@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: 22

TITLE: AUTO-FLIGHT - FAC - INSTALL STANDARD FAC CAA02 (SHARKLETS

AND ROPS PROJECT) ON A321 AIRCRAFT

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR 155488P13834

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

Since Flight Augmentation Computer (FAC) Standard CAA01 is not valid anymore for A321 aircraft, it is

needed to propose a way to install FAC Standard CAA02 on A321 aircraft by replacing FAC Standard

B0620.

This Service Bulletin recommends replacing FAC Standard CAA02 in place of FAC Standard B0620 for

A321 aircraft while providing dataloading capacity and improved performance. The new FAC CAA02

includes two main software improvements: Runway Overrun Prevention System (ROPS) and Sharklets

capability.

Accomplishment of this Service Bulletin allows the following improvements on FAC hardware:

- improve Central Processing Unit (CPU) and memory margins (to match end of life requirements),

- cover component obsolescence (at least 5 years after certification),

- increase reliability,

- reduce weight and power consumption,

- introduce dataloading capacity.

The FAC software evolutions in comparison with Standard B0620 are as follows:

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1. Sharklets capability: FAC CAA02 standard introduces software adaptation for A321/CFM/IAE

equipped with Sharklets (weight and CG, characteristic speeds). These tunings are activated by pinprogram AE-08G.

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

Sharklets installations.

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

account the Sharklets aerodynamic impact.

2. Introduction of ROPS function:

FAC CAA02 includes the software modifications necessary to perform the ROPS function:

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

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

messages requiring either to perform a Go Around or to apply the maximum braking. On FAC

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

Moreover, FAC CAA02 includes 2 adaptations of the ROPS functions:

- Compatibility with both Terrain Awareness and Warning System (TAWS) equipment: EGPWS and

T3CAS.

- For A321 aircraft, modifications for compatibility with ABS Brakes and restoration of nominal

tunings for Messier Bugatti brakes. MB brakes tunings will be activated through a dedicated pin

program (AA-02B).

3. Other modifications:

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

short power supply cut.

- Reduction of the Rudder Travel Limitation at high speed (new control law called Rudder Travel

Limitation Unit (RTLU*)). RTLU* control law aims at reducing Vertical Tail Plane (VTP) loads in

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

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

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

by pin program AE-08J and requires FWC standard H2F7.

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

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

pseudo THS position is sent to the FWC to trigger the new "Pitch trim MCDU CG disagree" alert.

This function requires FWC standard H2F6.

- Correction of Flight Guidance/Flight Augmentation Computer (FG/FAC) interface issue affecting

weight computation in FMS Landing System (FLS).

- Addition of a Post Flight Report (PFR) message in case of failure affecting Autopilot/Flight Director

(AP/FD) TCAS function (function introduced with FG C13 and I12).

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

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SUMMARY

- Other minor modifications without functional impact (FAC not healthy upon negative total True Air

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

Nose wheel failure, etc.).

For full improvements description, refer to the Modification Operational Impact (MOI) No. 155488.

The operational consequence of this Service Bulletin is the Flight Crew Operating Manual (FCOM)

update.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO

POTENTIAL AD NO A/C OPERATION AFFECTED YES

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

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

disruptions.

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Equipment BFEA01 1 See SB FACs, MEDIA

EFFECTIVITY

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

AAF AAR ABL ACA AEE AFL AFR AIC AMU AUA AWM AWW AZA

BAW BER BIE CCA CES CIB CSC CSN DKH DLH EIN EVA FHY

FIN G2X GFA GZQ HDA HRM HVN I2L IAW IBE IRM JST KGL

KHV KKK KZR LLM LMU MEA MLM MLR MON MSR NKS NLY NVR

NWS OHY PAL QTR RCT RJA RYW SAS SBI SVA SVR SWR TAI

TAM TAP TCX THY TNA USA UTA VKG WRC

CONCURRENT REQUIREMENTS

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

following Service Bulletin as per effectivity specified in this Service Bulletin:

Service Bulletin No. A320-22-1278

NOTE: Service Bulletin No. A320-22-1278 (AUTO FLIGHT - FAC (FLIGHT AUGMENTATION

COMPUTER) - INTRODUCE FAC SOFTWARE STANDARD BAM0620) applies

Modification No. 38777P10777.

REFERENCES / REPERCUSSIONS

TFU None

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SUMMARY

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT NO

EQUIPMENT YES

HARD YES

SOFT YES

OBRM NO

MANPOWER

Task 221454-831-801-001: Modification of the two FACs (FINs 1CC1 and 1CC2).

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.50

APPENDICES

Appendix 01 - Elapsed Time Assumption.

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SUMMARY

**CONF ALL

A

80VU

1CC2

1CC1

FR1

Z120

FR24A

A

N_SB_221454_5_SAAA_01_01

Figure A-FSAAA - Sheet 01

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SUMMARY

**CONF ALL

A A

A

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

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

1CCMD1

N_SB_221454_5_SBAA_01_00

Figure A-FSBAA - Sheet 01

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SERVICE BULLETIN

SUMMARY

**CONF ALL

C

B

A

C

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

ON AIRCRAFT CONFIGURATION (SEE FIG. A−FSBAA)

1CCMD1

B

Z210

FR24

FR1

A

N_SB_221454_5_SCAA_01_00

Figure A-FSCAA - Sheet 01

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SERVICE BULLETIN

SUMMARY

This Page Intentionally Left Blank

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

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SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

ATA SYSTEM: 22

TITLE: AUTO-FLIGHT - FAC - INSTALL STANDARD FAC CAA02 (SHARKLETS

AND ROPS PROJECT) ON A321 AIRCRAFT

MODIFICATION No.: 155488P13834

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

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

39468P11175 (Service Bulletin No. A320-22-1406) is not embodied.

