 2783 2784 2785 2786 2787 2788 2789 2790 2791 2792

002

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SERVICE BULLETIN

MSN CONFIGURATION

2794 2795 2796 2797 2798 2800 2801 2802 2803 2804 2805

2806 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 2844 2845 2846 2847 2848 2849 2850 2851 2852 2853

2854 2855 2856 2857 2858 2859 2860 2861 2863 2864 2865

2866 2867 2869 2871 2872 2873 2874 2875 2876 2877 2878

2879 2880 2881 2883 2884 2885 2886 2887 2888 2890 2891

2892 2893 2894 2896 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 3001 3002 3003 3004 3006

3007 3008 3009 3010 3011 3012 3014 3016 3017 3018 3019

3020 3021 3023 3024 3025 3026 3027 3028 3029 3030 3031

3032 3033 3035 3036 3037 3038 3039 3040 3041 3042 3043

3044 3045 3046 3047 3048 3049 3050 3052 3053 3055 3056

3057 3058 3059 3060 3061 3062 3063 3064 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

3097 3099 3100 3101 3103 3104 3105 3107 3108 3109 3111

002

0158 0173 0176 0185 0191 0207 0223 0224 0266 0274 0323

0356 0395 0629 0750 0755 0790 0821 0837 0906 0917 0933

0945 0960 0979 0982 1034 1047 1059 1067 1087 1099 1100

1101 1106 1119 1120 1127 1154 1165 1180 1181 1206 1208

1229 1231 1247 1255 1262 1288 1292 1318 1347 1362 1454

1516 1530 1540 1655 1667 1674 1694 1736 1756 1765 1793

1799 1816 2104 2143 2225 2242 2248 2264 2311 2347 2365

2391 2776 2807 2843 2870 2889 2897 3054 3102

001 002

0870 005 006

0927 1137 1150 1479 1868 2046 2165 2213 2228 2246 2259

2279 2280 2284 2286 2307 2314 2336 2352 2368 2384 2386

2403 2415 2456 2566 2716 3065 3096

006

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 20

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SERVICE BULLETIN

MSN CONFIGURATION

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 3165 3166 3167 3168 3170 3171 3172 3173 3174

3175 3176 3177 3178 3180 3181 3182 3183 3184 3185 3186

3187 3188 3189 3190 3192 3193 3194 3195 3196 3197 3200

3201 3202 3203 3204 3205 3206 3208 3210 3211 3213 3214

3215 3216 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 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 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 3371 3373 3374 3375 3376 3378 3381 3383 3384 3385

3386 3388 3389 3390 3391 3392 3393 3394 3395 3396 3398

3400 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 3438

3439 3440 3442 3444 3445 3446 3447 3448 3449 3450 3451

3452 3453 3454 3455 3456 3457 3460 3461 3463 3464 3465

3466 3467 3468 3469 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 3509 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 3585 3586 3588 3589 3590 3591 3594 3595 3596 3597

3598 3599 3601 3602 3603 3604 3605 3606 3607 3608 3609

3610 3611 3613 3614 3616 3617 3618 3620 3621 3622 3624

3626 3627 3628 3630 3631 3632 3634 3635 3638 3640 3641

3642 3643 3644 3646 3647 3648 3649 3650 3652 3654 3656

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 3724

3726 3727 3728 3729 3731 3732 3733 3734 3735 3739 3741

3742 3743 3745 3746 3747 3748 3750 3751 3753 3754 3755

3756 3757 3758 3759 3760 3762 3763 3765 3767 3768 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 3805 3807 3808

004

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REVISION No.: 00 - Mar 23/12 Page: 21

7

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

MSN CONFIGURATION

3809 3810 3811 3812 3813 3815 3817 3818 3819 3821 3822

3823 3824 3825 3826 3827 3828 3829 3831 3832 3833 3834

3835 3836 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 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 4006 4007 4008

4010 4011 4012 4013 4014 4015 4017 4018 4019 4020 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 4083

4084 4086 4087 4088 4089 4092 4093 4094 4097 4098 4100

4101 4102 4104 4105 4108 4109 4110 4111 4113 4114 4115

4118 4119 4120 4121 4122 4124 4125 4126 4127 4128 4129

4130 4132 4133 4135 4137 4139 4140 4141 4143 4144 4146

4147 4149 4150 4151 4152 4153 4154 4156 4157 4158 4159

4160 4161 4162 4163 4164 4165 4166 4167 4168 4169 4171

4172 4174 4175 4176 4177 4178 4179 4181 4182 4183 4185

4186 4187 4188 4190 4191 4192 4193 4195 4196 4197 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 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

4330 4331 4332 4333 4335 4336 4340 4342 4343 4344 4345

4346 4347 4348 4349 4350 4351 4353 4354 4355 4356 4357

4359 4361 4362 4363 4365 4366 4367 4368 4370 4371 4372

4373 4375 4376 4378 4379 4380 4381 4383 4384 4385 4386

4389 4390 4391 4392 4393 4394 4395 4396 4397 4398 4399

4400 4401 4402 4403 4404 4405 4407 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

004

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REVISION No.: 00 - Mar 23/12 Page: 22

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SERVICE BULLETIN

MSN CONFIGURATION

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 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 4781 4782 4784 4785 4786 4787 4789

4790 4791 4793 4794 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 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 4861 4862 4864 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 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 4992 4995

4998 5005 5018

004

3164 3199 3379 3615 3657 3723 3736 3804 3837 4004 4081

4090 4117 4170 4199 4296 4337 4339 4364 4388 4408 4632

4780 4795 4827 4860 4865 4955 5023

007

3169 3179 3209 3255 3320 3377 3380 3443 3651 3744 3769

3883 4021 4095 4106 4145

003 004

3402 004 007

(5) Configuration definition

**CONF 001

Config. 001 is valid for aircraft without an ACT installed on which Evaluation Service

Bulletin No. A320-28-1903 is accomplished and the restoration is not accomplished

(during the evaluation period) and with Mod No. 30248P10368 not embodied.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 23

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SERVICE BULLETIN

NOTE: Aircraft that have installed an ACT by Service Bulletin are to be considered as

Config. 005.

**CONF 002

Config. 002 is valid for aircraft without an ACT installed on which Evaluation Service

Bulletin No. A320-28-1903 is not accomplished or for aircraft on which the restoration of

Evaluation Service Bulletin No. A320-28-1903 is accomplished and with Mod No.

30248P10368 not embodied.

NOTE: Aircraft that have installed an ACT by Service Bulletin are to be considered as

Config. 006.

**CONF 003

Config. 003 is valid for aircraft without an ACT installed on which Evaluation Service

Bulletin No. A320-28-1903 is accomplished and the restoration of Evaluation Service

Bulletin No. A320-28-1903 is not accomplished (during the evaluation period) and with

Mod No. 30248P10368 embodied.

NOTE: These aircraft will not have to do the restoration of Evaluation Service Bulletin

No. A320-28-1903.

**CONF 004

Config. 004 is valid for aircraft without an ACT installed on which Evaluation Service

Bulletin No. A320-28-1903 is not accomplished or for aircraft on which the restoration of

Evaluation Service Bulletin No. A320-28-1903 is accomplished and with Mod No.

30248P10368 embodied.

NOTE: Aircraft that have installed an ACT by Service Bulletin are to be considered as

Config. 007.

**CONF 005

Config. 005 is valid for aircraft with an ACT installed on which Evaluation Service

Bulletin No. A320-28-1903 is accomplished and the restoration is not accomplished

(during the evaluation period) and with Mod No. 30248P10368 not embodied.

**CONF 006

Config. 006 is valid for aircraft with an ACT installed on which Evaluation Service

Bulletin No. A320-28-1903 is not accomplished or for aircraft on which the restoration of

Evaluation Service Bulletin No. A320-28-1903 is accomplished and with Mod No.

30248P10368 not embodied.

**CONF 007

Config. 007 is valid for aircraft with an ACT installed on which Evaluation Service

Bulletin No. A320-28-1903 is not accomplished or for aircraft on which the restoration of

Evaluation Service Bulletin No. A320-28-1903 is accomplished and with Mod No.

30248P10368 embodied.

(6) Material Effectivity

**CONF 001, 003, 005

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLA01 1

Kit 281188A01R00 1

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 24

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SERVICE BULLETIN

**CONF 002, 004, 006 thru 007

MATERIAL QTY PER A/C SEE NOTES

Consumable CMLA01 1

Kit 281188A02R00 1

**CONF ALL

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

The center tank fuel pumps (Pump 1 FIN 37QA / Pump 2 38QA) are supplied by control

relays (FIN 35QA / 36QA). These relays are installed in electrical panel 107VU. To

protect the pump feeder supply cable from the electrical panel 107VU and the pump

windings against ’earth’ faults, additional earth leakage protection is required.

Mod. No. 150690J2866 was issued to evaluate the additional earth leakage protection

available by replacing a control relay with Ground Fault Interrupter (GFI). As a result of

this mod, an evaluation Service Bulletin A320-28-1903 was issued to some operators to

evaluate the application of Mod. No. 150690J2866.

Additional earth leakage protection was evaluated through installation of a GFI 70QA in

electrical panel 107VU instead of control relay FIN 36QA.

(2) Objective/Action

This Service Bulletin introduces Mod. No. 150736J3138. This modification introduces

GFIs and related bases into the electrical supply circuits of the center tank fuel pump 1

(FIN 37QA) and pump 2 (FIN 38QA) on A318, A319 and A320 aircraft.

