@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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - GENERAL - INTRODUCE IMPROVED SLIDE RELEASE

CABLE FOR EMERGENCY EXIT HATCH

MODIFICATION No.: 150811K13931

This page transmits Revision No.05 of Service Bulletin No.A320-53-1227

ADDITIONAL WORK

**CONF ALL

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

REASON

Revision No. 05 issued following an AIRBUS decision to:

- correct the note Part Number in the Accomplishment instructions

- update the kit revision indicator.

CHANGES

SUMMARY

MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

MATERIAL PRICE INFORMATION TABLE

UPDATED

R

EFFECTIVITY OPERATOR LIST UPDATED R

PLANNING INFORMATION

EFFECTIVITY EFFECTIVITY RELATED INFORMATION

UPDATED

R

Material Effectivity MATERIAL EFFECTIVITY UPDATED

MATERIAL SET UPDATED

R

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 1

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

MATERIAL INFORMATION

MATERIAL - PRICE AND AVAILABILITY

Procurement Addresses PROCUREMENT ADDRESSES UPDATED

MATERIAL SET UPDATED

R

Price and Availability PRICE AND AVAILABILITY UPDATED

MATERIAL SET UPDATED

R

LIST OF COMPONENTS

Kit 531227D01R05 PART MATERIAL SET UPDATED

MATERIAL SET LABEL UPDATED

R

ACCOMPLISHMENT INSTRUCTIONS

TASK 531227- 831-848-001-Modification

Subtask 531227-831-202-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

NOTE UPDATED

R

Subtask 531227-831-202-002 AMM REFERENCE ADDED FOR CLARITY R

Subtask 531227-831-202-002 AMM REFERENCE ADDED FOR CLARITY R

Subtask 531227-831-202-001 SUBTASK SOLUTION UPDATED

MATERIAL LIST UPDATED

NOTE 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

Revision 01 is issued to :

update the EFFECTIVITY,

add note to EFFECTIVITY,

incorporate minor changes.

Revision No. 02 issued to:

change the compliance from Recommended to Mandatory,

remove the aircraft MSN 4007 and 4039 from the effectivity,

clarify the instruction for the removal of the slide release cable,

add a note to clarify additional washers for the clamp installation,

incorporate minor changes.

This Service Bulletin has been validated on A320 aircraft MSN 2524.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 2

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

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

A booklet including photographs taken during the validation of this Service Bulletin is available on

AirbusWorld - Maintenance and Engineering - Service Bulletin Information.

Revision No. 03 issued to:

add AMM 25-62-43 reference to the PROCEDURE paragraphs

add a sentence to state that the 40mm (1.57in.) hose has to be cut longitudinally

add the removal and installation procedures for panels 241/242FW, RW, NW, JW, KW, AX, BX and CX

clarify that FIN 151SW/152SW is for A319 aircraft and FIN 151CW/152CW is for A318 and A320

aircraft

replace Lockwire (CML 19-026) with Lockwire (CML 19-507).

Revision No. 04 issued following an AIRBUS decision to:

update the effectivity.

add a Note in accomplishment instructions, where appropriate, stating that use of clamp PN

MS21919WCH6 can be used at points where installation of clamp PN MS21919WCH5 is not possible

or difficult.

hose PN DAN79-07 length to be corrected from 0.7M to 0.08M (3.148in).

REVISION SEQUENCE

ORIGINAL: Mar 24/10

REVISION No. : 01 - May 31/10

REVISION No. : 02 - Mar 10/11

REVISION No. : 03 - Jul 28/11

REVISION No. : 04 - Feb 14/12

REVISION No. : 05 - Mar 27/12

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 3

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SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

This Page Intentionally Left Blank

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 4

6

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@A318/A319/A320/A321

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

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

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - GENERAL - INTRODUCE IMPROVED SLIDE RELEASE

CABLE FOR EMERGENCY EXIT HATCH

**CONF ALL

MODIFICATIONS

MODIFICATION CLASSIFICATION

MAJOR None

MINOR 150811K13931

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

There have been several in-service occurrences of difficulty in operating the overwing slide release

cable system. Some operators have reported that the cables are hard to operate and stick while doing

the functional test at C-check.

This Service Bulletin describes the work required to replace the overwing slide release cable PN

L32A319-160-001. The new parts have precise stainless steel ball bearing stripes instead of stamped

PTFE stripes.

Accomplishment of this Service Bulletin will improve the slide release system operation.

GENERAL EVALUATION

EVALUATION TABLE

COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO

POTENTIAL AD YES A/C OPERATION AFFECTED NO

RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO

COST SAVING NO ETOPS AFFECTED NO

STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO

NOTE (1): Service Bulletin must be accomplished.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 1

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SERVICE BULLETIN

SUMMARY

MATERIAL PRICE INFORMATION

**CONF 001

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 531227D01R05 1 5,840.00 Cables, clamps, bolts, screws, nuts,

washers and hose

**CONF 002

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 531227D01R05 1 5,840.00 Cables, clamps, bolts, screws, nuts,

washers and hose

**CONF 003

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 531227D01R05 1 5,840.00 Cables, clamps, bolts, screws, nuts,

washers and hose

**CONF 004

MATERIAL PRICE INFORMATION TABLE

MATERIAL SET QTY PER

A/C

PRICE PER

A/C (USD)

MAIN PARTS

Kit 531227D01R05 1 5,840.00 Cables, clamps, bolts, screws, nuts,

washers and hose

EFFECTIVITY

**CONF ALL

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

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 2

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SERVICE BULLETIN

SUMMARY

15T 46U 53U 62X 74T 79W 86Z 87Z 93V 94W 95V 99W AAF

AAR AAW ABQ ABY ACA ACI ADH AEE AFL AFR AHY AIJ ALK

AMC AMU ANA ANZ AUA AUH AVA AXM AZA BAB BAL BAW BEL

BER BGF BGH BHP BJN BKP BMA BON C9G CCA CCM CEB CES

CHH CIB CQH CQN CSA CSC CSN CSZ CYP D2F DAL DKH DLH

DRK EIN ETD EZD EZY FFT FHY FIN GAP GFA GIA GIR GLG

GMI GOW GWI GWY HAY HCC HDA I2L IAC IBE IGO IRA ISS

IWD IZM JBU JET JSA JST JZR KFR KGL KIL KNE KZR LAN

LBT LFX LJB LMJ LZB MAC MAU MLM MSC MSR NIA NKS NLV

NLY NMB OHY ONE PAL QTR RBA RBG RJA RKM ROT RZO SAA

SAS SBI SDM SFJ SKU SLK SMX SRQ SUD SVA SVR SVW SWR

SYA TAE TAI TAK TAM TAP TCW TCX TGW THY TJS TNA UAL

UEA UNA USA VIM VJC VKG VLG VOI VRD WAU WZZ

NOTE: This Service Bulletin is not applicable for aircraft with ACT provisions fitted.

This Service Bulletin has been validated on A320 aircraft MSN 2524.

A booklet including photographs taken during the validation of this Service Bulletin is available on

AirbusWorld - Maintenance and Engineering - Service Bulletin Information.

CONCURRENT REQUIREMENTS

None

REFERENCES / REPERCUSSIONS

TFU None

OEB None

AOT None

SIL None

LINE MAINTENANCE AFFECTED No

LIFE LIMIT None

OTHER None

NATURE OF THE WORK

AIRCRAFT YES

EQUIPMENT NO

HARD NO

SOFT NO

OBRM NO

MANPOWER

**CONF 001

Task 531227-831-848-001: Modification

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 3

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SERVICE BULLETIN

SUMMARY

**CONF 002

Task 531227-831-848-001: Modification

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF 003

Task 531227-831-848-001: Modification

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF 004

Task 531227-831-848-001: Modification

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

APPENDICES

**CONF ALL

None

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 4

6

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

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX

FRANCE

Tel : (33) 5 61 93 33 33

Telex : AIRBU 530526F

Fax : (33) 5 61 93 42 51

MANDATORY MANDATORY MANDATORY

ATA SYSTEM: 53

TITLE: FUSELAGE - GENERAL - INTRODUCE IMPROVED SLIDE RELEASE

CABLE FOR EMERGENCY EXIT HATCH

MODIFICATION No.: 150811K13931

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

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

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

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

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

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

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

AIRBUS prior written consent.

1. PLANNING INFORMATION

**CONF ALL

A. EFFECTIVITY

This Service Bulletin has been validated on A320 aircraft MSN 2524.

A booklet including photographs taken during the validation of this Service Bulletin is

available on AirbusWorld - Maintenance and Engineering - Service Bulletin Information.

NOTE: This Service Bulletin is not applicable for aircraft with ACT provisions fitted.

