Title: Nacelle & Pylon - Aft Movable Fairing - Rib 5 Redesign

@A318/A319/A320/A321
SERVICE BULLETIN
REVISION TRANSMITTAL SHEET
AIRBUS
CUSTOMER SERVICES DIRECTORATE
1 Rond Point Maurice Bellonte
31707 BLAGNAC CEDEX
FRANCE
Tel : (33) 5 61 93 33 33
Telex : AIRBU 530526F
Fax : (33) 5 61 93 42 51
ATA SYSTEM: 54
TITLE: NACELLE & PYLON - AFT MOVABLE FAIRING - RIB 5 REDESIGN

MODIFICATION No.: 155560P13625
This page transmits Revision No.01 of Service Bulletin No.A320-54-1028
ADDITIONAL WORK
**CONF ALL
No additional work is required by this revision for aircraft modified by any previous issue.
REASON
Revision No. 01 issued to update the procedure further to the validation of this Service Bulletin.
CHANGES
The main changes of this revision are:
- Effectivity updated
- Manpower paragraph and Gantt Chart updated
- Procurement addresses updated
- Consumable CMLA01 updated
- Component COMPA01 added
- Component COMPA02 added
- Accomplishment Instructions paragraph updated
- Minor changes applied
SUMMARY
REASON/DESCRIPTION/OPERATIONAL REASON UPDATED R
CONSEQUENCES
GENERAL EVALUATION GENERAL EVALUATION TABLE UPDATED R
MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE R
UPDATED
5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028
REVISION No.: 01 - Oct 23/15 Page: 1
Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

@A318/A319/A320/A321
SERVICE BULLETIN
MATERIAL PRICE INFORMATION TABLE R

UPDATED
UPDATED
UPDATED
UPDATED
EFFECTIVITY OPERATOR LIST UPDATED R
REFERENCES / REPERCUSSIONS REFERENCES/REPERCUSSIONS TABLE R
UPDATED
MANPOWER MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
APPENDICES APPENDICES UPDATED R
PLANNING INFORMATION
EFFECTIVITY EFFECTIVITY RELATED INFORMATION R
UPDATED
Configuration definition
CONF 001 CONFIGURATION DEFINITION UPDATED R
CONFIGURATION DESCRIPTION UPDATED
CONFIGURATION DESCRIPTION UPDATED
Material Effectivity MATERIAL EFFECTIVITY UPDATED R
MATERIAL SET UPDATED
MATERIAL SET QUANTITY UPDATED
MATERIAL EFFECTIVITY UPDATED R
MATERIAL EFFECTIVITY UPDATED R
REASON
Objective/Action OBJECTIVE/ACTION UPDATED R
MANPOWER MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
MANPOWER UPDATED R
REFERENCES REFERENCED DOCUMENTATION UPDATED R
REFERENCED DOCUMENTATION UPDATED R

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SERVICE BULLETIN
MATERIAL INFORMATION
MATERIAL - PRICE AND AVAILABILITY
Procurement Addresses PROCUREMENT ADDRESSES UPDATED R
Price and Availability PRICE AND AVAILABILITY UPDATED R
MATERIAL PRICE UPDATED
INDUSTRY SUPPORT INFORMATION INDUSTRY SUPPORT INFORMATION UPDATED R
LIST OF COMPONENTS
Kit 541028A01R06 PART MATERIAL SET UPDATED R
MATERIAL SET LABEL UPDATED
QUANTITY UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
KEYWORD UPDATED
QUANTITY UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
KEYWORD UPDATED
QUANTITY UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
KEYWORD UPDATED
QUANTITY UPDATED
ITEM NUMBER UPDATED
PART NUMBER UPDATED
KEYWORD UPDATED
LIST OF MATERIALS - OPERATOR
SUPPLIED
Consumable Materials
Consumable CMLA01 CONSUMABLE MATERIAL SET UPDATED R
QUANTITY UPDATED
CONSUMABLE UPDATED
Components COMPONENTS UPDATED R
Component COMPA01 PART MATERIAL SET ADDED N
Component COMPA02 PART MATERIAL SET ADDED N
PARTS TO BE RE-IDENTIFIED BY
OPERATOR
Reidentified part set REIDA04 PART MATERIAL SET UPDATED R
QUANTITY UPDATED
ACCOMPLISHMENT INSTRUCTIONS
TASK 541028- 831-801-001-Modification TASK SOLUTION UPDATED R
NOTE UPDATED

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SERVICE BULLETIN
Task associated data - 001 PANEL UPDATED R

ELAPSED TIME UPDATED
Subtask 541028-910-001-001 SUBTASK SOLUTION UPDATED R
REFERENCED DOCUMENTATION UPDATED
REFERENCES UPDATED
REFERENCES UPDATED
REFERENCES UPDATED
REFERENCES UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED

@A318/A319/A320/A321
SERVICE BULLETIN

NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
Subtask 541028-831-005-001 SUBTASK SOLUTION ADDED N
Subtask 541028-831-001-001 SUBTASK SOLUTION DELETED FOR D
APPLICABLE MSN
APPLICABLE MSN
APPLICABLE MSN
APPLICABLE MSN

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SERVICE BULLETIN

APPLICABLE MSN
APPLICABLE MSN
APPLICABLE MSN
APPLICABLE MSN
APPLICABLE MSN
APPLICABLE MSN
NOTE UPDATED
ZONE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED

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NOTE UPDATED
ZONE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
ZONE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
ZONE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
NOTE UPDATED
ZONE UPDATED
REFERENCES UPDATED
NOTE UPDATED
REFERENCES UPDATED
Fig. A-FBBAB FIGURE SOLUTION UPDATED R
Fig. A-FBBAB Sheet 03 SHEET DELETED D
Fig. A-FBCAA
Fig. A-FBCAA Sheet 01 SHEET UPDATED R
Fig. A-FBCAA Sheet 04 SHEET UPDATED R
Fig. A-FBCAB
Fig. A-FBCAB Sheet 04 SHEET UPDATED R
Fig. A-FBFAA FIGURE SOLUTION ADDED N
Fig. A-FBFAA Sheet 01 SHEET ADDED N
Fig. A-FBFAB FIGURE SOLUTION ADDED N
Fig. A-FBFAB Sheet 01 SHEET ADDED N

@A318/A319/A320/A321
SERVICE BULLETIN
Appendix 01 - Elapsed Time Assumption

APPENDIX CONTENT APPENDIX CONTENT UPDATED R
Fig. A-FAAAA
Fig. A-FAAAA Sheet 01 SHEET UPDATED R
FILLING INSTRUCTIONS
This Service Bulletin has been generated electronically and is reissued as a complete document.
Replace the complete document.
Put this Revision Transmittal Sheet in front of the Service Bulletin.
HISTORY OF PREVIOUS REVISIONS
No previous revision
REVISION SEQUENCE
ORIGINAL: Nov 25/14
REVISION No. : 01 - Oct 23/15

@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
AIRBUS
31707 BLAGNAC CEDEX
FRANCE
Tel : (33) 5 61 93 33 33
Fax : (33) 5 61 93 42 51
This summary is for information only and is not approved for modification of the aircraft.
ATA SYSTEM: 54

**CONF ALL
MODIFICATIONS
MODIFICATION CLASSIFICATION
MAJOR 155560P13625
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
Several pylon aft movable fairing Rib 5 have been found cracked or with loose fasteners during
maintenance inspections and recently, one pylon aft movable fairing tail cone was reported missing
after operation.
This Service Bulletin recommends to install new redesigned Rib 5 in order to prevent further cracks on
Rib 5 and to introduce additional fasteners to prevent tail cone loss.
Accomplishment of this Service Bulletin will improve the structural integrity of the pylon aft movable
fairing.
Accomplishment of Service Bulletin No. A320-54-1028 cancels inspection requirement of aft movable
fairing Rib 5 and fasteners as per Service Bulletin No. A320-54-1026.
GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB YES
POTENTIAL AD NO A/C OPERATION AFFECTED NO
RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO
COST SAVING NO ETOPS AFFECTED NO
STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO
VALIDATION ON AIRCRAFT YES BOOKLET AVAILABLE YES

@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational

disruptions.
NOTE: This Service Bulletin has been validated at original issue on A320 aircraft with
Manufacturer Serial Number (MSN) 2945.
NOTE: A booklet including photographs taken during the validation of this Service Bulletin is
available on AIRBUS|World - Maintenance and Engineering - AirN@v engineering (in
the concerned SB file).
MATERIAL PRICE INFORMATION
**CONF 001
MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER PRICE PER MAIN PARTS
A/C A/C (USD)
Kit 541028A01R06 1 7,200.00 Rib, Angle, Seal Bracket, Seal
TOTAL 14,400.00
Component COMPA01 2 See SB Teflon Tape
Component COMPA02 1 See SB Shims
**CONF 002

A/C A/C (USD)
Kit 541028A03R05 1 6,800.00 Rib, Angle
Kit 541028A04R05 1 6,800.00 Rib, Angle
TOTAL 13,600.00
**CONF 003

A/C A/C (USD)
TOTAL 14,400.00

@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
**CONF 004

A/C A/C (USD)
TOTAL 14,400.00
**CONF 005

A/C A/C (USD)
Kit 541028A03R05 1 6,800.00 Rib, Angle
Kit 541028A04R05 1 6,800.00 Rib, Angle
TOTAL 13,600.00
EFFECTIVITY
**CONF ALL
This Service Bulletin is applicable to this (these) operator(s) :
11S 15T 16T 17R 17S 20Q 27V 31X 35T 43S 46U 54S 74T
79W 89T 95W AAF AAL AAR AAW ABQ ABY ACA ACI ADR AEE
AFL AFR AIC AIJ ALK AMU ANZ AOJ APJ ASL AVA AWC AXM
AZA BAW BEC BEL BER BHP BJN BKP C2C CBJ CCA CCM CEB
CES CHB CQH CQN CRK CSA CSC CSN CSZ CTV CUA DCS DKH
DLH DRK EIN ELB ETD EVA EVE EWG EZY FFT FHY FIN FLI
GAF GAP GCR GFA GLG GMI GOW GSW GWI HDA HKE HKJ HVN
IAW IBE IBS IGO ISR IYE JAS JBU JJP JKT JSA JST JZR
KAC KAY KHV KNE KZR LAA LAN LAO LBT LJB LKE LLC LZB
MAC MEA MJF MJN MLM MON MOV MSC NIA NKS NLY NMB NWS
OBS ONE ORF PAL PGT PIC QAF QTR RJA RJD ROT RYW SAA
SAI SAS SBI SFJ SHU SKU SLK SVA SVR SVW SWR SYA TAI
TAM TAP TAR TBA TCX TGW THA THY TJS TNA TTW TVS UAE
UEA UKN UNA USA UTA UZB VIM VIP VIV VJC VLG VNL VOI
VRD WZZ
CONCURRENT REQUIREMENTS
None

@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
REFERENCES / REPERCUSSIONS
TFU 54.55.11.004
OEB None
AOT None
SIL None
ISI None
LINE MAINTENANCE AFFECTED No
LIFE LIMIT None
OTHER None
NATURE OF THE WORK
AIRCRAFT YES
EQUIPMENT NO
HARD NO
SOFT NO
OBRM NO
MANPOWER
**CONF 001
Task 541028-831-801-001: Modification

TOTAL MANHOURS 44.00
ELAPSED TIME (HOURS) 16.75
**CONF 002

**CONF 003

**CONF 004

**CONF 005


@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
APPENDICES
**CONF ALL

@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
**CONF 001, 003 thru 004
A
LH SIDE SHOWN
RH SIDE SYMMETRICAL
RIB5 TO BE REPLACED
B
LH SIDE SHOWN
RH SIDE SYMMETRICAL
N_SB_541028_5_SAAA_01_00
Figure A-FSAAA - Sheet 01

@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
**CONF 005
A
LH SHOWN
RH SYMMETRICAL
A
RIB5 TO BE REPLACED
B
LH SHOWN
RH SYMMETRICAL
N_SB_541028_5_SAAB_01_01
Figure A-FSAAB - Sheet 01

@A318/A319/A320/A321
SERVICE BULLETIN
SUMMARY
**CONF 002
A
LH SHOWN
RH SYMMETRICAL
A
RIB5 TO BE REPLACED
B
LH SHOWN
RH SYMMETRICAL
N_SB_541028_5_SAAC_01_00
Figure A-FSAAC - Sheet 01

@A318/A319/A320/A321
SERVICE BULLETIN
AIRBUS
31707 BLAGNAC CEDEX
FRANCE
Tel : (33) 5 61 93 33 33
Fax : (33) 5 61 93 42 51
ATA SYSTEM: 54

This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the
property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with
any information contained in it. It is delivered on the express condition that said document and the
information contained in it shall be treated as confidential, shall not be used for any purpose other than
that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall
not be duplicated in any manner (except for the purposes of performing the tasks described hereunder
and provided that any recipient of such document shall comply with the conditions herein), without
AIRBUS prior written consent.
1. PLANNING INFORMATION
**CONF ALL
A. EFFECTIVITY
NOTE: This modification is applicable by Service Bulletin only.
NOTE: This Service Bulletin is only applicable to aircraft on which modification No.
33687P8297 (IMPROVE THE AERODYNAMIC SHAPE OF A318 PW PYLON)
or modification No. 33844P8341 (IMPROVE AERODYNAMIC SHAPE OF
CFM PYLON) or modification No. 33847P8340 (IMPROVE AERODYNAMIC
SHAPE OF IAE PYLON) are embodied and on which modification No.
155559P13624 (REDESIGN OF THE PYLON AFT MOVABLE FAIRING RIB 5
(FORWARDFIT)) is not embodied.
NOTE: The intent of this modification is achieved in production on aircraft with

Manufacturer Serial Number (MSN) 5950 and subsequent through
modification No. 155559P13624 (REDESIGN OF THE AFT PYLON).
(1) Models
318-111 318-112 318-121 318-122 319-111 319-112 319-115 319-132

319-133 320-214 320-216 320-232 320-233 321-211 321-212 321-213
321-231 321-232
(2) Effectivity by MSN
2781 2802 2814 2832 2848 2871 2880 2900 2931 2945 2955 2970 2977 2992 2994
3001 3029-3030 3033-3034 3039 3048 3062 3066 3072 3074 3087 3089 3091 3105

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SERVICE BULLETIN
3107-3108 3115 3119-3120 3123 3127-3128 3130 3143 3146 3149-3150 3157-3158
3160 3164 3166-3167 3170-3172 3177-3178 3187 3190-3191 3193 3196-3197 3205
3210 3212-3214 3216-3217 3220 3222 3225 3227-3230 3233 3235 3238 3240-3241
3243 3247-3252 3254 3256 3258-3260 3262-3267 3269-3271 3273-3274 3276 3278
3280-3281 3284 3286-3288 3290 3294-3295 3298 3300-3302 3304-3314 3317 3319
3322 3324-3326 3328-3331 3333-3336 3339-3340 3342-3344 3347-3348 3351-3352
3354 3356-3360 3362 3364-3365 3367 3369 3371-3375 3381-3382 3384-3395
3397-3399 3401 3403-3404 3408-3414 3416-3417 3419-3421 3423-3424 3426-3428
3430-3434 3436 3438-3439 3441-3442 3444-3446 3448-3455 3457-3460 3462-3482
3484 3486-3495 3497-3505 3507-3511 3513-4329 4331-5949
(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
11S 4211
15T 3164
16T 4024 4679
17R 5768
17S 3333
20Q 4842
27V 3826
31X 4319
35T 5040
43S 4650
46U 3674 3734 3986 4053 5218 5900
54S 5261
74T 4768 5182
79W 3751
89T 3356
95W 4199
AAF 4268 4589 4675
AAL 5327 5678 5698 5704 5745 5753 5761 5781 5786 5788 5789 5798
5810 5827 5834 5842 5860 5884 5895 5904 5932 5938 5946
AAR 3641 3873 4112 4142 5035 5169 5173 5287 5350 5382 5462 5500
5636 5767 5774
AAW 3615 3657 4004 4521 5414 5448
ABQ 3974 5891 5943
ABY 4061 4243 4310 4468 4524 4806 4848 4890 4958 5017 5276 5307
5423 5452 5502 5576 5718 5772 5889 5903
ACA 3401 3884
ACI 3547
ADR 4282 4301
AEE 3033 3066 3074 3302 3322 3365 3392 3423 3439 3462 3478 3484
3519 3526 3527 3709 3714 3745 3748 3753 3773 3785 3812 3820
3829 3850 3878 3990 4065 4094 4165