These GFIs have the same ’footprint’ as the existing relay/micro-contactors and

physically replace them on the electrical panel. The new GFI sockets are fool-proofed to

prevent incorrectly fitment of a normal relay/micro-contactor or inappropriate GFI device.

(3) Advantages

These GFIs will replace the existing 3-phase relay/micro-contactors. The function of the

GFI is to electrically isolate the pump if a ground fault condition occurs downstream of

the GFI. The GFI gives additional earth leakage protection to the downstream circuit.

Accomplishment of this Service Bulletin will not change the characteristics of the aircraft.

(4) Operational/Maintenance Consequences

None

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 25

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SERVICE BULLETIN

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 281188-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the Contactor Box 107VU

**CONF 002

Task 281188-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the Contactor Box 107VU

**CONF 003

Task 281188-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the Contactor Box 107VU

**CONF 004

Task 281188-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the Contactor Box 107VU

**CONF 005

Task 281188-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the Contactor Box 107VU

**CONF 006

Task 281188-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the Contactor Box 107VU

**CONF 007

Task 281188-831-895-001: MODIFICATION

(1) Modify the Equipment and the Wiring in the Contactor Box 107VU

**CONF ALL

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 26

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SERVICE BULLETIN

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at or before 48 months from

the issue of this Service Bulletin.

This Service Bulletin has been classified Recommended. It is expected that an

Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA)

will be issued to change this classification to Mandatory. It is anticipated that the AD will

confirm the (thresholds and/or intervals and/or date) given above but reference should

be made to the AD for confirmation of the mandated accomplishment timescale.

F. APPROVAL

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

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.

**CONF 001

Task 281188-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

Modify the Equipment and the Wiring in the Contactor

Box 107VU

3.00

Tests 1.50

Close-Up 1.50

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

**CONF 002

Task 281188-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

Modify the Equipment and the Wiring in the Contactor

Box 107VU

6.00

Tests 1.50

Close-Up 1.50

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 27

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SERVICE BULLETIN

Task 281188-831-895-001: MODIFICATION

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 003

Task 281188-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

Modify the Equipment and the Wiring in the Contactor

Box 107VU

3.00

Tests 1.50

Close-Up 1.50

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

**CONF 004

Task 281188-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

Modify the Equipment and the Wiring in the Contactor

Box 107VU

6.00

Tests 1.50

Close-Up 1.50

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 005

Task 281188-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

Modify the Equipment and the Wiring in the Contactor

Box 107VU

3.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 7.50

ELAPSED TIME (HOURS) 7.50

**CONF 006

Task 281188-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

Modify the Equipment and the Wiring in the Contactor

Box 107VU

6.00

Tests 1.00

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 28

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SERVICE BULLETIN

Task 281188-831-895-001: MODIFICATION

Close-Up 1.50

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF 007

Task 281188-831-895-001: MODIFICATION

Get Access 2.00

On Aircraft

Modify the Equipment and the Wiring in the Contactor

Box 107VU

6.00

Tests 1.00

Close-Up 1.50

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001, 003, 005

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight -0.090 KG (-0.1984 LB)

Effect on Balance -0.626 KGM (-4.527 LB.FT )

**CONF 002, 004, 006 thru 007

The weight and balance estimates given in this Service Bulletin are based on the

Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of

MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07.

Manufacturers Empty Weight -0.180 KG (-0.3968 LB)

Effect on Balance -1.251 KGM (-9.048 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-41-53 11-00-00 12-34-24

20-21-15 28-25-00 52-40-00

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 29

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SERVICE BULLETIN

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A320-28-1903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 002

Aircraft Maintenance Manual (AMM) 06-41-53 11-00-00 12-34-24

20-21-15 28-25-00 52-40-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A320-28-1903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 003

Aircraft Maintenance Manual (AMM) 06-41-53 11-00-00 12-34-24

20-21-15 28-25-00 52-40-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A320-28-1903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 004

Aircraft Maintenance Manual (AMM) 06-41-53 11-00-00 12-34-24

20-21-15 28-25-00 52-40-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A320-28-1903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 30

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SERVICE BULLETIN

**CONF 005

Aircraft Maintenance Manual (AMM) 06-41-53 11-00-00 12-34-24

20-21-15 28-25-00 52-40-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A320-28-1903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 006

Aircraft Maintenance Manual (AMM) 06-41-53 11-00-00 12-34-24

20-21-15 28-25-00 52-40-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A320-28-1903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF 007

Aircraft Maintenance Manual (AMM) 06-41-53 11-00-00 12-34-24

20-21-15 28-25-00 52-40-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

Elec. Std. Practices Manual (ESPM) 20-33-00 20-46-50 20-52-21

20-55-00

Service Bulletin (SB) A320-28-1903

Standards Manual (SM)

Weight and Balance Manual (WBM) Chapter 1-00-07

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 28-21-00

Aircraft Wiring List (AWL)

Aircraft Wiring Manual (AWM)

Illustrated Parts Catalog (IPC) 28-21-08

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 31

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L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Relay NSA932843AA01 ABS1629-28A0 03 Not

Applicable

(1)

Base NSA932844AA E0673D0S 03 Not

Applicable

(1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. Old PN relay can be replaced by new PN relay if new PN socket is

installed. New PN relay must be replaced by new PN relay.

**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Relay NSA932843AA01 ABS1629-28A0 03 Not

Applicable

(1)

Base NSA932844AA E0673D0S 03 Not

Applicable

(1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. Old PN relay can be replaced by new PN relay if new PN socket is

installed. New PN relay must be replaced by new PN relay.

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Relay NSA932843AA01 ABS1629-28A0 03 Not

Applicable

(1)

Base NSA932844AA E0673D0S 03 Not

Applicable

(1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. Old PN relay can be replaced by new PN relay if new PN socket is

installed. New PN relay must be replaced by new PN relay.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 32

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**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Relay NSA932843AA01 ABS1629-28A0 03 Not

Applicable

(1)

Base NSA932844AA E0673D0S 03 Not

Applicable

(1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. Old PN relay can be replaced by new PN relay if new PN socket is

installed. New PN relay must be replaced by new PN relay.

**CONF 005

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Relay NSA932843AA01 ABS1629-28A0 03 Not

Applicable

(1)

Base NSA932844AA E0673D0S 03 Not

Applicable

(1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. Old PN relay can be replaced by new PN relay if new PN socket is

installed. New PN relay must be replaced by new PN relay.

**CONF 006

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Relay NSA932843AA01 ABS1629-28A0 03 Not

Applicable

(1)

Base NSA932844AA E0673D0S 03 Not

Applicable

(1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. Old PN relay can be replaced by new PN relay if new PN socket is

installed. New PN relay must be replaced by new PN relay.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 33

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**CONF 007

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Relay NSA932843AA01 ABS1629-28A0 03 Not

Applicable

(1)

Base NSA932844AA E0673D0S 03 Not

Applicable

(1)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE (1): Not interchangeable, but one way interchangeable with the following

conditions. Old PN relay can be replaced by new PN relay if new PN socket is

installed. New PN relay must be replaced by new PN relay.

**CONF ALL

M. SPARES

None

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 34

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 281188A01R00

Kit 281188A02R00

Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is:

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 HAMBURG

GERMANY

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 2590

For ordering by E-mail: airbus.kit@airbus.com

(2) Price and Availability

Kit 281188A01R00

Cost 1,680.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require Kits before this time, please include a retrofit planning schedule with

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

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

at the issue date of the Service Bulletin. The latest valid price and lead time for ordering

purposes shall be obtained through the AirbusSpares Portal or through a request for

quotation to airbus.kit@airbus.com.

Kit 281188A02R00

Cost 3,360.00 USD

Availability 90 calendar days from receipt of order

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

order. If you require Kits before this time, please include a retrofit planning schedule with

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

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 35

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

at the issue date of the Service Bulletin. The latest valid price and lead time for ordering

purposes shall be obtained through the AirbusSpares Portal or through a request for

quotation to airbus.kit@airbus.com.

B. INDUSTRY SUPPORT INFORMATION

As a special policy applied to this Service Bulletin, AIRBUS will provide a 15% reduction to

the applicable kits sales prices given in the paragraph Price and Availability for orders placed

before 31 Dec 2017.

C. LIST OF COMPONENTS

Kit 281188A01R00

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

NOTES

1 ABS1629-28A0 1 GFI (1) NSA932843AA01 03

2 E0673D0S 1 BASE (2) NSA932844AA 03

3 NAS1101-04-7 3 SCREW

4 ASNA2397-3L 3 WASHER

5 MS21042-04 3 NUT

D9100095214195 1 PLACARD

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

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

Common Support Data Dictionary (CSDD), Chapter 2.

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

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

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

to part number relationship.

Kit 281188A02R00

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

NOTES

1 ABS1629-28A0 2 GFI (1) NSA932843AA01 03

2 E0673D0S 2 BASE (2) NSA932844AA 03

3 NAS1101-04-7 6 SCREW

4 ASNA2397-3L 6 WASHER

5 MS21042-04 6 NUT

D9100095214295 1 PLACARD

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

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

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 36

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

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

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

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent (varsol/white

Spirit)

11-002 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 37

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This Page Intentionally Left Blank

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 38

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 281188-831-895-001 - MODIFICATION

WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY

KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION

(CDCCL). CDCCL IDENTIFIES AN ITEM THAT CAN BE THE SOURCE OF A

POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN

THE APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A

CDCCL ITEM CAN CAUSE A POSSIBLE FUEL TANK EXPLOSION.

