rJ)A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rand Point Maurice Bellante

31707 BLAGNAC CEOEX FRANCE

Tel: (33) 5 61 93 33 33

Telex: AIRBU 530526F

Fax: (33) 5 61 9342 51

MANDATORY

AlA SYSTEM: 27

MANDATORY MANDATORY MANDATORY

REPAIR

TITLE: FLIGHT CONTROLS· FLAP TRANSMISSION· INSPECT 5PLlNED COUPLINGS AND SLIDING

BEARING/PLUNGING JOINTS

1

I

MODIFICATION No. : NONE

ThiS page transmits Revision No. 01 of Service Bullelin No. A310-27-2099.

ADDITIONAL WORK

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

REASON

This Revision is issued to :

update the EFFECTIVITY,

introduce minor changes.

CHANGES

SUMMARY:

EFFECTIVITY

EFFECTIVITY updated

PLANNING INFORMATION:

EFFECTIVITY

1A EFFECTIVITY updated.

ACCOMPLISHMENT INSTRUCTIONS:

I

3_C.(1)(a)1 FIN 5487 and 5530 added.

I

3.C.(1 )(b)1 FIN 5487 and 5530 added.

DATE: Feb 17106

REVISION No. : 01 - Mar 21/08

SERVICE BULLETIN No.: A310-27-2099

Page'lof2

Prinled In France ICIAIRBUS 2008 All rights re.ervod
~A310

SERVICE BULLETIN

RErVISION TRANSMITIAL SHEET

TESTS

3.0. Wording revised.

Figure 1

Sheet 3 revised.

NOTE: Layout changes due 10 computerization of this revision are not identified.

FILING INSTRUCTIONS

This Service Bulletin has been 98°1 erated electronically and is reissued as a complete document.

Replace the complete document.

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

HISTORY OF PREVIOUS REViSIONS

No previous revisions.

REVISION SEQUENCE

ORIGINAL: Feb 17m6

REVISION No. : 01 - Mar 211GB

DATE: Feb 17/06

REVISION No.: 01 - Mar 21/08

SERVICE BULLETIN No.: A310-27-2099

Page 2

Printed In F'ance@AIRBUS2008AJI rights reser\l~d
~A310

SERVICE BULLETIN

SUMMARY

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellante

31707 BLAGNAC CEDEX FRANCE

Tel: (33) 5 61 93 33 33

Telex: AIRBU 530526F

Fax: (33) 5 61 93 42 51

MANDATORY

AlA SYSTEM: 27

This summary is for information only and is

nol approved for modification of the aircraft

MA~DATORY MANDATORY MANDATORY

TITLE: FLIGHT CONTROLS - FLAP TRANSMISSION - INSPECT 5PLlNED COUPLINGS AND SLIDING

BEARING/PLUNGING JOINTS

MODIFICATION No. : NONE

REASON/DESCRIPTIONfOPERATIONAL CONSEQUENCES

On the occasion of an inspection of Ihe A310 nap system, it was found that certain parts of the system need a

visual inspeclion 10 address corrosion and wear in order 10 maintain the system integrity.

This Service Bulletin details the visual inspection of the wiper rings of the splined couplings and the rubber

gaiters on the sliding bearings and plunging joints of the flap transmission.

I

The accomplishment of this Service Bulletin will maintain system integrity.

EVALUATION TABLE I

COMPLIANCE

,

Mandatqry CANCELS INSPECTION SB No

AD y" I AlC OPERATION AFFECTED No I

RELIABILITY AFFECTED No I PAX COMFORT AFFECTED No I

COST SAVING No I ETOPS AFFECTED No I

STRUCTURAL LIFE EXTN No I VENDOR S8 INVOLVED No

KIT PRICE (USD) No Kit

EFFECTIVITY

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

I

34W 58X 82Z 99Y A1l AIC ARG BAF BBC BLM CFC CSA DAH DGA F21 FOX GAF IRA IRM lYE JAB

JAV KAC KTC MGL MPD MPJ MWA PIA OAF OSC R1T RJA ROT RZO SBt SGX SUD TAP THY TSC

UAE UZB WHT

CONCURRENT REQUIREMENTS

None

DATE. Feb 17/06

REVISION No. ,01 - Mar 21/08

SERVICE BULLETIN No, : A310-27~2099

Page'1013

Prinled in France@AIRBUS 2008 All lights reserved
~A310

SERVICE BULLETIN

SUMMARY

REFERENCESIREPERCUSSIONS

TFU

OEB

AOT

Sil

LIFE LIMIT

: None

: None

: None

: None

: None

LINE MAINTENANCE AFFECTEi No

OTHERS None

NATURE OF THE WORK

AIRCRAFT : YES

EQUIPMENT: NO

HARD. NO

SOFT: NO

DBRM: NO

MANPOWER

TOTAL MAN HOURS

ELAPSED TIME (HOURS)