@A318/A319/A320/A321
SERVICE BULLETIN
OPERATOR MSN
AFL 3157 3191 3267 3334 3373 3410 3511 3545 3574 3627 3631 3640
3644 3699 3711 3778 3786 3789 3794 3823 3835 3923 3942 3954
3998 4058 4074 4099 4103 4116 4133 4148 4160 4453 4461 4498
4500 4579 4625 4649 4656 4684 4692 4712 4835 5044 5059 5271
5421 5536 5565 5572 5578 5580 5585 5614 5720 5755 5790 5873
5881 5913 5921
AFR 3372 3399 3419 3420 3441 3470 3777 3795 3814 3825 3859 3930
4063 4084 4105 4137 4139 4241 4251 4267 4295 4298 4335 4402
4601 4604 4664 4714 4747 4800 4820 4901 4908 5084 5129 5719
5802 5869
AIC 3130 3146 3212 3271 3288 3300 3305 3326 3340 3344 3367 3498
3551 3557 3573 3619 3620 3687 3752 3792 3822 3874 3918 3955
3970 4002 4009 4020 4029 4052 4078 4089 4096 4121 4138 4155
4164 4201 4212 4236 4237 4280
AIJ 3123 3149 3160 3286 3304 3312 3374 3508 3514 3667 3690 4235
4304 4411 4730 4733 4924 4933 5163 5221 5358 5372 5653 5665
5867 5878 5933
ALK 3397 3636 4694 4869 4915 5086
AMU 4197 5352 5459 5523
ANZ 4553 4584 4884 4926 5629 5682 5847
AOJ 4503
APJ 4887 4936 5015 5166 5304 5384 5440 5540 5640 5724 5874
ASL 3252 3317
AVA 3408 3467 3518 3647 3664 3691 3961 3980 3988 3992 4001 4011
4026 4046 4051 4100 4167 4175 4200 4281 4284 4345 4381 4487
4567 4599 4763 4789 4821 4862 4939 5057 5119 5195 5243 5360
5398 5454 5477 5622 5632 5840 5944
AWC 4701
AXM 3394 3404 3427 3448 3477 3486 3489 3505 3521 3536 3549 3568
3576 3582 3610 3628 3648 3679 3701 3715 3729 3765 3776 3813
3875 3963 3997 4019 4035 4070 4079 4088 4098 4126 4147 4263
4278 4293 4302 4333 4346 4361 4367 4386 4390 4404 4426 4458
4462 4477 4486 4557 4571 4582 4793 4797 4807 4882 4889 4917
4964 4969 4979 4980 4989 5098 5137 5149 5153 5165 5200 5215
5272 5283 5325 5344 5347 5353 5359 5397 5420 5428 5430 5431
5468 5505 5547 5593 5619 5627 5657 5703 5706 5762 5812 5824
5839 5846 5851 5863 5866 5888 5897 5905 5908 5914 5918
AZA 3115 3295 3362 3412 3563 3598 3609 3643 3666 3695 3732 3815
3846 3885 3906 3921 3956 3976 3978 4075 4108 4119 4143 4152
4195 4249 4520 4523 4536 4759 4764 4859 4875 4910 5018 5130
5294 5383 5424
BAW 3235 3254 3290 3301 3314 3351 3468 3499 3550 3607 3649 3697
3703 3721 3726 3912 3926 4007 4039 4185 4238 4265 4306 4464
4551 4725 4791 4975 5634 5784 5856 5948
BEC 5538
BEL 3790 3895 4275
BER 3178 3213 3328 3343 3464 3482 3502 3515 3516 3532 3708 3749
3865 3945 4013 4101 4161 4269 4291 4329 4334 4433 4510 4565
4728 5038 5126 5133 5522

@A318/A319/A320/A321
SERVICE BULLETIN
OPERATOR MSN
BHP 3604 4033 4187 4294 4631
BJN 3617 4956
BKP 3421 3424 3454 3694 3759 3911
C2C 5088 5907
CBJ 3520 3548 3561 3578 3580 3638 3768 3842 3849 3851 3914 3958
3982 4042 4388 4410 4412 4428 4440 4471 4483 4505 4513 4522
4529 4540 4580 4602 4677 5008 5072 5114 5185 5216 5331 5471
5630 5656 5722 5848
CCA 3250 3307 3329 3523 3601 3623 3653 3655 3665 3678 3722 3725
3766 3806 3940 3973 4022 4031 4062 4091 4131 4180 4221 4283
4317 4318 4348 4377 4472 4473 4494 4538 4566 4593 4617 4719
4771 4775 4803 4829 4834 4873 4895 4900 4949 4963 4985 4997
5014 5032 5054 5091 5124 5174 5199 5265 5346 5386 5419 5432
5435 5568 5573 5600 5664 5690 5743 5771
CCM 3882 3952 5887 5906
CEB 2994 3048 3762 3767 4447 4508 4537 4574 4852 4861 4870 4927
4993 5045 5067 5250 5320 5381 5442 5498 5669 5687 5917 5934
CES 3170 3197 3233 3247 3249 3262 3471 3481 3559 3593 3611 3612
3613 3639 3650 3677 3682 3692 3716 3775 3793 3797 3870 3904
3929 3937 3965 3969 4027 4037 4043 4045 4111 4144 4186 4198
4209 4220 4239 4240 4252 4297 4309 4340 4342 4355 4374 4423
4627 4638 4659 4685 4702 4709 4711 4718 4722 4723 4729 4746
4748 4765 4769 4776 4799 4831 4844 4857 4877 4886 4903 4938
4946 4967 4987 5047 5048 5053 5063 5135 5136 5144 5156 5192
5210 5227 5242 5267 5273 5309 5326 5330 5338 5363 5376 5380
5402 5412 5439 5461 5481 5508 5516 5519 5524 5527 5558 5575
5623 5628 5668 5691 5700 5705 5710 5711 5726 5735 5759 5770
5823 5826 5852 5864 5886 5920 5942
CHB 4262 4452 4482 4569 4644 4686 4687 4995 5105 5246 5626 5679
5740 5912
CQH 3747 3819 4072 4093 4168 4244 4331 4366 4373 4375 4499 4586
4738 4750 4760 4809 4816 4909 4978 4983 5022 5051 5108 5378
5403 5434 5446 5466 5562 5778 5816 5911
CQN 3836 3876 3901 3903 3941 5645 5713
CRK 5147 5189 5416 5514 5544
CSA 3436 3452 3660 3892 4258 4713
CSC 3158 3167 3196 3210 3386 3449 3583 3591 3680 3730 3893 3962
3996 4018 4068 4288 4326 4378 4420 4424 4525 4575 4619 4642
4660 4707 4731 4824 4830 4856 4905 4911 4923 5041 5121 5141
5160 5197 5208 5233 5286 5303 5389 5470 5543 5609 5646 5647
5650 5670 5765 5868 5896 5910 5937

@A318/A319/A320/A321
SERVICE BULLETIN
OPERATOR MSN
CSN 3217 3241 3251 3258 3269 3311 3342 3459 3493 3507 3552 3566
3587 3645 3681 3764 3784 3828 3847 3860 3867 3890 3910 3920
3934 3938 3951 3959 3981 3983 3999 4003 4017 4036 4038 4071
4140 4172 4184 4189 4194 4205 4217 4224 4225 4230 4232 4248
4260 4266 4271 4274 4279 4290 4292 4299 4322 4325 4338 4341
4350 4362 4365 4369 4370 4387 4396 4416 4430 4456 4507 4550
4613 4671 4696 4751 4782 4794 4808 4836 4854 4864 4880 4883
4912 4919 4928 4982 5061 5151 5168 5170 5183 5202 5214 5225
5237 5268 5279 5288 5410 5480 5484 5503 5506 5534 5561 5564
5579 5602 5611 5655 5671 5693 5730 5736 5750 5756 5797 5817
5832 5837 5875 5890 5930 5945 5949
CSZ 3528 3599 3696 3698 3756 3848 3855 3887 3898 3935 3971 4010
4028 4159 4176 4208 4214 4226 4300 4359 4407 4409 4435 4474
4514 4531 4620 4633 4666 4726 4845 4866 4876 4897 4920 4929
4977 4986 5002 5082 5110 5176 5369 5521 5550 5589 5639 5731
5766
CTV 3861 4961 5351 5379 5394 5399 5415 5511 5541 5551 5556 5560
5571 5574 5597 5777 5830
CUA 5023
DCS 3243
DKH 3596 3605 3967 3984 4064 4102 4154 4276 4401 4429 4573 4587
4652 4833 4840 4981 5013 5070 5071 5131 5226 5329 5339 5455
5491 5674 5737 5876
DLH 3265 3339 3360 3387 3434 3592 3625 3864 3936 3987 4005 4016
4047 4054 4073 4085 4097 4120 4141 4153 4182 4191 4261 4289
4324 4332 4360 4363 4398 4449 4455 4511 4545 4560 4585 4607
4626 4672 4710 4753 4792 4796 4819 4841 4881 4916 4976 4994
5028 5049 5087 5122 5181 5186 5203 5239 5284 5293 5413 5425
5441 5487 5694 5741 5769 5831 5935
DRK 3950
EIN 3501 3755 3781 3857 4572 4634 4678 4715
ELB 3705
ETD 3676 3693 3713 3902 4066 4077 4124 4934 5095 5348 5407 5714
5791 5821 5836 5882 5924
EVA 3886 5328 5354 5377 5485 5792 5808 5849
EVE 5642
EWG 5497 5525 5557 5601 5635 5658
EZY 3411 3413 3426 3432 3442 3466 3537 3544 3555 3569 3571 3608
3634 3675 3683 3702 3720 3735 3742 3746 3754 3763 3774 3788
3799 3805 3808 3810 3824 3843 3844 3845 3854 3871 3888 3909
3913 3922 3946 3953 3975 3979 3991 4006 4012 4014 4034 4040
4048 4056 4069 4076 4080 4087 4125 4129 4132 4157 4179 4196
4219 4233 4234 4250 4286 4313 4327 4380 4385 4418 4425 4427
4437 4444 4451 4554 4556 4588 4591 4624 4635 4636 4640 4646
4667 4676 4680 4693 4705 4708 4717 4721 4740 4744 4749 4778
4781 4785 4787 4837 5019 5020 5046 5052 5056 5064 5104 5111
5113 5116 5138 5146 5150 5187 5201 5224 5236 5249 5289 5318
5319 5542 5592 5638 5688 5702 5739 5757 5785 5927

@A318/A319/A320/A321
SERVICE BULLETIN
OPERATOR MSN
FFT 3205 3389 3431 4127 4204 4253 4254 4272 4307 4562 4641 4668
4688 4704 4727 4745 5526 5581 5661
FHY 3852 3891 4207 4658 5096
FIN 5758 5803 5922
FLI 3905 5079
GAF 3897 4060
GAP 3087 3187 3273 3310 3731 4777 4984 5007 5012 5103 5310
GCR 4600 4739 4825 5006 5117 5760 5799 5835 5850 5853 5894 5928
GFA 4030 4059 4083 4146 4158 4188 4218 4255 4502 4541 4780 4827
4860 4865 5025 5074 5171 5175 5180 5257 5321 5336
GLG 4379 4547
GMI 3533 3560 4663 4691 5085 5843
GOW 3306 3597 3616 3798 3827 3900 3915 4399 4438 5016 5112 5232
5463 5552 5675 5809 5811
GSW 3589 3818
GWI 3128 3172 3193 3352 3358 3375 3500 3534 3839 3841 4166 4227
4256 4285 4998 5043 5457 5467 5535 5569 5941
HDA 3369 3669 4023 4247 5024 5030 5362 5429
HKE 4970 5260 5264 5266 5341 5725 5738
HKJ 4228 4878
HVN 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
IAW 4044 4067 5115 5290 5464
IBE 3651 3744 5486 5570 5692
IBS 5501 5590 5729 5815
IGO 3357 3414 3453 3457 3497 3541 3618 3782 3863 3943 4008 4113
4156 4216 4312 4328 4384 4481 4488 4506 4518 4535 4552 4603
4609 4614 4630 4637 4752 4757 4762 4812 4813 4818 4868 4888
4918 4947 4954 4965 4973 5027 5036 5073 5076 5080 5090 5092
5094 5120 5155 5188 5190 5194 5228 5230 5231 5259 5262 5291
5298 5313 5335 5365 5375 5411 5426 5437 5449 5460 5473 5476
5507 5537 5577 5641 5676 5683 5712 5727 5744 5807 5829 5893
5898 5923
ISR 4354 4413
IYE 4653 4690
JAS 5478
JBU 2781 2802 2814 2832 2848 2871 2880 2900 2945 2970 2977 2992
3029 3039 3072 3091 3119 3150 3190 3228 3263 3287 3348 3381
3416 3451 3479 3488 3517 3554 3572 3622 3659 3707 3724 3760
3800 3811 4578 4612 4647 4904 5060 5142 5148 5302 5312 5349
5417 5677 5723 5782 5783 5854 5865 5909
JJP 5093 5145 5161 5245 5274 5281 5355 5492 5499 5520 5598 5618
5649 5695 5701 5717 5732 5796
JKT 5685
JSA 4443 4515 4772 4786 4872 4914 5305 5323 5390 5433 5472 5708
5813

@A318/A319/A320/A321
SERVICE BULLETIN
OPERATOR MSN
JST 3474 3495 3668 3717 3783 3899 3916 3917 3948 4177 4178 4229
4245 4257 4303 4343 4356 4434 4460 4466 4495 4497 4527 4899
4922 5039 5211 5270 5311 5334 5482 5489 5532 5566 5631 5775
5780 5814 5858 5871
JZR 3919 3939 4162 5033 5625 5833
KAC 3957
KAY 4470
KHV 5343 5427
KNE 3238 3256 3475 3530 3787 3802 3809 3817 3868 3889 3894 3933
4055 4735 5716
KZR 3614 5357 5401 5404 5613 5734 5870
LAA 4405 4450 4490 4526 5373 5405 5494
LAN 3264 3280 3319 3330 3535 3556 3663 3671 3770 3772 3779 4383
4400 4439 4476 4509 4516 4543 4546 4549 4563 4576 4597 4598
4605 4657 4697 4758 4767 4815 4839 4871 4892 4896 4921 4943
4972 5005 5097 5125 5178 5213 5229 5234 5263 5316 5324 5364
5408 5443 5453 5483 5493 5548 5554 5583 5586 5654 5666 5686
5707 5748 5764 5801 5818 5859 5929
LAO 4596 4639 5356 5396
LBT 3089 3480 3487 4623
LJB 3985
LKE 3240 5100 5172 5220
LLC 4203 4489
LZB 3309 3564 3780
MAC 4539 4568 5143 5206
MEA 3736 3804 3837 4296 4339 4632 5000 5152 5162 5253 5746
MJF 4353
MJN 3723 4117 4795
MLM 3932 4622
MON 3458 3522 3546 3575 5582 5606
MOV 3364 3403
MSC 3626 3840
NIA 3925
NKS 3393 3395 4206 4264 4321 4431 4548 4592 4595 4902 4951 4996
5029 5042 5132 5159 5370 5387 5458 5517 5624 5672 5804 5861
5880
NLY 3504 3661 3689 3728 3830 4231 4316 4368 4581 4594 4606 4611
4648 5648
NMB 3586 5366 5400
NWS 3034 3120
OBS 3758
ONE 3001 3030 3062 3214 3216 3371 3390 3438 3469 3509 3585 3602
3606 3635 3642 4222 4287 4336 4891 4913 4941 4942 5193 5278
5299 5754 5841
ORF 4992
PAL 3455 3553 3579 3652 5081 5140 5315 5371 5715 5747 5787 5820
5825 5838

@A318/A319/A320/A321
SERVICE BULLETIN
OPERATOR MSN
PGT 3831 5879 5902
PIC 3621 4459 4533
QAF 3994 4114 4170 5255
QTR 3274 4110 4130 4173 4183 4382 4406 4436 4479 4496 4530 4615
4700 4754 4784 4802 4810 4858 4930 4968 5010 5078 5127 5217
5361 5395
RJA 3428 3685 3803 3832 4670 4817 4853 5099 5128 5177
RJD 5277
ROT 2931 2955 3220 3225
RYW 5367
SAA 4990 5011 5637 5680
SAI 3105 3270
SAS 3227 3335
SBI 3446 3473 3490 3494 3866 3880 4032 4150 5001 5026 5031 5106
5134 5167 5559 5607
SFJ 4555 4720 5102 5393 5512 5652 5773 5862 5931
SHU 3108 3281 3298 3336 3838
SKU 3171 3331
SLK 3570 3821 4118 4215 4259 4457 5050 5089 5296 5531 5794
SVA 4015 4057 4081 4090 4092 4104 4115 4122 4135 4273 4314 4337
4349 4357 4364 4376 4391 4392 4393 4394 4397 4408 4414 4419
4432 4442 4454 4467 4484 4501 4517 4519 4542 4564 4577 4590
4811 4823 4838 4925 4955 4962 5009 5065 5223 5285 5314 5447
5509 5549
SVR 3107 3385 3388 3433 3472 3834
SVW 3542 3856 5445
SWR 4534 4618 4673 5037 5069 5518 5567
SYA 3853 3872
TAI 3248 3276 3510 3538 3869 4906 4944 5068 5219 5238 5280 5333
5406 5936
TAM 3222 3229 3266 3278 3284 3294 3313 3325 3391 3540 3565 3588
3594 3595 3630 3658 3662 3710 3727 3733 3750 3761 3816 3908
3972 4000 4163 4171 4192 4320 4352 4358 4389 4441 4446 4465
4544 4570 4662 4734 4756 4773 4953 4974 5066 5101 5107 5109
5184 5209 5222 5240 5342 5345 5528 5591 5621 5643 5749 5752
5845 5883 5947
TAP 3769 3883 4021 4095 4106 4145
TAR 4344 4689 5204 5474 5610
TBA 4766 4801 4846 5157 5256 5451 5529 5563 5855
TCX 5603 5872
TGW 3757 3801 4181 4210 4421 4445 4469 4491 4493 4532 4561 4608
4645 4879 4931 5496 5596 5605 5662 5697 5721 5805 5915
THA 5198 5248 5258 5301 5436 5553 5806 5828 5857 5892
THY 3259 3308 3382 3525 3539 3558 3567 3603 3637 3654 3673 3688
3718 3719 3738 3896 3931 3949 4629 4643 4654 4665 4682 4695
4698 4706 4755 4761 4774 4779 4788 4790 5077 5083 5118 5154
5205 5254 5388 5450 5465 5490 5546 5584 5633 5663 5667 5689