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.

Task Associated Data

**CONF 001

Zone

120 126 210

Modified FIN

35QA 35QAA 69QA 69QAA

Access

Door 822 824

Electrical panel 107VU

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

**CONF 002

Zone

120 126 210

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 39

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Modified FIN

35QA 35QAA 36QA 36QAA 69QA 69QAA 70QA 70QAA

Access

Door 822 824

Electrical panel 107VU

Manpower

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 003

Zone

120 126 210

Modified FIN

35QA 35QAA 69QA 69QAA

Access

Door 822 824

Electrical panel 107VU

Manpower

TOTAL MANHOURS 8.00

ELAPSED TIME (HOURS) 8.00

**CONF 004

Zone

120 126 210

Modified FIN

35QA 35QAA 36QA 36QAA 69QA 69QAA 70QA 70QAA

Access

Door 822 824

Electrical panel 107VU

Manpower

TOTAL MANHOURS 11.00

ELAPSED TIME (HOURS) 11.00

**CONF 005

Zone

120 126 210

Modified FIN

35QA 35QAA 69QA 69QAA

Access

Door 822 824

Electrical panel 107VU

Manpower

TOTAL MANHOURS 7.50

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 40

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ELAPSED TIME (HOURS) 7.50

**CONF 006

Zone

120 126 210

Modified FIN

35QA 35QAA 36QA 36QAA 69QA 69QAA 70QA 70QAA

Access

Door 822 824

Electrical panel 107VU

Manpower

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF 007

Zone

120 126 210

Modified FIN

35QA 35QAA 36QA 36QAA 69QA 69QAA 70QA 70QAA

Access

Door 822 824

Electrical panel 107VU

Manpower

TOTAL MANHOURS 10.50

ELAPSED TIME (HOURS) 10.50

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 281188-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002 As required

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 41

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SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-002

Task 20-21-15-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(b) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) For the installation of the relays (Refer to ESPM 20-46-50).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(f) For the installation of placards (Refer to AMM Task 11-00-00-400-002).

(g) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-001).

(h) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 281188-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 002

(1) Subtask 281188-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 42

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Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-002

Task 20-21-15-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(b) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) For the installation of the relays (Refer to ESPM 20-46-50).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(f) For the installation of placards (Refer to AMM Task 11-00-00-400-002).

(g) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-001).

(h) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 281188-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 43

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**CONF 003

(1) Subtask 281188-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-002

Task 20-21-15-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(b) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) For the installation of the relays (Refer to ESPM 20-46-50).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(f) For the installation of placards (Refer to AMM Task 11-00-00-400-002).

(g) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-001).

(h) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 281188-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 44

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

Service Bulletin.

**CONF 004

(1) Subtask 281188-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-002

Task 20-21-15-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(b) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) For the installation of the relays (Refer to ESPM 20-46-50).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(f) For the installation of placards (Refer to AMM Task 11-00-00-400-002).

(g) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-001).

(h) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 45

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(2) Subtask 281188-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 005

(1) Subtask 281188-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-002

Task 20-21-15-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(b) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) For the installation of the relays (Refer to ESPM 20-46-50).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(f) For the installation of placards (Refer to AMM Task 11-00-00-400-002).

(g) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-001).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 46

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SERVICE BULLETIN

(h) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 281188-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 006

(1) Subtask 281188-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-002

Task 20-21-15-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(b) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) For the installation of the relays (Refer to ESPM 20-46-50).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

(f) For the installation of placards (Refer to AMM Task 11-00-00-400-002).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 47

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(g) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-001).

(h) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 281188-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF 007

(1) Subtask 281188-910-001-001 - Standard Practices

Manpower Resources

Skills NON SPECIFIC

Material necessary to do the job

Consumable CMLA01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Dry Cleaning Solvent

(varsol/white Spirit)

11-002 As required

References

Aircraft Maintenance Manual (AMM) Task 11-00-00-400-002

Task 20-21-15-912-001

Consumable Material List (CML)

Elec. Std. Practices Manual (ESPM) 20-33-00

20-46-50

20-52-21

(a) For the specification of materials (Mat. No.) that you must use in this Service

Bulletin refer to Consumable Materials List (CML).

(b) Clean the surfaces at the location of the placards with:

Dry Cleaning

Solvent

(varsol/white Spirit)

11-002 As required

(c) Tag all the parts you must remove and retain to make the subsequent installation

easier.

(d) For the installation of the relays (Refer to ESPM 20-46-50).

(e) Obey the instructions for the general wiring installation (Refer to ESPM 20-33-00).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 48

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(f) For the installation of placards (Refer to AMM Task 11-00-00-400-002).

(g) To torque tighten the electrical component fasteners (Refer to AMM Task

20-21-15-912-001).

(h) Do a continuity test of the modified wires (Refer to ESPM 20-52-21).

(2) Subtask 281188-839-401-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 281188-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

52-40-00, Page Block 001

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

12-34-24-869-002).

(b) Put the access platform(s) in position.

(c) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 23 P (1)

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 34 K (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 25 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 27 Q (1)

49VU SDAC/1 AND 2/28VDC/ESS

BUS

12WV 05 F (1)

49VU SDAC/1/SPLY 3WV 04 F (1)

49VU SDAC/1/26VAC SYNC/AC

ESS BUS

5WV 02 F (1)

121VU EIS/SDAC/1/BUS1/26VAC

SYNC AC

9WV 04 Q (1)

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU EIS/SDAC/1/BUS2/26VAC

SYNC AC

7WV 03 Q (1)

49VU SDAC/2/26VAC SYNC/AC

ESS BUS

6WV 03 F (1)

121VU EIS/SDAC/2/SPLY 2WV 06 Q (1)

121VU EIS/SDAC/2/BUS1/26VAC

SYNC AC

10WV 05 Q (1)

121VU EIS/SDAC/2/BUS2/26VAC

SYNC AC

8WV 02 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(d) Open the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Open the Contactor Box 107VU.

NOTE: Retain the hardware.

**CONF 002

(1) Subtask 281188-941-001-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

52-40-00, Page Block 001

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

12-34-24-869-002).

(b) Put the access platform(s) in position.

(c) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 23 P (1)

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 34 K (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 26 P (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 37 K (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 25 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 27 Q (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 26 R (1)

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 28 Q (1)

49VU SDAC/1 AND 2/28VDC/ESS

BUS

12WV 05 F (1)

49VU SDAC/1/SPLY 3WV 04 F (1)

49VU SDAC/1/26VAC SYNC/AC

ESS BUS

5WV 02 F (1)

121VU EIS/SDAC/1/BUS1/26VAC

SYNC AC

9WV 04 Q (1)

121VU EIS/SDAC/1/BUS2/26VAC

SYNC AC

7WV 03 Q (1)

49VU SDAC/2/26VAC SYNC/AC

ESS BUS

6WV 03 F (1)

121VU EIS/SDAC/2/SPLY 2WV 06 Q (1)

121VU EIS/SDAC/2/BUS1/26VAC

SYNC AC

10WV 05 Q (1)

121VU EIS/SDAC/2/BUS2/26VAC

SYNC AC

8WV 02 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(d) Open the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Open the Contactor Box 107VU.

NOTE: Retain the hardware.

**CONF 003

(1) Subtask 281188-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

52-40-00, Page Block 001

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

12-34-24-869-002).

(b) Put the access platform(s) in position.

(c) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 23 P (1)

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 34 K (1)

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 25 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 27 Q (1)

49VU SDAC/1 AND 2/28VDC/ESS

BUS

12WV 05 F (1)

49VU SDAC/1/SPLY 3WV 04 F (1)

49VU SDAC/1/26VAC SYNC/AC

ESS BUS

5WV 02 F (1)

121VU EIS/SDAC/1/BUS1/26VAC

SYNC AC

9WV 04 Q (1)

121VU EIS/SDAC/1/BUS2/26VAC

SYNC AC

7WV 03 Q (1)

49VU SDAC/2/26VAC SYNC/AC

ESS BUS

6WV 03 F (1)

121VU EIS/SDAC/2/SPLY 2WV 06 Q (1)

121VU EIS/SDAC/2/BUS1/26VAC

SYNC AC

10WV 05 Q (1)

121VU EIS/SDAC/2/BUS2/26VAC

SYNC AC

8WV 02 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(d) Open the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Open the Contactor Box 107VU.

NOTE: Retain the hardware.

**CONF 004

(1) Subtask 281188-941-001-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

52-40-00, Page Block 001

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

12-34-24-869-002).

(b) Put the access platform(s) in position.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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(c) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 23 P (1)

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 34 K (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 26 P (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 37 K (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 25 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 27 Q (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 26 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 28 Q (1)

49VU SDAC/1 AND 2/28VDC/ESS

BUS

12WV 05 F (1)

49VU SDAC/1/SPLY 3WV 04 F (1)

49VU SDAC/1/26VAC SYNC/AC

ESS BUS

5WV 02 F (1)

121VU EIS/SDAC/1/BUS1/26VAC

SYNC AC

9WV 04 Q (1)

121VU EIS/SDAC/1/BUS2/26VAC

SYNC AC

7WV 03 Q (1)

49VU SDAC/2/26VAC SYNC/AC

ESS BUS

6WV 03 F (1)

121VU EIS/SDAC/2/SPLY 2WV 06 Q (1)

121VU EIS/SDAC/2/BUS1/26VAC

SYNC AC

10WV 05 Q (1)

121VU EIS/SDAC/2/BUS2/26VAC

SYNC AC

8WV 02 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(d) Open the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Open the Contactor Box 107VU.