(1) Models

318-111 318-112 318-121 319-111 319-112 319-114 319-115 319-131

319-132 319-133 320-211 320-214 320-216 320-232 320-233

(2) Effectivity by MSN

1791 1796 1800-1801 1803 1805 1808 1810 1815 1819-1820 1824 1826 1828 1831

1833 1837 1839 1841 1844 1846 1849 1851-1858 1860-1868 1870-1877 1879

1882-1886 1888-1904 1906-1907 1909-1918 1920 1922-1925 1927 1929 1931

1933-1940 1942-1945 1947-1949 1951-1952 1954-1955 1957-1959 1961-1965

1968-1969 1971 1973 1975-1976 1979-1983 1986-1987 1989-1991 1993 1996-1998

2000-2004 2006-2020 2022-2024 2026-2040 2042-2044 2047-2054 2056-2059

2061-2063 2065-2066 2068-2075 2077-2079 2081-2104 2106 2108-2109 2112-2114

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 1

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SERVICE BULLETIN

2116 2118-2189 2191 2193-2207 2209-2210 2212 2214-2215 2217-2219 2221-2225

2227 2229-2233 2235-2245 2248-2254 2256-2258 2260 2262 2264-2266 2268-2269

2271-2278 2281-2283 2285 2287-2289 2291-2302 2304 2306 2308 2310-2313

2316-2319 2321-2322 2325-2329 2331-2335 2338-2340 2343-2350 2353-2356

2358-2362 2364-2367 2369-2380 2382-2383 2385 2387-2409 2411-2414 2416-2420

2422-2423 2425-2439 2441-2455 2457-2461 2463-2471 2473-2475 2477-2479

2481-2486 2489-2499 2501-2506 2508-2520 2522-2529 2531-2535 2537-2542

2544-2548 2551-2552 2554-2562 2564-2565 2567-2589 2591 2593-2598 2600-2609

2611-2649 2651-2652 2654-2674 2676-2681 2683-2686 2688-2705 2708-2712

2714-2715 2717-2721 2723-2725 2727-2729 2731-2735 2737-2740 2742-2747

2749-2755 2757-2758 2760-2766 2768-2792 2794-2798 2800 2802-2808 2810-2822

2824-2836 2838-2861 2863-2867 2869-2881 2883-2894 2896-2902 2904-2911

2913-2915 2917-2918 2920 2922-2926 2928-2932 2934-2935 2937-2948 2950-2956

2958-2964 2966-2970 2972-2973 2975-2995 2997-2998 3000-3004 3006-3012 3014

3016-3021 3023-3033 3035-3045 3047-3050 3052-3064 3066 3068-3069 3071-3072

3074 3076-3080 3082-3084 3086-3091 3093-3095 3097 3099-3105 3107-3109 3111

3113-3119 3121-3125 3127-3129 3131-3132 3134-3145 3147-3162 3165-3190

3192-3197 3200-3206 3208-3211 3213-3216 3218-3221 3223-3228 3230-3232 3234

3236-3237 3239-3240 3242 3244-3246 3248 3250 3252-3253 3255-3259 3261

3263-3264 3266 3268-3273 3275-3282 3284-3289 3291-3293 3295-3296 3298-3301

3303-3306 3308-3314 3316-3321 3323-3325 3327-3328 3330-3333 3335-3338

3341-3349 3351-3354 3357-3359 3361-3366 3368 3370-3371 3373-3381 3383-3386

3388-3396 3398 3400 3402-3404 3406-3418 3420-3428 3430-3433 3435-3440

3442-3457 3460-3461 3463-3470 3472-3492 3494-3497 3499-3503 3505-3506

3508-3511 3514-3521 3524 3526 3528-3538 3540-3541 3543-3545 3547-3551

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

3601-3611 3613-3614 3616-3618 3620-3622 3624 3626-3628 3630-3631 3634-3635

3638 3640-3644 3646-3652 3654 3656 3658-3664 3666-3668 3670-3672 3674-3677

3679-3680 3683-3687 3689-3707 3709-3711 3713-3716 3718-3721 3724 3726-3729

3731-3735 3739 3741-3748 3750-3751 3753-3760 3762-3763 3765 3767-3783

3785-3791 3793-3795 3797-3803 3805 3807-3813 3815 3817-3819 3821-3825

3827-3829 3831-3836 3838-3846 3848-3855 3857 3859-3861 3863 3865-3866 3868

3870-3877 3880 3882-3883 3885-3892 3894-3896 3898 3900-3915 3917-3919

3921-3923 3925 3927 3929 3931-3933 3935 3937 3939 3941-3943 3945-3947

3949-3950 3952-3954 3956 3958-3959 3961-3963 3965 3967-3968 3970-3972

3974-3976 3978-3980 3982-3986 3988 3990-3992 3995 3997-4001 4003 4006 4008

4010-4015 4017-4021 4026-4030 4032-4038 4040 4043 4046 4048-4049 4051-4053

4055-4057 4059 4061 4063-4066 4068-4072 4075-4077 4079-4080 4083-4084

4086-4089 4092-4095 4097-4098 4100-4102 4104-4106 4108-4111 4113 4115

4118-4122 4124-4130 4132-4133 4135 4137 4139-4141 4143-4147 4149-4150

4152-4154 4156-4169 4171-4172 4174-4179 4181-4183 4185-4188 4190-4191 4193

4195-4197 4201-4203 4205-4208 4210 4212 4214 4216 4218-4220 4223 4225-4226

4229 4231-4232

(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

15T 2910

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 2

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SERVICE BULLETIN

OPERATOR MSN

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

53U 3316 3748 3812 3895 3905 3950 4190 4193

62X 3402

74T 2165

79W 3751

86Z 1918 1969 1993

87Z 2210 2998

93V 3932

94W 1998

95V 3379

99W 3038

AAF 1846 2870 3852

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

AAW 3224 3236 4203

ABQ 3364 3385 3388 3403 3974

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

4061

ACA 1805 1853 1864 1874 1940 2018 2145

ACI 2152

ADH 3138 3161 3328 3343 3502 3515 3532

AEE 2468 3033 3066 3074 3162 3365 3392 3423 3439 3478 3526 3709

3714 3745 3753 3773 3785 3829 3850 3990 4065 4094 4165

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

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

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

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

AFR 1873 1879 1885 1894 1900 1924 1938 1949 2035 2059 2071 2081

2100 2109 2140 2317 2344 2350 2582 2601 2686 2705 2721 2750

2918 2938 2951 2961 2967 2972 3008 3009 3420 3470 3777 3795

3825 3859 4063 4084 4105 4137 4139

AHY 2516 2588 2685 2788 2846 2853 2865 2991 3006

AIJ 2048 2189 2227 2539 3021 3123 3149 3160 3286 3304 3312 3374

3508 3514 3667 3690

ALK 2345 2564 2584 2908

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

AMU 1893 1912 1962

ANA 2061 3099 3147 3148 3189

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

2663

AUA 2131 2174 2262 2416 2494 2547 2652

AUH 2403

AVA 2066 2328 2333 2358 2367 2377 2394 2523 2544 2552 2575 2662

3408 3467 3518 3647 3664 3691 3961 3980 3988 3992 4001 4011

4026 4046 4051 4100 4167 4175

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

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SERVICE BULLETIN

OPERATOR MSN

AXM 2612 2633 2656 2683 2699 2760 2816 2826 2842 2881 2885 2926

2944 2956 2989 3000 3018 3064 3117 3140 3154 3173 3182 3194

3201 3223 3232 3261 3277 3291 3299 3327 3338 3353 3370 3394

3404 3427 3448 3477 3486 3489 3505 3521 3536 3549 3568 3576

3582 3610 3628 3648 3679 3701 3715 3729 3765 3776 3813 3875

3963 3997 4019 4035 4070 4079 4088 4098 4126 4147

AZA 2033 2057 2074 2083 2086 2101 2127 2869 2932 3076 3079 3080

3115 3178 3213 3295 3362 3412 3464 3482 3563 3598 3609 3643

3666 3695 3732 3815 3831 3846 3885 3906 3921 3956 3976 3978

4075 4108 4119 4143 4152 4195

BAB 2700 2763 3861 4055

BAL 2335 3492

BAW 1871 1883 1899 1907 1910 1958 2038 2040 3301 3314 3351 3468

3499 3550 3607 3649 3697 3703 3721 3726 3912 4185

BEL 2196 2230 3255 3790

BER 1931 2009 2619 3093 3121 3242 3289 3415 3447 3516 3661 3689

3700 3704 3728 3865 3872 3945 3995 4013 4101 4128 4161

BGF 3188

BGH 3139

BHP 2968 3055 3245 3422 3604 4033 4187

BJN 3617

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

BMA 1922 1987 2098 2188 2194 2389 2429 2441 2466 2694 2697 2720

2981 3049

BON 3142

C9G 2277

CCA 2000 2007 2015 2172 2202 2205 2237 2269 2285 2293 2298 2454

2499 2508 2525 2532 2545 2551 2559 2614 2643 2805 2819 2839

2847 2890 3195 3200 3215 3221 3226 3250 3337 3461 3506 3601

CCM 3882 3952

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

2994 3048 3272 3433 3472 3487 3646 3762 3767

CES 1906 1911 1964 1981 2022 2034 2036 2049 2056 2068 2155 2171

2182 2199 2212 2219 2221 2235 2239 2244 2274 2437 2451 2478

2493 2498 2562 2591 2606 2627 2693 2757 2825 3168 3170 3186

3197 3481 3559 3611 3613 3650 3677 3692 3716 3775 3793 3797

3870 3904 3929 3937 3965 4027 4037 4043 4111 4144 4186 4220

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

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

3982

CIB 1968

CQH 1852 1920 2939 3014 3023 3747 3819 4072 4093 4168

CQN 3836 3876 3901 3941

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

3892

CSC 2313 2348 2396 2431 2510 2534 2597 2639 3114 3116 3124 3158

3167 3196 3210 3386 3449 3591 3680 3962 4018 4068

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 4

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SERVICE BULLETIN

OPERATOR MSN

CSN 1971 1986 2004 2008 2200 2203 2232 2273 2354 2361 2371 2408

2426 2435 2484 2505 2506 2511 2519 2541 2546 2554 2555 2558

2574 2579 2637 2667 2680 2689 2701 2708 2714 2743 2770 2772

2796 2815 2824 2834 2855 2861 2877 2899 2901 2915 2940 2948

2950 2960 2969 2986 3020 3144 3258 3269 3311 3342 3828 3860

3890 3903 3910 3959 3983 3999 4003 4017 4036 4038 4071 4140

4172 4205 4225 4232

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

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

3887 3898 3935 3971 4010 4028 4159 4176 4208 4214 4226

CYP 2108 2275 2334 2343 2359 2383 2718 4197

D2F 1963 2747 2753

DAL 1796 1800 1810 1815 1820 1824 1828 1833 1839 1875 1897 1923

1959 1976 1982 1990 2002 2013 2026 2039 2047 2082 2087 2092

2095

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

4064 4102 4154

DLH 4097 4120 4141 4153 4182 4191

DRK 2306 2346

EIN 2191 2206 2217 2250 2256 2272 2294 2364 2374 2399 2409 2411

2432 2486 2542 2583 2635 2810 3129 3136 3169 3318 3345 3377

3501 3755 3781 3857

ETD 1944 1945 1947 1955 2167 3004 3050 3676 3693 3713 3902 4066

4077 4124

EZD 2137 2141 2147 3621

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

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

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

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

2548 2565 2578 2605 2636 2646 2677 2681 2691 2702 2709 2715

2727 2729 2735 2742 2744 2754 2765 2769 2777 2779 2782 2795

2803 2812 2818 2827 2829 2854 2860 2866 2873 2884 2923 2946

2959 3003 3036 3041 3053 3059 3061 3082 3084 3088 3090 3118

3122 3134 3137 3176 3184 3411 3413 3426 3432 3442 3466 3537

3544 3555 3569 3571 3608 3634 3675 3683 3702 3720 3735 3742

3746 3754 3763 3774 3788 3799 3805 3808 3810 3824 3843 3844

3845 3854 3871 3888 3909 3913 3922 3946 3953 3975 3979 3991

4006 4012 4014 4034 4040 4048 4056 4069 4076 4080 4087 4125

4129 4132 4157 4179 4196 4219

FFT 1803 1841 1939 1943 1980 1991 1997 2010 2012 2017 2019 2030

2051 2103 2198 2209 2218 2236 2240 2241 2253 2258 2260 2276

2287 2318 2325 2392 2400 2406 2448 2465 2483 2497 2518 2751

2806 2836 2857 3389 3431 4127

FHY 2524 4207

FIN 1791 1808 1913 1916 1989 2065 2124 2146 2154 2266

GAP 2162 2183

GFA 1884 1901 3706 4030 4059 4083 4146 4158 4188 4218

GIA 2598 2692

GIR 1973

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SERVICE BULLETIN

OPERATOR MSN

GLG 1866 1872 1882 1925 2078 2126

GMI 3019 3202 3407

GOW 3256 3306 3597 3616 3798 3827 3900 3915 3933

GWI 2607 2628 2632 2813 2833 2976 3011 3128 3172 3193 3352 3358

3375 3500 3534 3839 3841 4166

GWY 1860 1867

HAY 2745 3533 3560

HCC 2180

HDA 2229 2238 2428

I2L 3834

IAC 2593 2624 2629 2907 3271 3288 3300 3305 3344 3551 3620 3687

3822 3874 3918 3970 4020 4029 4052 4089 4121 4164 4201 4212

IBE 2225 2242 2248 2264 2311 2347 2365 2391 2776 2807 2843 2897

3054 3078 3102 3179 3209 3320 3380 3443 3651 3744

IGO 2844 2863 2883 2911 2958 2990 3086 3159 3192 3227 3335 3357

3414 3453 3457 3497 3541 3618 3782 3863 3943 4008 4113 4156

4216

IRA 2054

ISS 1896 1937 1983 2001 2102

IWD 2011 3758 3868 3889

IZM 2118 2404 2414 2452

JBU 1849 1861 1898 1904 1915 1917 1927 1948 2006 2020 2031 2042

2063 2075 2099 2125 2132 2136 2149 2150 2159 2160 2177 2201

2215 2231 2447 2449 2461 2489 2491 2504 2520 2535 2577 2580

2640 2647 2671 2710 2725 2755 2781 2802 2814 2832 2848 2871

2880 2900 2945 2970 2977 2992 3029 3039 3072 3091 3119 3150

3190 3228 3263 3287 3348 3381 3416 3451 3479 3488 3517 3554

3572 3622 3659 3707 3724 3760 3800 3811

JET 2698 2723 2797

JSA 2156 2164 2316 2356 2395 2401 2423 2453 2457 2604

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

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

3495 3547 3668 3743 3783 3917 4177 4178 4229

JZR 2569 2792 2822 3919 3939 4162

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

2664 2670 2676 2731 2817 2856 2874 2922 3012 3089 3105 3270

KGL 2029 2077

KIL 2214 2224 2249

KNE 1886 2123 3361 3396 3425 3475 3530 3787 3817 3894

KZR 2016 2128 2828 2987 3141 3484 3519 3614

LAN 1854 1858 1877 1903 2089 2096 2295 2304 2321 2572 2585 2845

2858 2864 2872 2886 2887 2892 2894 3264 3280 3319 3330 3371

3390 3438 3469 3509 3535 3556 3585 3602 3606 3635 3642 3663

3671 3770 3772 3779

LBT 3480

LFX 3589 3818

LJB 3985

LMJ 1868

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SERVICE BULLETIN

OPERATOR MSN

LZB 2540 2596 3028 3309 3564 3780

MAC 2166 3809 3833

MAU 1936

MLM 3363

MSC 2937 2966 3282 3323

MSR 2070 2073 2079 2088 2094

NIA 3183 3219

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

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

3393 3395 4206

NLV 2157

NLY 2529 2668 2749 2867 2902 4231

NMB 3346 3586

OHY 2571 2688

ONE 3001 3030 3062 3214 3216

PAL 2878 2925 2954 3087 3107 3108 3187 3205 3273 3310 3455 3553

3579 3652 3731