@A318/A319/A320/A321
SERVICE BULLETIN
OPERATOR MSN
TJS 3513 3632 4169
TNA 3577 3581 5055
TTW 4804 4874
TVS 4699
UAE 4822
UEA 3706 4347 4743 4988 5003 5191 5252
UKN 3260
UNA 4583 4732 5545
USA 3584 3629 3633 3712 3740 3796 3858 3879 3881 3924 3928 3944
3960 3977 3989 3993 4025 4041 4050 4082 4086 4107 4123 4134
4149 4202 4242 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
UTA 5681 5733 5779 5919
UZB 4371 4395 4417 4485 4492 4528 4651 4724 4770 4952
VIM 4270 4305 5158
VIP 4151
VIV 3743
VJC 3646 3739 3791 4049 4190 4193 4415 4475 4504 4512 4907 5295
5742 5822
VLG 3444 3476 3492 3529 3700 3704 3833 3907 3995 4128 4463 4478
4661 4674 4681 4742 4849 4855 4937 5479 5530 5533 5587 5599
5612 5616 5620 5673 5877 5885 5925 5940
VNL 5844 5901 5926
VOI 3450 3463 3491 3524 3543 3590 3624 3672 4403 4422 4741 4798
4828 4832 4950 5062 5207 5212 5308 5322 5337 5391 5488 5510
5595 5651 5776 5793 5819
VRD 3230 3324 3347 3359 3398 3417 3445 3460 3465 3503 3656 3670
3684 3686 4448 4480 4558 4559 4610 4616 4655 4805 4814 4851
4867 4894 4948 4959 4991 4999 5004 5034 5058 5179 5515
WZZ 3127 3143 3166 3177 3354 3384 3409 3430 3531 3562 3741 3771
3807 3877 3927 3947 3968 4109 4174 4223 4246 4308 4323 4351
4372 4621 4628 4683 4716 4736 5021 5075 5123 5139 5196 5539
5604 5608 5615 5617 5660

@A318/A319/A320/A321
SERVICE BULLETIN
(4) Configuration by MSN
MSN CONFIGURATION
2781 2802 2814 2832 2848 2871 2880 2900 2945 2970 2977 001
2992 2994 3029 3033 3039 3048 3066 3072 3074 3087 3089
3091 3105 3107 3115 3119 3123 3127 3143 3149 3150 3157
3158 3160 3164 3166 3167 3170 3177 3178 3187 3190 3196
3197 3205 3210 3213 3227 3228 3230 3240 3256 3259 3263
3264 3266 3270 3273 3278 3280 3284 3286 3287 3295 3301
3304 3306 3308 3310 3312 3313 3314 3319 3325 3328 3330
3335 3343 3348 3351 3354 3357 3359 3362 3365 3373 3374
3381 3384 3386 3389 3391 3392 3394 3398 3404 3408 3409
3410 3412 3414 3416 3420 3423 3427 3430 3431 3433 3439
3444 3446 3448 3449 3451 3453 3455 3457 3460 3464 3465
3468 3470 3472 3473 3474 3475 3476 3477 3478 3479 3480
3481 3482 3484 3486 3487 3488 3489 3490 3492 3494 3495
3497 3499 3501 3502 3503 3505 3508 3510 3511 3514 3515
3516 3517 3519 3521 3524 3526 3528 3529 3531 3532 3535
3536 3538 3540 3541 3543 3545 3547 3549 3550 3553 3554
3556 3558 3559 3562 3563 3565 3567 3568 3570 3572 3574
3576 3577 3579 3581 3582 3591 3594 3596 3597 3598 3599
3601 3603 3605 3607 3609 3610 3611 3613 3616 3618 3621
3622 3624 3626 3627 3628 3630 3631 3640 3641 3643 3644
3646 3648 3649 3650 3652 3654 3656 3658 3659 3662 3664
3666 3667 3668 3670 3672 3674 3676 3677 3679 3690 3692
3693 3695 3696 3697 3698 3699 3701 3703 3706 3707 3709
3711 3713 3714 3715 3716 3718 3719 3721 3723 3724 3726
3729 3731 3732 3734 3736 3739 3741 3743 3745 3747 3748
3750 3753 3755 3756 3758 3760 3762 3765 3767 3769 3771
3773 3775 3776 3777 3778 3780 3781 3782 3783 3785 3786
3787 3789 3791 3793 3795 3797 3798 3800 3802 3804 3805
3807 3809 3811 3812 3813 3815 3817 3819 3821 3823 3825
3827 3829 3831 3833 3835 3837 3840 3843 3846 3848 3850
3852 3855 3857 3859 3861 3863 3866 3868 3870 3871 3873
3875 3877 3880 3882 3883 3885 3887 3889 3891 3894 3896
3898 3900 3902 3904 3906 3907 3908 3909 3910 3912 3913
3915 3917 3919 3921 3922 3923 3925 3927 3929 3931 3933
3935 3937 3939 3941 3943 3945 3946 3947 3949 3952 3953
3954 3956 3959 3961 3963 3965 3967 3968 3971 3972 3974
3975 3976 3978 3979 3980 3984 3986 3988 3990 3991 3992
3995 3997 3999 4001 4003 4006 4008 4010 4011 4012 4013
4014 4015 4017 4019 4021 4023 4026 4027 4028 4030 4032
4033 4034 4035 4037 4043 4046 4049 4051 4053 4055 4057
4059 4061 4063 4064 4065 4066 4068 4070 4072 4075 4077
4079 4081 4083 4084 4086 4088 4090 4092 4093 4094 4095
4097 4098 4100 4101 4102 4104 4105 4106 4108 4109 4110
4111 4113 4115 4117 4118 4119 4120 4122 4124 4126 4128
4130 4133 4135 4137 4139 4140 4143 4144 4145 4146 4147
4149 4150 4152 4153 4154 4156 4157 4158 4159 4160 4161
4162 4165 4167 4168 4170 4172 4174 4175 4176 4177 4178
4179 4181 4183 4185 4186 4187 4188 4190 4191 4193 4195
4196 4197 4199 4201 4202 4203 4205 4206 4207 4208 4210

@A318/A319/A320/A321
SERVICE BULLETIN
MSN CONFIGURATION
4212 4214 4216 4218 4219 4220 4223 4225 4226 4229 4231 001
4232 4233 4234 4235 4236 4237 4238 4239 4240 4241 4242
4243 4244 4245 4246 4247 4248 4249 4250 4252 4253 4255
4257 4260 4261 4263 4264 4265 4267 4269 4270 4272 4273
4276 4278 4279 4281 4284 4286 4288 4289 4290 4291 4293
4294 4295 4296 4297 4298 4300 4302 4303 4304 4305 4306
4307 4308 4309 4310 4312 4314 4316 4317 4320 4321 4322
4323 4324 4325 4326 4328 4329 4331 4333 4335 4337 4339
4340 4342 4343 4344 4345 4346 4347 4348 4349 4350 4351
4354 4355 4356 4357 4359 4361 4362 4363 4364 4365 4366
4367 4368 4370 4371 4372 4373 4375 4376 4378 4379 4381
4383 4384 4386 4388 4390 4391 4392 4393 4394 4395 4396
4397 4398 4399 4400 4401 4402 4404 4405 4407 4408 4409
4411 4412 4413 4414 4415 4417 4419 4421 4423 4424 4426
4429 4431 4432 4433 4434 4435 4436 4438 4439 4440 4441
4442 4443 4445 4446 4447 4448 4449 4450 4453 4454 4456
4457 4458 4459 4460 4462 4463 4464 4465 4466 4468 4469
4471 4473 4474 4475 4476 4477 4478 4479 4480 4481 4482
4483 4484 4485 4486 4487 4488 4489 4490 4491 4492 4493
4495 4496 4497 4498 4499 4501 4502 4504 4505 4506 4507
4508 4509 4510 4512 4513 4514 4515 4516 4517 4518 4519
4520 4521 4523 4524 4525 4526 4527 4528 4531 4532 4533
4535 4536 4537 4539 4540 4541 4543 4544 4546 4547 4548
4549 4550 4551 4552 4553 4554 4555 4556 4557 4558 4559
4561 4562 4564 4565 4566 4567 4568 4569 4571 4572 4573
4574 4575 4576 4578 4579 4580 4581 4582 4584 4586 4587
4588 4589 4591 4592 4593 4594 4595 4596 4597 4599 4600
4601 4602 4603 4604 4606 4608 4609 4610 4612 4613 4614
4615 4616 4618 4619 4620 4621 4623 4625 4627 4628 4630
4631 4632 4633 4634 4636 4637 4639 4641 4642 4644 4645
4646 4647 4649 4651 4652 4653 4655 4656 4657 4658 4659
4661 4664 4666 4668 4670 4671 4673 4674 4675 4676 4677
4678 4680 4681 4683 4684 4685 4686 4687 4688 4689 4690
4692 4694 4696 4697 4699 4700 4701 4702 4704 4707 4708
4709 4711 4712 4714 4715 4716 4718 4720 4721 4722 4723
4724 4725 4726 4727 4729 4730 4733 4735 4736 4738 4739
4740 4741 4742 4743 4745 4747 4748 4749 4750 4751 4752
4754 4757 4758 4760 4762 4763 4765 4767 4769 4770 4772
4775 4776 4777 4780 4782 4784 4786 4789 4791 4793 4794
4795 4797 4798 4799 4800 4802 4803 4804 4805 4806 4807
4808 4809 4810 4812 4813 4814 4815 4816 4817 4818 4820
4821 4823 4825 4827 4828 4829 4831 4832 4833 4835 4836
4839 4840 4844 4845 4848 4849 4851 4852 4853 4854 4855
4857 4858 4860 4861 4862 4864 4865 4866 4867 4868 4869
4870 4872 4874 4876 4877 4879 4880 4882 4883 4884 4886
4887 4888 4889 4890 4891 4892 4894 4895 4896 4897 4899
4900 4902 4903 4904 4905 4906 4907 4908 4909 4911 4912
4913 4914 4915 4917 4918 4919 4920 4921 4922 4924 4926
4927 4928 4929 4930 4931 4933 4934 4936 4937 4938 4939
4941 4942 4943 4944 4946 4947 4948 4950 4951 4952 4953
4954 4955 4958 4959 4961 4963 4964 4965 4967 4968 4969

@A318/A319/A320/A321
SERVICE BULLETIN
MSN CONFIGURATION
4970 4972 4973 4974 4975 4977 4978 4979 4980 4981 4982 001
4983 4984 4985 4986 4987 4988 4989 4990 4991 4993 4996
4997 4999 5000 5001 5002 5003 5004 5006 5007 5008 5010
5011 5012 5013 5014 5015 5016 5017 5019 5020 5021 5022
5024 5026 5027 5029 5030 5031 5032 5033 5034 5036 5037
5039 5041 5042 5045 5046 5047 5048 5050 5051 5052 5053
5055 5056 5058 5060 5061 5062 5063 5064 5066 5067 5068
5069 5070 5071 5072 5073 5075 5076 5078 5080 5081 5082
5084 5086 5089 5090 5091 5092 5093 5094 5095 5096 5098
5100 5101 5102 5103 5104 5106 5107 5108 5109 5110 5111
5112 5113 5114 5115 5116 5117 5120 5121 5122 5123 5125
5127 5128 5129 5131 5132 5134 5135 5136 5137 5138 5139
5140 5141 5142 5143 5144 5145 5146 5147 5148 5149 5150
5151 5152 5153 5155 5156 5158 5159 5161 5162 5163 5165
5166 5167 5168 5170 5171 5172 5174 5175 5176 5178 5179
5181 5182 5183 5184 5185 5187 5188 5189 5190 5191 5194
5195 5196 5198 5200 5201 5202 5203 5204 5206 5207 5209
5211 5212 5213 5214 5215 5216 5217 5218 5220 5221 5222
5223 5224 5225 5226 5228 5229 5230 5231 5232 5234 5236
5238 5240 5242 5243 5245 5246 5248 5249 5250 5252 5253
5255 5258 5259 5260 5262 5263 5264 5266 5268 5270 5272
5274 5276 5278 5281 5283 5288 5289 5290 5291 5296 5298
5299 5301 5302 5304 5305 5307 5308 5310 5311 5312 5313
5315 5316 5318 5319 5320 5322 5323 5324 5325 5326 5329
5331 5333 5334 5335 5337 5339 5341 5342 5344 5347 5348
5349 5351 5352 5353 5355 5356 5358 5359 5360 5361 5362
5363 5364 5365 5367 5369 5370 5371 5372 5373 5375 5378
5379 5381 5384 5386 5387 5390 5391 5393 5394 5395 5396
5397 5398 5399 5401 5403 5405 5407 5408 5410 5411 5414
5415 5416 5417 5419 5420 5421 5423 5425 5426 5428 5429
5430 5431 5433 5434 5436 5437 5440 5441 5442 5443 5446
5448 5449 5452 5453 5454 5455 5458 5460 5461 5463 5464
5466 5468 5471 5472 5473 5474 5476 5477 5479 5480 5482
5483 5484 5486 5487 5488 5489 5491 5492 5493 5494 5496
5497 5498 5499 5501 5502 5503 5505 5506 5507 5508 5510
5511 5512 5514 5515 5516 5517 5518 5520 5521 5522 5524
5525 5526 5527 5530 5531 5532 5533 5536 5537 5539 5540
5541 5542 5544 5547 5548 5550 5551 5552 5553 5554 5556
5557 5559 5560 5561 5562 5564 5565 5566 5568 5570 5571
5572 5574 5576 5577 5578 5579 5580 5581 5583 5585 5586
5587 5589 5590 5591 5592 5593 5595 5596 5597 5598 5599
5600 5601 5602 5604 5605 5607 5608 5610 5611 5612 5613
5614 5615 5616 5617 5618 5619 5620 5621 5622 5624 5625
5626 5627 5628 5629 5630 5631 5632 5634 5635 5637 5638
5639 5640 5641 5642 5643 5645 5646 5648 5649 5651 5652
5653 5654 5656 5657 5658 5660 5661 5662 5664 5665 5666
5668 5669 5671 5672 5673 5675 5676 5677 5679 5680 5682
5683 5685 5686 5687 5688 5690 5691 5692 5693 5694 5695
5697 5701 5702 5703 5706 5707 5708 5710 5711 5712 5713
5714 5716 5717 5718 5719 5721 5722 5723 5724 5725 5726
5727 5729 5730 5731 5732 5734 5735 5737 5738 5739 5740

@A318/A319/A320/A321
SERVICE BULLETIN
MSN CONFIGURATION
5741 5742 5744 5746 5748 5749 5750 5752 5754 5756 5757 001
5759 5760 5762 5764 5766 5769 5771 5772 5773 5775 5776
5777 5778 5780 5782 5784 5785 5791 5793 5794 5796 5797
5799 5801 5802 5804 5805 5806 5807 5809 5811 5812 5813
5814 5815 5816 5817 5818 5819 5821 5822 5823 5824 5828
5829 5830 5831 5832 5833 5835 5837 5839 5840 5841 5844
5845 5846 5847 5848 5850 5851 5852 5853 5856 5857 5858
5859 5861 5862 5863 5864 5866 5867 5869 5870 5871 5873
5874 5875 5877 5878 5879 5880 5882 5883 5885 5887 5888
5889 5891 5892 5893 5894 5896 5897 5898 5900 5901 5902
5903 5905 5906 5908 5911 5912 5914 5915 5917 5918 5921
5923 5924 5925 5926 5927 5928 5929 5930 5931 5933 5934
5935 5937 5940 5942 5943 5945 5948
2931 2955 3001 3030 3062 3214 3216 3220 3225 3238 3333 004
3371 3390 3438 3469 3509 3530 3585 3602 3606 3617 3635
3642 3751 3886 3932 3985 4007 4039 4169 4211 4503 4650
4732 4878 5478 5545
3034 3120 3130 3146 3191 3212 3217 3222 3229 3233 3235 002
3241 3247 3249 3251 3254 3262 3265 3267 3274 3290 3294
3302 3307 3322 3326 3329 3334 3339 3340 3360 3367 3369
3372 3382 3387 3397 3399 3401 3419 3434 3441 3458 3459
3462 3471 3493 3498 3504 3507 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