NOTE: Retain the hardware.

**CONF 005

(1) Subtask 281188-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 53

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References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

52-40-00, Page Block 001

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

12-34-24-869-002).

(b) Put the access platform(s) in position.

(c) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 23 P (1)

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 34 K (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 25 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 27 Q (1)

49VU SDAC/1 AND 2/28VDC/ESS

BUS

12WV 05 F (1)

49VU SDAC/1/SPLY 3WV 04 F (1)

49VU SDAC/1/26VAC SYNC/AC

ESS BUS

5WV 02 F (1)

121VU EIS/SDAC/1/BUS1/26VAC

SYNC AC

9WV 04 Q (1)

121VU EIS/SDAC/1/BUS2/26VAC

SYNC AC

7WV 03 Q (1)

49VU SDAC/2/26VAC SYNC/AC

ESS BUS

6WV 03 F (1)

121VU EIS/SDAC/2/SPLY 2WV 06 Q (1)

121VU EIS/SDAC/2/BUS1/26VAC

SYNC AC

10WV 05 Q (1)

121VU EIS/SDAC/2/BUS2/26VAC

SYNC AC

8WV 02 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(d) Open the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Open the Contactor Box 107VU.

NOTE: Retain the hardware.

**CONF 006

(1) Subtask 281188-941-001-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 54

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References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

52-40-00, Page Block 001

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

12-34-24-869-002).

(b) Put the access platform(s) in position.

(c) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 23 P (1)

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 34 K (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 26 P (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 37 K (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 25 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 27 Q (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 26 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 28 Q (1)

49VU SDAC/1 AND 2/28VDC/ESS

BUS

12WV 05 F (1)

49VU SDAC/1/SPLY 3WV 04 F (1)

49VU SDAC/1/26VAC SYNC/AC

ESS BUS

5WV 02 F (1)

121VU EIS/SDAC/1/BUS1/26VAC

SYNC AC

9WV 04 Q (1)

121VU EIS/SDAC/1/BUS2/26VAC

SYNC AC

7WV 03 Q (1)

49VU SDAC/2/26VAC SYNC/AC

ESS BUS

6WV 03 F (1)

121VU EIS/SDAC/2/SPLY 2WV 06 Q (1)

121VU EIS/SDAC/2/BUS1/26VAC

SYNC AC

10WV 05 Q (1)

121VU EIS/SDAC/2/BUS2/26VAC

SYNC AC

8WV 02 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

(d) Open the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Open the Contactor Box 107VU.

NOTE: Retain the hardware.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 55

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**CONF 007

(1) Subtask 281188-941-001-002 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

Task 12-34-24-869-002

52-40-00, Page Block 001

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

12-34-24-869-002).

(b) Put the access platform(s) in position.

(c) Open, safety/lock and tag these circuit breakers:

PANEL DESIGNATION FIN LOCATION SEE

NOTES

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 23 P (1)

121VU FUEL/CTR TK/PUMP1 SPLY 29QA 34 K (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 26 P (1)

121VU FUEL/CTR TK/PUMP2 SPLY 30QA 37 K (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 25 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

31QA 27 Q (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 26 R (1)

121VU FUEL/CTR TK/PUMPS1 AND

2/CTL AND IND

32QA 28 Q (1)

49VU SDAC/1 AND 2/28VDC/ESS

BUS

12WV 05 F (1)

49VU SDAC/1/SPLY 3WV 04 F (1)

49VU SDAC/1/26VAC SYNC/AC

ESS BUS

5WV 02 F (1)

121VU EIS/SDAC/1/BUS1/26VAC

SYNC AC

9WV 04 Q (1)

121VU EIS/SDAC/1/BUS2/26VAC

SYNC AC

7WV 03 Q (1)

49VU SDAC/2/26VAC SYNC/AC

ESS BUS

6WV 03 F (1)

121VU EIS/SDAC/2/SPLY 2WV 06 Q (1)

121VU EIS/SDAC/2/BUS1/26VAC

SYNC AC

10WV 05 Q (1)

121VU EIS/SDAC/2/BUS2/26VAC

SYNC AC

8WV 02 Q (1)

NOTE (1): The location of the CB depends on the A/C configuration.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 56

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(d) Open the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Open the Contactor Box 107VU.

NOTE: Retain the hardware.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 281188-831-002-001 - Modify the Equipment and the Wiring in the

Contactor Box 107VU

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822, Door 824

Electrical panel 107VU

Work location Electrical panel 107VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 281188A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673D0S 1 BASE

3 NAS1101-04-7 3 SCREW

4 ASNA2397-3L 3 WASHER

5 MS21042-04 3 NUT

D9100095214195 PLACARD

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

References

Fig. A-FBAAA

Modification of the Equipment in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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References

Fig. A-FHAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

(a) Remove from position A08 (Refer to Fig. A-FBAAA Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 35QA.

(b) Loosen and release the relays plate without disconnect the relays (Refer to Fig. AFBAAA Sheet 01).

NOTE: For access, remove and retain all the necessary wiring bracket.

NOTE: Retain the hardware.

(c) Install the relay GFI 69QA.

1 Install at position A08 (Refer to Fig. A-FBAAA Sheet 02):

FIN 69QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

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2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 69QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 69QA as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set D9100095214195

(d) Attach the relays plate with the hardware retained at removal (Refer to Fig. AFBAAA Sheet 01).

**CONF 002

(1) Subtask 281188-831-002-003 - Modify the Equipment and the Wiring in the

Contactor Box 107VU

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822, Door 824

Electrical panel 107VU

Work location Electrical panel 107VU

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Kit 281188A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 2 GFI

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 59

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ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

2 E0673D0S 2 BASE

3 NAS1101-04-7 6 SCREW

4 ASNA2397-3L 6 WASHER

5 MS21042-04 6 NUT

D9100095214295 PLACARD

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

References

Fig. A-FBAAB

Modification of the Equipment in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWBAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Fig. A-FHBAA

Hook up Chart of the Modification of the

Wiring in the Contactor Box 107VU

Sheet 01

(a) Remove 35QA from position A08 (Refer to Fig. A-FBAAB Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 35QA.

(b) Remove 36QA from position A09 (Refer to Fig. A-FBAAB Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 60

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FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 36QA.

(c) Loosen and release the relays plate without disconnect the relays (Refer to Fig. AFBAAB Sheet 01).

NOTE: For access, remove and retain all the necessary wiring bracket.

NOTE: Retain the hardware.

(d) Install the relay GFI 69QA.

1 Install at position A08 (Refer to Fig. A-FBAAB Sheet 02):

FIN 69QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 61

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FIN 69QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 69QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

(e) Install the relay GFI 70QA.

1 Install at position A09 (Refer to Fig. A-FBAAB Sheet 02):

FIN 70QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHBAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 70QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 70QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 62

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(f) Attach the relays plate with the hardware retained at removal (Refer to Fig. AFBAAB Sheet 01).

**CONF 003

(1) Subtask 281188-831-002-002 - Modify the Equipment and the Wiring in the

Contactor Box 107VU

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822, Door 824

Electrical panel 107VU

Work location Electrical panel 107VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 281188A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673D0S 1 BASE

3 NAS1101-04-7 3 SCREW

4 ASNA2397-3L 3 WASHER

5 MS21042-04 3 NUT

D9100095214195 PLACARD

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

References

Fig. A-FBAAA

Modification of the Equipment in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWAAB

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FHAAB

Hook up Chart of the Modification of the

Wiring in the Contactor Box 107VU

Sheet 01

(a) Remove from position A08 (Refer to Fig. A-FBAAA Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 63

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FIN 35QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 35QA.

(b) Loosen and release the relays plate without disconnect the relays (Refer to Fig. AFBAAA Sheet 01).

NOTE: For access, remove and retain all the necessary wiring bracket.

NOTE: Retain the hardware.

(c) Install the relay GFI 69QA.

1 Install at position A08 (Refer to Fig. A-FBAAA Sheet 02):

FIN 69QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAB Sheet 01 and Fig. A-FWAAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHAAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 64

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SERVICE BULLETIN

FIN 69QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 69QA as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set D9100095214195

(d) Attach the relays plate with the hardware retained at removal (Refer to Fig. AFBAAA Sheet 01).

**CONF 004

(1) Subtask 281188-831-002-004 - Modify the Equipment and the Wiring in the

Contactor Box 107VU

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822, Door 824

Electrical panel 107VU

Work location Electrical panel 107VU

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Kit 281188A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 2 GFI

2 E0673D0S 2 BASE

3 NAS1101-04-7 6 SCREW

4 ASNA2397-3L 6 WASHER

5 MS21042-04 6 NUT

D9100095214295 PLACARD

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

References

Fig. A-FBAAB

Modification of the Equipment in the

Contactor Box 107VU

Sheet 01

Sheet 02

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 65

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References

Fig. A-FWAAB

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWBAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FHAAB

Hook up Chart of the Modification of the

Wiring in the Contactor Box 107VU

Sheet 01

Fig. A-FHBAA

Hook up Chart of the Modification of the

Wiring in the Contactor Box 107VU

Sheet 01

(a) Remove 35QA from position A08 (Refer to Fig. A-FBAAB Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 35QA.