QTR 1895 1957 2097 2121 2138 2161 2288 3071 4110 4130 4183

RBA 2023 2032 2135 2139 2195

RBG 2764 3152 3246

RJA 2649 2953 3428 3685 3803 3832

RKM 2158 3907

ROT 2931 2955 3220 3225

RZO 2390 2425 3891

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

SAS 2850 2888 3231 3292

SBI 1819 1870 2028 2369 2373 2464 2474 2618 2623 2641 3446 3473

3490 3494 3866 3880 4032 4150

SDM 1851 1863 1876 1890

SFJ 2620 2658 2695 3025

SKU 2283

SLK 2058 2252 2517 2568 2775 3104 3570 3821 4118

SMX 2995

SRQ 3757 3801

SUD 3040

SVA 4015 4057 4092 4104 4115 4122 4135

SVR 2175 2187 2278 2327

SVW 3100

SWR 1951 2024 2134

SYA 3853

TAE 2084 2659

TAI 1934 1952 2282 2301 2339 2434 2444 2791 2917 3042 3057 3103

3113 3248 3276 3378 3418 3510 3538 3577 3581

TAK 3171 3331

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

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SERVICE BULLETIN

OPERATOR MSN

TAM 1801 1826 1831 1837 1855 1857 1888 1891 2014 2044 2372 2393

2417 2467 2513 2602 2661 2734 2737 2783 2784 2838 2859 2896

2904 2924 3002 3032 3035 3047 3058 3111 3156 3180 3211 3240

3266 3278 3284 3313 3325 3391 3540 3565 3588 3594 3595 3630

3658 3662 3710 3727 3733 3750 3908 3972 4000 4163 4171

TAP 2178 3769 3883 4021 4095 4106 4145

TCW 1929 1975 2362

TCX 1942 1961 1965 2003 2114

TGW 2331 2340 2724 2728 4181 4210

THY 1856 1909 1996 2609 2626 2631 2655 2738 2739 2928 2934 2941

2984 3010 3185 3208 3239 3257 3259 3303 3308 3341 3558 3567

3603 3654 3718 3719 3896 3931 3949

TJS 4169

TNA 2914

UAL 1865

UEA 2654 2696 2762 2774 2820 2835 3024

UNA 3333 3886

USA 1844 1935 2193 2302 2312 2405 2422 2430 2458 2482 2570 2595

2613 2615 2630 2669 2690 4086 4149 4202

VIM 2732 2804 3125

VJC 3739 3791 4049

VKG 1889 1954

VLG 1862 1914 1933 1979 2027 2104 2143 2168 2207 2223 2388 2407

2479 2589 2678 2761 2785 2794 2798 2889 2962 2988 3083 3095

3109 3145 3151 3174 3203 3237 3293 3321 3376 3400 3529

VOI 2204 2296 2657 2666 2771 2780 2979 2997 3045 3069 3077 3175

3252 3253 3279 3317 3450 3463 3491 3524 3543 3590 3624 3672

3705

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

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

3445 3460 3465 3503 3656 3670 3684 3686

WAU 3531 3741

WZZ 1892 1902 2752 3127 3143 3166 3177 3354 3384 3409 3430 3562

3771 3807 3877 3927 3947 3968 4109 4174 4223

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SERVICE BULLETIN

(4) Configuration by MSN

MSN CONFIGURATION

1791 1796 1800 1801 1803 1805 1808 1810 1815 1819 1820

1824 1826 1828 1831 1833 1837 1839 1841 1844 1846 1851

1853 1855 1863 1866 1870 1872 1875 1876 1882 1884 1886

1890 1893 1897 1901 1912 1916 1923 1925 1934 1936 1938

1943 1947 1952 1955 1959 1962 1963 1971 1976 1980 1982

1986 1990 1997 2000 2002 2004 2007 2008 2010 2012 2013

2015 2019 2023 2026 2028 2030 2032 2033 2039 2047 2052

2057 2066 2069 2072 2074 2078 2083 2086 2087 2089 2091

2093 2095 2096 2098 2101 2103 2113 2122 2124 2126 2127

2131 2172 2174 2179 2186 2188 2194 2198 2200 2202 2203

2205 2209 2222 2232 2236 2237 2240 2241 2243 2253 2258

2260 2262 2264 2266 2268 2269 2273 2277 2281 2285 2287

2293 2295 2296 2298 2302 2304 2306 2308 2311 2313 2318

2321 2326 2332 2335 2339 2346 2348 2355 2362 2365 2369

2371 2373 2375 2379 2382 2383 2389 2392 2396 2400 2404

2406 2408 2414 2416 2418 2426 2429 2431 2433 2435 2438

2444 2448 2452 2454 2458 2464 2465 2466 2467 2468 2469

2470 2473 2474 2483 2485 2490 2494 2497 2499 2501 2505

2508 2510 2516 2518 2519 2525 2532 2534 2541 2545 2546

2547 2551 2554 2555 2557 2558 2559 2560 2561 2567 2568

2570 2572 2574 2579 2581 2585 2588 2593 2595 2597 2603

2607 2611 2614 2615 2617 2618 2621 2622 2624 2628 2629

2631 2632 2634 2639 2641 2643 2644 2648 2652 2655 2657

2659 2660 2662 2664 2666 2667 2669 2672 2673 2679 2684

2690 2693 2694 2697 2698 2700 2704 2711 2718 2720 2723

2733 2738 2739 2746 2751 2757 2762 2763 2771 2773 2774

2780 2784 2788 2797 2805 2806 2811 2815 2819 2825 2836

2839 2841 2843 2845 2847 2849 2850 2857 2858 2864 2870

2872 2878 2879 2886 2887 2888 2889 2890 2891 2892 2893

2894 2897 2898 2901 2905 2907 2913 2925 2929 2935 2938

2940 2942 2948 2954 2961 2963 2969 2978 2979 2981 2983

2985 2997 3007 3017 3020 3024 3026 3028 3032 3043 3045

3049 3054 3057 3069 3077 3078 3094 3102 3104 3108 3114

3116 3124 3142 3144 3165 3168 3169 3175 3179 3181 3186

3195 3200 3204 3209 3226 3231 3248 3250 3252 3253 3255

3258 3269 3271 3276 3279 3281 3285 3288 3292 3298 3300

3305 3311 3317 3320 3324 3336 3342 3344 3347 3377 3380

3393 3395 3406 3417 3421 3424 3428 3436 3443 3445 3450

3452 3454 3463 3467 3491 3518 3520 3548 3551 3561 3578

3580 3588 3590 3595 3614 3620 3638 3647 3651 3660 3663

3671 3680 3684 3685 3686 3687 3691 3694 3705 3710 3727

3733 3744 3757 3759 3768 3770 3772 3779 3790 3794 3801

3803 3822 3828 3832 3834 3836 3838 3842 3849 3851 3860

3874 3876 3890 3892 3901 3903 3905 3911 3914 3918 3942

3958 3962 3970 3982 3983 3998 4000 4018 4020 4029 4036

4038 4052 4071 4089 4121 4127 4141 4163 4164 4171 4182

002

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

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SERVICE BULLETIN

MSN CONFIGURATION

1849 1852 1854 1856 1857 1858 1860 1861 1862 1864 1865

1867 1868 1871 1873 1874 1877 1879 1883 1885 1888 1889

1891 1892 1894 1895 1896 1898 1899 1900 1902 1903 1904

1906 1907 1909 1910 1911 1913 1914 1915 1917 1918 1920

1922 1924 1927 1929 1931 1933 1935 1937 1940 1942 1944

1945 1948 1949 1951 1954 1957 1958 1961 1964 1965 1968

1969 1973 1975 1979 1981 1983 1987 1989 1993 1996 1998

2001 2003 2006 2009 2011 2014 2016 2018 2020 2022 2024

2027 2029 2031 2034 2036 2038 2040 2042 2044 2048 2049

2054 2056 2058 2061 2063 2065 2068 2070 2073 2075 2077

2079 2082 2084 2085 2088 2090 2092 2094 2097 2099 2102

2104 2106 2108 2112 2114 2116 2118 2121 2123 2125 2128

2130 2132 2133 2134 2135 2136 2137 2138 2139 2140 2141

2142 2143 2144 2145 2146 2147 2148 2149 2150 2151 2152

2153 2154 2155 2156 2157 2158 2159 2160 2161 2162 2163

2164 2165 2166 2167 2168 2169 2171 2173 2175 2177 2178

2180 2182 2183 2185 2187 2189 2191 2193 2195 2197 2199

2201 2204 2206 2207 2210 2212 2215 2217 2219 2221 2223

2225 2227 2229 2231 2233 2235 2238 2239 2242 2244 2248

2250 2252 2254 2256 2257 2272 2274 2275 2278 2282 2288

2291 2292 2294 2297 2299 2301 2310 2312 2316 2322 2325

2327 2329 2331 2334 2338 2340 2343 2345 2347 2349 2354

2356 2359 2361 2364 2366 2372 2374 2376 2388 2390 2391

2393 2395 2397 2399 2401 2403 2405 2407 2409 2411 2413

2417 2419 2422 2423 2425 2428 2430 2432 2434 2437 2439

2441 2443 2445 2447 2449 2451 2453 2455 2457 2459 2461

2475 2478 2479 2482 2484 2486 2489 2491 2493 2496 2498

2502 2504 2506 2509 2511 2513 2515 2517 2520 2522 2524

2526 2529 2531 2533 2535 2537 2539 2540 2542 2562 2564

2569 2571 2573 2576 2577 2580 2583 2584 2587 2589 2591

2594 2596 2598 2600 2602 2604 2606 2608 2609 2612 2613

2616 2619 2620 2623 2626 2627 2630 2633 2635 2637 2640

2642 2645 2647 2649 2651 2654 2656 2658 2661 2663 2665

2668 2670 2671 2674 2676 2678 2680 2683 2685 2688 2689

2692 2695 2696 2699 2701 2703 2705 2708 2710 2712 2714

2717 2719 2721 2724 2725 2728 2731 2732 2734 2737 2740

2743 2745 2747 2749 2752 2753 2755 2758 2760 2761 2764

2766 2768 2770 2772 2775 2776 2778 2781 2783 2785 2787

2789 2791 2792 2794 2796 2798 2800 2802 2804 2807 2808

2810 2814 2816 2817 2820 2822 2824 2826 2828 2830 2832

2834 2835 2838 2840 2842 2844 2846 2848 2851 2853 2855

2856 2859 2861 2863 2865 2867 2869 2871 2874 2875 2877

2880 2881 2883 2885 2896 2899 2900 2902 2904 2906 2908

2909 2911 2914 2915 2917 2920 2922 2924 2926 2928 2930

2932 2934 2937 2939 2941 2943 2944 2945 2947 2950 2952

2953 2956 2958 2960 2962 2964 2966 2968 2970 2973 2975

2977 2980 2982 2984 2986 2987 2988 2989 2990 2991 2992

2993 2994 2995 2998 3000 3002 3004 3006 3008 3010 3012

3014 3016 3018 3021 3023 3025 3027 3029 3031 3033 3035

001

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 10

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SERVICE BULLETIN

MSN CONFIGURATION

3037 3039 3040 3042 3044 3047 3048 3050 3052 3055 3056

3058 3060 3063 3064 3066 3068 3071 3072 3074 3076 3079

3080 3083 3086 3087 3089 3091 3093 3095 3097 3099 3101

3103 3105 3107 3109 3111 3113 3115 3117 3119 3121 3123

3125 3127 3129 3131 3132 3135 3136 3138 3140 3141 3143

3145 3147 3148 3149 3150 3151 3152 3153 3154 3155 3156

3157 3158 3159 3160 3161 3162 3166 3167 3170 3173 3174

3177 3178 3180 3182 3183 3185 3187 3189 3190 3192 3194

3196 3197 3201 3203 3205 3206 3208 3210 3211 3213 3215

3218 3219 3221 3223 3224 3227 3228 3230 3232 3234 3236

3237 3239 3240 3242 3244 3246 3256 3257 3259 3261 3263

3264 3266 3268 3270 3272 3273 3275 3277 3278 3280 3282

3284 3286 3287 3289 3291 3293 3295 3296 3299 3301 3303

3304 3306 3308 3310 3312 3313 3314 3316 3318 3319 3321

3323 3325 3327 3328 3330 3332 3335 3337 3338 3341 3343

3345 3348 3349 3351 3353 3354 3357 3359 3361 3362 3365

3366 3368 3370 3373 3374 3376 3378 3379 3381 3383 3384

3386 3389 3391 3392 3394 3396 3398 3400 3402 3404 3408

3409 3410 3412 3414 3416 3418 3420 3422 3423 3425 3427

3430 3431 3433 3435 3437 3439 3440 3444 3446 3448 3449

3451 3453 3455 3456 3457 3460 3461 3464 3465 3468 3470

3472 3473 3474 3475 3476 3477 3478 3479 3480 3481 3482

3483 3484 3485 3486 3487 3488 3489 3490 3492 3494 3495

3496 3497 3499 3501 3502 3503 3505 3506 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 3724

3726 3729 3731 3732 3734 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 3805 3807

3809 3811 3812 3813 3815 3817 3819 3821 3823 3825 3827

3829 3831 3833 3835 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 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 4083 4084

001

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 11

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SERVICE BULLETIN

MSN CONFIGURATION

4086 4088 4092 4093 4094 4095 4097 4098 4100 4101 4102

4104 4105 4106 4108 4109 4110 4111 4113 4115 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 4172 4174

4175 4176 4177 4178 4179 4181 4183 4185 4186 4187 4188

4190 4191 4193 4195 4196 4197 4201 4202 4203 4205 4206

4207 4208 4210 4212 4214 4216 4218 4219 4220 4223 4225

4226 4229 4231 4232

001

1939 1991 2017 2035 2051 2059 2071 2081 2100 2109 2218

2276 2317 2328 2333 2344 2350 2358 2367 2377 2394 2523

2544 2552 2575 2582 2601 2686 2750 2910 2918 2931 2951

2955 2967 2972 3001 3009 3030 3038 3062 3100 3214 3216

3220 3225 3333 3363 3371 3390 3438 3469 3509 3530 3585

3602 3606 3617 3635 3642 3751 3886 3932 3985 4169

003

2037 2043 2050 2053 2062 2119 2120 2129 2170 2176 2181

2184 2196 2214 2224 2230 2245 2249 2251 2265 2271 2283

2289 2300 2319 2353 2360 2370 2378 2380 2385 2387 2398

2402 2412 2420 2427 2436 2442 2446 2450 2460 2463 2471

2477 2481 2492 2495 2503 2512 2514 2527 2528 2538 2548

2556 2565 2578 2586 2605 2625 2636 2638 2646 2677 2681

2691 2702 2709 2715 2727 2729 2735 2742 2744 2754 2765

2769 2777 2779 2782 2786 2790 2795 2803 2812 2813 2818

2821 2827 2829 2831 2833 2852 2854 2860 2866 2873 2876

2884 2923 2946 2959 2976 3003 3011 3019 3036 3041 3053

3059 3061 3082 3084 3088 3090 3118 3122 3128 3134 3137

3139 3171 3172 3176 3184 3188 3193 3202 3245 3309 3331

3346 3352 3358 3364 3375 3385 3388 3403 3407 3411 3413

3415 3426 3432 3442 3447 3466 3500 3533 3534 3537 3544

3555 3560 3564 3569 3571 3586 3589 3604 3608 3634 3661

3675 3683 3689 3700 3702 3704 3720 3728 3735 3742 3746

3754 3763 3774 3788 3799 3808 3810 3818 3824 3839 3841

3844 3845 3853 3854 3865 3872 3888 3895 3950 4040 4048

4056 4069 4076 4080 4087 4125 4129 4132 4166

004

(5) Configuration definition

**CONF 001

Config. 001 is valid for all the A320 aircraft given in the effectivity of this Service Bulletin

on which modification 150811K13931 is not embodied.

**CONF 002

Config. 002 is valid for all the A319 aircraft given in the effectivity of this Service Bulletin

on which modification 150811K13931 is not embodied and modification 32208K7278 is

not embodied.

**CONF 003

Config. 003 is valid for all the A318 aircraft given in the effectivity of this Service Bulletin

on which modification 150811K13931 is not embodied.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 12

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SERVICE BULLETIN

**CONF 004

Config. 004 is valid for all the A319 aircraft given in the effectivity of this Service Bulletin

on which modification 150811K13931 is not embodied and modification 32208K7278 is

embodied.

(6) Material Effectivity

MATERIAL QTY PER A/C SEE NOTES

Kit 531227D01R05 1

Consumable CMLD01 As required

B. CONCURRENT REQUIREMENTS

None

C. REASON

(1) History

There have been several in-service occurrences of difficulty in operating the overwing

slide release cable system. Some operators have reported that the cables are hard to

operate and stick while doing the functional test at C-check.