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SERVICE BULLETIN
MSN CONFIGURATION
3108 3128 3171 3172 3193 3243 3248 3250 3252 3258 3260 003
3269 3271 3276 3281 3288 3298 3300 3305 3309 3311 3317
3324 3331 3336 3342 3344 3347 3352 3356 3358 3364 3375
3385 3388 3393 3395 3403 3411 3413 3417 3421 3424 3426
3428 3432 3436 3442 3445 3450 3452 3454 3463 3466 3467
3491 3500 3513 3518 3520 3533 3534 3537 3542 3544 3548
3551 3555 3560 3561 3564 3569 3571 3578 3580 3586 3588
3589 3590 3595 3604 3608 3614 3615 3620 3632 3634 3638
3647 3651 3657 3660 3661 3663 3671 3675 3680 3683 3684
3685 3686 3687 3689 3691 3694 3700 3702 3704 3705 3710
3720 3727 3728 3733 3735 3742 3744 3746 3754 3757 3759
3763 3768 3770 3772 3774 3779 3788 3790 3794 3799 3801
3803 3808 3810 3818 3822 3824 3826 3828 3832 3834 3836
3838 3839 3841 3842 3844 3845 3849 3851 3853 3854 3856
3860 3865 3872 3874 3876 3888 3890 3892 3895 3897 3901
3903 3905 3911 3914 3918 3942 3950 3957 3958 3962 3970
3982 3983 3994 3998 4000 4004 4018 4020 4024 4029 4036
4038 4040 4042 4048 4052 4056 4060 4069 4071 4076 4080
4087 4089 4114 4121 4125 4127 4129 4132 4141 4151 4163
4164 4166 4171 4182 4192 4200 4204 4215 4222 4227 4228
4254 4256 4258 4259 4262 4268 4275 4282 4285 4287 4301
4313 4319 4327 4332 4336 4353 4380 4385 4389 4403 4410
4418 4422 4425 4427 4428 4437 4444 4451 4452 4455 4470
4511 4522 4529 4563 4583 4598 4605 4622 4624 4629 4635
4640 4660 4663 4665 4667 4679 4691 4693 4695 4705 4713
4717 4734 4744 4755 4756 4759 4764 4766 4768 4773 4774
4778 4781 4785 4787 4790 4796 4801 4822 4837 4841 4842
4846 4859 4871 4875 4910 4956 4992 4995 4998 5005 5018
5023 5040 5043 5057 5079 5085 5088 5097 5105 5119 5130
5157 5193 5208 5219 5239 5256 5261 5267 5273 5277 5280
5284 5286 5293 5294 5327 5330 5338 5345 5366 5376 5380
5383 5389 5400 5406 5412 5424 5439 5445 5451 5457 5467
5529 5535 5563 5569 5609 5623 5650 5678 5698 5700 5704
5745 5753 5761 5765 5768 5781 5786 5788 5789 5792 5798
5810 5826 5827 5842 5855 5868 5886 5907 5910 5920 5941
5944

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SERVICE BULLETIN
MSN CONFIGURATION
4585 4590 4607 4611 4617 4626 4638 4643 4648 4654 4662 005
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 5295 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 5470 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 5758 5763 5767 5770 5774 5779 5783 5787
5790 5795 5800 5803 5808 5820 5825 5834 5836 5838 5843
5849 5854 5860 5865 5872 5876 5881 5884 5890 5895 5899
5904 5909 5913 5916 5919 5922 5932 5936 5938 5939 5946
5947 5949
(5) Configuration definition
**CONF 001
Config. 001 is valid for A320 aircraft.
**CONF 002
Config. 002 is valid for A321 aircraft on which MOD No. 152133P12359 is not embodied.
**CONF 003
**CONF 004
**CONF 005
Config. 005 is valid for A321 aircraft on which MOD No. 152133P12359 is embodied.
(6) Material Effectivity
**CONF 001, 003 thru 004
MATERIAL QTY PER A/C SEE NOTES

Kit 541028A01R06 1 (1)
Kit 541028A02R06 1 (2)
Consumable CMLA01 As required
Reidentified part set REIDA01 1

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Component COMPA01 2
Component COMPA02 1
NOTE (1): Kit 541028A01R06 concerns the modification of the LH pylon.
NOTE (2): Kit 541028A02R06 concerns the modification of the RH pylon.
**CONF 002

Kit 541028A03R05 1 (1)
Kit 541028A04R05 1 (2)
Component COMPA01 2
Component COMPA02 1
**CONF 005

Kit 541028A03R05 1 (1)
Kit 541028A04R05 1 (2)
Component COMPA01 2
Component COMPA02 1

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**CONF ALL
B. CONCURRENT REQUIREMENTS
None
C. REASON
(1) History
Several pylon aft movable fairing Rib 5 have been found cracked or with loose fasteners
during maintenance inspections and recently, one pylon aft movable fairing tail cone was
reported missing after operation.
(2) Objective/Action
This Service Bulletin recommends to install new redesigned Rib 5 in order to prevent
further cracks on Rib 5 and to introduce additional fasteners to prevent tail cone loss.
(3) Advantages
Accomplishment of this Service Bulletin will improve the structural integrity of the pylon
aft movable fairing.
Accomplishment of Service Bulletin No. A320-54-1028 cancels inspection requirement of

aft movable fairing Rib 5 and fasteners as per Service Bulletin No. A320-54-1026.
(4) Operational/Maintenance Consequences
None
D. DESCRIPTION
To accomplish this Service Bulletin it is necessary to :
**CONF 001
(1) Remove Rib 5 on LH Pylon
(2) Modify LH Fairing
(3) On Bench, Modify LH Tail Cone
(4) Modify and Install LH Rib 5
(5) Install LH tail Cone
(6) Remove Rib 5 on RH Pylon
(7) Modify RH Fairing

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SERVICE BULLETIN
(8) On Bench, Modify RH Tail Cone
(9) Modify and Install RH Rib 5
(10) Install RH tail Cone
**CONF 002
**CONF 003

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SERVICE BULLETIN
**CONF 004
**CONF 005

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**CONF ALL
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
Organisation Approval No. EASA.21J.031.
If an aircraft listed in the effectivity has a modification or repair embodied that is not of
AIRBUS origin, and which affects the content of this Service Bulletin, the operator is
responsible for obtaining approval by its airworthiness authority for any adaptation necessary
before incorporation of the Service Bulletin.
G. MANPOWER
The manpower estimates given in this Service Bulletin are based on the direct labor cost to
do the work. These estimates assume that the work will be done by experienced personnel,
and may need to be revised upwards to suit operator’s circumstances. The estimates do not
include the time to prepare, plan or inspect the work. Manufacture and procurement of parts
and tools, drying times for paints, sealants, etc., and general administration work are also not
included.
**CONF 001

Get Access 2.00
On Aircraft
Remove Rib 5 on LH Pylon 2.00
Modify LH Fairing 1.75
Modify and Install LH Rib 5 8.75
Install LH tail Cone 3.75
Remove Rib 5 on RH Pylon 2.00
Modify RH Fairing 1.75
Modify and Install RH Rib 5 8.75
Install RH tail Cone 3.75
On Bench
On Bench, Modify LH Tail Cone 3.75
On Bench, Modify RH Tail Cone 3.75
Close-Up 2.00

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SERVICE BULLETIN

NOTE: For an explanation of the manhours and elapsed time, refer to the Gantt
Chart, Fig. A-FAAAA given in Appendix 01.
**CONF 002

Get Access 2.00
On Aircraft
On Bench
Close-Up 2.00
**CONF 003

Get Access 2.00
On Aircraft
On Bench

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SERVICE BULLETIN

Close-Up 2.00
**CONF 004

Get Access 2.00
On Aircraft
On Bench
Close-Up 2.00
**CONF 005

Get Access 2.00
On Aircraft
On Bench

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SERVICE BULLETIN

Close-Up 2.00
**CONF ALL
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.
**CONF 001
Manufacturers Empty Weight +0.100 KG (+0.2204 LB)

Effect on Balance +1.746 KGM (+12.628 LB.FT )
**CONF 002, 005

**CONF 003

**CONF 004

**CONF ALL
I. ELECTRICAL LOAD DATA
Not Changed
J. REFERENCES
**CONF 001
Aircraft Maintenance Manual (AMM) 06-20-00 06-41-54 12-34-24

20-21-11 20-28-00 27-50-00
54-53-11 54-55-00
Consumable Material List (CML)

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Elec. Std. Practices Manual (ESPM) 20-51-20 20-55-00

Process and Material Specification (PMS) Process and Material Specification
(PMS) 01-06-12
Standards Manual (SM)
Structural Repair Manual (SRM) 51-23-00 51-24-00 51-40-00
51-42-00 51-43-00 51-44-00
Weight and Balance Manual (WBM) Chapter 1-00-07
**CONF 002

20-21-11 20-28-00 27-50-00
54-53-11 54-55-00
(PMS) 01-06-12
51-42-00 51-43-00 51-44-00
**CONF 003

20-21-11 20-28-00 27-50-00
54-53-11 54-55-00
(PMS) 01-06-12
51-42-00 51-43-00 51-44-00
**CONF 004

20-21-11 20-28-00 27-50-00
54-53-11 54-55-00
(PMS) 01-06-12
51-42-00 51-43-00 51-44-00

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**CONF 005

20-21-11 20-28-00 27-50-00
54-53-11 54-55-00
(PMS) 01-06-12
51-42-00 51-43-00 51-44-00
**CONF ALL
K. PUBLICATION AFFECTED
Illustrated Parts Catalog (IPC) 54-55-11
L. INTERCHANGEABILITY/MIXABILITY
Not Applicable
M. SPARES
None

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This Page Intentionally Left Blank

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SERVICE BULLETIN
2. MATERIAL INFORMATION
**CONF ALL
A. MATERIAL - PRICE AND AVAILABILITY
(1) Procurement Addresses
Customers with aircraft shown in the effectivity of this Service Bulletin should send a
purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is:
Kit 541028A01R06 AIRBUS Material, Logistics and Suppliers

Kit 541028A02R06 ATP II B,
Kit 541028A03R05 Hein-Sass-Weg 24
Kit 541028A04R05 21129 HAMBURG
GERMANY
For ordering by internet:
http://spares.airbus.com
For ordering by E-mail: airbus.kit@airbus.com
Telephone Hotlines:
A350/A380: +49 40 743 51775
A330/340, A300/310: +49 40 743 51616
A318/319/320/321: +49 40 743 51660
AIRBUS Material, Logistics and Suppliers do not stock standard hardware as competitive
multiple suppliers ensure access to minimum prices. AIRBUS recommends Customers
with aircraft shown in the effectivity of this Service Bulletin to send a purchase order to
KLX Aerospace Solutions. The address is:
Component COMPA01 AIRBUS MATERIAL AND LOGISTICS

Component COMPA02 MANAGEMENT
Standard Parts
WEG BEIM JAEGER 150
D-22335 HAMBURG
GERMANY
For ordering by internet:
http://spares.airbus.com
For ordering by fax: +49 40 50 76 4004
For ordering by E-mail:
standard.parts@airbus.com
(2) Price and Availability
Kit 541028A01R06
Cost 7,200.00 USD
Availability 210 calendar days from receipt of order
The availability given above is the standard lead time from the date of your purchase
order. If items are required before this time, please include a retrofit planning schedule
with your order so that we can try to comply with your requirements.

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The sales terms (costs and availability) are estimated in relation to economic conditions.
The latest valid price and lead time for ordering purposes shall be obtained through the
AirbusSpares portal or through a request for quotation to airbus.kit@airbus.com.
Kit 541028A02R06
Cost 7,200.00 USD
Kit 541028A03R05
Cost 6,800.00 USD
Kit 541028A04R05
Cost 6,800.00 USD
Component COMPA01
Operator supplied standard hardware parts required to accomplish this Service Bulletin,
are to be supplied from the operator’s stock.
Component COMPA02
Operator supplied standard hardware parts required to accomplish this Service Bulletin,
are to be supplied from the operator’s stock.

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SERVICE BULLETIN
B. INDUSTRY SUPPORT INFORMATION
For Kit 541028A01R06 to Kit 541028A04R05:
AIRBUS will share the costs of accomplishment of this Service Bulletin by providing the kits at
no charge for aircraft equipped with IAE or PW engines and for orders placed before Nov
30/18.
For aircraft equipped with CFM engines, kits are chargeable unless damage has been
detected on CFM pylon Rib 5.
In case of cracked Rib 5 on CFM pylon, AIRBUS will share the cost of accomplishment of this
Service bulletin by providing the kits at no charge for orders placed before Nov 30/18.
Damaged report of cracked Rib 5 has to be sent to AIRBUS retrofit management department.
For Component COMPA01 and Component COMPA02:
For the accomplishment of this Service Bulletin before Nov 30/18, AIRBUS will share the
costs by crediting the operator supplied standard hardware parts. Claims for this allowance
should be received not later than 90 days after completion of the last affected aircraft of your
fleet.
This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign.
For the organisation of this retrofit, you are kindly requested to contact AIRBUS retrofit
management department.
AIRBUS
31707 BLAGNAC CEDEX
France
Tel : (33) 5 67 19 06 22
E-mail : monitored.retrofit@airbus.com
Fax : (33) 5 61 93 27 45
C. LIST OF COMPONENTS
Kit 541028A01R06
ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE
NOTES
2 EN6081D4-24 26 RIVET
3 NAS1169C10L 22 WASHER
4 NAS1153E4 12 SCREW
5 NAS1726C3E 19 NUT
6 NAS6603-2 6 BOLT
7 ASNA2397-10L 6 WASHER
9 EN6081D4X24 13 RIVET
11 D5451884600095 1 RIB
14 D5451887820000 1 COVER

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NOTES
15 NSA5414-32-4 2 RIVET
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL
NOTE: If you find part numbers of hardware components in the related kit(s) which
you cannot identify in the LIST OF COMPONENTS of this Service Bulletin,
refer to Standards Manual (SM). The SM will give you the correct part number
to part number relationship.
Kit 541028A02R06
NOTES
2 EN6081D4-24 26 RIVET
5 NAS1726C3E 19 NUT
6 NAS6603-2 6 BOLT
12 D5451884600195 1 RIB
14 D5451887820000 1 COVER
15 NSA5414-32-4 2 RIVET
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL
Kit 541028A03R05
NOTES
2 EN6081D4-24 13 RIVET
5 NAS1726C3E 19 NUT
6 NAS6603-2 6 BOLT
11 D5451884700095 1 RIB
14 D5451887820000 1 COVER

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NOTES
25 D0041273120095 1 ANGLE
Kit 541028A04R05
NOTES
2 EN6081D4-24 13 RIVET
5 NAS1726C3E 19 NUT
6 NAS6603-2 6 BOLT
12 D5451884700195 1 RIB
14 D5451887820000 1 COVER
25 D0041273120095 1 ANGLE
D. LIST OF MATERIALS - OPERATOR SUPPLIED
(1) Consumable Materials
Consumable CMLA01
ITEM DESCRIPTION REFERENCE TO CML QTY PER A/C SEE

MAT. No. NOTES
Primer Polyurethane Paint - 04EAC2 As required
Corrosion Inhibiting
Top Coat Polyurethane - External 04JAA3 As required
Structure
Varnish-- Electrical Bonding 04TMB2 As required
Structure
Polysulfide Sealant-General 06AAA1 As required
Purpose Brushable
Polysulfide Sealant-General 06AAB1 As required
Purpose Fillet
Polysulfide Sealant-General 06AAC1 As required
Purpose Interfay

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ITEM DESCRIPTION REFERENCE TO CML QTY PER A/C SEE

MAT. No. NOTES
Non Aqueous Cleaner-General 08BAA9 As required
Non Aqueous Cleaner-Methyl-Ethyl- 08BBF1 As required
Ketone
(2) Components
Component COMPA01
NOTES
50 ABS5766BC30 1 (m) TAPE
NOTE: The above list of components is not an AIRBUS Kit, the required parts
shall be ordered as necessary through the given channel.
Component COMPA02
NOTES
13 D5451887920000 8 SHIM
23 D5451887920200 8 SHIM
33 D5451887920400 8 SHIM
(3) Equipment
None
E. PARTS TO BE RE-IDENTIFIED BY OPERATOR
Reidentified part set REIDA01
ITEM NEW PART N˚ KEYWORD ITEM OLD PART N˚ SEE

NOTES
1 D5451880200200 CONE (1) D5451880200000
41 D5451880200201 CONE (41) D5451880200001

NOTES
10 D5451880200300 CONE (10) D5451880200100
42 D5451880200301 CONE (42) D5451880200101

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NOTES
43 D5451880800200 CONE (43) D5451880800000
44 D5451880800201 CONE (44) D5451880800001

NOTES
45 D5451880800300 CONE (45) D5451880800100
46 D5451880800301 CONE (46) D5451880800101

NOTES
28 D5451880003600 FAIRING (28) D5451880000800
(28) D5451880002800
29 D5451880003601 FAIRING (29) D5451880000801
(29) D5451880002801

NOTES
30 D5451880003700 FAIRING (30) D5451880000900
(30) D5451880002900
31 D5451880003701 FAIRING (31) D5451880000901
(31) D5451880002901