(b) Remove 36QA from position A09 (Refer to Fig. A-FBAAB Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 36QA.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 66

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(c) Loosen and release the relays plate without disconnect the relays (Refer to Fig. AFBAAB Sheet 01).

NOTE: For access, remove and retain all the necessary wiring bracket.

NOTE: Retain the hardware.

(d) Install the relay GFI 69QA.

1 Install at position A08 (Refer to Fig. A-FBAAB Sheet 02):

FIN 69QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAB Sheet 01 and Fig. A-FWAAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHAAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 69QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 69QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 67

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(e) Install the relay GFI 70QA.

1 Install at position A09 (Refer to Fig. A-FBAAB Sheet 02):

FIN 70QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHBAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 70QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 70QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

(f) Attach the relays plate with the hardware retained at removal (Refer to Fig. AFBAAB Sheet 01).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 68

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**CONF 005

(1) Subtask 281188-831-002-001 - Modify the Equipment and the Wiring in the

Contactor Box 107VU

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822, Door 824

Electrical panel 107VU

Work location Electrical panel 107VU

Manpower Resources

Manhours 3.00

Minimum number of person 1

Subtask elapsed time 3.00

Skills ELECTRICAL

Material necessary to do the job

Kit 281188A01R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 1 GFI

2 E0673D0S 1 BASE

3 NAS1101-04-7 3 SCREW

4 ASNA2397-3L 3 WASHER

5 MS21042-04 3 NUT

D9100095214195 PLACARD

EN3155-017F1216 6 CONTACT

EN3155-017F1620 4 CONTACT

References

Fig. A-FBAAA

Modification of the Equipment in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

(a) Remove from position A08 (Refer to Fig. A-FBAAA Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 69

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Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 35QA.

(b) Loosen and release the relays plate without disconnect the relays (Refer to Fig. AFBAAA Sheet 01).

NOTE: For access, remove and retain all the necessary wiring bracket.

NOTE: Retain the hardware.

(c) Install the relay GFI 69QA.

1 Install at position A08 (Refer to Fig. A-FBAAA Sheet 02):

FIN 69QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 69QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 70

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SERVICE BULLETIN

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 69QA as shown in Fig. AFBAAA Sheet 02, supplied in:

Placard Set D9100095214195

(d) Attach the relays plate with the hardware retained at removal (Refer to Fig. AFBAAA Sheet 01).

**CONF 006

(1) Subtask 281188-831-002-003 - Modify the Equipment and the Wiring in the

Contactor Box 107VU

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822, Door 824

Electrical panel 107VU

Work location Electrical panel 107VU

Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Kit 281188A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 2 GFI

2 E0673D0S 2 BASE

3 NAS1101-04-7 6 SCREW

4 ASNA2397-3L 6 WASHER

5 MS21042-04 6 NUT

D9100095214295 PLACARD

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

References

Fig. A-FBAAB

Modification of the Equipment in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 71

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References

Fig. A-FWBAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FHAAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Fig. A-FHBAA

Hook up Chart of the Modification of the

Wiring in the Contactor Box 107VU

Sheet 01

(a) Remove 35QA from position A08 (Refer to Fig. A-FBAAB Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 35QA.

(b) Remove 36QA from position A09 (Refer to Fig. A-FBAAB Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 36QA.

(c) Loosen and release the relays plate without disconnect the relays (Refer to Fig. AFBAAB Sheet 01).

NOTE: For access, remove and retain all the necessary wiring bracket.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 72

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NOTE: Retain the hardware.

(d) Install the relay GFI 69QA.

1 Install at position A08 (Refer to Fig. A-FBAAB Sheet 02):

FIN 69QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAA Sheet 01 and Fig. A-FWAAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHAAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 69QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 69QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

(e) Install the relay GFI 70QA.

1 Install at position A09 (Refer to Fig. A-FBAAB Sheet 02):

FIN 70QAA

1 Base E0673D0S Item 2

Attach with

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 73

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3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHBAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 70QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 70QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

(f) Attach the relays plate with the hardware retained at removal (Refer to Fig. AFBAAB Sheet 01).

**CONF 007

(1) Subtask 281188-831-002-004 - Modify the Equipment and the Wiring in the

Contactor Box 107VU

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 822, Door 824

Electrical panel 107VU

Work location Electrical panel 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 74

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@A318/A319/A320/A321

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Manpower Resources

Manhours 6.00

Minimum number of person 1

Subtask elapsed time 6.00

Skills ELECTRICAL

Material necessary to do the job

Kit 281188A02R00

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 ABS1629-28A0 2 GFI

2 E0673D0S 2 BASE

3 NAS1101-04-7 6 SCREW

4 ASNA2397-3L 6 WASHER

5 MS21042-04 6 NUT

D9100095214295 PLACARD

EN3155-017F1216 12 CONTACT

EN3155-017F1620 8 CONTACT

References

Fig. A-FBAAB

Modification of the Equipment in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWAAB

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FWBAA

Modification of the Wiring in the

Contactor Box 107VU

Sheet 01

Sheet 02

Fig. A-FHAAB

Hook up Chart of the Modification of the

Wiring in the Contactor Box 107VU

Sheet 01

Fig. A-FHBAA

Hook up Chart of the Modification of the

Wiring in the Contactor Box 107VU

Sheet 01

(a) Remove 35QA from position A08 (Refer to Fig. A-FBAAB Sheet 01):

FIN 35QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 35QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 75

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3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 35QA.

(b) Remove 36QA from position A09 (Refer to Fig. A-FBAAB Sheet 01):

FIN 36QA

1 Relay NSA932843AA01 Item (1) Discard

FIN 36QAA

1 Base NSA932844AA Item (2) Discard

Attached with:

3 Screw Item (3) Discard

3 Washer Item (4) Discard

3 Nut Item (5) Discard

NOTE: Remove and discard the placards identified 36QA.

(c) Loosen and release the relays plate without disconnect the relays (Refer to Fig. AFBAAB Sheet 01).

NOTE: For access, remove and retain all the necessary wiring bracket.

NOTE: Retain the hardware.

(d) Install the relay GFI 69QA.

1 Install at position A08 (Refer to Fig. A-FBAAB Sheet 02):

FIN 69QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 76

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2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWAAB Sheet 01 and Fig. A-FWAAB Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHAAB Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

4 Contact EN3155-017F1620

FIN 69QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 69QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

(e) Install the relay GFI 70QA.

1 Install at position A09 (Refer to Fig. A-FBAAB Sheet 02):

FIN 70QAA

1 Base E0673D0S Item 2

Attach with

3 Screw NAS1101-04-7 Item 3

3 Washer ASNA2397-3L Item 4

3 Nut MS21042-04 Item 5

NOTE: Tighten the three nuts Item 5 to a torque value of 0.10 m.daN

(8.851 in.lb).

2 Modify the connections of the wires as shown in the wiring diagrams Fig. AFWBAA Sheet 01 and Fig. A-FWBAA Sheet 02 and as given in the hook-up

chart lines:

- 1 thru 20 (Refer to Fig. A-FHBAA Sheet 01).

NOTE: If necessary, use:

6 Contact EN3155-017F1216

and

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 77

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SERVICE BULLETIN

4 Contact EN3155-017F1620

FIN 70QA

1 GFI ABS1629-28A0 Item 1

NOTE: Tighten the three screws Item 3 to a torque value between 0.023

m.daN and 0.034 m.daN (2.036 in.lb and 3.009 in.lb).

3 Near the new relays, bond the placards identified 70QA as shown in Fig. AFBAAB Sheet 01, supplied in:

Placard Set D9100095214295

(f) Attach the relays plate with the hardware retained at removal (Refer to Fig. AFBAAB Sheet 01).

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 281188-800-401-003 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAC

Test of Ground Fault Interrupter 69QA

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 69QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAC Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 69QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(2) Subtask 281188-710-401-003 - Test of the Ground Fault Interrupter - 69QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 78

7

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

SERVICE BULLETIN

210 Work location Electrical panel 40VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAC

Test of Ground Fault Interrupter 69QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAC Sheet 02).

2 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump 37QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump FIN 37QA.

3 Operate the center tank fuel pump FIN 37QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

69QA, on the panel 107VU (Refer to Fig. A-UBAAC Sheet 01).

b Make sure that the GFI FIN 69QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 33QA (CTR TK PUMP 1).

4 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to set the center tank fuel

pump FIN 37QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 69QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAC Sheet 01).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 79

7

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

SERVICE BULLETIN

6 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump FIN 37QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump 37QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAC Sheet 02).

**CONF 002

(1) Subtask 281188-800-401-001 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAA

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 69QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 69QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 70QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 70QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 80

7

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

SERVICE BULLETIN

(2) Subtask 281188-710-401-001 - Test of the Ground Fault Interrupter - 69QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

210 Work location Electrical panel 40VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAA

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump 37QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump FIN 37QA.

3 Operate the center tank fuel pump FIN 37QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

69QA, on the panel 107VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 69QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 33QA (CTR TK PUMP 1).