(2) Objective/Action

This Service Bulletin describes the work required to replace the overwing slide release

cable PN L32A319-160-001. The new parts have precise stainless steel ball bearing

stripes instead of stamped PTFE stripes.

(3) Advantages

Accomplishment of this Service Bulletin will improve the slide release system operation.

(4) Operational/Maintenance Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

**CONF 001

Task 531227-831-848-001: Modification

(1) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

(2) Install the slide release cable to the flexible control assembly (5030WM and

5031WM)

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 13

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**CONF 002

Task 531227-831-848-001: Modification

(1) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

(2) Install the slide release cable to the flexible control assembly (5030WM and

5031WM)

**CONF 003

Task 531227-831-848-001: Modification

(1) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

(2) Install the slide release cable to the flexible control assembly (5030WM and

5031WM)

**CONF 004

Task 531227-831-848-001: Modification

(1) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

(2) Install the slide release cable to the flexible control assembly (5030WM and

5031WM)

**CONF ALL

E. COMPLIANCE

(1) Classification

MANDATORY: Service Bulletin must be accomplished.

(2) Accomplishment Timescale

This Service Bulletin has been classified Mandatory by the issue of an Airworthiness

Directive (AD) published by the European Aviation Safety Agency (EASA). The AD must

be used as the reference document for the mandated accomplishment timescale.

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.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 14

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SERVICE BULLETIN

G. MANPOWER

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

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

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

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

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

included.

**CONF 001

Task 531227-831-848-001: Modification

Get Access 7.50

On Aircraft

Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

5.00

Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

13.50

Tests 1.00

Close-Up 7.50

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF 002

Task 531227-831-848-001: Modification

Get Access 7.50

On Aircraft

Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

5.00

Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

13.5

Tests 1.00

Close-Up 7.50

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF 003

Task 531227-831-848-001: Modification

Get Access 7.50

On Aircraft

Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

5.00

Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

13.5

Tests 1.00

Close-Up 7.50

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 15

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SERVICE BULLETIN

Task 531227-831-848-001: Modification

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF 004

Task 531227-831-848-001: Modification

Get Access 7.50

On Aircraft

Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

5.00

Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

13.50

Tests 1.00

Close-Up 7.50

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF ALL

H. WEIGHT AND BALANCE

**CONF 001

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

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

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

A320

Manufacturers Empty Weight -0.158 KG (-0.3483 LB)

Effect on Balance -3.159 KGM (-22.849 LB.FT )

**CONF 002

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

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

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

A319

Manufacturers Empty Weight -0.158 KG (-0.3483 LB)

Effect on Balance -2.907 KGM (-21.026 LB.FT )

**CONF 003

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

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

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

A318

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 16

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SERVICE BULLETIN

Manufacturers Empty Weight -0.158 KG (-0.3483 LB)

Effect on Balance -2.786 KGM (-20.151 LB.FT )

**CONF 004

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

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

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

A319

Manufacturers Empty Weight -0.158 KG (-0.3483 LB)

Effect on Balance -2.907 KGM (-21.026 LB.FT )

**CONF ALL

I. ELECTRICAL LOAD DATA

Not Changed

J. REFERENCES

**CONF 001

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-40-00

12-34-24 20-21-11 21-20-00

25-21-41 25-23-43 25-23-44

25-23-47 25-23-48 25-55-11

25-62-00 25-62-43 52-10-00

52-21-11 52-30-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-76-00

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

**CONF 002

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-40-00

12-34-24 20-21-11 21-20-00

25-21-41 25-23-43 25-23-44

25-23-47 25-23-48 25-55-11

25-62-00 25-62-43 52-10-00

52-21-11 52-30-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-76-00

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 17

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

**CONF 003

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-40-00

12-34-24 20-21-11 21-20-00

25-21-41 25-23-43 25-23-44

25-23-47 25-23-48 25-55-11

25-62-00 25-62-43 52-10-00

52-21-11 52-30-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-76-00

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

**CONF 004

Aircraft Maintenance Manual (AMM) 06-20-00 06-31-53 06-40-00

12-34-24 20-21-11 21-20-00

25-21-41 25-23-43 25-23-44

25-23-47 25-23-48 25-55-11

25-62-00 25-62-43 52-10-00

52-21-11 52-30-00

Consumable Material List (CML)

ATA Common Support Data Dictionary (CSDD),

Chapter 2

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

Standards Manual (SM)

Structural Repair Manual (SRM) 51-76-00

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

**CONF ALL

K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 25-62-43

Illustrated Parts Catalog (IPC) 25-62-04 25-62-43

L. INTERCHANGEABILITY/MIXABILITY

**CONF 001

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Control Assy-Cable L32A319-160-001 L32A320-180 01 Not

Applicable

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

Common Support Data Dictionary (CSDD), Chapter 2.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

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**CONF 002

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Control Assy-Cable L32A319-160-001 L32A320-180 01 Not

Applicable

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

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 003

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Control Assy-Cable L32A319-160-001 L32A320-180 01 Not

Applicable

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

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF 004

DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE

NOTES

Control Assy-Cable L32A319-160-001 L32A320-180 01 Not

Applicable

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

Common Support Data Dictionary (CSDD), Chapter 2.

**CONF ALL

M. SPARES

None

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 19

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This Page Intentionally Left Blank

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 20

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SERVICE BULLETIN

2. MATERIAL INFORMATION

**CONF ALL

A. MATERIAL - PRICE AND AVAILABILITY

(1) Procurement Addresses

Kit 531227D01R05 Customers with aircraft shown in the

effectivity of this Service Bulletin should send

a purchase order to AIRBUS. Quote the

number of this Service Bulletin. The address

is:

AIRBUS Material, Logistics and Suppliers

Weg beim Jaeger 150

D-22335 Hamburg

Germany

For ordering by internet:

http://spares.airbus.com

For ordering by fax: +49 40 50 76 4012

For ordering by E-mail:

ifd.spares@airbus.com

(2) Price and Availability

Kit 531227D01R05

Cost 5,840.00 USD

Availability 90 calendar days from receipt of order

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

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

your order so that we can try to comply with your requirements. The sales terms (costs

and availability) are estimated in relation to economic conditions at the issue date of

the Service Bulletin. The latest valid price and lead time for ordering purposes shall

be obtained through the AirbusSpares portal or through a request for quotation to

airbus.kit@airbus.com.

B. INDUSTRY SUPPORT INFORMATION

AIRBUS will provide a 40% reduction to the applicable sales prices given in the paragraph

’Price and Availability’ for orders placed before 30 June 2013.

C. LIST OF COMPONENTS

Kit 531227D01R05

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

NOTES

1 L32A320-180 2 CABLE (1) L32A319-160-001 01

3 NAS1149C0332R 30 WASHER

4 NAS1149C0463R 2 WASHER

5 NSA5031H4-4 2 BOLT

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 21

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

NOTES

6 NSA5031-3-4 12 BOLT

7 NSA5031-4-4 2 BOLT

8 NSA5031-3-5 12 BOLT

9 NAS509-4C 2 NUT

10 NAS1726C4P 2 NUT

11 NAS1726C3P 16 NUT

12 DAN79-07 0.08 (ME) HOSE

13 NSA935401-03 4 TIE

14 MS21919WCH5 24 CLAMP

15 MS24665-153 2 PIN

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

Common Support Data Dictionary (CSDD), Chapter 2.

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

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

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

to part number relationship.

D. LIST OF MATERIALS - OPERATOR SUPPLIED

(1) Consumable Materials

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO CML

MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting low Adhesion

Sealant

09-018 As required

Corrosion Resistant Steel Lockwire 19-507 As required

(2) Components

None

(3) Equipment

None

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR

None

F. TOOLING

(1) Tooling - Price and Availability

None

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 22

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SERVICE BULLETIN

(2) Tools

To accomplish this Service Bulletin it is necessary to use the tools and equipment listed

in AMM 25-62-43, Page Block 401.

- Tools and equipment to test and adjust the escape slide release cable as per AMM

Task 25-62-43-400-001.

(3) Special Tools

To accomplish this Service Bulletin it is necessary to use the tools and equipment listed

in AMM 25-62-43, Page Block 401.

- Tools and equipment to test and adjust the escape slide release cable as per AMM

Task 25-62-43-400-001.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 23

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This Page Intentionally Left Blank

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 24

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SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

Task 531227-831-848-001 - Modification

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

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY INSTALLED IN

THE REGULATOR VALVE ASSEMBLY OF THE INFLATION RESERVOIR. THIS

PREVENTS ACCIDENTAL:

- DISCHARGE OF THE INFLATION RESERVOIR

- DEPLOYMENT OF THE ESCAPE-SLIDE

WHICH CAN CAUSE INJURY AND/OR DAMAGE.

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 ELECTRICAL WIRING AND COMPONENTS

- REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND

OTHER CONTAMINATION.

THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION

AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION.

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

Task Associated Data

**CONF 001

Zone

151 152 240 241 242 820 830

From 241 to 242

Access

Door 826 831

Panel 151CW 152CW 241AX 241BX 241CX 241FW 241JW 241KW

241LW 241MW 241NW 241PW 241QW 241RW 241SW 241TW

241UW 241VW 241WW 242AX 242BX 242CX 242FW 242JW

242KW 242LW 242MW 242NW 242PW 242QW 242RW 242SW

242TW 242UW 242VW 242WW

Manpower

TOTAL MANHOURS 34.50

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 25

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ELAPSED TIME (HOURS) 25.25

**CONF 002

Zone

151 152 240 241 242 820 830

From 241 to 242

Access

Door 826 831

Panel 151SW 152SW 241AX 241BX 241CX 241FW 241JW 241KW

241LW 241MW 241NW 241PW 241QW 241RW 241SW 241TW

241UW 241VW 241WW 242AX 242BX 242CX 242FW 242JW

242KW 242LW 242MW 242NW 242PW 242QW 242RW 242SW

242TW 242UW 242VW 242WW

Manpower

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF 003

Zone

151 152 240 241 242 820 830

From 241 to 242

Access

Door 826 831

Panel 151CW 152CW 241AX 241BX 241CX 241FW 241JW 241KW

241LW 241MW 241NW 241PW 241QW 241RW 241SW 241TW

241UW 241VW 241WW 242AX 242BX 242CX 242FW 242JW

242KW 242LW 242MW 242NW 242PW 242QW 242RW 242SW

242TW 242UW 242VW 242WW

Manpower

TOTAL MANHOURS 34.50

ELAPSED TIME (HOURS) 25.25

**CONF 004

Zone

151 152 240 241 242 820 830

From 241 to 242

Access

Door 826 831

Panel 151SW 152SW 241AX 241BX 241CX 241FW 241JW 241KW

241LW 241MW 241NW 241PW 241QW 241RW 241SW 241TW

241UW 241VW 241WW 242AX 242BX 242CX 242FW 242JW

242KW 242LW 242MW 242NW 242PW 242QW 242RW 242SW

242TW 242UW 242VW 242WW

Manpower

TOTAL MANHOURS 34.50

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 26

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ELAPSED TIME (HOURS) 25.25

**CONF ALL

A. GENERAL

**CONF 001

(1) Subtask 531227-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

From 241

To 242

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-40-00, Page Block 001

Task 20-21-11-911-001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-76-00

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

the Consumable Materials List (CML)).

(b) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(c) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(d) For the identification of access panels (Refer to AMM 06-40-00, Page Block 001).

(e) Tag the parts that you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-001).

(h) For the procedure to use sealant (Refer to SRM 51-76-00).

(2) Subtask 531227-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 27

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SERVICE BULLETIN

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

Service Bulletin.

**CONF 002

(1) Subtask 531227-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

From 241

To 242

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-40-00, Page Block 001

Task 20-21-11-911-001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-76-00

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

the Consumable Materials List (CML)).

(b) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(c) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(d) For the identification of access panels (Refer to AMM 06-40-00, Page Block 001).

(e) Tag the parts that you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-001).

(h) For the procedure to use sealant (Refer to SRM 51-76-00).

(2) Subtask 531227-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 28

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**CONF 003

(1) Subtask 531227-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

From 241

To 242

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-40-00, Page Block 001

Task 20-21-11-911-001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-76-00

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

the Consumable Materials List (CML)).

(b) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(c) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(d) For the identification of access panels (Refer to AMM 06-40-00, Page Block 001).

(e) Tag the parts that you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-001).

(h) For the procedure to use sealant (Refer to SRM 51-76-00).

(2) Subtask 531227-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 29

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**CONF 004

(1) Subtask 531227-910-201-001 - Standard Practices

Work Zones and Access Panels

Zone Access/Work location

From 241

To 242

Manpower Resources

Skills NON SPECIFIC

References

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

06-31-53, Page Block 001

06-40-00, Page Block 001

Task 20-21-11-911-001

Consumable Material List (CML)

Structural Repair Manual (SRM) 51-76-00

(a) For the specification of materials (Mat. No.) given in this Service Bulletin (Refer to

the Consumable Materials List (CML)).

(b) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001).

(c) For the identification of zones (Refer to AMM 06-20-00, Page Block 001).

(d) For the identification of access panels (Refer to AMM 06-40-00, Page Block 001).

(e) Tag the parts that you must remove and retain to make the subsequent installation

easier.

(f) Put all the retained hardware in identified plastic bags and attach the bags to the

related unit.

(g) To torque tighten the standard threaded fasteners (Refer to AMM Task

20-21-11-911-001).

(h) For the procedure to use sealant (Refer to SRM 51-76-00).

(2) Subtask 531227-839-201-001 - Administrative

Manpower Resources

Skills NON SPECIFIC

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

Service Bulletin.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 30

6

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

**CONF ALL

B. PREPARATION

**CONF 001

(1) Subtask 531227-941-201-001 - Job Set-up External

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

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

Task 52-10-00-010-001

52-30-00, Page Block 201

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

12-34-24-869-002).