NOTES
D0001039000095 FAIRING D0001039000000
D0001039000195 FAIRING D0001039000100

NOTES
D0001039000096 FAIRING D0001039000000
D0001039000196 FAIRING D0001039000100

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NOTES
D0001039000097 FAIRING D0001039000000
D0001039000197 FAIRING D0001039000100
F. TOOLING
None

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3. ACCOMPLISHMENT INSTRUCTIONS
Task 541028-831-801-001 - Modification
WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS
INCLUDED IN THE REFERENCED PROCEDURES.
CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP

ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY
AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE
WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING,
COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO
THIS:
- PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS

NECESSARY ON WIRING AND COMPONENTS.
- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.
THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.
IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00.
NOTE: The accomplishment instructions of this Service Bulletin include procedures given
in other documents or in other sections of the Service Bulletin. When the words
"refer to" are used and the operator has a procedure accepted by the local
authority he belongs to, the accepted alternative procedure can be used. When the
words "in accordance with" are used then the given procedure must be followed.
NOTE: The access and close-up instructions, not comprising return to service tests, in this
Service Bulletin do not constitute or affect the technical intent of the Service
Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or
close-up steps to add flexibility to their maintenance operations as long as the
technical intent of the Service Bulletin is met within the set parameters.
NOTE: Manual titles given in the accomplishment instructions are referred to by acronyms.
Refer to paragraph 1.J., References, for the definition of acronyms.
NOTE: Discarded parts must be managed at the operator’s discretion.
Task Associated Data
**CONF 001
Zone
470 480
Access
Panel 477AL 487AR
Manpower

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**CONF 002
Zone
470 480
Access
Panel 477AL 487AR
Manpower
**CONF 003
Zone
470 480
Access
Panel 477AL 487AR
Manpower
**CONF 004
Zone
470 480
Access
Panel 477AL 487AR
Manpower
**CONF 005
Zone
470 480
Access
Panel 477AL 487AR
Manpower

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**CONF ALL
A. GENERAL
**CONF 001
(1) Subtask 541028-910-001-001 - Standard Practices
Manpower Resources
Skills NON SPECIFIC
References
Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001
06-41-54, Page Block 001
Task 20-21-11-911-001
Task 20-28-00-912-001
Elec. Std. Practices Manual (ESPM) 20-51-20
Structural Repair Manual (SRM) 51-23-00
51-24-00
51-40-00
51-42-00
51-43-00
51-44-00
(a) For the specification of materials (Mat. No.) given in this Service Bulletin, refer to
Consumable Materials List (CML).
(b) For the identification of zones, refer to AMM 06-20-00, Page Block 001.
(c) For the identification of access panels, refer to AMM 06-41-54, Page Block 001.
(d) To torque tighten the standard threaded fasteners, refer to AMM Task
20-21-11-911-001.
(e) If alternative and substitute fasteners have to be used, you must make sure that the
associated nut/collar are compatible in accordance with SRM 51-40-00 "Mating
Part" column.
(f) If the length of any fastener specified in this Service Bulletin does not meet
installation standards given in SRM Chapter 51, then a fastener of the same
specification, or an approved substitute, with a length which meets the installation
standards given in SRM Chapter 51 may be used. In addition, washers may be
installed for fastener grip length in accordance with SRM Chapter 51.
(g) Remove and install fasteners in accordance with SRM 51-42-00.
(h) Apply sealant in accordance with SRM 51-24-00.
(i) Obtain fastener hole diameters and drill data in accordance with SRM 51-44-00.
(j) Obtain alternative and substitute fastener data, in accordance with SRM 51-43-00.

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(k) Cut the rivets to the necessary length.
(l) For the electrical bonding, refer to ESPM 20-51-20 and AMM Task
20-28-00-912-001.
(m) Tag all the parts you must remove and retain to make the subsequent installation
easier.
(n) Renew the protective finish in accordance with SRM 51-23-00.
(2) Subtask 541028-839-001-001 - Administrative
Manpower Resources
Skills NON SPECIFIC
Write in the applicable aircraft records that you have done all the work given in this
Service Bulletin.
**CONF 002
Manpower Resources
Skills NON SPECIFIC
References
06-41-54, Page Block 001
Task 20-21-11-911-001
Task 20-28-00-912-001
51-24-00
51-40-00
51-42-00
51-43-00
51-44-00
20-21-11-911-001.
Part" column.

@A318/A319/A320/A321
SERVICE BULLETIN
20-28-00-912-001.
easier.
Manpower Resources
Skills NON SPECIFIC
Service Bulletin.
**CONF 003
Manpower Resources
Skills NON SPECIFIC
References
06-41-54, Page Block 001
Task 20-21-11-911-001
Task 20-28-00-912-001
51-24-00
51-40-00
51-42-00
51-43-00
51-44-00

@A318/A319/A320/A321
SERVICE BULLETIN
20-21-11-911-001.
Part" column.
20-28-00-912-001.
easier.
Manpower Resources
Skills NON SPECIFIC
Service Bulletin.
**CONF 004
Manpower Resources
Skills NON SPECIFIC

@A318/A319/A320/A321
SERVICE BULLETIN
References
06-41-54, Page Block 001
Task 20-21-11-911-001
Task 20-28-00-912-001
51-24-00
51-40-00
51-42-00
51-43-00
51-44-00
20-21-11-911-001.
Part" column.
20-28-00-912-001.
easier.

@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Skills NON SPECIFIC
Service Bulletin.
**CONF 005
Manpower Resources
Skills NON SPECIFIC
References
06-41-54, Page Block 001
Task 20-21-11-911-001
Task 20-28-00-912-001
51-24-00
51-40-00
51-42-00
51-43-00
51-44-00
20-21-11-911-001.
Part" column.

@A318/A319/A320/A321
SERVICE BULLETIN
20-28-00-912-001.
easier.
Manpower Resources
Skills NON SPECIFIC
Service Bulletin.
**CONF ALL
B. PREPARATION
**CONF 001
(1) Subtask 541028-941-001-001 - Job Set-up on LH Pylon
Work Zones and Access Panels

Zone Access/Work location
470
Manpower Resources
Skills NON SPECIFIC
References
Aircraft Maintenance Manual (AMM) Task 12-34-24-869-002
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001
NOTE: The items given in this note shall be considered as the basic Aircraft
configuration before you start a maintenance task:
- Aircraft on the ground resting on landing gear (the ground safety

locks and the wheel chocks are in position on the landing gear)
- Engine shut down, thrust reversers closed and locked
- Aircraft in clean configuration

@A318/A319/A320/A321
SERVICE BULLETIN
- 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.
(a) Make sure that the aircraft is electrically grounded, refer to AMM Task
12-34-24-869-002.
(b) Put an access platform in position at zone 470.
(c) Put the warning notices in position in the cockpit to tell persons not to operate the
flight controls.
(d) Extend the flaps on the ground, refer to AMM Task 27-50-00-866-008.
(e) Remove the access panel 477AL of LH pylon, refer to AMM Task
54-53-11-000-002 for access.
NOTE: The subsequent procedure can be performed on aircraft or on bench. If

you intend to accomplish this modification on bench, remove the AFT
movable fairing, refer to AMM Task 54-55-00-000-001.
(2) Subtask 541028-941-002-001 - Job Set-up on RH Pylon

480
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001


@A318/A319/A320/A321
SERVICE BULLETIN
12-34-24-869-002.
flight controls.
(e) Remove the access panel 487AR of RH pylon, refer to AMM Task
54-53-11-000-002 for access.

**CONF 002

470
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001


@A318/A319/A320/A321
SERVICE BULLETIN
12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.


480
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001


@A318/A319/A320/A321
SERVICE BULLETIN
12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.

**CONF 003

470
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001


@A318/A319/A320/A321
SERVICE BULLETIN
12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.


480
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001


@A318/A319/A320/A321
SERVICE BULLETIN
12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.

**CONF 004

470
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001

@A318/A319/A320/A321
SERVICE BULLETIN

12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.


480
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001

@A318/A319/A320/A321
SERVICE BULLETIN

12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.

**CONF 005

470
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001

@A318/A319/A320/A321
SERVICE BULLETIN

12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.


480
Manpower Resources
Skills NON SPECIFIC
References
Task 27-50-00-866-008
Task 54-53-11-000-002
Task 54-55-00-000-001

@A318/A319/A320/A321
SERVICE BULLETIN

12-34-24-869-002.
flight controls.
54-53-11-000-002 for access.

**CONF ALL
C. PROCEDURE
**CONF 001
(1) Subtask 541028-831-005-001 - Remove Rib 5 on LH Pylon

470 Access Panel 477AL

@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Manhours 2.00
Minimum number of person 2
Subtask elapsed time 1.75
Skills AIRFRAME
References
Fig. A-FBAAA Sheet 01
Removal of the Tail Cone
Fig. A-FBBAA Sheet 01
Removal of the Rib 5 and the Angle Sheet 02
(a) Remove the old parts:
Refer to Fig. A-FBAAA and Fig. A-FBBAA
In accordance with SRM 51-42-00.
1 Remove the tail cone:
Refer to Fig. A-FBAAA and Fig. A-FBBAA.
1 Tail Cone Item (1) Retain
attached with:
11 Screw Item (2) Discard
11 Washer Item (3) Discard
2 Remove the rivets from the rear angle:
Refer to Fig. A-FBBAA
13 Rivet Item (4) Discard
3 Remove the Rib 5 with the seal assy and rear angle from the fairing:
Refer to Fig. A-FBBAA.
1 Rib 5 Item (11) Discard
1 Seal Assy Item (26) Discard
1 Angle Item (25) Discard
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
(2) Subtask 541028-831-018-001 - Modify LH Fairing

Manpower Resources
Manhours 1.75
Skills AIRFRAME
Material necessary to do the job
Kit 541028A01R06
ITEM NEW PART N˚ QTY (UM) KEYWORD SEE
NOTES
11 D5451884600095 1 RIB

NOTES
28 D5451880003600 FAIRING (28) D5451880000800
(28) D5451880002800
29 D5451880003601 FAIRING (29) D5451880000801
(29) D5451880002801
Consumable CMLA01
ITEM DESCRIPTION REFERENCE TO QTY PER A/C SEE
CML MAT. No. NOTES
Non Aqueous Cleaner- 08BBF1 As required
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001
Process and Material Specification Process and Material Specification (PMS)
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00

@A318/A319/A320/A321
SERVICE BULLETIN
References
Fig. A-FBCAA Sheet 01
Installation of the new Rib 5 Sheet 02
Sheet 03
Sheet 04
Fig. A-FBEAA Sheet 01
Hole Typical view
(a) Clean the surface of the composite parts and the surface of the spar with:
Non Aqueous 08BBF1 As required

Cleaner-Methyl-
Ethyl-Ketone
(b) Install the new parts, refer to Fig. A-FBCAA.
In accordance with SRM 51-40-00, SRM 51-42-00, SRM 51-43-00, SRM 51-44-00,
SRM 51-24-00.
Refer to AMM Task 20-21-11-911-001 and AMM Task 20-28-00-912-001.
Refer to ESPM 20-51-20.
1 Temporarily attach the new Rib 5 on the fairing using the existing holes of the
fairing.
1 Rib D5451884600095 Item 11
2 On the fairing, predrill the new hole at location Y0 through the new Rib 5.
3 Drill to 2.5 mm (0.0984 in.) diameter in the fairing at the hole of Rib 5.
4 Remove the new Rib 5 from the fairing.
NOTE: Drill the fairing, only when Rib 5 is removed.
5 Drill holes to final diameter and countersink 1 hole on the fairing to the
dimension given in Fig. A-FBCAA Sheet 02 thru Fig. A-FBCAA Sheet 04 and
Fig. A-FBEAA.
6 Reidentify the fairing:
Use indelible ink marking, refer to PMS 01-06-12
1 Fairing D5451880002800 Item (28)
or
1 Fairing D5451880000800 Item (28)
becomes
1 Fairing D5451880003600 Item 28

@A318/A319/A320/A321
SERVICE BULLETIN
or
1 Fairing D5451880002801 Item (29)
or
1 Fairing D5451880000801 Item (29)
becomes
1 Fairing D5451880003601 Item 29
NOTE: If old identification PN is not identifiable or erroneous or the

identification plate is missing, the new identification of the
fairing becomes:
1 Fairing D5451880003600 Item 28
7 On the label of the fairing:
a Modify the quantity of the fasteners (+1) and washers (+1), strikethrough
NAS1102E3 and write instead NAS1153E with indelible ink marking.
Refer to PMS 01-06-12
Quantity must be 67.
(3) Subtask 541028-831-009-001 - On Bench, Modify LH Tail Cone

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
11 D5451884600095 RIB
15 NSA5414-32-4 2 RIVET
Component COMPA01
NOTES

@A318/A319/A320/A321
SERVICE BULLETIN
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

NOTES
1 D5451880200200 CONE (1) D5451880200000
41 D5451880200201 CONE (41) D5451880200001
References
(PMS) 01-06-12
Hole Typical view
Fig. A-FBFAA Sheet 01
Installation of the Teflon Tape on the
Tail Cone
Sheet 03
Sheet 04
(a) Remove the shim from the tail cone:
Refer to Fig. A-FBAAA.
1 Shim Item (9) Discard
attached with:
(b) Remove the Teflon tape from the tail cone:
Refer to Fig. A-FBFAA
Teflon Tape Item (50) Discard

@A318/A319/A320/A321
SERVICE BULLETIN
(c) Countersink the holes from the inside and then fill the holes of the removed shim
fasteners on the tail cone with:
2 Rivet NSA5414-32-4 Item 15
(d) Install the Teflon tape on the tail cone:
1 (m) Teflon Tape ABS5766BC30 Item 50
(e) Temporarily attach the new Rib 5 on the tail cone using the existing holes of the tail
cone.
1 Rib D5451884600095 Item 11
(f) Predrill 3 new holes to 2.5 mm (0.0984 in.) from new Rib 5 on to the tail cone.
(g) Through the Rib 5 access hole, measure the gap between the tail cone and the
new Rib 5 as shown on Fig. A-FBCAA Sheet 03, section A-A typical view.
- If the gap measured is between 0 mm and 0.5 mm (0.0197 in.), install the shim
Item 13.
- If the gap measured is between 0.5 mm (0.0197 in.) and 0.8 mm (0.0315 in.),
install the shim Item 23.
- If the gap measured is more than 1.2 mm (0.472 in.), contact AIRBUS.
(h) Remove the new Rib 5 from the tail cone.
NOTE: Drill the tail cone, only when cone is removed from the Rib 5.
(i) Drill holes to final diameter and countersink the holes on the tail cone to the
dimension given in Fig. A-FBCAA Sheet 02 thru Fig. A-FBCAA Sheet 04 and Fig.
A-FBEAA.
(j) Install on the tail cone:
NOTE: According to the gap measured between the new Rib 5 and the tail
cone:
Refer to Fig. A-FBCAA Sheet 03.
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

@A318/A319/A320/A321
SERVICE BULLETIN
or
2 Shim D5451887920400 Item 33
NOTE: The two shims to install can be different according to the gap.
(k) Reidentify the tail cone:
1 Tail Cone D5451880200000 Item (1)
becomes
1 Tail Cone D5451880200200 Item 1

or
1 Tail Cone D5451880200001 Item (41)
becomes
1 Tail Cone D5451880200201 Item 41

identification plate is missing, the new identification of the tail cone
becomes:
1 Tail Cone D5451880200200 Item 1
(l) On the label of the tail cone:
1 Modify the quantity of the fasteners (+3) and washers (+3), strikethrough
(4) Subtask 541028-831-017-001 - Modify and Install LH Rib 5

Manpower Resources
Manhours 8.75
Skills AIRFRAME

@A318/A319/A320/A321
SERVICE BULLETIN
Kit 541028A01R06
NOTES
2 EN6081D4-24 26 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
11 D5451884600095 RIB
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL

NOTES
D0001039000095 FAIRING D0001039000000
Consumable CMLA01
CML MAT. No. NOTES
Top Coat Polyurethane - 04JAA3 As required
External Structure
Purpose Brushable
Purpose Interfay
Non Aqueous Cleaner- 08BAA9 As required
General
References
(PMS) 01-06-12
Sheet 03
Sheet 04
(a) Temporarily put in position the new Rib 5 and the rear angle Item 25 on the spar.
1 Angle D0041273120095 Item 25
(b) Drill the holes on the rear angle Item 25 to align with the holes of the spar.