4 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to set the center tank fuel

pump FIN 37QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 81

7

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@A318/A319/A320/A321

SERVICE BULLETIN

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 69QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump FIN 37QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump 37QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

(3) Subtask 281188-710-402-001 - Test of the Ground Fault Interrupter - 70QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAA

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump 38QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump FIN 38QA.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 82

7

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@A318/A319/A320/A321

SERVICE BULLETIN

3 Operate the center tank fuel pump FIN 38QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

70QA, on the panel 107VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 70QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 34QA (CTR TK PUMP 2).

4 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to set the center tank fuel

pump FIN 38QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 70QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump FIN 38QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump 38QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

**CONF 003

(1) Subtask 281188-800-401-003 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAC

Test of Ground Fault Interrupter 69QA

Sheet 01

Sheet 02

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 83

7

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

SERVICE BULLETIN

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 69QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAC Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 69QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(2) Subtask 281188-710-401-003 - Test of the Ground Fault Interrupter - 69QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

210 Work location Electrical panel 40VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAC

Test of Ground Fault Interrupter 69QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAC Sheet 02).

2 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump 37QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump FIN 37QA.

3 Operate the center tank fuel pump FIN 37QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

69QA, on the panel 107VU (Refer to Fig. A-UBAAC Sheet 01).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 84

7

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SERVICE BULLETIN

b Make sure that the GFI FIN 69QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 33QA (CTR TK PUMP 1).

4 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to set the center tank fuel

pump FIN 37QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 69QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAC Sheet 01).

6 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump FIN 37QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump 37QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAC Sheet 02).

**CONF 004

(1) Subtask 281188-800-401-001 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAA

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 69QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 69QA) until it latches in the closed (not tripped)

position.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 85

7

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

SERVICE BULLETIN

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 70QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAA Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 70QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(2) Subtask 281188-710-401-001 - Test of the Ground Fault Interrupter - 69QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

210 Work location Electrical panel 40VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAA

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump 37QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump FIN 37QA.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 86

7

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

3 Operate the center tank fuel pump FIN 37QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

69QA, on the panel 107VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 69QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 33QA (CTR TK PUMP 1).

4 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to set the center tank fuel

pump FIN 37QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 69QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump FIN 37QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump 37QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

(3) Subtask 281188-710-402-001 - Test of the Ground Fault Interrupter - 70QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAA

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 87

7

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

SERVICE BULLETIN

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAA Sheet 02).

2 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump 38QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump FIN 38QA.

3 Operate the center tank fuel pump FIN 38QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

70QA, on the panel 107VU (Refer to Fig. A-UBAAA Sheet 01).

b Make sure that the GFI FIN 70QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 34QA (CTR TK PUMP 2).

4 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to set the center tank fuel

pump FIN 38QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 70QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAA Sheet 01).

6 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump FIN 38QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump 38QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAA Sheet 02).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 88

7

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

SERVICE BULLETIN

**CONF 005

(1) Subtask 281188-800-401-004 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAD

Test of Ground Fault Interrupter 69QA

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 69QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAD Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 69QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(2) Subtask 281188-710-401-004 - Test of the Ground Fault Interrupter - 69QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

210 Work location Electrical panel 40VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAD

Test of Ground Fault Interrupter 69QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAD Sheet 02).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 89

7

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SERVICE BULLETIN

2 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump 37QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump FIN 37QA.

3 Operate the center tank fuel pump FIN 37QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

69QA, on the panel 107VU (Refer to Fig. A-UBAAD Sheet 01).

b Make sure that the GFI FIN 69QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 33QA (CTR TK PUMP 1).

4 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to set the center tank fuel

pump FIN 37QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 69QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAD Sheet 01).

6 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump FIN 37QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump 37QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAD Sheet 02).

**CONF 006

(1) Subtask 281188-800-401-002 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 90

7

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SERVICE BULLETIN

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAB

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 69QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAB Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 69QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 70QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAB Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 70QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(2) Subtask 281188-710-401-002 - Test of the Ground Fault Interrupter - 69QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

210 Work location Electrical panel 40VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAB

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 91

7

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SERVICE BULLETIN

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAB Sheet 02).

2 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump 37QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump FIN 37QA.

3 Operate the center tank fuel pump FIN 37QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

69QA, on the panel 107VU (Refer to Fig. A-UBAAB Sheet 01).

b Make sure that the GFI FIN 69QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 33QA (CTR TK PUMP 1).

4 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to set the center tank fuel

pump FIN 37QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 69QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAB Sheet 01).

6 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump FIN 37QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump 37QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAB Sheet 02).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 92

7

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SERVICE BULLETIN

(3) Subtask 281188-710-402-002 - Test of the Ground Fault Interrupter - 70QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAB

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAB Sheet 02).

2 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump 38QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump FIN 38QA.

3 Operate the center tank fuel pump FIN 38QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

70QA, on the panel 107VU (Refer to Fig. A-UBAAB Sheet 01).

b Make sure that the GFI FIN 70QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 34QA (CTR TK PUMP 2).

4 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to set the center tank fuel

pump FIN 38QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 93

7

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SERVICE BULLETIN

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 70QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAB Sheet 01).

6 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump FIN 38QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump 38QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAB Sheet 02).

**CONF 007

(1) Subtask 281188-800-401-002 - Preparation for Test Procedure

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Fig. A-UBAAB

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

(a) Examine the ABS1629-28A0 Ground Fault Interrupter (GFI), FIN 69QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAB Sheet 01).

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 69QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(b) Examine the ABS1629-28A0 GFI, FIN 70QA

1 On the panel 107VU, make sure that the GFI is in the reset (non-tripped)

condition (metal shaft is not seen on the trip RESET plunger) (Refer to Fig. AUBAAB Sheet 01).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 94

7

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SERVICE BULLETIN

2 If the metal shaft is in the open (tripped) position, push it (into the

ABS1629-28A0 GFI, FIN 70QA) until it latches in the closed (not tripped)

position.

3 Make sure that you cannot see the metal shaft.

(2) Subtask 281188-710-401-002 - Test of the Ground Fault Interrupter - 69QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

210 Work location Electrical panel 40VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAB

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Left-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAB Sheet 02).

2 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump 37QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump FIN 37QA.

3 Operate the center tank fuel pump FIN 37QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

69QA, on the panel 107VU (Refer to Fig. A-UBAAB Sheet 01).

b Make sure that the GFI FIN 69QA trips (the metal shaft on the trip

RESET indicator comes out).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 95

7

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SERVICE BULLETIN

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 33QA (CTR TK PUMP 1).

4 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to set the center tank fuel

pump FIN 37QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 69QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAB Sheet 01).

6 Push the P/BSW FIN 33QA (CTR TK PUMP 1) to operate the center tank fuel

pump FIN 37QA:

a Make sure that the center tank fuel pump FIN 37QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 33QA (CTR TK PUMP 1) to stop the center tank

fuel pump 37QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAB Sheet 02).

(3) Subtask 281188-710-402-002 - Test of the Ground Fault Interrupter - 70QA

Work Zones and Access Panels

Zone Access/Work location

126 Work location Electrical panel 107VU

Manpower Resources

Skills ELECTRICAL

References

Aircraft Maintenance Manual (AMM) Task 28-25-00-869-001

Fig. A-UBAAB

Test of Ground Fault Interrupter

69QA/70QA

Sheet 01

Sheet 02

WARNING: MAKE SURE THAT THE CENTER TANK HAS SUFFICIENT FUEL TO

MAKE SURE THAT THE TRANSFER FUEL PUMP WILL NOT RUN IN

THE DRY CONDITION.

(a) Do a Fuel Transfer Test (Right-hand Pump)

1 On the panel 40VU, set the Push-Button Switch (P/BSW) FIN 48QA (MODE

SEL) to MAN (manual) (Refer to Fig. A-UBAAB Sheet 02).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 96

7

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SERVICE BULLETIN

2 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump 38QA operates correctly (to

move some of the fuel from the center tank) and gives the correct flight

deck indications (as indicated in the ground transfer procedure) (Refer to

AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump FIN 38QA.

3 Operate the center tank fuel pump FIN 38QA to do a fuel transfer (Refer to

AMM Task 28-25-00-869-001):

a While the pump operates push the ’auto-test’ P/BSW on the GFI FIN

70QA, on the panel 107VU (Refer to Fig. A-UBAAB Sheet 01).

b Make sure that the GFI FIN 70QA trips (the metal shaft on the trip

RESET indicator comes out).

c Make sure that the related PUMP FAULT light illuminates on the P/BSW

FIN 34QA (CTR TK PUMP 2).

4 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to set the center tank fuel

pump FIN 38QA to OFF. Make sure that the illuminated FAULT legend goes

off and the OFF legend illuminates on the related P/BSW.

5 On the panel 107VU, push in the trip RESET button of the GFI FIN 70QA until

it latches in the closed (not tripped) position. Make sure that you cannot see

the metal shaft (Refer to Fig. A-UBAAB Sheet 01).