MATERIAL INFORMATION

AIRCRAFT DATA

None

APPENDICES

None

DATE: Feb 17/06

REVISION No. : 01 - Mar 21/08

14.00

7.00

SERVICE BULLETIN No.: A310-27-Z099

Page: 2

Printed In France@AIRSUS 2008 All righls reserved
~A310

SERVICE BULLETIN

SUMMARY

I

LEFT SIDE SHOWN,

RIGHT SIDE MIRROR

IMAGE

POWER CONTROL UNIT

5<87

(5530).......---- _ .......----

.----

5<70

(5513)

.----'---

2

.----'--- .----

5472

(5515)

'\ Z581(681)

2515(675

Z572(67211

"

5474"2\

/(5S17)\V

5485

(5528)

1 RIGHT ANGLE

;;;: GEAR80X~

;'f NOTE:

0--

g 0) INSPECT THE WIPER RING

~0INSPECT THE GAllER

w

w

DATE: Feb 17/06 SERVICE BULLETIN No. : A310-27-2099

REVISION No.: 01 - Mar21/08 Page, 3

Print. In Franco@AIRBUS2006AII righls r"s"rve~
DATE. Feb 17/06

REVISION No. : 01 - Mar 21/08

I$!A310

SERVICE BULLETIN

This Page Intentionally Left Blank

SERVICE BULLETIN No. : A310-27-2099

Page: 4

Prlnlei! In Franca © AIRBUS 2006 All righl$ re$mv~d
($)A310

SERVICE BULLETIN

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rond Point Maurice Bellante

31707 BLAGNAC CEDEX FRANCE

Tel: (33) 5 61 93 33 33

Telex: AIRBU 530526F

Fax: (33) 5 61 93 42 51

MANDATORY

AlA SYSTEM: 27

MANDATORY MANDATORY MANDATORY

TITLE: FLIGHT CONTROLS· FLAP rr-ANSMISSION • INSPECT 5PLlNED COUPLINGS AND SLIDING

BEARING/PLUNGING JOINTS

MODIFICATION No. : NONE

This document contains AIRBUS PROP·RIETARY 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 il. II is delivered on the express condition that the said document and the information contained

in it shall be treated as confidential, shall nol 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 documenl shall comply with the conditions herein), without AIRBUS prior wrillen consent.

1. PLANNING INFORMATION

A. EFFECTIVITY

(1) Models

310-203 310-203C 310~204310-221 310-222 310-304 310-308 310-322 310-324 310-325

(2) Aircraft

(a)

DATE.Feb 17/06

Effectivity by MSN

:::2 :~c;~,:;,:"::: ;'O::i:::~;::~c:~3: ~::'·0245 02480251025402571

026402670273027802810283028802910293029703030309 0313 0316 0318

032003260331033303350338033903420343034503460349 0353 0355-0357

03590360036203640367036903700372 0375 0378 0379 0386 0389 0390 0392

0394 0397 0399 0400 0406 0407 0410 0413 0416 0418 0419 042104220425

0427-0431043404360437043904410444-04490451-04580467 0468 0472 0473

0475047604780480-04920494-0500050205030519 0520 0522-0524 0526 0527

0531053405350537-053905410542054405450547-055205620564 0565 0567

056805710573057405760585-05950597-060006200622 0624 0634 0636

06380640064206440646-0654 0656 0658 0660 0661 066306650667 0669

SERVICEBULLETINNo. : A310-27-2099

REVISIONNo. : 01 - Mar21/08

Pri"le~ i" FranceC AIRSUS 2008 All rights reserved

Page:1of16
I

($;A310

SERVICE BULLETIN

0671 0672 067~ 0676 0678 0680 0682 0684 0686 0687 0689 0691 06930695

0697 0700 0702 0704 0706

(b) Effectivityby 0f"ato;

The OperalorfMSN relationship is provided for information only and is correct at l~e

time of issue inlaccordance with the information available to AIRBUS. Any future I

changes resulli 9 from transfer of an aircraft from one operator to another will natbe

reflected in this list unless the Servlce Bulletin is revised for another reason.