@A318/A319/A320/A321
SERVICE BULLETIN
(c) Drill 13 holes on new Rib 5 to align the holes of the angle Item 25.
(d) Ream the 26 holes to the dimensions given in Fig. A-FBCAA Sheet 02 and Fig. A-
FBCAA Sheet 04.
(e) Remove from the fairing and the spar the new Rib 5 and the rear angle Item 25.
(f) On bench:
1 Deburr the 26 holes on the new Rib 5.
2 Clean the surfaces to be sealed with:
Non Aqueous 08BAA9 As required

Cleaner-General
3 Temporarily put in position the new Seal Assy on the new Rib 5 using the
positioning holes of the new Rib 5.
1 Seal Bracket D5451886620000 Item 26
1 Seal D5451886820000 Item 27
4 Drill the holes on the new Rib 5 to align with the holes of the new Seal Assy.
5 Ream and deburr the 13 holes to the dimension given in Fig. A-FBCAA Sheet
02 and Fig. A-FBCAA Sheet 04.
(g) Install on the spar:
Refer to Fig. A-FBCAA Sheet 02 and Fig. A-FBCAA Sheet 04.
1 Angle D0041273120095 Item 25
attached with:
13 Rivet EN6081D4X24 Item 9
Attach to angle bracket:
1 Rib D5451884600095 Item 11
with:
13 Rivet EN6081D4-24 Item 2
NOTE: Between the new Rib 5 and the fairing, the spar and the angle
bracket, apply:
In accordance with SRM 51-24-00
Polysulfide Sealant- 06AAC1 As required

General Purpose
Interfay

@A318/A319/A320/A321
SERVICE BULLETIN
NOTE: Wet install the fasteners with:
Polysulfide Sealant- 06AAA1 As required

General Purpose
Brushable
(h) Install the new Rib 5 on the fairing with:
8 Washer NAS1169C10L Item 3
8 Screw NAS1153E5 Item 8
5 Nut NAS1726C3E Item 5

General Purpose
Brushable
(i) Install on the new Rib 5:
1 Seal D5451886820000 Item 27
with:
NOTE: Between the Rib and the Seal Assy, apply:

General Purpose
Interfay

General Purpose
Brushable
(j) Apply primer and paint to all newly installed rivet heads. Use:
Primer 04EAC2 As required

Polyurethane Paint
- Corrosion
Inhibiting

@A318/A319/A320/A321
SERVICE BULLETIN
Top Coat 04JAA3 As required

Polyurethane -
External Structure
(k) Reidentify the fairing assy, label located on the spar:
1 Fairing Assy-Movable, D0001039000000

Painted
becomes

Painted

identification plate is missing, the new identification of the fairing
assy becomes:

Painted
(5) Subtask 541028-831-013-001 - Install LH tail Cone

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
1 D5451880200200 CONE
41 D5451880200201 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References
(PMS) 01-06-12
Sheet 03
Sheet 04
(a) Install the tail cone on the new Rib 5:
1 Tail Cone D5451880200200 Item 1

or
1 Tail Cone D5451880200201 Item 41
with:

@A318/A319/A320/A321
SERVICE BULLETIN
NOTE: Do not put sealant between the tail cone and the Rib 5.

General Purpose
Brushable
(b) Do a seal bead between the fairing and the tail cone with:
Refer to Fig. A-FBCAA.
Polysulfide Sealant- 06AAB1 As required

General Purpose
Fillet
and touch up paint defect with:

Polyurethane -
External Structure
(c) Perform a bonding check:
Refer to ESPM 20-51-20
Refer to AMM Task 20-28-00-912-001
Apply lacquer. Use:
Varnish-- Electrical 04TMB2 As required

Bonding Structure
(d) Install on the new Rib 5:
1 Cover Plate D5451887820000 Item 14
attached with:
6 Washer ASNA2397-10L Item 7
6 Bolt NAS6603-2 Item 6
NOTE: Between the new Rib and the Cover Plate, apply:

General Purpose
Interfay

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Brushable
(e) On the stamp of the access panel 477AL:
Strikethrough NAS1102E3 and write instead NAS1153E with indelible ink marking.
(6) Subtask 541028-831-006-001 - Remove Rib 5 on RH Pylon

480 Access Panel 487AR
Manpower Resources
Manhours 2.00
Skills AIRFRAME
References
(a) Remove the old parts, refer to Fig. A-FBAAA and Fig. A-FBBAA.
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:
(7) Subtask 541028-831-016-001 - Modify RH Fairing

Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
12 D5451884600195 1 RIB

NOTES
30 D5451880003700 FAIRING (30) D5451880000900
(30) D5451880002900
31 D5451880003701 FAIRING (31) D5451880000901
(31) D5451880002901
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone

@A318/A319/A320/A321
SERVICE BULLETIN
References
Task 20-28-00-912-001
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.
fairing.
1 Rib D5451884600195 Item 12
Fig. A-FBEAA.

@A318/A319/A320/A321
SERVICE BULLETIN
1 Fairing D5451880002900 Item (30)
or
1 Fairing D5451880000900 Item (30)
becomes
1 Fairing D5451880003700 Item 30
or
1 Fairing D5451880002901 Item (31)
or
1 Fairing D5451880000901 Item (31)
becomes
1 Fairing D5451880003701 Item 31

fairing becomes:
1 Fairing D5451880003700 Item 30
(8) Subtask 541028-831-010-001 - On Bench, Modify RH Tail Cone

Manpower Resources
Manhours 3.75
Skills AIRFRAME

@A318/A319/A320/A321
SERVICE BULLETIN
Kit 541028A02R06
NOTES
12 D5451884600195 RIB
15 NSA5414-32-4 2 RIVET
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

NOTES
10 D5451880200300 CONE (10) D5451880200100
42 D5451880200301 CONE (42) D5451880200101
References
(PMS) 01-06-12
Hole Typical view
Tail Cone
Sheet 03
Sheet 04

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:
cone.
1 Rib D5451884600195 Item 12
Item 13.
A-FBEAA.

@A318/A319/A320/A321
SERVICE BULLETIN
cone:
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
1 Tail Cone D5451880200100 Item (10)
becomes
1 Tail Cone D5451880200300 Item 10

or
1 Tail Cone D5451880200101 Item (42)
becomes
1 Tail Cone D5451880200301 Item 42

becomes:
1 Tail Cone D5451880200300 Item 10

@A318/A319/A320/A321
SERVICE BULLETIN
(9) Subtask 541028-831-015-001 - Modify and Install RH Rib 5

Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
2 EN6081D4-24 26 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
12 D5451884600195 RIB
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL

NOTES
D0001039000195 FAIRING D0001039000100
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable
Purpose Interfay
General

@A318/A319/A320/A321
SERVICE BULLETIN
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
FBCAA Sheet 04.
(f) On bench:

Cleaner-General
1 Seal D5451886820000 Item 27
1 Angle D0041273120095 Item 25
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
1 Rib D5451884600195 Item 12
with:
bracket, apply:

General Purpose
Interfay

General Purpose
Brushable

General Purpose
Brushable
1 Seal D5451886820000 Item 27
with:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Interfay

General Purpose
Brushable

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

Painted
becomes

Painted

assy becomes:

Painted
(10) Subtask 541028-831-014-001 - Install RH tail Cone

Manpower Resources
Manhours 3.75
Skills AIRFRAME

@A318/A319/A320/A321
SERVICE BULLETIN
Kit 541028A02R06
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
10 D5451880200300 CONE
42 D5451880200301 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880200300 Item 10

@A318/A319/A320/A321
SERVICE BULLETIN
or
1 Tail Cone D5451880200301 Item 42
with:

General Purpose
Brushable

General Purpose
Fillet

Polyurethane -
External Structure
Apply lacquer. Use:

Bonding Structure
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Interfay

General Purpose
Brushable
(e) On the stamp of the access panel 487AR:
**CONF 002

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References
Fig. A-FBAAB Sheet 01
Fig. A-FBBAC Sheet 01
Refer to Fig. A-FBAAB and Fig. A-FBBAC
Refer to Fig. A-FBAAB and Fig. A-FBBAC.

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:
Refer to Fig. A-FBBAC.
3 Remove the Rib 5 with the seal assy and the rear angle from the fairing:
attached with:

Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
11 D5451884700095 1 RIB

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
28 D5451880003600 FAIRING (28) D5451880000800
(28) D5451880002800
29 D5451880003601 FAIRING (29) D5451880000801
(29) D5451880002801
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Fig. A-FBCAB Sheet 01
Sheet 03
Sheet 04
Hole Typical view

Cleaner-Methyl-
Ethyl-Ketone
(b) Install the new parts, refer to Fig. A-FBCAB.
SRM 51-24-00.

@A318/A319/A320/A321
SERVICE BULLETIN
fairing.
1 Rib D5451884700095 Item 11
dimension given in Fig. A-FBCAB Sheet 02 thru Fig. A-FBCAB Sheet 04 and
Fig. A-FBEAA.
1 Fairing D5451880000800 Item (28)
or
1 Fairing D5451880002800 Item (28)
becomes
1 Fairing D5451880003600 Item 28
or
1 Fairing D5451880000801 Item (29)
or
1 Fairing D5451880002801 Item (29)
becomes
1 Fairing D5451880003601 Item 29

fairing becomes:
1 Fairing D5451880003600 Item 28

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
11 D5451884700095 RIB
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

NOTES
43 D5451880800200 CONE (43) D5451880800000
44 D5451880800201 CONE (44) D5451880800001
References
(PMS) 01-06-12

@A318/A319/A320/A321
SERVICE BULLETIN
References
Hole Typical view
Fig. A-FBFAB Sheet 01
Tail Cone
Sheet 03
Sheet 04
(a) Remove the Teflon tape from the tail cone:
Refer to Fig. A-FBFAB
(b) Install the Teflon tape on the tail cone:
(c) Temporarily attach new Rib 5 on the tail cone using the existing holes of the tail
cone.
1 Rib D5451884700095 Item 11
(d) Predrill 3 new holes to 2.5 mm (0.0984 in.) from new Rib 5 on to the tail cone.
(e) Through the Rib 5 access hole, measure the gap between the tail cone and the
new Rib 5 as shown on Fig. A-FBCAB Sheet 03, section A-A typical view.
Item 13.
(f) Remove the new Rib 5 from the tail cone.
(g) Drill holes to final diameter and countersink the holes on the tail cone to the
dimension given in Fig. A-FBCAB Sheet 02 thru Fig. A-FBCAB Sheet 04 and Fig.
A-FBEAA.

@A318/A319/A320/A321
SERVICE BULLETIN
(h) Install on the tail cone:
cone:
Refer to Fig. A-FBCAB Sheet 03.
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
(i) Reidentify the tail cone:
1 Tail Cone D5451880800000 Item (43)
becomes
1 Tail Cone D5451880800200 Item 43

or
1 Tail Cone D5451880800001 Item (44)
becomes
1 Tail Cone D5451880800201 Item 44

becomes:
1 Tail Cone D5451880800200 Item 43
(j) On the label of the tail cone:

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
2 EN6081D4-24 13 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
11 D5451884700095 RIB
25 D0041273120095 1 ANGLE

NOTES
D0001039000096 FAIRING D0001039000000
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable
Purpose Interfay
General
References
(PMS) 01-06-12

@A318/A319/A320/A321
SERVICE BULLETIN
References
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
(d) Ream the 26 holes to the dimensions given in Fig. A-FBCAB Sheet 02 and Fig. A-
FBCAB Sheet 04.
(e) Remove from the fairing and the spar the new Rib 5 and the angle Item 25.
(f) On bench:

Cleaner-General
Refer to Fig. A-FBCAB Sheet 02 and Fig. A-FBCAB Sheet 04.
1 Angle D0041273120095 Item 25
attached with:
attach to angle bracket:
1 Rib D5451884700095 Item 11
with:
bracket, apply:

General Purpose
Interfay

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Brushable

General Purpose
Brushable
(i) Apply primer and paint to all newly installed rivet heads. Use:

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure
(j) Reidentify the fairing assy, label located on the spar:

Painted
becomes

Painted

assy becomes:

Painted

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
43 D5451880800200 CONE
44 D5451880800201 CONE
Consumable CMLA01
CML MAT. No. NOTES
Top Coat Polyurethane - 04JAA3
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References

@A318/A319/A320/A321
SERVICE BULLETIN
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880800200 Item 43

or
1 Tail Cone D5451880800201 Item 44
with:

General Purpose
Brushable
Refer to Fig. A-FBCAB.

General Purpose
Fillet

Polyurethane -
External Structure

@A318/A319/A320/A321
SERVICE BULLETIN
Apply lacquer. Use:

Bonding Structure
attached with:

General Purpose
Interfay

General Purpose
Brushable

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References

@A318/A319/A320/A321
SERVICE BULLETIN
References
Fig. A-FBBAC Sheet 01
(a) Remove the old parts, refer to Fig. A-FBAAB and Fig. A-FBBAC.
Refer to Fig. A-FBAAB and Fig. A-FBBAC.
attached with:
3 Remove the Rib 5 with the seal assy and the rear angle from the fairing:
attached with:


@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A04R05
NOTES
12 D5451884700195 1 RIB

NOTES
30 D5451880003700 FAIRING (30) D5451880000900
(30) D5451880002900
31 D5451880003701 FAIRING (31) D5451880000901
(31) D5451880002901
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

@A318/A319/A320/A321
SERVICE BULLETIN

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.
fairing.
1 Rib D5451884700195 Item 12
Fig. A-FBEAA.
1 Fairing D5451880000900 Item (30)
or
1 Fairing D5451880002900 Item (30)
becomes
1 Fairing D5451880003700 Item 30
or
1 Fairing D5451880000901 Item (31)
or
1 Fairing D5451880002901 Item (31)
becomes

@A318/A319/A320/A321
SERVICE BULLETIN
1 Fairing D5451880003701 Item 31

fairing becomes:
1 Fairing D5451880003700 Item 30
Manpower Resources
Manhours 3.75
Skills NON SPECIFIC
Kit 541028A04R05
NOTES
12 D5451884700195 RIB
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
45 D5451880800300 CONE (45) D5451880800100
46 D5451880800301 CONE (46) D5451880800101
References
(PMS) 01-06-12
Hole Typical view
Tail Cone
Sheet 03
Sheet 04
(c) Temporarily attach the new Rib 5 on the tail cone using the existing holes of the tail
cone.
1 Rib D5451884700195 Item 12
Item 13.

@A318/A319/A320/A321
SERVICE BULLETIN
(f) Remove the tail cone from the new Rib 5.
A-FBEAA.
cone:
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
1 Tail Cone D5451880800100 Item (45)
becomes
1 Tail Cone D5451880800300 Item 45

or
1 Tail Cone D5451880800101 Item (46)
becomes
1 Tail Cone D5451880800301 Item 46

becomes:
1 Tail Cone D5451880800300 Item 45

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A04R05
NOTES
2 EN6081D4-24 13 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
12 D5451884700195 RIB
25 D0041273120095 1 ANGLE

NOTES
D0001039000196 FAIRING D0001039000100
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable

@A318/A319/A320/A321
SERVICE BULLETIN

CML MAT. No. NOTES
Purpose Interfay
General
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
FBCAB Sheet 04.
(f) On bench:

Cleaner-General
1 Angle D0041273120095 Item 25
attached with:
1 Rib D5451884700195 Item 12
with:

@A318/A319/A320/A321
SERVICE BULLETIN
bracket, apply:

General Purpose
Interfay

General Purpose
Brushable

General Purpose
Brushable

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

Painted
becomes

@A318/A319/A320/A321
SERVICE BULLETIN

Painted

assy becomes:

Painted

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A04R05
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
45 D5451880800300 CONE
46 D5451880800301 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure

@A318/A319/A320/A321
SERVICE BULLETIN

CML MAT. No. NOTES
Purpose Brushable
Purpose Fillet
Purpose Interfay
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880800300 Item 45

or
1 Tail Cone D5451880800301 Item 46
with:

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Fillet

Polyurethane -
External Structure
Apply lacquer. Use:

Bonding Structure
attached with:

General Purpose
Interfay

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 003

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:

Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
11 D5451884600095 1 RIB

NOTES
28 D5451880003600 FAIRING (28) D5451880000800
(28) D5451880002800
29 D5451880003601 FAIRING (29) D5451880000801
(29) D5451880002801
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001

@A318/A319/A320/A321
SERVICE BULLETIN
References
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.
fairing.
1 Rib D5451884600095 Item 11
Fig. A-FBEAA.
1 Fairing D5451880002800 Item (28)

@A318/A319/A320/A321
SERVICE BULLETIN
or
1 Fairing D5451880000800 Item (28)
becomes
1 Fairing D5451880003600 Item 28
or
1 Fairing D5451880002801 Item (29)
or
1 Fairing D5451880000801 Item (29)
becomes
1 Fairing D5451880003601 Item 29

fairing becomes:
1 Fairing D5451880003600 Item 28

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
11 D5451884600095 RIB

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
15 NSA5414-32-4 2 RIVET
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

NOTES
1 D5451880200200 CONE (1) D5451880200000
41 D5451880200201 CONE (41) D5451880200001
References
(PMS) 01-06-12
Hole Typical view
Tail Cone
Sheet 03
Sheet 04
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
cone.
1 Rib D5451884600095 Item 11
Item 13.
A-FBEAA.
cone:

@A318/A319/A320/A321
SERVICE BULLETIN
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
1 Tail Cone D5451880200000 Item (1)
becomes
1 Tail Cone D5451880200200 Item 1

or
1 Tail Cone D5451880200001 Item (41)
becomes
1 Tail Cone D5451880200201 Item 41

becomes:
1 Tail Cone D5451880200200 Item 1


@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
2 EN6081D4-24 26 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
11 D5451884600095 RIB
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL

NOTES
D0001039000095 FAIRING D0001039000000
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable
Purpose Interfay
General
References
(PMS) 01-06-12
Sheet 03
Sheet 04

@A318/A319/A320/A321
SERVICE BULLETIN
1 Angle D0041273120095 Item 25
FBCAA Sheet 04.
(f) On bench:

Cleaner-General
1 Seal D5451886820000 Item 27
1 Angle D0041273120095 Item 25
attached with:
1 Rib D5451884600095 Item 11
with:
bracket, apply:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Interfay

General Purpose
Brushable

General Purpose
Brushable
1 Seal D5451886820000 Item 27
with:

General Purpose
Interfay

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

Painted
becomes

Painted

assy becomes:

Painted

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
1 D5451880200200 CONE
41 D5451880200201 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880200200 Item 1

or
1 Tail Cone D5451880200201 Item 41
with:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Brushable

General Purpose
Fillet

Polyurethane -
External Structure
Apply lacquer. Use:

Bonding Structure
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Interfay

General Purpose
Brushable

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:

Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
12 D5451884600195 1 RIB

NOTES
30 D5451880003700 FAIRING (30) D5451880000900
(30) D5451880002900
31 D5451880003701 FAIRING (31) D5451880000901
(31) D5451880002901

@A318/A319/A320/A321
SERVICE BULLETIN
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.
fairing.
1 Rib D5451884600195 Item 12

@A318/A319/A320/A321
SERVICE BULLETIN
Fig. A-FBEAA.
1 Fairing D5451880002900 Item (30)
or
1 Fairing D5451880000900 Item (30)
becomes
1 Fairing D5451880003700 Item 30
or
1 Fairing D5451880002901 Item (31)
or
1 Fairing D5451880000901 Item (31)
becomes
1 Fairing D5451880003701 Item 31

fairing becomes:
1 Fairing D5451880003700 Item 30


@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
12 D5451884600195 RIB
15 NSA5414-32-4 2 RIVET
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

NOTES
10 D5451880200300 CONE (10) D5451880200100
42 D5451880200301 CONE (42) D5451880200101
References
(PMS) 01-06-12
Hole Typical view
Tail Cone

@A318/A319/A320/A321
SERVICE BULLETIN
References
Sheet 03
Sheet 04
attached with:
cone.
1 Rib D5451884600195 Item 12
Item 13.