(b) Put access platforms in position below the FWD passenger/crew door 831 and the

AFT cargo compartment door 826.

(c) Open the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-010-001).

(d) Open the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

(2) Subtask 531227-941-202-001 - Job Set-up Internal

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241VW, Panel 241UW,

Panel 241LW, Panel 241PW, Panel 241SW,

Panel 241CX, Panel 241BX, Panel 241KW,

Panel 241AX, Panel 241JW, Panel 241NW,

Panel 241RW, Panel 241FW

242 Access Panel 242MW, Panel 242QW, Panel 242TW,

Panel 242WW, Panel 242VW, Panel 242UW,

Panel 242LW, Panel 242PW, Panel 242SW,

Panel 242CX, Panel 242BX, Panel 242KW,

Panel 242AX, Panel 242JW, Panel 242NW,

Panel 242RW, Panel 242FW

151 Access Panel 151CW

152 Access Panel 152CW

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 31

6

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

SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-001

Task 25-21-41-000-001

Task 25-23-43-000-001

Task 25-23-44-000-001

Task 25-23-47-000-002

Task 25-23-48-000-001

Task 25-55-11-000-003

Task 25-62-00-081-001

Task 25-62-43-000-001

Task 52-21-11-000-001

WARNING: MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY

INSTALLED IN THE REGULATOR VALVE ASSEMBLY OF THE

INFLATION RESERVOIR. THIS PREVENTS ACCIDENTAL:

- DISCHARGE OF THE INFLATION RESERVOIR

- DEPLOYMENT OF THE ESCAPE-SLIDE WHICH CAN CAUSE

INJURY AND/OR DAMAGE.

(a) Install the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-000-001 and AMM Task 25-62-00-081-001).

(b) Remove the passenger seats in the area of the emergency exit between Frame 38

and Frame 47, as necessary (Refer to AMM Task 25-21-41-000-001).

(c) Remove the emergency exit hatches (Refer to AMM Task 52-21-11-000-001).

(d) Remove the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242MW,

242QW, 242TW, 242WW, 242CX (Refer to AMM Task 25-23-48-000-001).

(e) Remove the upper sidewall panels 241BX, 242BX, 241VW, 242VW (Refer to AMM

Task 25-23-43-000-001).

(f) Remove the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-000-001).

(g) Remove the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW,

242FW, 242LW, 242PW, 242SW (Refer to AMM Task 25-23-47-000-002).

(h) Remove the air conditioning distribution duct(s) between Frame 38 and Frame 47,

as necessary (Refer to AMM Task 21-20-00-010-001).

(i) Remove the aft cargo compartment panels 151CW, 152CW (Refer to AMM Task

25-55-11-000-003).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 32

6

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

(j) To get access to the cable assembly:

1 Loosen the cable ties holding the electrical wires, as necessary.

2 Remove bracket PN D2127249820000 at Frame 47, as necessary.

3 Push back the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

**CONF 002

(1) Subtask 531227-941-201-001 - Job Set-up External

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

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

Task 52-10-00-010-001

52-30-00, Page Block 201

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

12-34-24-869-002).

(b) Put access platforms in position below the FWD passenger/crew door 831 and the

AFT cargo compartment door 826.

(c) Open the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-010-001).

(d) Open the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

(2) Subtask 531227-941-202-002 - Job Set-up Internal

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241CX, Panel 241BX,

Panel 241VW, Panel 241KW, Panel 241AX,

Panel 241JW, Panel 241NW, Panel 241RW,

Panel 241UW, Panel 241FW, Panel 241LW,

Panel 241PW, Panel 241SW

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 33

6

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

SERVICE BULLETIN

242 Access Panel 242MW, Panel 242QW, Panel 242TW,

Panel 242WW, Panel 242CX, Panel 242BX,

Panel 242VW, Panel 242KW, Panel 242AX,

Panel 242JW, Panel 242NW, Panel 242RW,

Panel 242UW, Panel 242FW, Panel 242LW,

Panel 242PW, Panel 242SW

151 Access Panel 151SW

152 Access Panel 152SW

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-001

Task 25-21-41-000-001

Task 25-23-43-000-001

Task 25-23-44-000-001

Task 25-23-47-000-002

Task 25-23-48-000-001

Task 25-55-11-000-003

Task 25-62-00-081-001

Task 25-62-43-000-001

Task 52-21-11-000-001

WARNING: MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY

INSTALLED IN THE REGULATOR VALVE ASSEMBLY OF THE

INFLATION RESERVOIR. THIS PREVENTS ACCIDENTAL:

- DISCHARGE OF THE INFLATION RESERVOIR

- DEPLOYMENT OF THE ESCAPE-SLIDE WHICH CAN CAUSE

INJURY AND/OR DAMAGE.

(a) Install the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-000-001 and AMM Task 25-62-00-081-001).

(b) Remove the passenger seats in the area of the emergency exit between Frame 38

and Frame 47, as necessary (Refer to AMM Task 25-21-41-000-001).

(c) Remove the emergency exit hatches (Refer to AMM Task 52-21-11-000-001).

(d) Remove the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242MW,

242QW, 242TW, 242WW, 242CX (Refer to AMM Task 25-23-48-000-001).

(e) Remove the upper sidewall panels 241BX, 242BX, 241VW, 242VW (Refer to AMM

Task 25-23-43-000-001).

(f) Remove the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-000-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 34

6

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

SERVICE BULLETIN

(g) Remove the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW,

242FW, 242LW, 242PW, 242SW (Refer to AMM Task 25-23-47-000-002).

(h) Remove the air conditioning distribution duct(s) between Frame 38 and Frame 47,

as necessary (Refer to AMM Task 21-20-00-010-001).

(i) Remove the aft cargo compartment panels 151SW, 152SW (Refer to AMM Task

25-55-11-000-003).

(j) To get access to the cable assembly:

1 Loosen the cable ties holding the electrical wires, as necessary.

2 Remove bracket PN D2127249820000 at Frame 47, as necessary.

3 Push back the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

**CONF 003

(1) Subtask 531227-941-201-001 - Job Set-up External

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

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

Task 52-10-00-010-001

52-30-00, Page Block 201

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

12-34-24-869-002).

(b) Put access platforms in position below the FWD passenger/crew door 831 and the

AFT cargo compartment door 826.

(c) Open the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-010-001).

(d) Open the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 35

6

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

SERVICE BULLETIN

(2) Subtask 531227-941-202-001 - Job Set-up Internal

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241VW, Panel 241UW,

Panel 241LW, Panel 241PW, Panel 241SW,

Panel 241CX, Panel 241BX, Panel 241KW,

Panel 241AX, Panel 241JW, Panel 241NW,

Panel 241RW, Panel 241FW

242 Access Panel 242MW, Panel 242QW, Panel 242TW,

Panel 242WW, Panel 242VW, Panel 242UW,

Panel 242LW, Panel 242PW, Panel 242SW,

Panel 242CX, Panel 242BX, Panel 242KW,

Panel 242AX, Panel 242JW, Panel 242NW,

Panel 242RW, Panel 242FW

151 Access Panel 151CW

152 Access Panel 152CW

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-001

Task 25-21-41-000-001

Task 25-23-43-000-001

Task 25-23-44-000-001

Task 25-23-47-000-002

Task 25-23-48-000-001

Task 25-55-11-000-003

Task 25-62-00-081-001

Task 25-62-43-000-001

Task 52-21-11-000-001

WARNING: MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY

INSTALLED IN THE REGULATOR VALVE ASSEMBLY OF THE

INFLATION RESERVOIR. THIS PREVENTS ACCIDENTAL:

- DISCHARGE OF THE INFLATION RESERVOIR

- DEPLOYMENT OF THE ESCAPE-SLIDE WHICH CAN CAUSE

INJURY AND/OR DAMAGE.

(a) Install the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-000-001 and AMM Task 25-62-00-081-001).

(b) Remove the passenger seats in the area of the emergency exit between Frame 38

and Frame 47, as necessary (Refer to AMM Task 25-21-41-000-001).

(c) Remove the emergency exit hatches (Refer to AMM Task 52-21-11-000-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 36

6

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

(d) Remove the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242MW,

242QW, 242TW, 242WW, 242CX (Refer to AMM Task 25-23-48-000-001).

(e) Remove the upper sidewall panels 241BX, 242BX, 241VW, 242VW (Refer to AMM

Task 25-23-43-000-001).

(f) Remove the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-000-001).

(g) Remove the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW,

242FW, 242LW, 242PW, 242SW (Refer to AMM Task 25-23-47-000-002).

(h) Remove the air conditioning distribution duct(s) between Frame 38 and Frame 47,

as necessary (Refer to AMM Task 21-20-00-010-001).

(i) Remove the aft cargo compartment panels 151CW, 152CW (Refer to AMM Task

25-55-11-000-003).

(j) To get access to the cable assembly:

1 Loosen the cable ties holding the electrical wires, as necessary.

2 Remove bracket PN D2127249820000 at Frame 47, as necessary.

3 Push back the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

**CONF 004

(1) Subtask 531227-941-201-001 - Job Set-up External

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

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

Task 52-10-00-010-001

52-30-00, Page Block 201

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

12-34-24-869-002).

(b) Put access platforms in position below the FWD passenger/crew door 831 and the

AFT cargo compartment door 826.

(c) Open the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-010-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 37

6

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

SERVICE BULLETIN

(d) Open the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

(2) Subtask 531227-941-202-002 - Job Set-up Internal

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241CX, Panel 241BX,

Panel 241VW, Panel 241KW, Panel 241AX,

Panel 241JW, Panel 241NW, Panel 241RW,

Panel 241UW, Panel 241FW, Panel 241LW,

Panel 241PW, Panel 241SW

242 Access Panel 242MW, Panel 242QW, Panel 242TW,

Panel 242WW, Panel 242CX, Panel 242BX,

Panel 242VW, Panel 242KW, Panel 242AX,

Panel 242JW, Panel 242NW, Panel 242RW,

Panel 242UW, Panel 242FW, Panel 242LW,

Panel 242PW, Panel 242SW

151 Access Panel 151SW

152 Access Panel 152SW

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-010-001

Task 25-21-41-000-001

Task 25-23-43-000-001

Task 25-23-44-000-001

Task 25-23-47-000-002

Task 25-23-48-000-001

Task 25-55-11-000-003

Task 25-62-00-081-001

Task 25-62-43-000-001

Task 52-21-11-000-001

WARNING: MAKE SURE THAT THE SAFETY/LOCK PIN IS CORRECTLY

INSTALLED IN THE REGULATOR VALVE ASSEMBLY OF THE

INFLATION RESERVOIR. THIS PREVENTS ACCIDENTAL:

- DISCHARGE OF THE INFLATION RESERVOIR

- DEPLOYMENT OF THE ESCAPE-SLIDE WHICH CAN CAUSE

INJURY AND/OR DAMAGE.

(a) Install the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-000-001 and AMM Task 25-62-00-081-001).

(b) Remove the passenger seats in the area of the emergency exit between Frame 38

and Frame 47, as necessary (Refer to AMM Task 25-21-41-000-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 38

6

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

SERVICE BULLETIN

(c) Remove the emergency exit hatches (Refer to AMM Task 52-21-11-000-001).

(d) Remove the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242MW,

242QW, 242TW, 242WW, 242CX (Refer to AMM Task 25-23-48-000-001).

(e) Remove the upper sidewall panels 241BX, 242BX, 241VW, 242VW (Refer to AMM

Task 25-23-43-000-001).

(f) Remove the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-000-001).

(g) Remove the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW,

242FW, 242LW, 242PW, 242SW (Refer to AMM Task 25-23-47-000-002).

(h) Remove the air conditioning distribution duct(s) between Frame 38 and Frame 47,

as necessary (Refer to AMM Task 21-20-00-010-001).

(i) Remove the aft cargo compartment panels 151SW, 152SW (Refer to AMM Task

25-55-11-000-003).

(j) To get access to the cable assembly:

1 Loosen the cable ties holding the electrical wires, as necessary.

2 Remove bracket PN D2127249820000 at Frame 47, as necessary.

3 Push back the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

**CONF ALL

C. PROCEDURE

**CONF 001

(1) Subtask 531227-831-201-003 - Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Manhours 5.00

Minimum number of person 2

Subtask elapsed time 2.50

Skills CABIN

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 39

6

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

SERVICE BULLETIN

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Resistant Steel

Lockwire

19-507 As required

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-000-001

Fig. A-GBAAA

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

WARNING: YOU MUST BE CAREFUL WHEN YOU REMOVE LOCKWIRE. IF YOU

PULL LOCKWIRE WITH FORCE FROM A COMPONENT IT CAN

CAUSE YOU INJURY.

(a) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

Refer to AMM 25-62-43-000-001.

Refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02

NOTE: Take care not to damage the insulation blankets when removing the

slide release cable.