OPERATOR

34W

58X

82Z

99Y

A1L

AIC

ARG

BAF

BBC

BLM

eFe

eSA

oAH

oGA

F2I

FOX

GAF

IRA

DATE Feb 17106

REVISION No. : 01 - Mar 21/08

Prlnl

MSN

0399

0431

0550 0551

0489

0648

039204060407041304280429053805440598065406650669

0680 0684 0693 0695 0697

0640 0686

0367 0372

0594 0650 0700

0488

0425 0441 0444 0446 0482

0564056706720674

0291 0293

041804210422

0309

~~~~~;~~~~~~~~;~;~~~~~~~:~~~:~~~~~b;

~~~~~~~~~~~~~~~~~~~~6i~6~;~~;~~~~~6;;~6;~~6~~i

04000439044904520454 0456 0457 0458 0467 0492 0500 05~4

05390542 0549 0552 0589 0593 0634 0638

0434 0484 0498 0499 0503 0522 0523

03380370 0375 0379 0389 0390 0436 0671

SERVICE BULLETIN No. : A310-27-2099

Page: 2

In Fmnce © AIRBUS 20U8 All rignls reserved
~A310

SERVICE BULLETIN

OPERATOR MSN

IRM 0537 0586

lYE 05350568 0702 0704

JAB 0320 0419

JAV 0357 0481

KAC 06470649 0663

KTC 0524

MGL 0526

MPD 0451 045304550642

MPJ 0410

MWA 0652

PIA 047305850587 0590 0653 0656 0660 0676 0678 0682 0687

0689 0691

QAF 0667

osc 0620

R1T 0591

RJA 04160445049004910531

ROT 0636 0644

RZO 0571 06240651 0661

S8t 0427043004680475048604870520

SGX 05190562

SUO 0437 0548

TAP 0483049404950541 05650573

THY 0386 0476 0478 0480 0496 0497 0502

TSC 044704720485052705450547058805950597059906000658

UAE 0592 0622 0646

UZB 057405760706

DATE: Feb 17/06 SERVICE BULLETIN No., A310-27-2099

REVISION No, : 01 - Mar 21108 Page: 3
~A310

SERVICE BULLETIN

OPERATOR

WHT

MSN

0448

(0) Effectivity by MSN and KitJConfiguralion

I

No AIRBUS kit is required for the accomplishment of this Service Bulletin

(3) Spares

None

B. CONCURRENT REQUIREMENTS

None

c. REASON

(1) History

On the occasion of an inspection of the A310 flap system, it was found that certain parts.of

the system need a vis al inspection to address corrosion and wear in order to maintain

the system integrity_

12)

13)

(4)

Objective/Action

This Service Bulletin ,8taiiS the visual inspection of the wiper rings of the splined couplings

and the rubber gaiters on the sliding bearings and plunging joints of the flap transmission'.

Advantages

The accomplishment qf this Service Bulletin will maintain system integrity.

operationallMaintena~ce Consequences

None

D. DESCRIPTION

To accomplish this Service Bulletin it is necessary to :

(1) Inspeclion

(a)

(2) Repair

DATE, Feb 17/06

~ISU~:~U~~~::lr' t:: :1:: ~:~::::~Ol~ :::::llned couplings of the flap transmission

shafts

£. Visually Inspect the rubber gaiters on [he sildlng beanng/plunglng JOints of

the flap transmission.

SERVICE BULLETIN No.: A310-27-2099

REVISION No.: 01 - Mar 21108

Printed in Fran"" © AIRBUS200BAllrights re,erven

Page 4
~A310

SERVICE BULLETIN

(a) Replace the aRplicable components.

1 Remove the applicable components as follows.

Remo~ the flap transmission shafts for workshop inspection/check.

Inspect and repair the flap transmission shafts in workshop.

Remove the sliding bearings for workshop inspection/check.

'nspecl and repair the sliding bearings in workshOp.

Removl the plunging joints for workshop inspection/check.

I

Inspect and repair the plunging joints in workshop

,g Inslall serviceable components.

~ Install the serviceable flap transmission shafts.

b Install the serviceable sliding bearings.

f. Install !;he serviceable plunging joints.