@A318/A319/A320/A321
SERVICE BULLETIN
A-FBEAA.
cone:
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
1 Tail Cone D5451880200100 Item (10)
becomes
1 Tail Cone D5451880200300 Item 10

or
1 Tail Cone D5451880200101 Item (42)
becomes
1 Tail Cone D5451880200301 Item 42

becomes:
1 Tail Cone D5451880200300 Item 10

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
2 EN6081D4-24 26 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
12 D5451884600195 RIB
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL

NOTES
D0001039000195 FAIRING D0001039000100
Consumable CMLA01
CML MAT. No. NOTES
External Structure

@A318/A319/A320/A321
SERVICE BULLETIN

CML MAT. No. NOTES
Purpose Brushable
Purpose Interfay
General
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
FBCAA Sheet 04.
(f) On bench:

Cleaner-General
1 Seal D5451886820000 Item 27

@A318/A319/A320/A321
SERVICE BULLETIN
1 Angle D0041273120095 Item 25
attached with:
1 Rib D5451884600195 Item 12
with:
bracket, apply:

General Purpose
Interfay

General Purpose
Brushable

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN
1 Seal D5451886820000 Item 27
with:

General Purpose
Interfay

General Purpose
Brushable

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

Painted
becomes

Painted

assy becomes:

Painted

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
10 D5451880200300 CONE
42 D5451880200301 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References

@A318/A319/A320/A321
SERVICE BULLETIN
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880200300 Item 10

or
1 Tail Cone D5451880200301 Item 42
with:

General Purpose
Brushable

General Purpose
Fillet

Polyurethane -
External Structure

@A318/A319/A320/A321
SERVICE BULLETIN
Apply lacquer. Use:

Bonding Structure
attached with:

General Purpose
Interfay

General Purpose
Brushable
**CONF 004

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References

@A318/A319/A320/A321
SERVICE BULLETIN
References
attached with:
attached with:


@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
11 D5451884600095 1 RIB

NOTES
28 D5451880003600 FAIRING (28) D5451880000800
(28) D5451880002800
29 D5451880003601 FAIRING (29) D5451880000801
(29) D5451880002801
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

@A318/A319/A320/A321
SERVICE BULLETIN

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.
fairing.
1 Rib D5451884600095 Item 11
Fig. A-FBEAA.
1 Fairing D5451880002800 Item (28)
or
1 Fairing D5451880000800 Item (28)
becomes
1 Fairing D5451880003600 Item 28
or
1 Fairing D5451880002801 Item (29)
or
1 Fairing D5451880000801 Item (29)
becomes

@A318/A319/A320/A321
SERVICE BULLETIN
1 Fairing D5451880003601 Item 29

fairing becomes:
1 Fairing D5451880003600 Item 28

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
11 D5451884600095 RIB
15 NSA5414-32-4 2 RIVET
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
33 D5451887920400 2 SHIM

NOTES
1 D5451880200200 CONE (1) D5451880200000
41 D5451880200201 CONE (41) D5451880200001
References
(PMS) 01-06-12
Hole Typical view
Tail Cone
Sheet 03
Sheet 04
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
cone.
1 Rib D5451884600095 Item 11
Item 13.
A-FBEAA.
cone:
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33

@A318/A319/A320/A321
SERVICE BULLETIN
1 Tail Cone D5451880200000 Item (1)
becomes
1 Tail Cone D5451880200200 Item 1

or
1 Tail Cone D5451880200001 Item (41)
becomes
1 Tail Cone D5451880200201 Item 41

becomes:
1 Tail Cone D5451880200200 Item 1

Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
2 EN6081D4-24 26 RIVET

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
11 D5451884600095 RIB
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL

NOTES
D0001039000095 FAIRING D0001039000000
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable
Purpose Interfay
General
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
FBCAA Sheet 04.

@A318/A319/A320/A321
SERVICE BULLETIN
(f) On bench:

Cleaner-General
1 Seal D5451886820000 Item 27
1 Angle D0041273120095 Item 25
attached with:
1 Rib D5451884600095 Item 11
with:
bracket, apply:

General Purpose
Interfay

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Brushable
1 Seal D5451886820000 Item 27
with:

General Purpose
Interfay

General Purpose
Brushable

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

@A318/A319/A320/A321
SERVICE BULLETIN

Painted
becomes

Painted

assy becomes:

Painted

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A01R06
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
1 D5451880200200 CONE
41 D5451880200201 CONE

@A318/A319/A320/A321
SERVICE BULLETIN
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880200200 Item 1

or
1 Tail Cone D5451880200201 Item 41
with:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Brushable

General Purpose
Fillet

Polyurethane -
External Structure
Apply lacquer. Use:

Bonding Structure
attached with:

General Purpose
Interfay

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:

Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
12 D5451884600195 1 RIB

NOTES
30 D5451880003700 FAIRING (30) D5451880000900
(30) D5451880002900
31 D5451880003701 FAIRING (31) D5451880000901
(31) D5451880002901
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001

@A318/A319/A320/A321
SERVICE BULLETIN
References
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.
fairing.
1 Rib D5451884600195 Item 12
Fig. A-FBEAA.

@A318/A319/A320/A321
SERVICE BULLETIN
1 Fairing D5451880002900 Item (30)
or
1 Fairing D5451880000900 Item (30)
becomes
1 Fairing D5451880003700 Item 30
or
1 Fairing D5451880002901 Item (31)
or
1 Fairing D5451880000901 Item (31)
becomes
1 Fairing D5451880003701 Item 31

fairing becomes:
1 Fairing D5451880003700 Item 30

Manpower Resources
Manhours 3.75
Skills AIRFRAME

@A318/A319/A320/A321
SERVICE BULLETIN
Kit 541028A02R06
NOTES
12 D5451884600195 RIB
15 NSA5414-32-4 2 RIVET
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

NOTES
10 D5451880200300 CONE (10) D5451880200100
42 D5451880200301 CONE (42) D5451880200101
References
(PMS) 01-06-12
Hole Typical view
Tail Cone
Sheet 03
Sheet 04

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:
cone.
1 Rib D5451884600195 Item 12
Item 13.
A-FBEAA.

@A318/A319/A320/A321
SERVICE BULLETIN
cone:
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
1 Tail Cone D5451880200100 Item (10)
becomes
1 Tail Cone D5451880200300 Item 10

or
1 Tail Cone D5451880200101 Item (42)
becomes
1 Tail Cone D5451880200301 Item 42

becomes:
1 Tail Cone D5451880200300 Item 10

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A02R06
NOTES
2 EN6081D4-24 26 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
12 D5451884600195 RIB
25 D0041273120095 1 ANGLE
26 D5451886620000 1 BRACKET
27 D5451886820000 1 SEAL

NOTES
D0001039000195 FAIRING D0001039000100
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable
Purpose Interfay
General

@A318/A319/A320/A321
SERVICE BULLETIN
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
FBCAA Sheet 04.
(f) On bench:

Cleaner-General
1 Seal D5451886820000 Item 27
1 Angle D0041273120095 Item 25
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN
1 Rib D5451884600195 Item 12
with:
bracket, apply:

General Purpose
Interfay

General Purpose
Brushable

General Purpose
Brushable
1 Seal D5451886820000 Item 27
with:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Interfay

General Purpose
Brushable

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

Painted
becomes

Painted

assy becomes:

Painted

Manpower Resources
Manhours 3.75
Skills AIRFRAME

@A318/A319/A320/A321
SERVICE BULLETIN
Kit 541028A02R06
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
10 D5451880200300 CONE
42 D5451880200301 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880200300 Item 10

@A318/A319/A320/A321
SERVICE BULLETIN
or
1 Tail Cone D5451880200301 Item 42
with:

General Purpose
Brushable

General Purpose
Fillet

Polyurethane -
External Structure
Apply lacquer. Use:

Bonding Structure
attached with:

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Interfay

General Purpose
Brushable
**CONF 005

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References
Fig. A-FBBAB Sheet 01
Refer to Fig. A-FBAAB and Fig. A-FBBAB
Refer to Fig. A-FBAAB and Fig. A-FBBAB.

@A318/A319/A320/A321
SERVICE BULLETIN
attached with:
Refer to Fig. A-FBBAB.
3 Remove the Rib 5 and the rear angle from the fairing:
attached with:

Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
11 D5451884700095 1 RIB

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
28 D5451880003600 FAIRING (28) D5451880000800
(28) D5451880002800
29 D5451880003601 FAIRING (29) D5451880000801
(29) D5451880002801
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.

@A318/A319/A320/A321
SERVICE BULLETIN
fairing.
1 Rib D5451884700095 Item 11
Fig. A-FBEAA.
1 Fairing D5451880000800 Item (28)
or
1 Fairing D5451880002800 Item (28)
becomes
1 Fairing D5451880003600 Item 28
or
1 Fairing D5451880000801 Item (29)
or
1 Fairing D5451880002801 Item (29)
becomes
1 Fairing D5451880003601 Item 29

fairing becomes:
1 Fairing D5451880003600 Item 28

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
11 D5451884700095 RIB
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

NOTES
43 D5451880800200 CONE (43) D5451880800000
44 D5451880800201 CONE (44) D5451880800001
References
(PMS) 01-06-12

@A318/A319/A320/A321
SERVICE BULLETIN
References
Hole Typical view
Tail Cone
Sheet 03
Sheet 04
(c) Temporarily attach the new Rib 5 on the tail using the existing holes of the tail
cone.
1 Rib D5451884700095 Item 11
Item 13.
(f) Remove new Rib 5 from the tail cone.
(g) Drill holes to final diameter and and countersink the holes on the tail cone to the
A-FBEAA.

@A318/A319/A320/A321
SERVICE BULLETIN
cone:
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
1 Tail Cone D5451880800000 Item (43)
becomes
1 Tail Cone D5451880800200 Item 43

or
1 Tail Cone D5451880800001 Item (44)
becomes
1 Tail Cone D5451880800201 Item 44

becomes:
1 Tail Cone D5451880800200 Item 43
1 Modify the quantity of the fasteners (+3) and washers(+3), strikethrough


@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
2 EN6081D4-24 13 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
11 D5451884700095 RIB
25 D0041273120095 1 ANGLE

NOTES
D0001039000097 FAIRING D0001039000000
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable
Purpose Interfay
General
References
(PMS) 01-06-12

@A318/A319/A320/A321
SERVICE BULLETIN
References
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
FBCAB Sheet 04.
(f) On bench:

Cleaner-General
1 Angle D0041273120095 Item 25
attached with:
1 Rib D5451884700095 Item 11
with:
bracket, apply:

General Purpose
Interfay

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Brushable

General Purpose
Brushable

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

Painted
becomes

Painted

assy becomes:

Painted

@A318/A319/A320/A321
SERVICE BULLETIN

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A03R05
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
43 D5451880800200 CONE
44 D5451880800201 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure
Purpose Brushable
Purpose Fillet
Purpose Interfay
References

@A318/A319/A320/A321
SERVICE BULLETIN
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880800200 Item 43

or
1 Tail Cone D5451880800201 Item 44
with:

General Purpose
Brushable
Refer to Fig. A-FBCAB

General Purpose
Fillet

Polyurethane -
External Structure

@A318/A319/A320/A321
SERVICE BULLETIN
Apply lacquer. Use:

Bonding Structure
Refer to Fig. A-FBCAB Sheet 02 and Fig. A-FBCAB Sheet 04
attached with:

General Purpose
Interfay

General Purpose
Brushable

Manpower Resources
Manhours 2.00
Skills AIRFRAME
References

@A318/A319/A320/A321
SERVICE BULLETIN
References
Fig. A-FBBAB Sheet 01
(a) Remove the old parts, refer to Fig. A-FBAAB and Fig. A-FBBAB.
Refer to Fig. A-FBAAB and Fig. A-FBBAB.
attached with:
3 Remove the Rib 5 and the rear angle from the fairing:
attached with:


@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Manhours 1.75
Skills AIRFRAME
Kit 541028A04R05
NOTES
12 D5451884700195 1 RIB

NOTES
30 D5451880003700 FAIRING (30) D5451880000900
(30) D5451880002900
31 D5451880003701 FAIRING (31) D5451880000901
(31) D5451880002901
Consumable CMLA01
CML MAT. No. NOTES
Methyl-Ethyl-Ketone
References
Task 20-28-00-912-001
(PMS) 01-06-12
51-40-00
51-42-00
51-43-00
51-44-00
Sheet 03
Sheet 04
Hole Typical view

@A318/A319/A320/A321
SERVICE BULLETIN

Cleaner-Methyl-
Ethyl-Ketone
SRM 51-24-00.
fairing.
1 Rib D5451884700195 Item 12
Fig. A-FBEAA.
1 Fairing D5451880000900 Item (30)
or
1 Fairing D5451880002900 Item (30)
becomes
1 Fairing D5451880003700 Item 30
or
1 Fairing D5451880000901 Item (31)
or
1 Fairing D5451880002901 Item (31)
becomes

@A318/A319/A320/A321
SERVICE BULLETIN
1 Fairing D5451880003701 Item 31

fairing becomes:
1 Fairing D5451880003700 Item 30
Manpower Resources
Manhours 3.75
Skills NON SPECIFIC
Kit 541028A04R05
NOTES
12 D5451884700195 RIB
Component COMPA01
NOTES
Component COMPA02
NOTES
13 D5451887920000 2 SHIM
23 D5451887920200 2 SHIM
33 D5451887920400 2 SHIM

@A318/A319/A320/A321
SERVICE BULLETIN

NOTES
45 D5451880800300 CONE (45) D5451880800100
46 D5451880800301 CONE (46) D5451880800101
References
(PMS) 01-06-12
Hole Typical view
Tail Cone
Sheet 03
Sheet 04
(c) Temporarily attach new Rib 5 on the tail cone using the existing holes of the tail
cone.
1 Rib D5451884700195 Item 12
Item 13.

