# @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:

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN SUMMARY 1. Sharklets capability: FAC CAA02 standard introduces software adaptation for A321/CFM/IAEequipped 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 REVISION No.: 00 - Feb 12/14 Page: 2 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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
DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 3 5

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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 4 5

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

**CONF ALL



## A 80VU 1CC2 1CC1 FR1 Z120 FR24A 

### A

N_SB_221454_5_SAAA_01_01 Figure A-FSAAA - Sheet 01

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 5 5

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

**CONF ALL



### A **A**



## A **NOTE:** THE LOCATION OF THE STOWAGE BOX DEPENDS ON AIRCRAFT CONFIGURATION (SEE FIG. A−FSCAA). 1CCMD1

N_SB_221454_5_SBAA_01_00 Figure A-FSBAA - Sheet 01

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 6 5

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# @A318/A319/A320/A321 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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 7 5

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

This Page Intentionally Left Blank

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# @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: 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 DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 1 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 2 5

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# @A318/A319/A320/A321 SERVICE BULLETIN (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
DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 3 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 4 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 5 5

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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 6 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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. DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 7 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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.
DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 8 5

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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 9 5

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# @A318/A319/A320/A321 SERVICE BULLETIN 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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 10 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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 priorto 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).

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 11 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 12 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 13 5

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# @A318/A319/A320/A321 SERVICE BULLETIN
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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 14 5

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

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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# @A318/A319/A320/A321 SERVICE BULLETIN (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
DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 17 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 18 5

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

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 REVISION No.: 00 - Feb 12/14 Page: 20 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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 5

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# @A318/A319/A320/A321 SERVICE BULLETIN

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

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

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

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# @A318/A319/A320/A321 SERVICE BULLETIN 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) 2 1

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 5

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

# @A318/A319/A320/A321 SERVICE BULLETIN 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 REVISION No.: 00 - Feb 12/14 Page: 1 5

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

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

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

DATE: Feb 12/14 SERVICE BULLETIN No.: A320-22-1454 REVISION No.: 00 - Feb 12/14 Page: 1 5

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