E. COMPLIANCE

(1) Classification

Mandatory

(2) Accomplishment Timescale

Threshold:

- II is mandatory to accomplish this Service Bulletin before 2500 FC after receipt of the

Service Bulletin. I

Interval:

- The inspection has to be repeated every 2500 FC.

European Airworthiness Safety Authority (EASA) regulatory action is expected for this

Service Bulletin by the issue of a Consigne de Navigabilite (CN) (Airworthiness Directive

(AD». It is anticipated that the CN will confirm the thresholds and/or interv·als given above

but references should be made to the CN for confirmation of the mandated accomplishment

timescale.

F. APPROVAL

Approved under EASA Design Organisation Approval No. EASA.21J.031.

If an aircrafllisted in the effeetivily has a modification or repair embodied that is not of AIRBUS

origin, and which affects the bontent of this Service Bulletin, the operator is responsible for

DATE: Feb 17/06

REVISION No.: 01 - Mar21/08

SERVICE BULLETIN No, : A310-27-2099

Page: 5

P<1nl••~ i~Fra~ce iClAIRBUS 2008 All rights r~"e,ved
r$JA310

SERVICE BULLETIN

obtaining approval by its airwmrthiness authority for any adaptation necessary before incorporation

of the Service Bulletin.

G. MANPOWER

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

work. These estimates aSSUrhe thai the work will be done by experienced personnel, and may

need to be revised upwards I? suit operators' circumstances. The estimates do nol include the

lime to prepare, plan or inspect the work, Manufacture and procurement of parts and IDols, dryi 9

lime for paints, sealants, elc. bnd general administration work are also not included.

Get Access 5.50

Inspection 3.00

Close-up 5.50

TOTAL MAN HOURS 14.00

ELAPSED TIME (HOURS) 7.00

H. WEIGHT AND BALANCE

Not changed

I, ELECTRICAL LOAD DATA

Not changed

J. REFERENCES

K.

L.

CMM

Aircraft Maintenance Manual .(AMM}

Compo"e"' M,'"'e"",, M,l"" (CMM)

Consumable Material List (CML)

PUBLICATIONS AFFECTED!

Ai",," M,'"''"'"'' M'"""iIAMM)

::U;;::::::SE:::~~y(;:lB'LlTY

No! applicable

: 27-52-26

: 06-41-57 24-00-00 27-50-00 27-54-00

27-54-1427-54-1527-54-1932-12-11

: 27-08-0227-52-2227-52-2327-52-24

27-54-19

; 27-51-0327-52-2627-54-05

DATE: Feb 17/06

REVISION No .. 01 - Mar 21/08

SERVICE BULLETIN No. ,A31Q-27-2099

Page 6

Prlnt~d in Fr~nce© AIRBUS 2008 All rlghls resorved
e;)A310

SERVICE BULLETIN

2_ MATERIAL INFORMATION

A. MATERIAL - PRICE AND AVAilABILITY

(1) Material

Replacement of remoyed components shoulq be negotiated directly with Goodrich

Actuating Systems Ltd. Apply 10 .

AMERICAS GOODRICH CUSTOMER SERVICE

4115 CORPORATE CENTER DRIVE

MONROE

NC 28110

USA

PHONE; +1 (0) 704 282 2500

FAX: +1 (0) 704 282 2560

AOG: +44 (0) 121 451 5904

EUROPE, MIDDLE EAST AND AFRICA

GOODRICH CONTROL SYSTEMS

STRATFORD ROAD

SOLIHULL

WEST MIDLANDS 890 4LA

ENGLAND

PHONE: +44 (0) 121 451 5755

FAX: +44 (0) 121 451 5949

AOG: +44 (0) 121 451 5904

ASIA/PACIFIC GOODRICH CONTROL SYSTEMS PTE

35/37 lOYANG WAY

SINGAPORE 508733

REPUBLIC OF SINGAPORE

PHONE: +65 (0) 545 9975

FAX: +65 (0) 543 0419

ADG : +44 (0) 121 451 5904

(2) Price and Availability

B.

c.

No AIRBUSfGOODRlyH kit will be provided. Parls required to accomplish this Service

INDUS:~;:U::~oR:el::d::::I:Na Spares Purchase Order.

AIRBUS will not provide indultrial support for accomplishment of this Service Bulielin.