@A318/A319/A320/A321
SERVICE BULLETIN
(f) Remove the tail cone from the new Rib 5.
dimension given in Fig. A-FBCAB Sheet 02 thru Fig. A-FBCAB Sheet 04.and Fig.
A-FBEAA.
cone:
2 Shim D5451887920000 Item 13

or
2 Shim D5451887920200 Item 23

or
2 Shim D5451887920400 Item 33
1 Tail Cone D5451880800100 Item (45)
becomes
1 Tail Cone D5451880800300 Item 45

or
1 Tail Cone D5451880800101 Item (46)
becomes
1 Tail Cone D5451880800301 Item 46

becomes:
1 Tail Cone D5451880800300 Item 45

@A318/A319/A320/A321
SERVICE BULLETIN
1 Modify the quantity of the fasteners (+3) and washers(+3), strikethrough


Manpower Resources
Manhours 8.75
Skills AIRFRAME
Kit 541028A04R05
NOTES
2 EN6081D4-24 13 RIVET
5 NAS1726C3E 5 NUT
8 NAS1153E5 8 SCREW
12 D5451884700195 RIB
25 D0041273120095 1 ANGLE

NOTES
D0001039000197 FAIRING D0001039000100
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Purpose Brushable

@A318/A319/A320/A321
SERVICE BULLETIN

CML MAT. No. NOTES
Purpose Interfay
General
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Angle D0041273120095 Item 25
FBCAB Sheet 04.
(f) On bench:

Cleaner-General
1 Angle D0041273120095 Item 25
attached with:
1 Rib D5451884700195 Item 12
with:

@A318/A319/A320/A321
SERVICE BULLETIN
bracket, apply:

General Purpose
Interfay

General Purpose
Brushable

General Purpose
Brushable

Polyurethane Paint
- Corrosion
Inhibiting

Polyurethane -
External Structure

Painted
becomes

@A318/A319/A320/A321
SERVICE BULLETIN

Painted

assy becomes:

Painted

Manpower Resources
Manhours 3.75
Skills AIRFRAME
Kit 541028A04R05
NOTES
5 NAS1726C3E 14 NUT
6 NAS6603-2 6 BOLT
8 NAS1153E5 2 SCREW
14 D5451887820000 1 COVER

NOTES
45 D5451880800300 CONE
46 D5451880800301 CONE
Consumable CMLA01
CML MAT. No. NOTES
External Structure
Structure

@A318/A319/A320/A321
SERVICE BULLETIN

CML MAT. No. NOTES
Purpose Brushable
Purpose Fillet
Purpose Interfay
References
(PMS) 01-06-12
Sheet 03
Sheet 04
1 Tail Cone D5451880800300 Item 45

or
1 Tail Cone D5451880800301 Item 46
with:

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN

General Purpose
Fillet

Polyurethane -
External Structure
Apply lacquer. Use:

Bonding Structure
attached with:

General Purpose
Interfay

General Purpose
Brushable

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF ALL
D. TEST
**CONF 001
None
**CONF 002
None
**CONF 003
None
**CONF 004
None
**CONF 005
None
**CONF ALL
E. CLOSE-UP
**CONF 001
(1) Subtask 541028-942-001-001 - Close-up on LH Pylon

470
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
NOTE: If necessary, install the AFT movable fairing, refer to AMM Task
54-55-00-400-001.
(a) Make sure that the work areas are clean and clear of tools and other items of
equipment.
(b) Remove the access platform(s).
(c) Remove the warning notices in the cockpit.

@A318/A319/A320/A321
SERVICE BULLETIN
(d) Retract the flaps on the Ground, refer to AMM Task 27-50-00-866-009.
(e) Install the access panel 477AL of LH pylon, refer to AMM Task 54-53-11-400-002.
(f) Put the aircraft back to its initial configuration.
(2) Subtask 541028-942-002-001 - Close-up on RH Pylon

480
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.
equipment.
(e) Install the access panel 487AR of RH pylon, refer to AMM Task 54-53-11-400-002.
**CONF 002

470
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001

@A318/A319/A320/A321
SERVICE BULLETIN
54-55-00-400-001.
equipment.

480
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.
equipment.
**CONF 003

470

@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.
equipment.

480
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.
equipment.

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 004

470
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.
equipment.

480
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.

@A318/A319/A320/A321
SERVICE BULLETIN
equipment.
**CONF 005

470
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.
equipment.

480

@A318/A319/A320/A321
SERVICE BULLETIN
Manpower Resources
Skills NON SPECIFIC
References
Task 54-53-11-400-002
Task 54-55-00-400-001
54-55-00-400-001.
equipment.

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
A
A LH SHOWN
RH SYMMETRICAL
(1) LH
(10) RH
(2)
(3)
01
(2)
(3)
(9)
(2)
(3) (15)
(2)
(3)
(28)OR (29) LH
(30)OR (31) RH
477AL
(487AR)
B
LH SHOWN
RH SYMMETRICAL
NOTE:
FASTENERS NOT AFFECTED
01 FILL THE HOLES WITH RIVETS ITEM 15 N_SB_541028_5_BAAA_01_03
Figure A-FBAAA - Sheet 01


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002, 005
A A
LH SHOWN
RH SYMMETRICAL
(1) LH
(10) RH
(2)
(3)
(2)
(3)
(2)
(3)
(2)
(3)
(32) OR (33) LH
(34) OR (35) RH
477AL
(487AR)
B
LH SHOWN
RH SYMMETRICAL
NOTE:
FASTENERS NOT AFFECTED N_SB_541028_5_BAAB_01_03
Figure A-FBAAB - Sheet 01


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
RIB5
A A
LH SHOWN
RH SYMMETRICAL
B
LH SHOWN
RH SYMMETRICAL
N_SB_541028_5_BBAA_01_01
Figure A-FBBAA - Sheet 01

Removal of the Rib 5 and the Angle

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
RIB5 (11) LH
(12) RH
(3)
(5)
(3)
(5)
(3)
(5)
(3)
(5) C (3)
(5)
RIB5
(26)
(11) LH
(4) x13 (12) RH
(25)
(28)OR (29)LH
(30)OR (31)RH
D
N_SB_541028_5_BBAA_02_02
Figure A-FBBAA - Sheet 02


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 005
RIB5
A A
LH SHOWN
RH SYMMETRICAL
B
LH SHOWN
RH SYMMETRICAL
N_SB_541028_5_BBAB_01_01
Figure A-FBBAB - Sheet 01


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 005
RIB5 (11) LH
(12) RH
(3)
(5)
(3)
(5)
(3)
(5)
(3)
(5) C (3)
(5)
RIB5 (11) LH
(12) RH
(4) x13
(25)
(32) OR (33) LH
(34) OR (35) RH
D
N_SB_541028_5_BBAB_02_04
Figure A-FBBAB - Sheet 02


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002
RIB5
A A
LH SHOWN
RH SYMMETRICAL
C
D
B
LH SHOWN
RH SYMMETRICAL
N_SB_541028_5_BBAC_01_00
Figure A-FBBAC - Sheet 01


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002
RIB5 (11) LH
(12) RH
(3)
(5)
(3)
(5)
(3)
(5)
(3)
(5) C (3)
(5)
(26)
(4) x13
RIB5
(11) LH
(12) RH
(25)
(32) OR (33) LH
(34) OR (35) RH
D
N_SB_541028_5_BBAC_02_02
Figure A-FBBAC - Sheet 02


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
RIB5
A A
LH SHOWN
RH SYMMETRICAL
N_SB_541028_5_BCAA_01_03
Figure A-FBCAA - Sheet 01

Installation of the new Rib 5

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
27
04 14
11LH 26
12 RH
06
25
04
C
03
TAIL CONE
1 OR 41 LH
10 OR 42 RH
02
28 OR 29 LH
30 OR 31 RH
01
FAIRING
Y=0 04
D
N_SB_541028_5_BCAA_02_04


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
1 LH
10 RH TAIL CONE
05
05
05
A
05
A
E
13
OR
23
OR
33
11 LH
12 RH
RIB5
A A
TYPICAL VIEW
N_SB_541028_5_BCAA_03_05


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
HOLE FINAL HOLE DIAMETER

ITEM PN DESCRIPTION
SYMBOL MIN MAX
3.250 mm 3.350 mm
(4) 2 EN6081D4−24 RIVET (0.128 in) (0.132 in)
(3) 3 NAS1169C10L WASHER
(5) 8 NAS1153E5 SCREW
5 NAS1726C3E NUT
5 NAS1726C3E NUT
6 NAS6603−2 SCREW
7 ASNA2397−10L WASHER
3 NAS1169C10L WASHER
8 NAS1153E5 SCREW
5 NAS1726C3E NUT
3.66 mm 3.76 mm
(4) 9 EN6081D4X24 RIVET (0.144 in) (0.148 in)
NOTE:
WET INSTALL ALL FASTENERS WITH MATERIAL No 06AAA1
APPLY INTERFAY SEALANT BETWEEN METALLIC PARTS WITH MATERIAL No 06AAC1
PROTECT THE NEWLY INSTALLED RIVET HEADS WITH MATERIAL No 04EAC2 AND 04JAA3
01 DRILL AND COUNTERSINK 1 HOLE ON THE FAIRING AT Y0
02 DRILL AND COUNTERSINK 3 HOLES ON THE TAIL CONE
03 MAKE A SEAL BEAD BETWEEN FAIRING AND TAIL CONE WITH MATERIAL No 06AAB1 AND TOUCH UP
PAINT DEFECT WITH MATERIAL No 04JAA3
04 DO THE 3 ELECTRICAL BONDING ON THE FAIRING. APPLY MATERIAL No 04TMB2
05 DO THE 4 ELECTRICAL BONDING ON THE TAIL CONE. APPLY MATERIAL No 04TMB2
06 NEW FASTENERS TO BE INSTALLED DURING INSTALLATION OF THE ACCESS PANEL
N_SB_541028_5_BCAA_04_07


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002, 005
RIB5
A
A LH SHOWN
RH SYMMETRICAL
D B
LH SHOWN
RH SYMMETRICAL
N_SB_541028_5_BCAB_01_03
Figure A-FBCAB - Sheet 01


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002, 005
04 14
11 LH
12 RH
06
25
04
C
03
TAIL CONE
43 OR 44 LH
45 OR 46 RH
02
28 OR 29 LH
30 OR 31 RH
01
FAIRING
Y=0 04
D
N_SB_541028_5_BCAB_02_04


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002, 005
43 OR 44 LH
05 45 OR 46 RH
TAIL CONE
05
05
A
05
E
13
OR
23
OR
33
11 LH
12 RH
RIB5
A A
TYPICAL VIEW
N_SB_541028_5_BCAB_03_06


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002, 005
HOLE FINAL HOLE DIAMETER

ITEM PN DESCRIPTION
SYMBOL MIN MAX
3.250 mm 3.350 mm
(4) 2 EN6081D4−24 RIVET (0.128 in) (0.132 in)
5 NAS1726C3E NUT
5 NAS1726C3E NUT
6 NAS6603−2 SCREW
7 ASNA2397−10L WASHER
3 NAS1169C10L WASHER
8 NAS1153E5 SCREW
5 NAS1726C3E NUT
3.66 mm 3.76 mm
(4) 9 EN6081D4X24 RIVET (0.144 in) (0.148 in)
NOTE:
WET INSTALL ALL FASTENERS WITH MATERIAL No 06AAA1
APPLY INTERFAY SEALANT BETWEEN METALLIC PARTS WITH MATERIAL No 06AAC1
PROTECT THE NEWLY INSTALLED RIVET HEADS WITH MATERIAL No 04EAC2 AND 04JAA3
01 DRILL AND COUNTERSINK 1 HOLE ON THE FAIRING AT Y0
02 DRILL AND COUNTERSINK 3 HOLES ON THE TAIL CONE
03 MAKE A SEAL BEAD BETWEEN FAIRING AND TAIL CONE WITH MATERIAL No 06AAB1 AND TOUCH UP
PAINT DEFECT WITH MATERIAL No 04JAA3
04 DO THE 3 ELECTRICAL BONDING ON THE FAIRING. APPLY MATERIAL No 04TMB2
05 DO THE 4 ELECTRICAL BONDING ON THE TAIL CONE. APPLY MATERIAL No 04TMB2
06 NEW FASTENERS TO BE INSTALLED DURING INSTALLATION OF THE ACCESS PANEL
N_SB_541028_5_BCAB_04_07


@A318/A319/A320/A321
SERVICE BULLETIN
**CONF ALL
TAIL CONE
OR +0.1° +0.2 mm
FAIRING 100° 0° 2.2 mm 0 mm
(0.086 in) (+0.007 in)
(0 in)
+0.2 mm
6.4 mm 0 mm
(0.252 in) (+0.007 in)

(0 in)
N_SB_541028_5_BEAA_01_00
Figure A-FBEAA - Sheet 01

Hole Typical view

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 001, 003 thru 004
ON BENCH
13 mm
(0.512 in)
C
13 mm (50)
01
50
C (0.512 in)
FWD A
13 mm
(0.512 in)
(50)
01
50
(50)
01 13 mm
50
13 mm (0.512 in)
(0.512 in)
122 mm
(4.803 in)
13 mm
(0.512 in)
F
FWD B W C (50)
01
D 50
NOTE:
01 TEFLON PART ADHESIVE TAPE ITEM 50 STORAGE TIME EXCEEDANCE IS ACCEPTABLE
AS LONG AS THE GRIP IS SUFFICIENT FOR PART INSTALLATION N_SB_541028_5_BFAA_01_01
Figure A-FBFAA - Sheet 01

Installation of the Teflon Tape on the Tail Cone

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF 002, 005
ON BENCH
13 mm
(0.512 in)
13 mm (50)
01
50
C (0.512 in)
FWD A
13 mm
(0.512 in)
(50)
01
50
(50)
01 13 mm
50
15 mm (0.512 in)
(0.591 in)
122 mm
(4.803 in)
13 mm
(0.512 in)
F
FWD B W C (50)
01
D 50
NOTE:
01 TEFLON PART ADHESIVE TAPE ITEM 50 STORAGE TIME EXCEEDANCE IS ACCEPTABLE
AS LONG AS THE GRIP IS SUFFICIENT FOR PART INSTALLATION N_SB_541028_5_BFAB_01_01
Figure A-FBFAB - Sheet 01

Installation of the Teflon Tape on the Tail Cone

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF ALL
(1) For an explanation of the manhours and elapsed time, refer to the following Gantt Chart.

@A318/A319/A320/A321
SERVICE BULLETIN
**CONF ALL
01
ELAPSED TIME ASSUMPTION SERVICE BULLETIN No A320−54−1028
02
STEPS MH PER ET/S
GET ACCESS 2.00 2 1.25
REMOVE RIB 5 ON LH PYLON 2.00 2 1.75
MODIFY LH FAIRING 1.75 1 1.75
ON BENCH, MODIFY LH TAIL CONE 3.75 2 2.50
MODIFY AND INSTALL LH RIB 5 8.75 2 5.00
INSTALL LH TAIL CONE 3.75 2 3.25
REMOVE RIB 5 ON RH PYLON 2.00 2 1.75
MODIFY RH FAIRING 1.75 1 1.75
ON BENCH, MODIFY RH TAIL CONE 3.75 2 2.50
MODIFY AND INSTALL RH RIB 5 8.75 2 5.00
INSTALL RH TAIL CONE 3.75 2 3.25
CLOSE−UP 2.00 2 1.25
0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17
SB ELAPSED TIME
TOTAL MANHOURS 44.00 (HOURS)
SB ELAPSED TIME 16.75
NOTE:
01 THIS CHART IS ONLY A PROPOSAL.
OPERATORS MAY DETERMINE THAT ANOTHER WAY
TO DO THE WORK IS MORE SUITABLE FOR THEM.
MH : MANHOURS
PER : NUMBER OF PERSONS 02 IF A VSB IS INVOLVED, THE ASSOCIATED MANHOURS
ET/S: ELAPSED TIME PER STEP ARE NOT REFLECTED IN THIS GANTT CHART. N_SB_541028_5_AAAA_01_06
Figure A-FAAAA - Sheet 01

Gantt Chart

@A318/A319/A320/A321
SERVICE BULLETIN
REPORTING SHEET

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
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.

@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 4 3 2 1

- Quality rating of the Accomplishment Instructions 4 3 2 1
- Quality rating of the Illustrations 4 3 2 1
- 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
31707 BLAGNAC CEDEX FRANCE
Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51
Or via your Resident Customer Support Office.

Title: Nacelle & Pylon - Aft Movable Fairing - Rib 5 Redesign

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@A318/A319/A320/A321

TITLE: NACELLE & PYLON - AFT MOVABLE FAIRING - RIB 5 REDESIGN

The main changes of this revision are:

- Manpower paragraph and Gantt Chart updated

- Procurement addresses updated

- Consumable CMLA01 updated

- Component COMPA01 added

- Component COMPA02 added

- Accomplishment Instructions paragraph updated

- Minor changes applied

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 1

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

MATERIAL PRICE INFORMATION TABLE R

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 2

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

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 3

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

Task associated data - 001 PANEL UPDATED R

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 4

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

Subtask 541028-941-001-001 SUBTASK SOLUTION UPDATED R

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 5

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

Subtask 541028-831-013-001 SUBTASK SOLUTION ADDED N

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 6

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

Subtask 541028-942-001-001 SUBTASK SOLUTION UPDATED R

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 7

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

Appendix 01 - Elapsed Time Assumption

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

HISTORY OF PREVIOUS REVISIONS

ORIGINAL: Nov 25/14

REVISION No. : 01 - Oct 23/15

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 8

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

TITLE: NACELLE & PYLON - AFT MOVABLE FAIRING - RIB 5 REDESIGN

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 1

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

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

MATERIAL PRICE INFORMATION

MATERIAL PRICE INFORMATION TABLE

MATERIAL PRICE INFORMATION TABLE

MATERIAL PRICE INFORMATION TABLE

5 DATE: Nov 25/14 SERVICE BULLETIN No.: A320-54-1028

REVISION No.: 01 - Oct 23/15 Page: 2

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

MATERIAL PRICE INFORMATION TABLE

MATERIAL PRICE INFORMATION TABLE

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