1 To disconnect the control cable between Frame 40 and Frame 41 (Refer to

AMM Task 25-62-43-000-001) LH and RH, remove, as shown in View B:

Corrosion Resistant

Steel Lockwire

19-507 As required

2 Nut NAS1726C4P Item (10) Discard

2 Bolt NSA5031-4-4 Item (7) Discard

2 Nut NAS509-4C Item (9) Discard

2 Washer NAS1149C0463R Item (4) Discard

2 Bolt NSA5031H4-4 Item (5) Discard

2 Flange D5337025520000 Item (2) Retain

and

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 40

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@A318/A319/A320/A321

SERVICE BULLETIN

2 Pin-Cotter MS24665-153 Item (15) Discard

2 Pin-Clevis D5337048420200 Item (16) Retain

6 Washer NAS1149C0332R Item (3) Discard

2 To disconnect the control cable between Frame 46 and Frame 47 (Refer to

AMM Task 25-62-43-000-001) in the AFT cargo compartment, LH and RH,

remove and discard, as shown in View G:

and loosen the bracket attach nuts:

3 Between Frame 40 and Frame 47 LH and RH, remove, as shown in View C,

D, E, F and H:

2 Control Assy-Cable L32A319-160-001 Item (1) Discard

and

24 Clamp MS21919WCH6 Item (14) Discard

12 Bolt NSA5031-3-5 Item (8) Discard

12 Bolt NSA5031-3-4 Item (6) Discard

24 Washer NAS1149C0332R Item (3) Discard

16 Nut NAS1726C3P Item (11) Discard

(2) Subtask 531227-831-202-001 - Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Manhours 13.50

Minimum number of person 2

Subtask elapsed time 6.75

Skills CABIN

AIRFRAME

Material necessary to do the job

Kit 531227D01R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 L32A320-180 2 CABLE

3 NAS1149C0332R 30 WASHER

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 41

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@A318/A319/A320/A321

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

4 NAS1149C0463R 2 WASHER

5 NSA5031H4-4 2 BOLT

6 NSA5031-3-4 12 BOLT

7 NSA5031-4-4 2 BOLT

8 NSA5031-3-5 12 BOLT

9 NAS509-4C 2 NUT

10 NAS1726C4P 2 NUT

11 NAS1726C3P 16 NUT

12 DAN79-07 0.08 (ME) HOSE

13 NSA935401-03 4 TIE

14 MS21919WCH5 24 CLAMP

15 MS24665-153 2 PIN

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting low

Adhesion Sealant

09-018 As required

Corrosion Resistant Steel

Lockwire

19-507 As required

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

Consumable Material List (CML)

Fig. A-GBAAA

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

(a) Install the cable with orientation marking visible towards the inside of the aircraft

(Minimum radius 180 mm (7.08 inch).

Refer to AMM 25-62-43-400-001.

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03

NOTE: Take care not to damage the insulation blankets when installing the

slide release cable.

1 Position the control cable between Frame 40 and Frame 47 LH and RH, and

install, as shown in View A:

2 Cable L32A320-180 Item 1

and attach with:

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 42

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@A318/A319/A320/A321

SERVICE BULLETIN

24 Clamp MS21919WCH5 Item 14

NOTE: Clamp PN MS21919WCH6 can be used at points where

installation of clamp PN MS21919WCH5 is not possible or

easily achieved.

24 Washer NAS1149C0332R Item 3

12 Bolt NSA5031-3-4 Item 6

12 Bolt NSA5031-3-5 Item 8

16 Nut NAS1726C3P Item 11

NOTE: Take care when installing the slide release cable, Item

1, between the skin and the frames. To avoid mishandling

damage to the slide release cable, it is advisable to use two

people when installing the cable. One person to guide the

cable between the skin and the frames and one to support

the cable, make sure that the cable is relaxed and untwisted

before securing in position.

NOTE: Install one or two additional washers, Item 3, for clamp

installation shown in Fig. A-GBAAA View C, D, E, F and H, as

necessary.

2 Install at Frame 40 LH and RH, as shown in View B:

2 Flange D5337025520000 Item (2) Retained at

removal

with:

Corrosion Inhibiting

low Adhesion

Sealant

09-018 As required

and

2 Bolt NSA5031-4-4 Item 7

2 Nut NAS1726C4P Item 10

and

2 Bolt NSA5031H4-4 Item 5

2 Washer NAS1149C0463R Item 4

2 Nut NAS509-4C Item 9

and connect to the bellcrank with:

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 43

6

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

SERVICE BULLETIN

2 Pin-Clevis D5337048420200 Item (16) Retained at

removal

6 Washer NAS1149C0332R Item 3

2 Pin MS24665-153 Item 15

3 Cut

0.08 (ME) Hose DAN79-07 Item 12

to a length of 40 mm (1.575 inch) then cut hose longitudinally and install at

Frame 41 LH and RH, with

4 Tie NSA935401-03 Item 13

as shown in View H.

4 Install and connect the control cable between Frame 46 and Frame 47 in the

AFT cargo compartment, LH and RH, as shown in View G.

5 After adjustments to the control cable make sure that all nuts are secure and

install, as shown in View J and K:

Corrosion Resistant

Steel Lockwire

19-507 As required

**CONF 002

(1) Subtask 531227-831-201-002 - Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Manhours 5.00

Minimum number of person 2

Subtask elapsed time 2.50

Skills CABIN

AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Resistant Steel

Lockwire

19-507 As required

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 44

6

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

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-000-001

Fig. A-GBAAB

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

WARNING: YOU MUST BE CAREFUL WHEN YOU REMOVE LOCKWIRE. IF YOU

PULL LOCKWIRE WITH FORCE FROM A COMPONENT IT CAN

CAUSE YOU INJURY.

(a) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

Refer to AMM 25-62-43-000-001.

Refer to Fig. A-GBAAB Sheet 01 and Fig. A-GBAAB Sheet 02

NOTE: Take care not to damage the insulation blankets when removing the

slide release cable.

1 To disconnect the control cable between Frame 40 and Frame 41 (Refer to

AMM Task 25-62-43-000-001) LH and RH, remove, as shown in View B:

Corrosion Resistant

Steel Lockwire

19-507 As required

2 Nut NAS1726C4P Item (10) Discard

2 Bolt NSA5031-4-4 Item (7) Discard

2 Nut NAS509-4C Item (9) Discard

2 Washer NAS1149C0463R Item (4) Discard

2 Bolt NSA5031H4-4 Item (5) Discard

2 Flange D5337025520000 Item (2) Retain

and

2 Pin-Cotter MS24665-153 Item (15) Discard

2 Pin-Clevis D5337048420200 Item (16) Retain

6 Washer NAS1149C0332R Item (3) Discard

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 45

6

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

SERVICE BULLETIN

2 To disconnect the control cable between Frame 46 and Frame 47 (Refer to

AMM Task 25-62-43-000-001) in the AFT cargo compartment, LH and RH,

remove and discard, as shown in View G:

Corrosion Resistant

Steel Lockwire

19-507 As required

and loosen the bracket attach nuts:

3 Between Frame 40 and Frame 47 (Refer to AMM Task 25-62-43-000-001 LH

and RH, remove, as shown in View C, D, E, F and H:

2 Control Assy-Cable L32A319-160-001 Item (1) Discard

and

24 Clamp MS21919WCH6 Item (14) Discard

12 Bolt NSA5031-3-5 Item (8) Discard

12 Bolt NSA5031-3-4 Item (6) Discard

24 Washer NAS1149C0332R Item (3) Discard

16 Nut NAS1726C3P Item (11) Discard

(2) Subtask 531227-831-202-002 - Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

Manpower Resources

Manhours 13.5

Minimum number of person 2

Subtask elapsed time 6.75

Skills CABIN

AIRFRAME

Material necessary to do the job

Kit 531227D01R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 L32A320-180 2 CABLE

3 NAS1149C0332R 30 WASHER

4 NAS1149C0463R 2 WASHER

5 NSA5031H4-4 2 BOLT

6 NSA5031-3-4 12 BOLT

7 NSA5031-4-4 2 BOLT

8 NSA5031-3-5 12 BOLT

9 NAS509-4C 2 NUT

10 NAS1726C4P 2 NUT

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 46

6

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

SERVICE BULLETIN

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

11 NAS1726C3P 16 NUT

12 DAN79-07 0.08 (ME) HOSE

13 NSA935401-03 4 TIE

14 MS21919WCH5 24 CLAMP

15 MS24665-153 2 PIN

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting low

Adhesion Sealant

09-018 As required

Corrosion Resistant Steel

Lockwire

19-507 As required

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

Fig. A-GBAAB

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

(a) Install the cable with orientation marking visible towards the inside of the aircraft

(Minimum radius 180 mm (7.08 inch).

Refer to AMM 25-62-43-400-001.

Refer to Fig. A-GBAAB Sheet 01, Fig. A-GBAAB Sheet 02 and Fig. A-GBAAB

Sheet 03

NOTE: Take care not to damage the insulation blankets when installing the

slide release cable.

1 Position the control cable between Frame 40 and Frame 47 LH and RH, and

install, as shown in View A:

2 Cable L32A320-180 Item 1

and attach with:

24 Clamp MS21919WCH5 Item 14

NOTE: Clamp PN MS21919WCH6 can be used at points where

installation of clamp PN MS21919WCH5 is not possible or

easily achieved.

24 Washer NAS1149C0332R Item 3

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 47

6

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

SERVICE BULLETIN

12 Bolt NSA5031-3-4 Item 6

12 Bolt NSA5031-3-5 Item 8

16 Nut NAS1726C3P Item 11

NOTE: Take care when installing the slide release cable, Item

1, between the skin and the frames. To avoid mishandling

damage to the slide release cable, it is advisable to use two

people when installing the cable. One person to guide the

cable between the skin and the frames and one to support

the cable, make sure that the cable is relaxed and untwisted

before securing in position.

NOTE: Install one or two additional washers, Item 3, for clamp

installation shown in Fig. A-GBAAB View C, D, E, F and H, as

necessary.

2 Install at Frame 40 LH and RH, as shown in View B:

2 Flange D5337025520000 Item (2) Retained at

removal

with:

Corrosion Inhibiting

low Adhesion

Sealant

09-018 As required

and

2 Bolt NSA5031-4-4 Item 7

2 Nut NAS1726C4P Item 10

and

2 Bolt NSA5031H4-4 Item 5

2 Washer NAS1149C0463R Item 4

2 Nut NAS509-4C Item 9

and connect to the bellcrank with:

2 Pin-Clevis D5337048420200 Item (16) Retained at

removal

6 Washer NAS1149C0332R Item 3

2 Pin MS24665-153 Item 15

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 48

6

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

SERVICE BULLETIN

3 Cut

0.08 (ME) Hose DAN79-07 Item 12

to a length of 40 mm (1.575 inch) then cut hose longitudinally and install at

Frame 41 LH and RH, with

4 Tie NSA935401-03 Item 13

as shown in View H.

4 Install and connect the control cable between Frame 46 and Frame 47 in the

AFT cargo compartment, LH and RH, as shown in View G.

5 After adjustments to the control cable make sure that all nuts are secure and

install, as shown in View J and K:

Corrosion Resistant

Steel Lockwire

19-507 As required

**CONF 003

(1) Subtask 531227-831-201-002 - Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Manhours 5.00

Minimum number of person 2

Subtask elapsed time 2.50

Skills CABIN

AIRFRAME

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Resistant Steel

Lockwire

19-507 As required

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-000-001

Fig. A-GBAAB

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 49

6

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

SERVICE BULLETIN

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

WARNING: YOU MUST BE CAREFUL WHEN YOU REMOVE LOCKWIRE. IF YOU

PULL LOCKWIRE WITH FORCE FROM A COMPONENT IT CAN

CAUSE YOU INJURY.

(a) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

Refer to AMM 25-62-43-000-001.

Refer to Fig. A-GBAAB Sheet 01 and Fig. A-GBAAB Sheet 02

NOTE: Take care not to damage the insulation blankets when removing the

slide release cable.

1 To disconnect the control cable between Frame 40 and Frame 41 (Refer to

AMM Task 25-62-43-000-001) LH and RH, remove, as shown in View B:

Corrosion Resistant

Steel Lockwire

19-507 As required

2 Nut NAS1726C4P Item (10) Discard

2 Bolt NSA5031-4-4 Item (7) Discard

2 Nut NAS509-4C Item (9) Discard

2 Washer NAS1149C0463R Item (4) Discard

2 Bolt NSA5031H4-4 Item (5) Discard

2 Flange D5337025520000 Item (2) Retain

and

2 Pin-Cotter MS24665-153 Item (15) Discard

2 Pin-Clevis D5337048420200 Item (16) Retain

6 Washer NAS1149C0332R Item (3) Discard

2 To disconnect the control cable between Frame 46 and Frame 47 (Refer to

AMM Task 25-62-43-000-001) in the AFT cargo compartment, LH and RH,

remove and discard, as shown in View G:

Corrosion Resistant

Steel Lockwire

19-507 As required

and loosen the bracket attach nuts:

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 50

6

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

SERVICE BULLETIN

3 Between Frame 40 and Frame 47 (Refer to AMM Task 25-62-43-000-001 LH

and RH, remove, as shown in View C, D, E, F and H:

2 Control Assy-Cable L32A319-160-001 Item (1) Discard

and

24 Clamp MS21919WCH6 Item (14) Discard

12 Bolt NSA5031-3-5 Item (8) Discard

12 Bolt NSA5031-3-4 Item (6) Discard

24 Washer NAS1149C0332R Item (3) Discard

16 Nut NAS1726C3P Item (11) Discard

(2) Subtask 531227-831-202-002 - Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

Manpower Resources

Manhours 13.5

Minimum number of person 2

Subtask elapsed time 6.75

Skills CABIN

AIRFRAME

Material necessary to do the job

Kit 531227D01R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 L32A320-180 2 CABLE

3 NAS1149C0332R 30 WASHER

4 NAS1149C0463R 2 WASHER

5 NSA5031H4-4 2 BOLT

6 NSA5031-3-4 12 BOLT

7 NSA5031-4-4 2 BOLT

8 NSA5031-3-5 12 BOLT

9 NAS509-4C 2 NUT

10 NAS1726C4P 2 NUT

11 NAS1726C3P 16 NUT

12 DAN79-07 0.08 (ME) HOSE

13 NSA935401-03 4 TIE

14 MS21919WCH5 24 CLAMP

15 MS24665-153 2 PIN

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 51

6

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

SERVICE BULLETIN

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting low

Adhesion Sealant

09-018 As required

Corrosion Resistant Steel

Lockwire

19-507 As required

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

Fig. A-GBAAB

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

(a) Install the cable with orientation marking visible towards the inside of the aircraft

(Minimum radius 180 mm (7.08 inch).

Refer to AMM 25-62-43-400-001.