LIST OF COMPONENTS

None

D. LIST OF MATERIALS - OP6RATOR SUPPLIED

(1) Consumable MaterialJ

DATE· Feb 17/06

REVISION No. : 01 - Mar 21/08

SERViCE BULLETIN No, A310-27-2099

Page. 7

Printo~ in Fiance © AIRBUS 2008 All right. reserved
~A310

SERVICE BULLETIN

DESCRIPTION REFERENCE TO CMl QTY PER Ale INST/DISP

MAT No.

Cleaning agent Mal. No. 11-026 As required

(2) Components

ITEM NEW PART No. OT~ UM KEYWORD ITEM OLD PART No. INT INST DISP

551A3500-03 5 GAITER

551A0702-Q2 5 GAITER

551A0403-02 5 GAITER

CH127676-13 5 STRAP

CH127676-6 5 STRAP see NOTE

551A0902-01 10 WIP.RING

NOTE: Or MS3367-1

E. PARTS TO BE RE·IDENTIFIED BY THE OPERATOR

None

F. TOOLING - PRICE AND AVAILABILITY

To accomplish this Service Bulletin it is necessary to use lhe lools tisled in AMM 27-50-00.

G. SPECIAL TOOLS

None

DATE' Feb 17/06

REVISION No. : 01 - Mar 21/08

SERVICE BULLETIN No . A310-27-2099

Page: 8

Printed In Fr~ncQ ~ I\IKBU$ 2008 All Mghls re.erved
~A310

SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL

WARNING: MAKE SURE T~AT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES.

WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION

BEFORE YOU START A TASK ON OR NEAR:

- THE FLIGHT bONTROLS

- THE FLiGHTICONTROLSURFACES

- THE LANDING GEAR AND THE ASSOCIATED DOORS

- OR ANY COJpONENT THAT MOVES.

MOVEMENT OF COMPONENTS CAN KilL OR INJURE PERSONS.

(1) Preparation

101

(b)

Ie)

Idl

lei

If I

Make sure that the aircraft is electrically grounded (Refer to AMM 24--00-00, Page

block 301).

Position the safety barriers.

Fully extend the flaps (Refer 10AMM 27-50-00, Page block 301)_

Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER, on the f1apfslat conlrol

lever (Refer to rM27~50·00, Page block 501).

Open the main gear main doors (Refer to AMM 32-12-11, Page block 301 l·

Open, safety a~d tag this (these) circuit breaker(s):

7:~~ip~~NT7}C~~~;H~~~';IL~~I~~"' ~~MM:AdRT~OEN~80~gb;~yCOCKPIT

DESIGN) embodied.

PANEL DESIGNATION FIN LOCATION

127VU FLT CTUFLAPS/SYS 1 & CTL 10CV 705/l64

SUPPLYJLAND RECOVERY

127VU FLT CTUFLAPSJSYS 1 & CTl 5CV 7051L65

SUPPLY/NORM

127VU FLT CTUFLAPSISYS 2 & CTL 6CV 705/L66

SUPPLY/NORM

Config. 02: Concerns aircraft with the Mod. No. 4803S5726

(EQUIPMENT/FURNISHING - FlIGHT·COMPARTMENT - MODIFY COCKPIT

DESIGN) embodied.

PANEL DESIGNATION FIN LOCATION

DATE: Feb 17/06

REVISION No.: 01 - Mar 21/08

SERVICE BULLETIN No.: A310-27-2099

Page: 9
I$JA310

SERVICE BULLETIN

133VU FLT CTlISFCC/NqRM 6CV 3311V61

SUPPLY/FLAPS/81'S 2

133VU FLT CTLlSFCC/NORM 5CV 332/U61

SUPPlYfFLAPS/S1S 1

133VU ~~Tp~~~:~~:~~~;+~ ,RECOVERYI 10CV 335/R67

(9) Put the access plalform(s) in position.

(h) Open the access doors (Refer to AMM 27-54-19, Page block 401).

(2) Standard Practices

(,)

(b)

(e)

For material specifications (Mat. No.) given in this Service Bulletin (Refer to

Consumable Mrteria, Lisl (CML) ),

For location of the access panels (Refer to AMM 06-41-57, Page block 001),

Clean the workl area with cleaning agent (Mat. No. 11-026).

B. INSPECTION

(1) Visually inspect the flap transmission shafts.