6 Push the P/BSW FIN 34QA (CTR TK PUMP 2) to operate the center tank fuel

pump FIN 38QA:

a Make sure that the center tank fuel pump FIN 38QA operates correctly

(to move some of the fuel from the center tank) and gives the correct

flight deck indications (as indicated in the ground transfer procedure)

(Refer to AMM Task 28-25-00-869-001).

b Push the P/BSW FIN 34QA (CTR TK PUMP 2) to stop the center tank

fuel pump 38QA.

7 On the panel 40VU, push the P/BSW FIN 48QA (MODE SEL) to de-select

MAN (manual) mode (Refer to Fig. A-UBAAB Sheet 02).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 97

7

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SERVICE BULLETIN

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 281188-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

52-40-00, Page Block 001

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

equipment.

(b) Close the Contactor Box 107VU with the hardware retained at removal.

(c) Restore the systems and the aircraft to normal operating condition.

(d) Close the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Remove the access platform(s).

**CONF 002

(1) Subtask 281188-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

52-40-00, Page Block 001

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

equipment.

(b) Close the Contactor Box 107VU with the hardware retained at removal.

(c) Restore the systems and the aircraft to normal operating condition.

(d) Close the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Remove the access platform(s).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 98

7

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SERVICE BULLETIN

**CONF 003

(1) Subtask 281188-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

52-40-00, Page Block 001

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

equipment.

(b) Close the Contactor Box 107VU with the hardware retained at removal.

(c) Restore the systems and the aircraft to normal operating condition.

(d) Close the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Remove the access platform(s).

**CONF 004

(1) Subtask 281188-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

52-40-00, Page Block 001

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

equipment.

(b) Close the Contactor Box 107VU with the hardware retained at removal.

(c) Restore the systems and the aircraft to normal operating condition.

(d) Close the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Remove the access platform(s).

**CONF 005

(1) Subtask 281188-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 99

7

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@A318/A319/A320/A321

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

52-40-00, Page Block 001

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

equipment.

(b) Close the Contactor Box 107VU with the hardware retained at removal.

(c) Restore the systems and the aircraft to normal operating condition.

(d) Close the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Remove the access platform(s).

**CONF 006

(1) Subtask 281188-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

52-40-00, Page Block 001

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

equipment.

(b) Close the Contactor Box 107VU with the hardware retained at removal.

(c) Restore the systems and the aircraft to normal operating condition.

(d) Close the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Remove the access platform(s).

**CONF 007

(1) Subtask 281188-942-002-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001

52-40-00, Page Block 001

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

equipment.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 100

7

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@A318/A319/A320/A321

SERVICE BULLETIN

(b) Close the Contactor Box 107VU with the hardware retained at removal.

(c) Restore the systems and the aircraft to normal operating condition.

(d) Close the avionics-compartment doors 822 and 824 (Refer to AMM 06-41-53, Page

Block 001 and AMM 52-40-00, Page Block 001).

(e) Remove the access platform(s).

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 101

7

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SERVICE BULLETIN

**CONF 001, 003, 005

FR1

FR20

FR24

FR16

FR9

FR15

107VU

A

B C

A

D

D

B

BEFORE

(5)

(2)

(3)

(1)

(4)

(3 POS)

(3 POS)

(3 POS)

35QA

N_SB_281188_5_BAAA_01_00

Figure A-FBAAA - Sheet 01

Modification of the Equipment in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 102

7

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SERVICE BULLETIN

**CONF 001, 003, 005

AFTER

E

C

(3 POS)

(3 POS)

(3 POS)

2

1 5

4

3

N_SB_281188_5_BAAA_02_00

69QA E

Figure A-FBAAA - Sheet 02

Modification of the Equipment in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 103

7

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SERVICE BULLETIN

**CONF 002, 004, 006 thru 007

FR1

FR20

FR24

FR16

FR9

FR15

107VU

A

B C

A

D

B

BEFORE

(5)

(2)

(3)

(1)

(4)

(3 POS)

(3 POS)

(3 POS)

35QA

36QA

D

N_SB_281188_5_BAAB_01_00

Figure A-FBAAB - Sheet 01

Modification of the Equipment in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 104

7

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@A318/A319/A320/A321

SERVICE BULLETIN

**CONF 002, 004, 006 thru 007

AFTER

E

C

(3 POS)

(3 POS)

(3 POS)

2

1 5

4

3

E

69QA

70QA

N_SB_281188_5_BAAB_02_00

Figure A-FBAAB - Sheet 02

Modification of the Equipment in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 105

7

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SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

Figure A-FWAAA - Sheet 01

Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 106

7

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SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

Figure A-FWAAA - Sheet 02

Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 107

7

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SERVICE BULLETIN

**CONF 003 thru 004, 007

Figure A-FWAAB - Sheet 01

Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 108

7

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SERVICE BULLETIN

**CONF 003 thru 004, 007

Figure A-FWAAB - Sheet 02

Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 109

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SERVICE BULLETIN

**CONF 001 thru 002, 005 thru 006

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 35QA−A 8 2821−0151 B 1M QF16 107VU 1260VC 49 M1O

 2 107VU 69QA−A C1 EN3155−017F1216 2821−0151 B 1M QF16 107VU 1260VC 49 M1N

 3 107VU 35QA−A 2 2821−0151 R 1M QF16 107VU 1260VC 47 M1O

 4 107VU 69QA−A A1 EN3155−017F1216 2821−0151 R 1M QF16 107VU 1260VC 47 M1N

 5 107VU 35QA−A 6 2821−0151 Y 1M QF16 107VU 1260VC 48 M1O

 6 107VU 69QA−A B1 EN3155−017F1216 2821−0151 Y 1M QF16 107VU 1260VC 48 M1N

 7 107VU 35QA−A 7 2821−0154 B 1M QF16 107VU 1264VC 48 M1O

 8 107VU 69QA−A C2 EN3155−017F1216 2821−0154 B 1M QF16 107VU 1264VC 48 M1N

 9 107VU 35QA−A 1 2821−0154 R 1M QF16 107VU 1264VC 46 M1O

10 107VU 69QA−A A2 EN3155−017F1216 2821−0154 R 1M QF16 107VU 1264VC 46 M1N

11 107VU 35QA−A 5 2821−0154 Y 1M QF16 107VU 1264VC 47 M1O

12 107VU 69QA−A B2 EN3155−017F1216 2821−0154 Y 1M QF16 107VU 1264VC 47 M1N

13 107VU 35QA−A Z 2821−0162 1M CF24 107VU 1176VT 5C M1O

14 107VU 69QA−A X2 EN3155−017F1620 2821−0162 1M CF24 107VU 1176VT 5C M1N

15 107VU 35QA−A X 2821−0451 1M CF24 107VU 1176VT 1J M1O

16 107VU 69QA−A X1 EN3155−017F1620 2821−0451 1M CF24 107VU 1176VT 1J M1N

17 107VU 35QA−A 3 3154−1008 1M CF24 107VU 1176VT 5J M1O

18 107VU 69QA−A 12 EN3155−017F1620 3154−1008 1M CF24 107VU 1176VT 5J M1N

19 107VU 35QA−A B 3154−2033 1M CF24 107VU 1176VT 13C M1O

20 107VU 69QA−A 11 EN3155−017F1620 3154−2033 1M CF24 107VU 1176VT 13C M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHAAA - Sheet 01

Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 110

7

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SERVICE BULLETIN

**CONF 003 thru 004, 007

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 35QA−A 8 2821−0151 B 1M QF16 107VU 1260VC 49 M1O

 2 107VU 69QA−A C1 EN3155−017F1216 2821−0151 B 1M QF16 107VU 1260VC 49 M1N

 3 107VU 35QA−A 2 2821−0151 R 1M QF16 107VU 1260VC 47 M1O

 4 107VU 69QA−A A1 EN3155−017F1216 2821−0151 R 1M QF16 107VU 1260VC 47 M1N

 5 107VU 35QA−A 6 2821−0151 Y 1M QF16 107VU 1260VC 48 M1O

 6 107VU 69QA−A B1 EN3155−017F1216 2821−0151 Y 1M QF16 107VU 1260VC 48 M1N

 7 107VU 35QA−A 7 2821−0154 B 1M QF16 107VU 1264VC 48 M1O

 8 107VU 69QA−A C2 EN3155−017F1216 2821−0154 B 1M QF16 107VU 1264VC 48 M1N

 9 107VU 35QA−A 1 2821−0154 R 1M QF16 107VU 1264VC 46 M1O

10 107VU 69QA−A A2 EN3155−017F1216 2821−0154 R 1M QF16 107VU 1264VC 46 M1N

11 107VU 35QA−A 5 2821−0154 Y 1M QF16 107VU 1264VC 47 M1O

12 107VU 69QA−A B2 EN3155−017F1216 2821−0154 Y 1M QF16 107VU 1264VC 47 M1N

13 107VU 35QA−A Z 2821−0162 1M CF24 107VU 1176VT 5C M1O

14 107VU 69QA−A X2 EN3155−017F1620 2821−0162 1M CF24 107VU 1176VT 5C M1N

15 107VU 35QA−A X 2821−0451 1M CF24 107VU 1176VT 14P M1O

16 107VU 69QA−A X1 EN3155−017F1620 2821−0451 1M CF24 107VU 1176VT 14P M1N

17 107VU 35QA−A 3 3154−1008 1M CF24 107VU 1176VT 5J M1O

18 107VU 69QA−A 12 EN3155−017F1620 3154−1008 1M CF24 107VU 1176VT 5J M1N

19 107VU 35QA−A B 3154−2033 1M CF24 107VU 1176VT 13C M1O

20 107VU 69QA−A 11 EN3155−017F1620 3154−2033 1M CF24 107VU 1176VT 13C M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHAAB - Sheet 01