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

160011P12126 (Service Bulletin No. A320-22-1461) is not embodied.

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

152729P12494 (Service Bulletin No. A320-22-1375) is not embodied.

(1) Models

321-111 321-112 321-131 321-211 321-212 321-213 321-231 321-232

(2) Effectivity by MSN

0364 0385 0412 0434 0458 0468 0473-0474 0477 0484 0488 0493-0495 0498 0502

0505 0509 0513-0522 0524 0526 0529 0532 0535 0538 0541 0544 0550 0552 0555

0557 0560 0563-0564 0567 0570 0576 0581 0583 0586 0591 0593 0595 0597 0599

0604 0606 0614 0620 0631 0633 0642 0652 0663-0664 0666 0668 0674-0675 0677

0680 0684 0687 0692 0699 0715 0725 0731 0746 0761 0765 0771 0775 0777 0781

0787 0792 0796 0802 0806 0808 0810-0811 0815 0819 0823 0827 0835 0841 0848

0852 0855 0864 0878 0887 0891 0901 0908 0915 0920 0926 0935 0940-0941 0954

0959 0961 0963 0968 0970 0974 0983 0987 0991 0993 0995 1004 1006 1008 1012

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1015 1017 1021 1023-1024 1027 1042 1045 1060 1080 1094 1133 1144 1153 1161