Refer to Fig. A-GBAAB Sheet 01, Fig. A-GBAAB Sheet 02 and Fig. A-GBAAB

Sheet 03

NOTE: Take care not to damage the insulation blankets when installing the

slide release cable.

1 Position the control cable between Frame 40 and Frame 47 LH and RH, and

install, as shown in View A:

2 Cable L32A320-180 Item 1

and attach with:

24 Clamp MS21919WCH5 Item 14

NOTE: Clamp PN MS21919WCH6 can be used at points where

installation of clamp PN MS21919WCH5 is not possible or

easily achieved.

24 Washer NAS1149C0332R Item 3

12 Bolt NSA5031-3-4 Item 6

12 Bolt NSA5031-3-5 Item 8

16 Nut NAS1726C3P Item 11

NOTE: Take care when installing the slide release cable, Item

1, between the skin and the frames. To avoid mishandling

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 52

6

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

SERVICE BULLETIN

damage to the slide release cable, it is advisable to use two

people when installing the cable. One person to guide the

cable between the skin and the frames and one to support

the cable, make sure that the cable is relaxed and untwisted

before securing in position.

NOTE: Install one or two additional washers, Item 3, for clamp

installation shown in Fig. A-GBAAB View C, D, E, F and H, as

necessary.

2 Install at Frame 40 LH and RH, as shown in View B:

2 Flange D5337025520000 Item (2) Retained at

removal

with:

Corrosion Inhibiting

low Adhesion

Sealant

09-018 As required

and

2 Bolt NSA5031-4-4 Item 7

2 Nut NAS1726C4P Item 10

and

2 Bolt NSA5031H4-4 Item 5

2 Washer NAS1149C0463R Item 4

2 Nut NAS509-4C Item 9

and connect to the bellcrank with:

2 Pin-Clevis D5337048420200 Item (16) Retained at

removal

6 Washer NAS1149C0332R Item 3

2 Pin MS24665-153 Item 15

3 Cut

0.08 (ME) Hose DAN79-07 Item 12

to a length of 40 mm (1.575 inch) then cut hose longitudinally and install at

Frame 41 LH and RH, with

4 Tie NSA935401-03 Item 13

as shown in View H.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 53

6

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

SERVICE BULLETIN

4 Install and connect the control cable between Frame 46 and Frame 47 in the

AFT cargo compartment, LH and RH, as shown in View G.

5 After adjustments to the control cable make sure that all nuts are secure and

install, as shown in View J and K:

Corrosion Resistant

Steel Lockwire

19-507 As required

**CONF 004

(1) Subtask 531227-831-201-003 - Remove the slide release cable from the flexible

control assembly (5030WM and 5031WM)

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Manhours 5.00

Minimum number of person 2

Subtask elapsed time 2.50

Skills CABIN

Material necessary to do the job

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Resistant Steel

Lockwire

19-507 As required

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-000-001

Fig. A-GBAAA

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

WARNING: YOU MUST BE CAREFUL WHEN YOU REMOVE LOCKWIRE. IF YOU

PULL LOCKWIRE WITH FORCE FROM A COMPONENT IT CAN

CAUSE YOU INJURY.

(a) Remove the slide release cable from the flexible control assembly (5030WM and

5031WM)

Refer to AMM 25-62-43-000-001.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 54

6

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

SERVICE BULLETIN

Refer to Fig. A-GBAAA Sheet 01 and Fig. A-GBAAA Sheet 02

NOTE: Take care not to damage the insulation blankets when removing the

slide release cable.

1 To disconnect the control cable between Frame 40 and Frame 41 (Refer to

AMM Task 25-62-43-000-001) LH and RH, remove, as shown in View B:

Corrosion Resistant

Steel Lockwire

19-507 As required

2 Nut NAS1726C4P Item (10) Discard

2 Bolt NSA5031-4-4 Item (7) Discard

2 Nut NAS509-4C Item (9) Discard

2 Washer NAS1149C0463R Item (4) Discard

2 Bolt NSA5031H4-4 Item (5) Discard

2 Flange D5337025520000 Item (2) Retain

and

2 Pin-Cotter MS24665-153 Item (15) Discard

2 Pin-Clevis D5337048420200 Item (16) Retain

6 Washer NAS1149C0332R Item (3) Discard

2 To disconnect the control cable between Frame 46 and Frame 47 (Refer to

AMM Task 25-62-43-000-001) in the AFT cargo compartment, LH and RH,

remove and discard, as shown in View G:

and loosen the bracket attach nuts:

3 Between Frame 40 and Frame 47 LH and RH, remove, as shown in View C,

D, E, F and H:

2 Control Assy-Cable L32A319-160-001 Item (1) Discard

and

24 Clamp MS21919WCH6 Item (14) Discard

12 Bolt NSA5031-3-5 Item (8) Discard

12 Bolt NSA5031-3-4 Item (6) Discard

24 Washer NAS1149C0332R Item (3) Discard

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 55

6

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

SERVICE BULLETIN

16 Nut NAS1726C3P Item (11) Discard

(2) Subtask 531227-831-202-001 - Install the slide release cable to the flexible control

assembly (5030WM and 5031WM)

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Manhours 13.50

Minimum number of person 2

Subtask elapsed time 6.75

Skills CABIN

AIRFRAME

Material necessary to do the job

Kit 531227D01R05

ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE

NOTES

1 L32A320-180 2 CABLE

3 NAS1149C0332R 30 WASHER

4 NAS1149C0463R 2 WASHER

5 NSA5031H4-4 2 BOLT

6 NSA5031-3-4 12 BOLT

7 NSA5031-4-4 2 BOLT

8 NSA5031-3-5 12 BOLT

9 NAS509-4C 2 NUT

10 NAS1726C4P 2 NUT

11 NAS1726C3P 16 NUT

12 DAN79-07 0.08 (ME) HOSE

13 NSA935401-03 4 TIE

14 MS21919WCH5 24 CLAMP

15 MS24665-153 2 PIN

Consumable CMLD01

ITEM DESCRIPTION REFERENCE TO

CML MAT. No.

QTY PER A/C SEE

NOTES

Corrosion Inhibiting low

Adhesion Sealant

09-018 As required

Corrosion Resistant Steel

Lockwire

19-507 As required

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

Consumable Material List (CML)

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 56

6

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

SERVICE BULLETIN

References

Fig. A-GBAAA

Modification of the Release Cable for the

Overwing Emergency Exit

Sheet 01

Sheet 02

Sheet 03

WARNING: WEAR GOGGLES WHEN YOU REMOVE OR INSTALL THE

LOCKWIRE. CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU

DO THE TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.

(a) Install the cable with orientation marking visible towards the inside of the aircraft

(Minimum radius 180 mm (7.08 inch).

Refer to AMM 25-62-43-400-001.

Refer to Fig. A-GBAAA Sheet 01, Fig. A-GBAAA Sheet 02 and Fig. A-GBAAA

Sheet 03

NOTE: Take care not to damage the insulation blankets when installing the

slide release cable.

1 Position the control cable between Frame 40 and Frame 47 LH and RH, and

install, as shown in View A:

2 Cable L32A320-180 Item 1

and attach with:

24 Clamp MS21919WCH5 Item 14

NOTE: Clamp PN MS21919WCH6 can be used at points where

installation of clamp PN MS21919WCH5 is not possible or

easily achieved.

24 Washer NAS1149C0332R Item 3

12 Bolt NSA5031-3-4 Item 6

12 Bolt NSA5031-3-5 Item 8

16 Nut NAS1726C3P Item 11

NOTE: Take care when installing the slide release cable, Item

1, between the skin and the frames. To avoid mishandling

damage to the slide release cable, it is advisable to use two

people when installing the cable. One person to guide the

cable between the skin and the frames and one to support

the cable, make sure that the cable is relaxed and untwisted

before securing in position.

NOTE: Install one or two additional washers, Item 3, for clamp

installation shown in Fig. A-GBAAA View C, D, E, F and H, as

necessary.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 57

6

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

SERVICE BULLETIN

2 Install at Frame 40 LH and RH, as shown in View B:

2 Flange D5337025520000 Item (2) Retained at

removal

with:

Corrosion Inhibiting

low Adhesion

Sealant

09-018 As required

and

2 Bolt NSA5031-4-4 Item 7

2 Nut NAS1726C4P Item 10

and

2 Bolt NSA5031H4-4 Item 5

2 Washer NAS1149C0463R Item 4

2 Nut NAS509-4C Item 9

and connect to the bellcrank with:

2 Pin-Clevis D5337048420200 Item (16) Retained at

removal

6 Washer NAS1149C0332R Item 3

2 Pin MS24665-153 Item 15

3 Cut

0.08 (ME) Hose DAN79-07 Item 12

to a length of 40 mm (1.575 inch) then cut hose longitudinally and install at

Frame 41 LH and RH, with

4 Tie NSA935401-03 Item 13

as shown in View H.

4 Install and connect the control cable between Frame 46 and Frame 47 in the

AFT cargo compartment, LH and RH, as shown in View G.

5 After adjustments to the control cable make sure that all nuts are secure and

install, as shown in View J and K:

Corrosion Resistant

Steel Lockwire

19-507 As required

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 58

6

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

SERVICE BULLETIN

**CONF ALL

D. TEST

**CONF 001

(1) Subtask 531227-720-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Skills CABIN

AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

(a) Adjust and do the functional test of the flexible control assembly (Refer to AMM

25-62-43-400-001).

**CONF 002

(1) Subtask 531227-720-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Skills CABIN

AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

(a) Adjust and do the functional test of the flexible control assembly (Refer to AMM

25-62-43-400-001).

**CONF 003

(1) Subtask 531227-720-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

240

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 59

6

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SERVICE BULLETIN

Manpower Resources

Skills CABIN

AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

(a) Adjust and do the functional test of the flexible control assembly (Refer to AMM

25-62-43-400-001).

**CONF 004

(1) Subtask 531227-720-201-001 - Test

Work Zones and Access Panels

Zone Access/Work location

240

Manpower Resources

Skills CABIN

AIRFRAME

References

Aircraft Maintenance Manual (AMM) Task 25-62-43-400-001

(a) Adjust and do the functional test of the flexible control assembly (Refer to AMM

25-62-43-400-001).

**CONF ALL

E. CLOSE-UP

**CONF 001

(1) Subtask 531227-942-202-001 - Close access

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241FW, Panel 241LW, Panel 241PW,

Panel 241SW, Panel 241KW, Panel 241AX,

Panel 241JW, Panel 241NW, Panel 241RW,

Panel 241UW, Panel 241VW, Panel 241BX,

Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241CX

151 Access Panel 151CW

152 Access Panel 152CW

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 60

6

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@A318/A319/A320/A321

SERVICE BULLETIN

242 Access Panel 242LW, Panel 242FW, Panel 242PW,

Panel 242SW, Panel 242KW, Panel 242AX,

Panel 242JW, Panel 242NW, Panel 242RW,

Panel 242UW, Panel 242VW, Panel 242BX,

Panel 242CX, Panel 242MW, Panel 242QW,

Panel 242TW, Panel 242WW

Manpower Resources

Skills NON SPECIFIC

CABIN

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-001

Task 25-21-41-400-001

Task 25-23-43-400-001

Task 25-23-44-400-001

Task 25-23-47-400-002

Task 25-23-48-400-001

Task 25-55-11-400-003

Task 25-62-00-081-001

Task 25-62-43-400-001

Task 52-21-11-400-001

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

equipment.

(b) To close access to the cable assembly:

1 Replace the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

2 Install bracket PN D2127249820000 at Frame 47, as necessary.

3 Reposition and secure all electrical wires that were loosened, as necessary.

(c) Install the aft cargo compartment panels 151CW, 152CW (Refer to AMM Task

25-55-11-400-003).

(d) Install the air conditioning distribution duct(s) between Frame 38 and Frame 47, as

necessary (Refer to AMM Task 21-20-00-410-001).

(e) Install the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW, 242LW,

242FW, 242PW, 242SW (Refer to AMM Task 25-23-47-400-002).

(f) Install the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-400-001).

(g) Install the upper side panels 241VW, 241BX, 242VW, 242BX (Refer to AMM Task

25-23-43-400-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 61

6

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@A318/A319/A320/A321

SERVICE BULLETIN

(h) Install the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242CX,

242MW, 242QW, 242TW, 242WW (Refer to AMM Task 25-23-48-400-001).

(i) Install the emergency exit hatches (Refer to AMM Task 52-21-11-400-001).

(j) Install the passenger seats in the area of the emergency exit between Frame 38

and Frame 47 (Refer to AMM Task 25-21-41-400-001).

(k) Remove the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-400-001 and AMM Task 25-62-00-081-001).

(2) Subtask 531227-942-203-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-001

52-30-00, Page Block 201

(a) Close the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-410-001).

(b) Close the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

**CONF 002

(1) Subtask 531227-942-202-002 - Close access

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241FW, Panel 241LW, Panel 241PW,

Panel 241SW, Panel 241KW, Panel 241AX,

Panel 241JW, Panel 241NW, Panel 241RW,

Panel 241UW, Panel 241VW, Panel 241BX,

Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241CX

242 Access Panel 242LW, Panel 242FW, Panel 242PW,

Panel 242SW, Panel 242KW, Panel 242AX,

Panel 242JW, Panel 242NW, Panel 242RW,

Panel 242UW, Panel 242VW, Panel 242BX,

Panel 242CX, Panel 242MW, Panel 242QW,

Panel 242TW, Panel 242WW

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 62

6

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

SERVICE BULLETIN

151 Access Panel 151SW

152 Access Panel 152SW

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-001

Task 25-21-41-400-001

Task 25-23-43-400-001

Task 25-23-44-400-001

Task 25-23-47-400-002

Task 25-23-48-400-001

Task 25-55-11-400-003

Task 25-62-00-081-001

Task 25-62-43-400-001

Task 52-21-11-400-001

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

equipment.