Hook up Chart of the Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 111

7

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SERVICE BULLETIN

**CONF 002, 004, 006 thru 007

Figure A-FWBAA - Sheet 01

Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 112

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SERVICE BULLETIN

**CONF 002, 004, 006 thru 007

Figure A-FWBAA - Sheet 02

Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 113

7

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SERVICE BULLETIN

**CONF 002, 004, 006 thru 007

END1 LEAD END2

Instructions Zone or

Panel Elec.Ident. Term Terminal P/N

Wire

Ident. Co Rte Gauge

Lenght

mm Inch

Zone or

Panel Elec.Ident. Term Terminal P/N

L

i

n

e

 1 107VU 36QA−A 8 2821−0195 B 2M QF16 107VU 1262VC 48 M1O

 2 107VU 70QA−A C1 EN3155−017F1216 2821−0195 B 2M QF16 107VU 1262VC 48 M1N

 3 107VU 36QA−A 2 2821−0195 R 2M QF16 107VU 1262VC 46 M1O

 4 107VU 70QA−A A1 EN3155−017F1216 2821−0195 R 2M QF16 107VU 1262VC 46 M1N

 5 107VU 36QA−A 6 2821−0195 Y 2M QF16 107VU 1262VC 47 M1O

 6 107VU 70QA−A B1 EN3155−017F1216 2821−0195 Y 2M QF16 107VU 1262VC 47 M1N

 7 107VU 36QA−A 7 2821−0198 B 2M QF16 107VU 1266VC 48 M1O

 8 107VU 70QA−A C2 EN3155−017F1216 2821−0198 B 2M QF16 107VU 1266VC 48 M1N

 9 107VU 36QA−A 1 2821−0198 R 2M QF16 107VU 1266VC 46 M1O

10 107VU 70QA−A A2 EN3155−017F1216 2821−0198 R 2M QF16 107VU 1266VC 46 M1N

11 107VU 36QA−A 5 2821−0198 Y 2M QF16 107VU 1266VC 47 M1O

12 107VU 70QA−A B2 EN3155−017F1216 2821−0198 Y 2M QF16 107VU 1266VC 47 M1N

13 107VU 36QA−A Z 2821−0205 2M CF24 107VU 1176VT 3E M1O

14 107VU 70QA−A X2 EN3155−017F1620 2821−0205 2M CF24 107VU 1176VT 3E M1N

15 107VU 36QA−A X 2821−0452 2M CF24 107VU 1176VT 12L M1O

16 107VU 70QA−A X1 EN3155−017F1620 2821−0452 2M CF24 107VU 1176VT 12L M1N

17 107VU 36QA−A 3 3154−1004 2M CF24 107VU 1176VT 6A M1O

18 107VU 70QA−A 12 EN3155−017F1620 3154−1004 2M CF24 107VU 1176VT 6A M1N

19 107VU 36QA−A B 3154−2027 2M CF24 107VU 1176VT 12A M1O

20 107VU 70QA−A 11 EN3155−017F1620 3154−2027 2M CF24 107VU 1176VT 12A M1N

21

22

23

24

25

 M1O = OLD HOOK−UP ON END 1

 M1N = NEW HOOK−UP ON END 1

Figure A-FHBAA - Sheet 01

Hook up Chart of the Modification of the Wiring in the Contactor Box 107VU

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 114

7

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SERVICE BULLETIN

**CONF 002, 004

TRIPPED

NOT TRIPPED

GFI METAL

SHAFT IN OPEN

POSITION

AUTO−TEST

BUTTON

C

107VU

N_SB_281188_7_BAAA_01_00

GFI

B

69QA

70QA

GFI METAL

SHAFT IN CLOSED

POSITION

C

FR24

FR20

FR16

FR15

FR9

A D

A

B

FR1

Z120

GROUND FAULT

INTERRUPTER

(GFI)

Figure A-UBAAA - Sheet 01

Test of Ground Fault Interrupter 69QA/70QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 115

7

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SERVICE BULLETIN

**CONF 002, 004

N_SB_281188_7_BAAA_02_00

D

E

40VU

E

F

U

E

L

F

U

E

L

ENG 1 APU X FEED

OPEN

ON

CTR TK CTR TK

PUMP 2

A

U

T

O

PUMP 1 MODE SEL

FAULT

OFF

FAULT

MAN

FAULT

OFF

FAULT

OFF

R TK PUMPS

FAULT

OFF

FAULT

OFF

1 2

ENG 2

FAULT

OFF

1 2 L TK PUMPS

33QA 48QA 34QA

Figure A-UBAAA - Sheet 02

Test of Ground Fault Interrupter 69QA/70QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 116

7

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SERVICE BULLETIN

**CONF 006 thru 007

TRIPPED

NOT TRIPPED

GFI METAL

SHAFT IN OPEN

POSITION

AUTO−TEST

BUTTON

C

107VU

GFI

B

GFI METAL

SHAFT IN CLOSED

POSITION

FR24

FR20

FR16

FR15

FR9

A D

A

B

FR1

Z120

N_SB_281188_7_BAAB_01_00

69QA

70QA

C

GROUND FAULT

INTERRUPTER

(GFI)

Figure A-UBAAB - Sheet 01

Test of Ground Fault Interrupter 69QA/70QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 117

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SERVICE BULLETIN

**CONF 006 thru 007

F

U

E

L

F

U

E

L

ENG 1 APU X FEED

OPEN

ON

CTR TK CTR TKPUMP 2

A

U

T

O

PUMP 1 MODE SEL

FAULT

OFF

FAULT

MAN

FAULT

OFF

FAULT

FWD FAULT

OFF

R TK PUMPS

FAULT

OFF

FAULT

OFF

1 2

ENG 2

FAULT

OFF

1 2 L TK PUMPS A

U

T

O

ACT

D

E

40VU

E

N_SB_281188_7_BAAB_02_00

33QA 48QA 34QA

Figure A-UBAAB - Sheet 02

Test of Ground Fault Interrupter 69QA/70QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 118

7

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SERVICE BULLETIN

**CONF 001, 003

TRIPPED

NOT TRIPPED

GFI METAL

SHAFT IN OPEN

POSITION

AUTO−TEST

BUTTON

C

107VU

GFI

B

69QA

GFI METAL

SHAFT IN CLOSED

POSITION

FR24

FR20

FR16

FR15

FR9

A D

A

B

FR1

Z120

GROUND FAULT

INTERRUPTER

(GFI)

N_SB_281188_7_BAAC_01_00

C

Figure A-UBAAC - Sheet 01

Test of Ground Fault Interrupter 69QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 119

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SERVICE BULLETIN

**CONF 001, 003

D

E

40VU

E

F

U

E

L

F

U

E

L

ENG 1 APU X FEED

OPEN

ON

CTR TK CTR TK

PUMP 2

A

U

T

O

PUMP 1 MODE SEL

FAULT

OFF

FAULT

MAN

FAULT

OFF

FAULT

OFF

R TK PUMPS

FAULT

OFF

FAULT

OFF

1 2

ENG 2

FAULT

OFF

1 2 L TK PUMPS

33QA 48QA

N_SB_281188_7_BAAC_02_00

Figure A-UBAAC - Sheet 02

Test of Ground Fault Interrupter 69QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 120

7

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SERVICE BULLETIN

**CONF 005

TRIPPED

NOT TRIPPED

GFI METAL

SHAFT IN OPEN

POSITION

AUTO−TEST

BUTTON

C

107VU

GFI

B

69QA

GFI METAL

SHAFT IN CLOSED

POSITION

FR24

FR20

FR16

FR15

FR9

A D

A

B

FR1

Z120

GROUND FAULT

INTERRUPTER

(GFI)

C

N_SB_281188_7_BAAD_01_00

Figure A-UBAAD - Sheet 01

Test of Ground Fault Interrupter 69QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 121

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SERVICE BULLETIN

**CONF 005

F

U

E

L

F

U

E

L

ENG 1 APU X FEED

OPEN

ON

CTR TK CTR TKPUMP 2

A

U

T

O

PUMP 1 MODE SEL

FAULT

OFF

FAULT

MAN

FAULT

OFF

FAULT

FWD FAULT

OFF

R TK PUMPS

FAULT

OFF

FAULT

OFF

1 2

ENG 2

FAULT

OFF

1 2 L TK PUMPS A

U

T

O

ACT

D

E

40VU

E

33QA 48QA

N_SB_281188_7_BAAD_02_00

Figure A-UBAAD - Sheet 02

Test of Ground Fault Interrupter 69QA

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 122

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SERVICE BULLETIN

REPORTING SHEET

TITLE: FUEL- MAIN FUEL PUMP SYSTEM - INTRODUCE GROUND FAULT

INTERRUPTERS (GFI) TO CENTER TANK FUEL PUMPS

MODIFICATION No.: 150736J3138

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 1

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SERVICE BULLETIN

QUALITY PERCEPTION FORM

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

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

improve the quality of our Service Bulletins.

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

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

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

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

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

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

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Mar 23/12 SERVICE BULLETIN No.: A320-28-1188

REVISION No.: 00 - Mar 23/12 Page: 1

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