1174 1185 1188 1195 1199 1202 1204 1207 1214 1219-1220 1227 1233 1238 1241

1250 1260 1273 1276 1293 1299 1307 1356 1366 1399 1403 1408 1412 1417 1421

1425 1428 1431 1433 1436 1438 1442 1447 1451 1455 1458 1462 1465 1472 1476

1481 1487 1492 1496 1499 1503 1511 1517 1519 1521 1525 1531 1536 1539 1554

1572 1587 1596 1602 1607 1611 1614 1619 1623 1629 1632 1636 1638 1642 1651

1658 1666 1670 1675 1681 1690-1691 1695 1701 1704 1707 1711 1713 1716 1720

1724 1726 1734 1748 1763 1772 1776 1783 1788 1794 1798 1807 1811 1817 1836

1843 1848 1850 1859 1869 1878 1881 1887 1905 1921 1926 1928 1932 1941 1946

1950 1953 1956 1960 1966-1967 1970 1972 1974 1977-1978 1984 1988 1994-1995

2005 2021 2041 2045 2055 2060 2064 2067 2076 2080 2105 2107 2110 2115 2117

2190 2208 2211 2216 2220 2226 2234 2247 2255 2261 2267 2270 2290 2303 2305

2309 2315 2320 2323-2324 2330 2337 2342 2351 2357 2363 2381 2410 2462 2472

2476 2480 2488 2521 2530 2536 2543 2549 2553 2563 2590 2599 2610 2653 2682

2687 2707 2713 2726 2730 2736 2741 2756 2759 2767 2793 2799 2809 2823 2862

2868 2882 2895 2903 2912 2916 2919 2927 2933 2936 2957 2965 2971 2974 2996

2999 3005 3013 3015 3022 3034 3051 3067 3070 3075 3081 3098 3106 3112 3120

3126 3130 3146 3191 3198 3207 3212 3217 3222 3229 3233 3235 3241 3247 3249

3251 3254 3262 3265 3267 3274 3283 3290 3294 3297 3302 3307 3315 3322 3326

3329 3334 3339-3340 3350 3355 3360 3367 3369 3372 3382 3387 3397 3399 3401

3405 3419 3429 3434 3441 3458-3459 3462 3471 3493 3498 3504 3507 3512

3522-3523 3525 3527 3539 3546 3552 3557 3566 3573 3575 3583-3584 3587

3592-3593 3600 3612 3619 3623 3625 3629 3633 3636-3637 3639 3645 3653 3655

3665 3669 3673 3678 3681-3682 3688 3708 3712 3717 3722 3725 3730 3737-3738

3740 3749 3752 3761 3764 3766 3784 3792 3796 3806 3814 3816 3820 3830 3847

3858 3862 3864 3867 3869 3878-3879 3881 3884 3893 3899 3916 3920 3924 3926

3928 3930 3934 3936 3938 3940 3944 3948 3951 3955 3960 3964 3966 3969 3973

3977 3981 3987 3989 3993 3996 4002 4005 4009 4016 4022 4025 4031 4041

4044-4045 4047 4050 4054 4058 4062 4067 4073-4074 4078 4082 4085 4091 4096

4099 4103 4107 4112 4116 4123 4131 4134 4136 4138 4142 4148 4155 4173 4180

4184 4189 4194 4198 4209 4213 4217 4221 4224 4230 4251 4266 4271 4274 4277

4280 4283 4292 4299 4311 4315 4318 4334 4338 4341 4352 4358 4360 4369 4374

4377 4382 4387 4406 4416 4420 4430 4461 4467 4472 4494 4500 4530 4534 4538

4542 4545 4560 4570 4577 4585 4590 4607 4611 4617 4626 4638 4643 4648 4654

4662 4669 4672 4682 4698 4703 4706 4710 4719 4728 4731 4737 4746 4753 4761

4771 4779 4783 4788 4792 4811 4819 4824 4826 4830 4834 4838 4843 4847 4850

4856 4863 4873 4881 4885 4893 4898 4901 4916 4923 4925 4932 4935 4940 4945

4949 4957 4960 4962 4966 4971 4976 4994 5009 5025 5028 5035 5038 5044 5049

5054 5059 5065 5074 5077 5083 5087 5099 5118 5124 5126 5133 5154 5160 5164

5169 5173 5177 5180 5186 5192 5197 5199 5205 5210 5227 5233 5235 5237 5241

5244 5247 5251 5254 5257 5265 5269 5271 5275 5279 5282 5285 5287 5292 5297

5300 5303 5306 5309 5314 5317 5321 5328 5332 5336 5340 5343 5346 5350 5354

5357 5368 5374 5377 5382 5385 5388 5392 5402 5404 5409 5413 5418 5422 5427

5432 5435 5438 5444 5447 5450 5456 5459 5462 5465 5469 5475 5481 5485 5490

5495 5500 5504 5509 5513 5519 5523 5528 5534 5538 5543 5546 5549 5555 5558

5567 5573 5575 5582 5584 5588 5594 5603 5606 5633 5636 5644 5647 5655 5659

5663 5667 5670 5674 5681 5684 5689 5696 5699 5705 5709 5715 5720 5728 5733

5736 5743 5747 5751 5755 5763 5767 5774 5779 5790 5795 5800 5881 5890 5899

5913 5916 5919 5939 5958 5980 5994 6013 6027 6035 6049 6100 6104

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(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