Refer 10 Figure 1

Refer 10 Figure 2

(,)

(bl

(e)

DATE. Feb 17/06

Visually inspect the wiper rings in the splined couplings of the flap transmission

shafts.

Make sure that the wiper rings in the crown spline joints of the flap drive shafts

are not damaged, protruding or missing, refer 10 Figure 1, Sheet 2, Details

2

BMakndC. I'h h . .. I· .. II I II d·

a e sure I at t e wiper rings In the crown sp Ine JOints are correc y inS a e In

their relaled grooves, refer to Figure 1, Sheel 2, Details Band C.

[

Visually inspec! the rubber gaiters on the sliding bearing/plunging joints of the

flap transmissi6n.

[

1 Make surejthat the gaiters and straps are not damaged or missing, refer to

Figure 1, Sheet 3, Details 0 and E,

2 Make sure that the gaiters are properly secured by their straps and that the

gaiters are correctly installed, refer to Figure 1, Sheet 3, Delails D and E.

If no damage, missing or incorrect installation is found on the wiper rings and

rubber gaiters i

1 Repeat the' inspection every 2500 Fe.

SERVICE BULLETIN No. : A310-27-2099

REVISION No, .01 - Mar 21/08

Printed in France © AIRBUS 2005 All rights ros~fved

Page.10
~A310

SERVICE BULLETIN

(d) If damage. missing or incorrect installation is found on the wiper rings and rubber

gaiters, refer to the repair para. (1).

C. REPAIR

I

I

I

I

1') Replace the applicable components,

NOTE: Do not re+ove a component from the aircraft if no serviceable one is in slock.

- Component must be replaced within 400 FH.

I'i Remo," 'he '+"ble compo"e"', e, follow,.

1 Remove thy flap transmission shafts for workshop inspection/check (Refer to

AMM 27-Sl19, Page block 401):

- 5470, 54

1

72, 5485, 5487, 5491 thru 5501 (odd numbers only),

- 5513,5515,5528,5530,5534 thru 5544 (even numbers only).

2 inspect anJ repair the flap transmission shafts in workshop in accordance willi

the relevanl CMM 27-52-23, CMM 27-52-24 and CMM 27-52-26.

3 Remove th~ sliding bearings for workshop inspection/check (Refer to AMM

27-54-15, lage block 401) ,

- 5480, 54

1

82, 5523 and 5525.

~ Inspect an9 repair the sliding bearings in workshop in accordance with the

CMM 27 -OS-02.

5 Remove th~ plunging joints for workshop inspection/check (Refer to AMM

27-54-14, lage block 401) :

- 5474, 5'rS, 5517 and 5521.

6 Inspect anq repair the plunging joints in workshop in accordance with the

CMM 27-52-22.

[

(b) Install serviceable components

1 Install the s~rvlceable flap transmiSSion shafts (Refer to AMM 27-54-19, Page

biock 401) I

5470, 5r2. 5485, 5487, 5491 thru 5501 (odd numbers only),

5513, 5T5, 5528. 5530, 5534 thru 5544 (even numbers only) .

.f Install the sirViceable sliding bearing (Refer to AMM 27-54-15, Page block 401) :

- 5480, 5Y2, 5523 and 5525.

3 install the serviceable plunging joints (Refer to AMM 27-54-14, Page block 401):

DATE: Feb 17/06

REVISION No. '01 - Mar 21/08

SERVICE BULLETIN No,. A310-27-2099

Page:11

Prinle in France© AIRBUS 2008 All right. re.crved
~A310

SERVICE BULLETIN

- 5474,54:78,5517 and 5521

4 Repeat the inspection every 2500 FC,

D. TEST

Only in case of repair, do the operational test of the flap system after removal/installation of the

shafts, sliding bearings and ~Iunging joints (Refer to AMM 27-54-00, Page block 501).

E. CLOSE UP

(1)

(2)

(3)

(4)

Make sure that the WOrkareas are clean and clear of tools and other items of equipment.

Close the access dOOr .(Refer to AMM 27-54-19, Page block 401).

Close the main gear main doors (Refer to AMM 32-12-11, Pa~e block 301),

Remove the safely CliJs and tags and close this (these) circuit breaker(s):

Config. 01 concer~s aircraft without the Mod. No. 4803S5726

(EQUIPMENT/FURNISHING - FLIGHT-COMPARTMENT - MODIFY COCKPIT DESIGN)

embodied.