(b) To close access to the cable assembly:

1 Replace the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

2 Install bracket PN D2127249820000 at Frame 47, as necessary.

3 Reposition and secure all electrical wires that were loosened, as necessary.

(c) Install the aft cargo compartment panels 151SW, 152SW (Refer to AMM Task

25-55-11-400-003).

(d) Install the air conditioning distribution duct(s) between Frame 38 and Frame 47, as

necessary (Refer to AMM Task 21-20-00-410-001).

(e) Install the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW, 242LW,

242FW, 242PW, 242SW (Refer to AMM Task 25-23-47-400-002).

(f) Install the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-400-001).

(g) Install the upper side panels 241VW, 241BX, 242VW, 242BX (Refer to AMM Task

25-23-43-400-001).

(h) Install the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242CX,

242MW, 242QW, 242TW, 242WW (Refer to AMM Task 25-23-48-400-001).

(i) Install the emergency exit hatches (Refer to AMM Task 52-21-11-400-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 63

6

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SERVICE BULLETIN

(j) Install the passenger seats in the area of the emergency exit between Frame 38

and Frame 47 (Refer to AMM Task 25-21-41-400-001).

(k) Remove the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-400-001 and AMM Task 25-62-00-081-001).

(2) Subtask 531227-942-203-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-001

52-30-00, Page Block 201

(a) Close the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-410-001).

(b) Close the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

**CONF 003

(1) Subtask 531227-942-202-001 - Close access

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241FW, Panel 241LW, Panel 241PW,

Panel 241SW, Panel 241KW, Panel 241AX,

Panel 241JW, Panel 241NW, Panel 241RW,

Panel 241UW, Panel 241VW, Panel 241BX,

Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241CX

151 Access Panel 151CW

152 Access Panel 152CW

242 Access Panel 242LW, Panel 242FW, Panel 242PW,

Panel 242SW, Panel 242KW, Panel 242AX,

Panel 242JW, Panel 242NW, Panel 242RW,

Panel 242UW, Panel 242VW, Panel 242BX,

Panel 242CX, Panel 242MW, Panel 242QW,

Panel 242TW, Panel 242WW

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 64

6

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

SERVICE BULLETIN

Manpower Resources

Skills NON SPECIFIC

CABIN

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-001

Task 25-21-41-400-001

Task 25-23-43-400-001

Task 25-23-44-400-001

Task 25-23-47-400-002

Task 25-23-48-400-001

Task 25-55-11-400-003

Task 25-62-00-081-001

Task 25-62-43-400-001

Task 52-21-11-400-001

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

equipment.

(b) To close access to the cable assembly:

1 Replace the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

2 Install bracket PN D2127249820000 at Frame 47, as necessary.

3 Reposition and secure all electrical wires that were loosened, as necessary.

(c) Install the aft cargo compartment panels 151CW, 152CW (Refer to AMM Task

25-55-11-400-003).

(d) Install the air conditioning distribution duct(s) between Frame 38 and Frame 47, as

necessary (Refer to AMM Task 21-20-00-410-001).

(e) Install the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW, 242LW,

242FW, 242PW, 242SW (Refer to AMM Task 25-23-47-400-002).

(f) Install the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-400-001).

(g) Install the upper side panels 241VW, 241BX, 242VW, 242BX (Refer to AMM Task

25-23-43-400-001).

(h) Install the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242CX,

242MW, 242QW, 242TW, 242WW (Refer to AMM Task 25-23-48-400-001).

(i) Install the emergency exit hatches (Refer to AMM Task 52-21-11-400-001).

(j) Install the passenger seats in the area of the emergency exit between Frame 38

and Frame 47 (Refer to AMM Task 25-21-41-400-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 65

6

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

SERVICE BULLETIN

(k) Remove the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-400-001 and AMM Task 25-62-00-081-001).

(2) Subtask 531227-942-203-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-001

52-30-00, Page Block 201

(a) Close the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-410-001).

(b) Close the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

**CONF 004

(1) Subtask 531227-942-202-002 - Close access

Work Zones and Access Panels

Zone Access/Work location

241 Access Panel 241FW, Panel 241LW, Panel 241PW,

Panel 241SW, Panel 241KW, Panel 241AX,

Panel 241JW, Panel 241NW, Panel 241RW,

Panel 241UW, Panel 241VW, Panel 241BX,

Panel 241MW, Panel 241QW, Panel 241TW,

Panel 241WW, Panel 241CX

242 Access Panel 242LW, Panel 242FW, Panel 242PW,

Panel 242SW, Panel 242KW, Panel 242AX,

Panel 242JW, Panel 242NW, Panel 242RW,

Panel 242UW, Panel 242VW, Panel 242BX,

Panel 242CX, Panel 242MW, Panel 242QW,

Panel 242TW, Panel 242WW

151 Access Panel 151SW

152 Access Panel 152SW

Manpower Resources

Skills NON SPECIFIC

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 66

6

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

SERVICE BULLETIN

References

Aircraft Maintenance Manual (AMM) Task 21-20-00-410-001

Task 25-21-41-400-001

Task 25-23-43-400-001

Task 25-23-44-400-001

Task 25-23-47-400-002

Task 25-23-48-400-001

Task 25-55-11-400-003

Task 25-62-00-081-001

Task 25-62-43-400-001

Task 52-21-11-400-001

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

equipment.

(b) To close access to the cable assembly:

1 Replace the insulation blankets, as necessary.

NOTE: Take care not to damage the insulation blankets.

2 Install bracket PN D2127249820000 at Frame 47, as necessary.

3 Reposition and secure all electrical wires that were loosened, as necessary.

(c) Install the aft cargo compartment panels 151SW, 152SW (Refer to AMM Task

25-55-11-400-003).

(d) Install the air conditioning distribution duct(s) between Frame 38 and Frame 47, as

necessary (Refer to AMM Task 21-20-00-410-001).

(e) Install the upper sidewall panel assembly 241FW, 241LW, 241PW, 241SW, 242LW,

242FW, 242PW, 242SW (Refer to AMM Task 25-23-47-400-002).

(f) Install the lower sidewall panels 241KW, 241AX, 241JW, 241NW, 241RW,

242KW, 242AX, 242JW, 242NW, 242RW, 241UW, 242UW (Refer to AMM Task

25-23-44-400-001).

(g) Install the upper side panels 241VW, 241BX, 242VW, 242BX (Refer to AMM Task

25-23-43-400-001).

(h) Install the cove light panels 241MW, 241QW, 241TW, 241WW, 241CX, 242CX,

242MW, 242QW, 242TW, 242WW (Refer to AMM Task 25-23-48-400-001).

(i) Install the emergency exit hatches (Refer to AMM Task 52-21-11-400-001).

(j) Install the passenger seats in the area of the emergency exit between Frame 38

and Frame 47 (Refer to AMM Task 25-21-41-400-001).

(k) Remove the safety/lock pin in the regulator valve assembly of the inflation reservoir

(Refer to AMM Task 25-62-43-400-001 and AMM Task 25-62-00-081-001).

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 67

6

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@A318/A319/A320/A321

SERVICE BULLETIN

(2) Subtask 531227-942-203-001 - Close-up

Work Zones and Access Panels

Zone Access/Work location

830 Access Door 831

820 Access Door 826

Manpower Resources

Skills NON SPECIFIC

References

Aircraft Maintenance Manual (AMM) Task 52-10-00-410-001

52-30-00, Page Block 201

(a) Close the FWD passenger/crew door 831 (Refer to AMM Task 52-10-00-410-001).

(b) Close the AFT cargo compartment door 826 (Refer to AMM 52-30-00, Page Block

201).

(c) Remove the access platform(s).

(d) Restore the systems and the aircraft to normal operating condition.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 68

6

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

SERVICE BULLETIN

**CONF 001, 004

A

EXAMPLE

Z240

FR38

FR47

(1) 1

(1)1

(2)

(7) 7

(5) 5

(9) 9

(3) 3

(15) 15

(3) 3

(16)

(3) 3

ORIENTATION (10)10

LINE

B

B

C

C

(4) 4

40 mm

(1.574 in)

D

E

F

G

H

J

5030WM

(8) 8

(3) 3

(14)14

(11)11

C

(5031WM)

LH SHOWN

RH SYMMETRICAL

LH

RH

A

LOCATION OF

CABLE PN.

N_SB_531227_6_BAAA_01_04

Figure A-GBAAA - Sheet 01

Modification of the Release Cable for the Overwing Emergency Exit

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 69

6

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

SERVICE BULLETIN

**CONF 001, 004

EXAMPLE

F

E

D

(14)14

(3) 3

(6) 6

(14)14

(3) 3

(6) 6

(3) 3

(14) 14

(11) 11

(1) 1

FR47

ORIENTATION

LINE

G

K

(6) 6

(6) 6

(3) 3

(11) 11

(12)12

(13)13

(13)13

(14)14

40 mm

(1.574 in)

FR41

H

N_SB_531227_6_BAAA_02_03

Figure A-GBAAA - Sheet 02

Modification of the Release Cable for the Overwing Emergency Exit

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 70

6

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

SERVICE BULLETIN

**CONF 001, 004

67.0 mm ± 2.0 mm

2.638 in ± 0.079 in

11.5 mm ± 1.7 mm

0.453 in ± 0.067 in

FR47

K

FWD

VIEW LOOKING AFT

J

NOTE:

01 SAFETY WITH LOCKWIRE, MAT. NO. 19−507 AFTER ADJUSTMENT

01

01

01

N_SB_531227_6_BAAA_03_02

Figure A-GBAAA - Sheet 03

Modification of the Release Cable for the Overwing Emergency Exit

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 71

6

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

SERVICE BULLETIN

**CONF 002 thru 003

A

EXAMPLE

Z240

FR38

FR47

(1) 1

(1)1

(2)

(7) 7

(5) 5

(9) 9

(3) 3

(15) 15

(3) 3

(16)

(3) 3

ORIENTATION (10)10

LINE

B

B

C

C

(4) 4

40 mm

(1.574 in)

D

E

F

G

H

J

5030WM

(8) 8

(3) 3

(14)14

(11)11

C

(5031WM)

LH SHOWN

RH SYMMETRICAL

LH

RH

A

LOCATION OF

CABLE PN.

N_SB_531227_6_BAAB_01_04

Figure A-GBAAB - Sheet 01

Modification of the Release Cable for the Overwing Emergency Exit

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 72

6

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

SERVICE BULLETIN

**CONF 002 thru 003

EXAMPLE

(6) 6

(3) 3

(11) 11

(12)12

(13)13

(13)13

(14)14

40 mm

(1.574 in)

FR41

H

F

E

D

(14)14

(3) 3

(6) 6

(14)14

(3) 3

(6) 6

(3) 3

(14) 14

(11) 11

(1) 1

FR47

ORIENTATION

LINE

G

K

(6) 6

N_SB_531227_6_BAAB_02_02

Figure A-GBAAB - Sheet 02

Modification of the Release Cable for the Overwing Emergency Exit

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 73

6

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

SERVICE BULLETIN

**CONF 002 thru 003

67.0 mm ± 2.0 mm

2.638 in ± 0.079 in

11.5 mm ± 1.7 mm

0.453 in ± 0.067 in

FR47

K

FWD

VIEW LOOKING AFT

J

NOTE:

01 SAFETY WITH LOCKWIRE, MAT. NO. 19−507 AFTER ADJUSTMENT

01

01

01

N_SB_531227_6_BAAB_03_02

Figure A-GBAAB - Sheet 03

Modification of the Release Cable for the Overwing Emergency Exit

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 74

6

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

SERVICE BULLETIN

REPORTING SHEET

TITLE: FUSELAGE - GENERAL - INTRODUCE IMPROVED SLIDE RELEASE

CABLE FOR EMERGENCY EXIT HATCH

MODIFICATION No.: 150811K13931

Please complete the appropriate item (A or B):

A - SB WILL BE embodied YES/NO (if NO please comment)

If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of

embodiment:

B - SB HAS BEEN embodied on aircraft:

Operator comments:

From Airline:

Name/Title:

Signature: Date:

If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to

next normal revision or prior to SB embodiment, please indicate required service(s):

Either: Modification Operational Impact (MOI), if available YES/NO

Or : Intermediate revision YES/NO

Important Information: This SB will only be incorporated in your maintenance and operational

documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With

the next feasible revision, this will result in

- Updating of maintenance documentation to show pre and post SB data.

- Updating of maintenance and operational documentation to show post SB data after embodiment.

If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically

include them in the manual revisions. Refer to SIL 00-037 for detailed information.

Please return this completed sheet to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn: SDC32 Technical Data and Documentation Services

FAX: (+33) 5 61 93 28 06

e-mail: sb.reporting@airbus.com

or via your Resident Customer Support Office.

Alternatively, SB lists via letters or fax are also accepted.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 1

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@A318/A319/A320/A321

SERVICE BULLETIN

QUALITY PERCEPTION FORM

Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data

that you provide us will be used to analyse areas of difficulties and to take corrective action to further

improve the quality of our Service Bulletins.

We thank you for the time you have taken in completing this form.

(Please rate on a scale of 1 to 4, with 4 being the highest score)

- Quality rating of this SB 4321

- Quality rating of the Accomplishment Instructions 4321

- Quality rating of the Illustrations 4321

- Is this SB easy to understand ? Y/N

If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a

short description of the issue.

Planning Material Instructions

X Effectivity X Kit content X Preparation

X Reason X List of Materials Operator Supplied X Mod/Inspection

X Manpower X Industry support X Test

X References X Re-identification X Close-Up

X Publication X Tooling X Illustrations

Comments:

Operator: Date:

Name/Title:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Attn : SEM4 Service Bulletins Management

FAX : (33) 5 61 93 42 51

Or via your Resident Customer Support Office.

DATE: Mar 24/10 SERVICE BULLETIN No.: A320-53-1227

REVISION No.: 05 - Mar 27/12 Page: 1

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