AAF 0808 1006

AAR 0802 1174 1356 1511 1670 1734 2041 2110 2226 2247 2290 3297

4112 4142 5035 5169 5173 5287 5350 5382 5462 5500 5636 5767

5774

ABL 1227 1636 1970 2045

ACA 1602 1611 1623 1632 1638 1726 1748 1772 1783 1811

AEE 3462 3527 3820 3878

AFL 2330 2337 2342 2903 2912 2957 2965 3191 3267 3334 4058 4074

4099 4103 4116 4148 4461 4500 5044 5059 5271 5720 5755 5790

5881 5913

AFR 0498 0509 0521 0529 0544 0777 0796 1133 1299 1476 1658 1691

1859 3051 3098 3372 3399 3401 3419 3441 3814 3884 3930 4251

4901

AIC 3130 3146 3212 3326 3340 3367 3498 3557 3573 3619 3752 3792

3955 4002 4009 4078 4096 4138 4155 4280

AMU 0620 0631 0908 1850 1926 5459 5523

AUA 0552 0570 0581 0920 0935 1458

AWM 0765

AWW 0557 0597 2919 3302 3322

AZA 0434 0477 0488 0494 0495 0513 0514 0515 0516 0524 0526 0532

0576 0583 0586 0593 0599 0819 0848 0940 0959 1220

BAW 1690 1711 2190 2305 2320 2323 2324 2351 2363 2536 2653 2799

3081 3235 3254 3290 3512 3926

BER 1629 1966 1988 1994 2005 3708 3749 4334 4728 5038 5126 5133

BIE 0519 0827 0891

CCA 3307 3329 3523 3623 3653 3655 3665 3678 3722 3725 3766 3806

3940 3973 4022 4031 4062 4091 4131 4180 4221 4283 4318 4377

4472 4494 4538 4617 4719 4771 4834 4873 4949 5054 5124 5199

5265 5346 5432 5435 5573 5743 6013

CES 2309 2315 2543 2549 2882 2895 3233 3247 3249 3262 3471 3593

3612 3639 3682 3969 4045 4198 4209 4374 4638 4746 5192 5210

5227 5309 5402 5481 5519 5558 5575 5705

CIB 1607 5603

CSC 0550 0591 0878 0915 3583 3730 3893 3996 4420 4731 4824 4830

4856 4923 5160 5197 5233 5303 5543 5647 5670

CSN 1596 1614 1776 1788 1974 1995 2067 2080 2521 2530 2713 2741

2759 2767 2809 2936 2971 3067 3075 3112 3217 3241 3251 3459

3493 3507 3552 3566 3587 3645 3681 3764 3784 3847 3867 3920

3934 3938 3951 3981 4184 4189 4194 4217 4224 4230 4266 4271

4274 4292 4299 4338 4341 4369 4387 4416 4430 5237 5279 5534

5655 5736 5890 6049 6104

DKH 5674

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OPERATOR MSN

DLH 0412 0458 0468 0473 0474 0484 0493 0502 0505 0518 0560 0563

0564 0567 0595 0652 0692 0699 0887 0901 1080 1161 1188 1214

1260 1273 3265 3339 3360 3387 3434 3592 3625 3864 3936 3987

4005 4016 4047 4054 4073 4085 4360 4545 4560 4585 4607 4626

4672 4710 4753 4792 4819 4881 4916 4976 4994 5028 5049 5087

5186 5413

EIN 0926 1023 1094

EVA 5328 5354 5377 5485

FHY 0771 0855

FIN 0941 0961 1185 1241 1978 2208

G2X 0674

GFA 5025 5074 5180 5257 5321 5336

GZQ 1878

HDA 0633 0993 1024 1695 1984 2021 3369 3669

HRM 0517 0535 0642 0666

HVN 2255 2261 2267 2303 2974 3005 3013 3022 3198 3315 3355 3600

3737 3862 3964 3966 4136 4213 4277 4311 4315 4669 4703 4737

4783 4826 4863 4945 4971 5164 5241 5247 5251 5275 5297 5306

5340 5385 5392 5418 5438 5456 5469 5495 5555 5699 5709 5916

5958 5994

I2L 1004

IAW 4044 4067

IBE 1021 1027 1572 1681 1716 1836 2115 2220 2270 2357 2381 2472

2488 2563 2599 2736 2756 2996

IRM 1202

JST 1195 1408 3717 3899 3916 3948

KGL 0663 0668 0787 0852 0954 1060 1293 1554

KHV 2480 5343 5427

KKK 0604 0614 0675 0761 0823 0968 0974 1438 1451 1503 1950 1953

KZR 1042 1204 5357 5404

LLM 1956 1967

LMU 1366

MEA 1977 2055

MLM 5538

MLR 1946 3106

MON 0864 0983 1015 1045 1153 1207 1421 1428 1433 1707 1763 1794

1941 2105 2234 2730 2793 3546 3575 5582 5606

MSR 0680 0687 0715 0725

NKS 2476 2590

NLY 3504 3830 4611 4648

NVR 2211 2216 2410

NWS 1219 1233 1276 1843 2927 2933 3034 3120

OHY 0364 0385 0792 0806 0810 0811 0835 0963 0970 0995 1008

PAL 5715 5747

QTR 1487 1928 2107 3274 3397 3636 4173 4382 4406 4530

RCT 1017

RJA 3522 5099 5177

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OPERATOR MSN

RYW 3458

SAS 1587 1619 1642 1675 1798 1807 1817 1848

SBI 2064 2076 2726 3070

SVA 4467 4542 4577 4590 4811 4838 4925 4962 5009 5065 5285 5314

5447 5509 5549

SVR 0775 0815 0841 0991 1012 1199 1720 1905 2117 2707

SWR 0520 0522 0541 0664 0987 1144 4534 5567

TAI 2553 2610 2687 2862 3869

TAM 3222 3229 3294 3761 3816 4352 4358 4570 4662 5528

TAP 1307 1399 1713

TCX 0677 1238 1250 2060

THY 2823 2868 2916 2999 3015 3126 3207 3283 3350 3382 3405 3429

3525 3539 3637 3673 3688 3738 4643 4654 4682 4698 4706 4761

4779 4788 5077 5083 5118 5154 5205 5254 5388 5450 5465 5490

5546 5584 5633 5663 5667 5689

TNA 0538 0555 0606 0731 0746

USA 1403 1412 1417 1425 1431 1436 1442 1447 1455 1462 1465 1472

1481 1492 1496 1499 1517 1519 1521 1525 1531 1536 1539 1651

1666 1701 1704 1724 3584 3629 3633 3712 3740 3796 3858 3879

3881 3924 3928 3944 3960 3977 3989 3993 4025 4041 4050 4082

4107 4123 4134 4843 4847 4850 4885 4893 4898 4932 4935 4940

4957 4960 4966 5235 5244 5269 5282 5292 5300 5317 5332 5368

5374 5409 5422 5444 5475 5504 5513 5588 5594 5644 5659 5684

5696 5728 5751 5763 5795 5800 5899 5939 5980 6027 6035 6100

UTA 5681 5733 5779 5919

VKG 1881 1887 1921 1932 1960 1972

WRC 0684 0781 1869 2462 2682

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(4) Configuration by MSN

MSN CONFIGURATION

0364 0385 0412 0434 0458 0468 0473 0474 0477 0484 0488

0493 0494 0495 0498 0502 0505 0509 0513 0514 0515 0516

0517 0518 0519 0520 0521 0522 0524 0526 0529 0532 0535

0538 0541 0544 0550 0552 0555 0557 0560 0563 0564 0567

0570 0576 0581 0583 0586 0591 0593 0595 0597 0599 0604

0606 0614 0620 0631 0633 0642 0652 0663 0664 0666 0668

0674 0675 0677 0680 0684 0687 0692 0699 0715 0725 0731

0746 0761 0765 0771 0775 0777 0781 0787 0792 0796 0802

0806 0808 0810 0811 0815 0819 0823 0827 0835 0841 0848

0852 0855 0864 0878 0887 0891 0901 0908 0915 0920 0926

0935 0940 0941 0954 0959 0961 0963 0968 0970 0974 0983

0987 0991 0993 0995 1004 1006 1008 1012 1015 1017 1021

1023 1024 1027 1042 1045 1060 1080 1094 1133 1144 1153

1161 1174 1185 1188 1195 1199 1202 1204 1207 1214 1219

1220 1227 1233 1238 1241 1250 1260 1273 1276 1293 1299

1307 1356 1366 1399 1403 1408 1412 1417 1421 1425 1428

1431 1433 1436 1438 1442 1447 1451 1455 1458 1462 1465

1472 1476 1481 1487 1492 1496 1499 1503 1511 1517 1519