335/R67

LOCATION

332/U61

705/L65

705/L64

705JL66

FIN

5ev

10CV

6ev

10CV

5ev

DESIGNATION

FlT CTLIFlAPS/SYS 1 & CTl

SUPPLY/LAND RE80VERY

FLT CTLIFlAPS/S1

1 S 1 & CTl

SUPPLY/NORM

FLT CTLIFLAPS/S}S 2 & CTl

SUPPLY/NORM

Config. 02 : Concernslaircraft with the Mod. No, 4803S5726 (EQUIPMENT/FURNISHING -

FLIGHT-COMPARTMENT - MODIFY COCKPIT DESIGN) embodied.

DESIGNATION I FIN LOCATION

FLT CTLlSFCC/NdRM 6CV 3311V61

SUPPlY/FlAPS/S\S 2

FLT CTLlSFCClNqRM

SUPPlY/FlAPS/S1S 1

FlT CTLlSFCC/LA~D RECOVERYI

SUPPlY/FLAPS/S'l(S 1

127VU

127VU

133VU

127VU

133VU

PANEL

133VU

PANEL

(5)

(6)

(7)

Fully retract the flaps ,Refer to AMM 27-50-00, Page block 301 l.

Remove the access platform(s).

Remove the safety ba~riers.

F. DOCUMENTATION

Write in the applicable aircraft records that you have done alilhe work given in this Service Bulle in.

DATE' Feb 17/06 SERVICE BULLETIN No. A310-27~2099

REVISION No.. 01 ~Mar21/08 Page. 12
I$JA310

SERVICE BULLETiN

1

LEFT SIDE SHOWN,

RIGHT SIDE MIRROR

IMAGE

POWER CONTROL UNIT

5<87

(5530}........__---

----

B

..Q.

5<70

(5513)

-------

B

..Q.

-------

B

..Q.

5472

(5515)

'\ ZSB1(681)

Z575{675)

2572(672)1

"

5<"

;(5517)

d

fUGHT ANGLE

GEARBOX

Figure 1, Sheet 1

Inspecllhe Flap Transmission

DATE: Feb 17/06 SERVICE BULLETIN No. : A310-27-2099

REVISION No. : 01 - Mar 21/08 Page: 13
($JA310

SERVICE BULLETIN

2. INCORRECT INSTALLATION

WIPER RING IS MISSING

1. CORRECT WIPER RING

INSTALLATION

3. INCORRECT INSTALLATION

PROTRUDING WIPER RIN I

WIPER RING

TYPICAL

Figure 1, Sheet 2

Inspect the Flap Transmission

DATE. Feb 17/06 SERVICE BULLETIN No. : A310~27-2099

REVISION No.: 01 - Mar21108 Page. 14
~A310

SERVICE BULLETIN

[Q]

TYPICAL

SLIDING BEARING

[[]

TYPICAL

STRAP

GAITER

STRAP

PLUNGING JOINT

I

Figure 1, Sheel 3

Inspect the Flap Transmission

DATE: Feb 17106 SERVICE BULLETIN No.. A310-27-2099

REVISION No. : 01 - Ma,21/08 Page.15
~A310

SERVICE BULLETIN

VISUAL INSPECTION OF FLAP I

TRANSMISSION-SHAFTS IN ACCORDANCE

WITH THIS SERVICE BULLETIN 1

REPEAT THE

INSPECTION

EVERY 2,500 Fe,

ANY DAMAGE, OR MISSING

PARTS, OR INCORRECT

INSTALLATION FOUND,

ESPECIALLY ON THE

• WIPER RINGS

• RUBBER GArrERS

YES

IS THERE A SERVICEABLE

COMPONENT AVAILA8lE?

REPLACE WITHIN 400 FH

NO

'E'

Figure 2, Sheet 1

Inspection Flow CharI

INSTAll A SERVICEABLE

COMPONENT

ACCORDING TO

THE RELEVANT I\MM

REMOVE COMPONENT ON

WHICH DAMAGED PART IS

FlTIED IN ACCORDANCE

WITH THE RELEVANT AMM.

INSPECT FOR FURTHER

WEAR IN ACCORDANCE

WITH THE RELEVANT CMM.