1521 1525 1531 1536 1539 1554 1572 1587 1596 1602 1607

1611 1614 1619 1623 1629 1632 1636 1638 1642 1651 1658

1666 1670 1675 1681 1690 1691 1695 1701 1704 1707 1711

1713 1716 1720 1724 1726 1734 1748 1763 1772 1776 1783

1788 1794 1798 1807 1811 1817 1836 1843 1848 1850 1859

1869 1878 1881 1887 1905 1921 1926 1928 1932 1941 1946

1950 1953 1956 1960 1966 1967 1970 1972 1974 1977 1978

1984 1988 1994 1995 2005 2021 2041 2045 2055 2060 2064

2067 2076 2080 2105 2107 2110 2115 2117 2190 2208 2211

2216 2220 2226 2234 2247 2255 2261 2267 2270 2290 2303

2305 2309 2315 2320 2323 2324 2330 2337 2342 2351 2357

2363 2381 2410 2462 2472 2476 2480 2488 2521 2530 2536

2543 2549 2553 2563 2590 2599 2610 2653 2682 2687 2707

2713 2726 2730 2736 2741 2756 2759 2767 2793 2799 2809

2823 2862 2868 2882 2895 2903 2912 2916 2919 2927 2933

2936 2957 2965 2971 2974 2996 2999 3005 3013 3015 3022

3034 3051 3067 3070 3075 3081 3098 3106 3112 3120 3126

3130 3146 3191 3198 3207 3212 3217 3222 3229 3233 3235

3241 3247 3249 3251 3254 3262 3265 3267 3274 3283 3290

3294 3297 3302 3307 3315 3322 3326 3329 3334 3339 3340

3350 3355 3360 3367 3369 3372 3382 3387 3397 3399 3401

3405 3419 3429 3434 3441 3458 3459 3462 3471 3493 3498

3504 3507 3512 3522 3523 3525 3527 3539 3546 3552 3557

3566 3573 3575 3583 3584 3587 3592 3593 3600 3612 3619

3623 3625 3629 3633 3636 3637 3639 3645 3653 3655 3665

3669 3673 3678 3681 3682 3688 3708 3712 3717 3722 3725

3730 3737 3738 3740 3749 3752 3761 3764 3766 3784 3792

3796 3806 3814 3816 3820 3830 3847 3858 3862 3864 3867

3869 3878 3879 3881 3884 3893 3899 3916 3920 3924 3926

3928 3930 3934 3936 3938 3940 3944 3948 3951 3955 3960

3964 3966 3969 3973 3977 3981 3987 3989 3993 3996 4002

001

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MSN CONFIGURATION

4005 4009 4016 4022 4025 4031 4041 4044 4045 4047 4050

4054 4058 4062 4067 4073 4074 4078 4082 4085 4091 4096

4099 4103 4107 4112 4116 4123 4131 4134 4136 4138 4142

4148 4155 4173 4180 4184 4189 4194 4198 4209 4213 4217

4221 4224 4230 4251 4266 4271 4274 4277 4280 4283 4292

4299 4311 4315 4318 4334 4338 4341 4352 4358 4360 4369

4374 4377 4382 4387 4406 4416 4420 4430 4461 4467 4472

4494 4500 4530 4534 4538 4542 4545 4560 4570 4577 4585

4590 4607 4611 4617 4626 4638 4643 4648 4654 4662 4669

4672 4682 4698 4703 4706 4710 4719 4728 4731 4737 4746

4753 4761 4771 4779 4783 4788 4792 4811 4819 4824 4826

4830 4834 4838 4843 4847 4850 4856 4863 4873 4881 4885

4893 4898 4901 4916 4923 4925 4932 4935 4940 4945 4949

4957 4960 4962 4966 4971 4976 4994 5009 5025 5028 5035

5038 5044 5049 5054 5059 5065 5074 5077 5083 5087 5099

5118 5124 5126 5133 5154 5160 5164 5169 5173 5177 5180

5186 5192 5197 5199 5205 5210 5227 5233 5235 5237 5241

5244 5247 5251 5254 5257 5265 5269 5271 5275 5279 5282

5285 5287 5292 5297 5300 5303 5306 5309 5314 5317 5321

5328 5332 5336 5340 5343 5346 5350 5354 5357 5368 5374

5377 5382 5385 5388 5392 5402 5404 5409 5413 5418 5422

5427 5432 5435 5438 5444 5447 5450 5456 5459 5462 5465

5469 5475 5481 5485 5490 5495 5500 5504 5509 5513 5519

5523 5528 5534 5538 5543 5546 5549 5555 5558 5567 5573

5575 5582 5584 5588 5594 5603 5606 5633 5636 5644 5647

5655 5659 5663 5667 5670 5674 5681 5684 5689 5696 5699

5705 5709 5715 5720 5728 5733 5736 5743 5747 5751 5755

5763 5767 5774 5779 5790 5795 5800 5881 5890 5899 5913

5916 5919 5939 5958 5980 5994 6013 6027 6035 6049 6100

6104

001

(5) Configuration definition

**CONF 001

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

standard configuration.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Equipment BFEA01 1

B. CONCURRENT REQUIREMENTS

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

the following Service Bulletin as per effectivity specified in this Service Bulletin:

Service Bulletin No. A320-22-1278

NOTE: Service Bulletin No. A320-22-1278 (AUTO FLIGHT - FAC (FLIGHT

AUGMENTATION COMPUTER) - INTRODUCE FAC SOFTWARE

STANDARD BAM0620) applies Modification No. 38777P10777.

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C. REASON

(1) History

Since Flight Augmentation Computer (FAC) Standard CAA01 is not valid anymore for

A321 aircraft, it is needed to propose a way to install FAC Standard CAA02 on A321

aircraft by replacing FAC Standard B0620.

(2) Objective/Action

This Service Bulletin recommends replacing FAC Standard CAA02 in place of FAC

Standard B0620 for A321 aircraft while providing dataloading capacity and improved

performance. The new FAC CAA02 includes two main software improvements: Runway

Overrun Prevention System (ROPS) and Sharklets capability.

(3) Advantages

Accomplishment of this Service Bulletin allows the following improvements on FAC

hardware:

- improve Central Processing Unit (CPU) and memory margins (to match end of life

requirements),

- cover component obsolescence (at least 5 years after certification),

- increase reliability,

- reduce weight and power consumption,

- introduce dataloading capacity.

The FAC software evolutions in comparison with Standard B0620 are as follows:

1. Sharklets capability: FAC CAA02 standard introduces software adaptation for

A321/CFM/IAE equipped with Sharklets (weight and CG, characteristic speeds). These

tunings are activated by pin-program AE-08G.

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

consumption of Sharklets installations.

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

to take into account the Sharklets aerodynamic impact.

2. Introduction of ROPS function:

FAC CAA02 includes the software modifications necessary to perform the ROPS

function:

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

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

triggers aural alerts and PFD messages requiring either to perform a Go Around or

to apply the maximum braking. On FAC CAA02, this function is activated by a

dedicated pin program AB-06C.

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Moreover, FAC CAA02 includes 2 adaptations of the ROPS functions:

- Compatibility with both Terrain Awareness and Warning System (TAWS) equipment:

EGPWS and T3CAS.

- For A321 aircraft, modifications for compatibility with ABS Brakes and restoration of

nominal tunings for Messier Bugatti brakes. MB brakes tunings will be activated

through a dedicated pin program (AA-02B).

3. Other modifications:

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

occurring in case of short power supply cut.

- Reduction of the Rudder Travel Limitation at high speed (new control law called

Rudder Travel Limitation Unit (RTLU*)). RTLU* control law aims at reducing Vertical

Tail Plane (VTP) loads in case of inadequate and inappropriate use of the rudder

pedals in flight.

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

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

modification can be activated by pin program AE-08J and requires FWC standard

H2F7.

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

computation using the CG position computed from Multifunction Control and Display

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

the new "Pitch trim MCDU CG disagree" alert. This function requires FWC standard

H2F6.

- Correction of Flight Guidance/Flight Augmentation Computer (FG/FAC) interface

issue affecting weight computation in FMS Landing System (FLS).

- Addition of a Post Flight Report (PFR) message in case of failure affecting

Autopilot/Flight Director (AP/FD) TCAS function (function introduced with FG C13

and I12).

- Other minor modifications without functional impact (FAC not healthy upon negative

total True Air Temperature Correction of loss of flight plan upon Landing Gear

Control and Interface Unit (LGCIU) Nose wheel failure, etc.).

(4) Operational/Maintenance Consequences

For full improvements description, refer to the Modification Operational Impact (MOI) No.

155488.

The operational consequence of this Service Bulletin is the Flight Crew Operating

Manual (FCOM) update.

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

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Task 221454-831-801-001: Modification of the two FACs (FINs 1CC1 and 1CC2).

(1) Replace the two FACs (FINs 1CC1 and 1CC2), in the Electronics Rack 80VU.

(2) Install the Media-Disk (FIN 1CCMD1) in the Cockpit, in the stowage box.

E. COMPLIANCE

(1) Classification

RECOMMENDED: Service Bulletin recommended to be accomplished to prevent

significant operational disruptions.

(2) Accomplishment Timescale

Accomplishment of this Service Bulletin is recommended at the earliest opportunity

where manpower and facilities are available.

F. APPROVAL

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

Organization Approval No. EASA.21J.031.

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

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

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

before incorporation of the Service Bulletin.

G. MANPOWER

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

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

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

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

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

included.

For an explanation of the manhours and elapsed time, refer to the Gantt Chart given in

Appendix 01 - Elapsed Time Assumption.

Task 221454-831-801-001: Modification of the two FACs (FINs 1CC1 and 1CC2).

Get Access 0.50

On Aircraft

Replace the two FACs (FINs 1CC1 and 1CC2), in the

Electronics Rack 80VU.

1.00

Install the Media-Disk (FIN 1CCMD1) in the Cockpit, in

the stowage box.

0.50

Tests 0.50

Close-Up 0.50

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.50

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H. WEIGHT AND BALANCE

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

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

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

Manufacturers Empty Weight -3.400 KG (-7.496 LB)

Effect on Balance -31.827 KGM (-230.205 LB.FT )

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-41-52 12-34-24 22-66-00

22-66-34 31-32-00 52-10-00

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Service Bulletin (SB) A320-22-1278

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

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 22-64-00

Aircraft Wiring List (AWL)

Flight Crew Operating Manual (FCOM)

Illustrated Parts Catalog (IPC) 22-66-34 22-67-08

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

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

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

SEDOR4 - AIRBUS Customer Services Technical Data

Fax No.: (33) 5 61 93 28 06

E-mail: sb.reporting@airbus.com

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

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

- The Maintenance & Engineering Community, in:

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

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

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

our Customer Services Aircraft In-Service Data (SEDOR4).

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L. INTERCHANGEABILITY/MIXABILITY

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

FAC B397BAM0620 C13206AA00 03 NO (1) (2) (3)

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Only the mixability configuration(s) and condition(s) stated in this Service

Bulletin are approved.

NOTE (1): Interchangeability conditions:

- When the old PN B397BAM0620 is removed, it can be replaced by:

. the old PN B397BAM0620,

. or the new PN C13206AA00, with LRU IDENT C13206AA02 as a

set.

- When the new PN C13206AA00 with LRU IDENT C13206AA02 is

removed, it can only be replaced by the new PN C13206AA00 with LRU

IDENT C13206AA02.

NOTE (2): Mixability conditions:

- FAC CAA02 is not mixable with FAC B0620,

- FAC CAA02 is mixable with FAC B0623 under the condition that ROPS

function is not activated on aircraft (ROPS is not implemented in FAC

B0623),

- FAC CAA02 is mixable with FAC B0621 on aircraft equipped with Wing

Tip Fence under the condition that ROPS function is not activated on

aircraft.

NOTE (3): FAC PN C13206AA00 loaded with software PN C13206AA01 is not certified

on A321 aircraft.

M. SPARES

FAC B397BAM0620

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2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Vendor parts are to be procured from:

Equipment BFEA01 THALES AVIONICS SAS

105 Avenue du General Eisenhower

BP 63647

31036 TOULOUSE CEDEX 1

FRANCE

Attn: Retrofit Manager

Telephone: +33 (0)5 61 19 76 95

Fax: +33 (0)5 61 19 68 20

e-mail: retrofit@fr.thalesgroup.com

(2) Price and Availability

No AIRBUS kit will be provided.

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

B. INDUSTRY SUPPORT INFORMATION

Industry support terms for the equipment must be negotiated with the equipment supplier.