DATE, Feb 17/06

REVISION No.: 01 - Mar21/08

SERVICE BULLETIN No.: A310-27-2099

Page: 16
..............••.. ·.•..••.. I

~A310

SERVICE BULLETIN

REPORTING SHEET

TITLE: FLIGHT CONTROLS - FLAP TRANSMISSION· INSPECT SPLINED COUPLINGS AND SLJDING

BEARING/PLUNGING JOINTS

MODIFICATION No. : NONE

Please complete the appropriate item fA or B):

A - S8 WILL BE embodied 1.. --. . " YES/NO (if NO please comment)

If YES, aircraft concerned (as per S8 effectivity by default) and planned dates (month/year) of embOdiemeit:

.......................................................... 1. .

... 1.... .. .. . ..J.

B - S8 HAS BEEN embodied on aircra,: _ , .__ 1..

....... ·· 1·· ············ ••.1

Operator comments:. 1.._

I·························· .

I················ .

From Airline: ,,__'. . __. ,..__ .

Namerrille:.. .. ._.. _.. .. .

Signature. . . I Date .. ..

If operallonal documentation is affected (see ParaQraph 1.K of thiS S8): If Information IS needed prior to next

normal revision or prior to S8 embodiment. please indicate required service(s):

Either : Advance data .1. __ _._.. .. _. .. _ _ YES/NO

:portant Info~~:tt:~:e~~~:e::::~~::: I~:v::::r~~~~;~~';~ .~.~.; '~~i~':~'~'a'~'~-e-~.~~.:p:~~~~nal documentation

if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible

reVision, this will result in I

- updating of maintenance docume~tation to show pre and post S8 data. j

- updating of maintenance and operational documentation to show post S8 data

after embodiment. J

If this S8 requires previous or simultan ~us accomplishment of other SSs, Airbus shall automatically incl de

them in the manual revisions. Refer to SIL 00-037 for detailed information.

I

Please return this completed sheet to:

AIRBUS I

CUSTOMER SERVICES PIRECTORATE

1 Rond Point Maurice Bellonte

31707 BLAGNAC CEDEX FRANCE

Altn: SEDCC1 TechnicaJloata and Oocumentation Services

FAX: ('''"33) 5 61 93 28 O~

e-mail: sb.reporting@airbLs.com ,

Or via your Resident Customer Support Office.

Alternatively, 58 lists via letters or fax are also accepted.

DATE: Feb 17/06

REVISION No .. 01 - Mar 21/08

SERVICE BULLETIN No.: A310-27-2099

Page:1of1

P(i~!e I~ Fr.~ca @AIRBUS2008All rights reserved
rsJA310

SERVICE BULLETIN

REPORTING QUALITY

TITLE; FLIGHT CONTROLS· FLAP l1RANSMISSION • INSPECT SPUNED COUPLINGS AND SLIDING

BEARING/PLUNGING JOINTS

MODIFICATION No. : NONE

4 3 2 ,1

l

'

432 1

432

-Quality rating of the Illustrations

Use this form 10 tell us what is your perception of the quality of this Service Bulletin,The reported dala thal ~ou

provide us will be used to analyse areaslof difficulties and 10 take corrective aelion to ruther improve the quality

of our Service Bulletins.

We thank you for the time you have taken in completing this form,

I

(Please rate on a scale 0jl to 4, with 4 being the highest score)

-Quality rating of this S8

-Quality rating of the Accomplish ent Instructions

-Is this S8 easy Lounderstand? Y I N

If you have had difficulties in the acco plishment of this SB please quole below the area(s) and give a sHort

description of the issue,

Planning

X Effectivity

X Reason

X Manpower

X References

X Publication

Material

X Kit Conlent

X List of Materials

Operator Supplied

X Re-idenlificalion

X Tooling

Instructions

X Preparation

X Mod/Inspection

X Test

X Close-up

X Illustrations

Comments:

Operator .

Namerritle:

Dale:

Please return this form to:

AIRBUS

CUSTOMER SERVICES DIRECTORATE

1 Rand Point Maurice ellonte

31707 BLAGNAC CEDEk FRANCE

Attn: SEMB Service BUIIJlins Management

FAX: (T33) 5 61 934251

Or via your Residenl Customer Support Office.

DATE: Feb 17/06 SERVICE BULLETIN No .. A310-27-2099

REVISION No.. 01 - Mar 21/08 Page. 1 011

Pri~( d i~France © AIRBUS 2008 All right, reserved