C. LIST OF COMPONENTS

No Kit

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

None

(2) Components

None

(3) Equipment

Equipment BFEA01

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

NOTES

C13206AA00 2 FAC B397BAM0620 03 (1)

F1422927 1 MEDIA

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

Common Support Data Dictionary (CSDD), Chapter 2.

NOTE: Operators shall order FAC Hardware PN C13206AA00 already loaded

with Software PN G2856AAA02.

NOTE (1): The above list of components is not an AIRBUS Kit, the required parts

must be ordered as necessary through the given channel.

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

None

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3. ACCOMPLISHMENT INSTRUCTIONS

Task 221454-831-801-001 - Modification of the two FACs (FINs 1CC1 and 1CC2).

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

INCLUDED IN THE REFERENCED PROCEDURES.

CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY

AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE

WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,

COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO

THIS:

- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.

NOTE: The airbus accomplishment instructions of this Service Bulletin refer to procedures

included in other AIRBUS documents. When the words "refer to" are used and the

operator has an accepted alternative procedure, the accepted alternative procedure

can be used. Then the words "in accordance with" are included in the instruction,

the procedure in the AIRBUS document must be used.

NOTE: The access and close-up instructions, not comprising return to service tests, in this

Service Bulletin do not constitute or affect the technical intent of the Service

Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or

close-up steps to add flexibility to their maintenance operations as long as the

technical intent of the Service Bulletin is met within the set parameters.

NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.

Refer to paragraph 1.J., References, for the definition of acronyms.

NOTE: The fact that the FAC becomes data-loadable implies a modification of PN:

- Current situation: one PN (FINs 1CC1 and 1CC2) for hardware and software,

- With data loading: one PN (FINs 1CC1 and 1CC2) for hardware, one PN (FINs

1CC1SW1 and 1CC2SW1) for software and one PN (FIN 1CCMD1) for Media

Disk.

Task Associated Data

Zone

120 210

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Modified FIN

1CC1 1CC1SW1 1CC2 1CC2SW1 1CCMD1

Access

Door 824 831 841

Manpower

TOTAL MANHOURS 3.00

ELAPSED TIME (HOURS) 2.50

A. GENERAL

(1) Subtask 221454-839-001-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

B. PREPARATION

(1) Subtask 221454-941-001-001 - Job Set-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

Task 12-34-24-869-002

Task 22-66-34-000-002

Task 52-10-00-010-001

(a) The following items shall be considered as the basic Aircraft configuration before

you start a maintenance task:

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

wheel chocks are in position on the landing gear).

- Engine shut down, thrust reversers closed and locked.

- Aircraft in clean configuration.

- Parking brake applied.

- Aircraft electrical network de-energized.

- Hydraulic systems depressurized.

- Access to the cockpit and cabin is available.

- All circuit breakers are in closed position.

- All controls in NORM, AUTO or OFF position.

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

12-34-24-869-002.

(c) Put the access platform(s) in position at the FWD passenger/crew door(s) 831 or

841.

(d) Open the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-52, Page

Block 001 and AMM Task 52-10-00-010-001.

(e) Do the Job Set-up procedure as specified in the removal of the two FACs (FINs

1CC1 and 1CC2), refer to AMM Task 22-66-34-000-002.

C. PROCEDURE

(1) Subtask 221454-960-001-001 - Replace the two FACs (FINs 1CC1 and 1CC2), in the

Electronics Rack 80VU.

Work Zones and Access Panels

Zone Access/Work location

120 Access Door 824

Work location Electrical panel 80VU

Manpower Resources

Manhours 1.00

Minimum number of person 1

Subtask elapsed time 1.00

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

C13206AA00 2 FAC (1)

NOTE: Operators shall order FAC Hardware PN C13206AA00 already loaded

with Software PN G2856AAA02.

NOTE (1): The above list of components is not an AIRBUS Kit, the required parts

must be ordered as necessary through the given channel.

References

Aircraft Maintenance Manual (AMM) Task 22-66-34-000-002

Task 22-66-34-400-002

(a) Remove:

Refer to AMM Task 22-66-34-000-002

FIN 1CC1

1 FAC B397BAM0620

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and

FIN 1CC2

1 FAC B397BAM0620

(b) Install:

Refer to AMM Task 22-66-34-400-002

FIN 1CC1

1 FAC C13206AA00

and

FIN 1CC2

1 FAC C13206AA00

NOTE: The Hardware PN C13206AA00 (FINs 1CC1 and 1CC2) must

be loaded with Software PN G2856AAA02 (FINs 1CC1SW1 and

1CC2SW1).

(2) Subtask 221454-470-002-001 - Install the Media-Disk (FIN 1CCMD1) in the Cockpit,

in the stowage box.

Work Zones and Access Panels

Zone Access/Work location

210 Access Door 831, Door 841

Manpower Resources

Manhours 0.50

Minimum number of person 1

Subtask elapsed time 0.50

Skills NON SPECIFIC

Material necessary to do the job

Equipment BFEA01

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

F1422927 1 MEDIA

NOTE: Operators shall order FAC Hardware PN C13206AA00 already loaded

with Software PN G2856AAA02.

References

Fig. A-FBBAA

Location of the Media-Disk

Sheet 01

Fig. A-FBCAA

Location of the Media-Disk

Sheet 01

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

Refer to Fig. A-FBBAA or Fig. A-FBCAA

1 Install:

FIN 1CCMD1

1 Software-Media FAC F1422927

NOTE: The disk FIN 1CCMD1 contains the software PN G2856AAA02

(FINs 1CC1SW1 and 1CC2SW1).

D. TEST

(1) Subtask 221454-700-002-001 - Test

Manpower Resources

Skills NON SPECIFIC

References

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

Task 22-66-34-400-002

Task 31-32-00-860-001

(a) Job set-up:

1 Remove the safety clips and/or tags and close/unlock the circuit breakers as

specified after the installation of the two FACs (FINs 1CC1 and 1CC2), refer to

AMM Task 22-66-34-400-002.

(b) Procedure:

1 Do the test procedure as specified after the installation of the two FACs (FINs

1CC1 and 1CC2), refer to AMM Task 22-66-34-400-002.

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

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

NOTE: If the AMM Task reference is not available in the operator’s last

AMM issue, do these steps:

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

LRU IDENTIFICATION.

Do the procedure to get access to the SYSTEM REPORT/TEST Menu Page,

refer to AMM Task 31-32-00-860-001.

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

REVISION No.: 00 - Feb 12/14 Page: 19

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ACTION RESULT

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

- FAC1 (2) is ON

- No ECAM message related to FAC1 (2) is

shown

- FAULT indication is not shown on the

pushbutton switch 12CC1 (2) on the panels

23VU (24VU).

2. On the MCDU:

- Push the line key adjacent to the AFS indication.

On the MCDU:

- The AFS menu page comes into view.

3. Push the line key adjacent to the LRU

IDENTIFICATION indication.

- The LRU IDENTIFICATION page comes into

view.

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

the LRU IDENTIFICATION page is C13206AA02.

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

NOTE: A fictive PN C13206AA02 is created to represent the complete

computer (hardware C13206AA00 and software G2856AA02).

It is the one that is indicated to the crew or to the maintenance

team when they perform a LRU IDENTIFICATION.

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

A/C Config Report:

ACTION RESULT

1. On the MCDU:

- Push the line key adjacent to the CFDS

indication.

- Push the NEXT key.

- Push the AVIONICS CONFIG REPORT key.

- Push the START key.

- Push the line key adjacent to the FAC.

On the MCDU:

- The CFDS menu page comes into view.

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

same as the PN on the media disk.

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

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

PORTABLE (Refer to the portable data-loader user-guide).

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

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4 If a Portable Data Loader (PDL) is used, remove the PDL as follows:

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

<1> Disconnect the cable from the PORTABLE DATA LOADER

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

SYSTEMS data loader connector (2TD).

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

fasteners.

5 Close-up:

a Put the aircraft back to its initial configuration.

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

until the CFDS MENU page comes into view.

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

E. CLOSE-UP

(1) Subtask 221454-942-001-001 - Close-up

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001

Task 22-66-34-400-002

Task 52-10-00-410-001

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

equipment.

(b) Do the close-up procedure as specified in the installation of the two FACs (FINs

1CC1 and 1CC2), refer to AMM Task 22-66-34-400-002.

(c) Close the FWD passenger/crew door(s) 831 or 841, refer to AMM 06-41-52, Page

Block 001 and AMM Task 52-10-00-410-001.

(d) Remove the access platform(s).

(e) Remove the system and the aircraft to normal operating condition.

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

REVISION No.: 00 - Feb 12/14 Page: 21

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**CONF ALL

A

80VU

1CC2

1CC1

FR1

Z120

FR24A

A

N_SB_221454_5_BAAA_01_01

Figure A-FBAAA - Sheet 01

Location of the two FACs

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

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**CONF ALL

A A

A

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

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

1CCMD1

N_SB_221454_5_BBAA_01_00

Figure A-FBBAA - Sheet 01

Location of the Media-Disk

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

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

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**CONF ALL

C

B

C

NOTE:

THE LOCATION OF THE STOWAGE BOX DEPENDS

ON AIRCRAFT CONFIGURATION (SEE FIG. A−FBBAA)

1CCMD1

A

B

Z210

FR24

FR1

A

N_SB_221454_5_BCAA_01_00

Figure A-FBCAA - Sheet 01

Location of the Media-Disk

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

REVISION No.: 00 - Feb 12/14 Page: 24

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Appendix 01 - Elapsed Time Assumption.

**CONF ALL

(1) The following Gantt Chart is only a proposal. Operators may determine that another way to do the

work is more suitable for them.

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

REVISION No.: 00 - Feb 12/14 Page: 1

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Appendix 01 - Elapsed Time Assumption.

**CONF ALL

ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320−22−1454

GET ACCESS

MH ET/S

TOTAL MANHOURS

SB ELAPSED TIME

3.00

2.50

STEPS

0.50 0.50

0

REPLACE THE TWO FACS 1.00 1.00

INSTALL THE MEDIA−DISK 0.50 0.50

TEST 0.50 0.50

CLOSE−UP 0.50 0.50

MH

ET/S:

PER

MANHOURS

ELAPSED TIME PER STEP

NUMBER OF PERSONS

01

02

THIS CHART IS ONLY A PROPOSAL

OPERATORS MAY DETERMINE THAT ANOTHER WAY

TO DO THE WORK IS MORE SUITABLE FOR THEM

01

02

NOTE:

PER

1

1

1

1

1

:

:

SB ELAPSED TIME

(HOURS)

1 2

IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS

ARE NOT REFLECTED IN THIS GANTT CHART

(FINS 1CC1 AND 1CC2)

(FIN 1CCMD1)

N_SB_221454_5_AAAA_01_00

Figure A-FAAAA - Sheet 01

Gantt Chart

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

REVISION No.: 00 - Feb 12/14 Page: 2

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REPORTING SHEET

TITLE: AUTO-FLIGHT - FAC - INSTALL STANDARD FAC CAA02 (SHARKLETS

AND ROPS PROJECT) ON A321 AIRCRAFT

MODIFICATION No.: 155488P13834

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: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

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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: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454

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