# 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 JOINTS1 

### I MODIFICATION No. : NONE ThiS page transmits Revision No. 01 of Service Bullelin No. A310-27-2099. ADDITIONAL WORK No additional work is required bythis revision foraircraft 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 ICI

AIRBUS 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 10computerization ofthis revision are not identified. FILING INSTRUCTIONS This Service Bulletin has been

# 98°1erated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in fronl ofthe 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 PrintedIn F'ance@AIRBUS2008AJI rightsreser\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 isfor information only and is nol approved for modification ofthe 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, itwas found that certain parts ofthe system need a visual inspeclion 10address corrosion and wear in order 10maintain the system integrity. This Service Bulletin details the visual inspection ofthe wiper rings ofthe splined couplings and the rubber gaiters on the sliding bearings and plunging joints ofthe flap transmission.



# I The accomplishment ofthis Service Bulletin will maintain system integrity. EVALUATION TABLE 

# I COMPLIANCE 

# , CANCELS INSPECTION SB 

### No Mandatqry 

### 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 

### LINEMAINTENANCE 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 

# ~0 INSPECT THE GAllER w w

DATE: Feb 17/06 SERVICE BULLETIN No. :A310-27-2099 REVISION No.: 01 - Mar21/08 Page, 3 Print. InFranco@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! InFranca ©AIRBUS 2006 Allrighl$ 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 ofAIRBUS; no intellectual property right or licence isgranted by AIRBUS in connection with any information contained in il. II isdelivered on the express condition that the said document and the information contained in itshall be treated as confidential, shall nol be used for any purpose other than that for which it is hereby delivered. Itshall 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 

### 310-203310-203C310~204310-221310-222310-304310-308310-322310-324310-325 (2) Aircraft (a)



### DATE.Feb 17/06 Effectivity by MSN 

# :::2

# :~c;~,:;,:"::: ;'O::i:::~ ;::~c:~3: ~::'·02450248 0251 025402571 026402670273027802810283028802910293029703030309 031303160318 032003260331033303350338033903420343034503460349 03530355-0357 03590360036203640367036903700372 0375037803790386038903900392 03940397039904000406040704100413041604180419042104220425 0427-0431043404360437043904410444-04490451-04580467 046804720473 0475047604780480-04920494-0500050205030519 05200522-052405260527 0531053405350537-053905410542054405450547-055205620564 05650567 056805710573057405760585-05950597-060006200622 062406340636 06380640064206440646-0654 0656065806600661066306650667 0669

SERVICEBULLETIN

No.:A310-27-2099 REVISION

No.:01
-Mar21/08 Pri"le~ i" FranceCAIRSUS2008All rightsreserved Page:1of16

# I ($;A310 SERVICE BULLETIN



### 0671 0672067~0676 0678 0680 0682068406860687 0689 0691 06930695 0697 0700 0702 0704 0706 

### (b) Effectivityby0f"ato; The OperalorfMSN relationship is provided for information only and iscorrect atl~e time of issue inlaccordance with the information available to AIRBUS. Any future

# I changes resulli 9from 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 

### 05940650 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 07020704 JAB 0320 0419 JAV 0357 0481 KAC 06470649 0663 KTC 0524 MGL 0526 MPD 0451 045304550642 MPJ 0410 MWA 0652 PIA 047305850587 05900653 0656 0660 0676 0678 06820687



### 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 0386047604780480049604970502 TSC 

### 044704720485052705450547058805950597059906000658 UAE 0592 0622 0646 UZB 057405760706 DATE: Feb 17/06 SERVICE BULLETIN No., A310-27-2099 REVISION No, :01 - Mar21108 Page: 3

# ~A310 SERVICE BULLETIN

OPERATOR WHT MSN



### 0448 (0) Effectivity by MSN and KitJConfiguralion



# I No AIRBUS kit is required for the accomplishment ofthis Service Bulletin (3) Spares None B. CONCURRENT REQUIREMENTS 

### None 

## c. REASON (1) History On the occasion of an inspection ofthe A310 flap system, itwas found that certain parts.of the system need avis 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 ofthe wiper rings ofthe splined couplings and the rubber gaiters on the sliding bearings and plunging joints ofthe flap transmission'. Advantages The accomplishment qfthis Service Bulletin will maintain system integrity. operationallMaintena~ce Consequences 

### None D. DESCRIPTION Toaccomplish 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 JOintsof the flap transmission.

SERVICE BULLETIN No.: A310-27-2099 REVISION No.: 01 - Mar

### 21108 Printed in Fran"" ©AIRBUS 200B Allrightsre,erven Page 4

# ~A310 SERVICE BULLETIN

(a) Replace the aRplicable components. 1 Remove the applicable components asfollows.

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 

### inworkshOp. 

### Removl the plunging 

### joints forworkshop 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 !;heserviceable plunging joints. E. COMPLIANCE (1) Classification Mandatory (2) AccomplishmentTimescale 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 bythe issue of a Consigne de Navigabilite (CN) (Airworthiness Directive (AD». Itis anticipated that the CN will confirm the thresholds and/or interv·als given above but references should be made to the CN for confirmation ofthe mandated accomplishment timescale. 

### F. APPROVAL Approved under EASA Design Organisation Approval No. EASA.21J.031. Ifan aircrafllisted inthe effeetivily has a modification or repair embodied that is not ofAIRBUS 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 ofthe Service Bulletin. G. MANPOWER The manpower estimates given inthis 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~din Fr~nce©AIRBUS2008All rlghlsresorved

# 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. NoAIRBUSfGOODRlyH kitwill be provided. Parls required toaccomplish 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 - Mar21/08 SERViCE BULLETIN No, A310-27-2099 Page. 7
Printo~ in Fiance © AIRBUS 2008 All right. reserved

# ~A310 SERVICE BULLETIN

DESCRIPTION 

### REFERENCE TOCMl QTY PER Ale INST/DISP 

### MATNo. Cleaning agent 

### Mal. No. 11-026 As required (2) Components 

## OT~ ITEM NEW PARTNo. 

### 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 Toaccomplish this Service Bulletin it is necessary to use lhe lools tisled in AMM 27-50-00. G. SPECIALTOOLS 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 ALLTHE WARNINGS AND ALL THE CAUTIONS

INCLUDED IN THE REFERENCED PROCEDURES. WARNING: PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION

BEFORE YOU START ATASK ON OR NEAR:

- THE FLIGHT bONTROLS



### -THEFLiGHTICONTROLSURFACES

-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 

## IfI 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

# rM 27~50·00, 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;~y COCKPIT 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 

### FLTCTlISFCC/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) Puttheaccess plalform(s) in position. (h) Open theaccess doors (Refer toAMM 27-54-19, Page block401). (2) Standard Practices 

### (,) (b) 

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

### Mrteria, Lisl (CML) ), For location ofthe access panels (Refer toAMM 06-41-57, Page block 001), Clean the 

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

### B. INSPECTION (1) Visually inspecttheflaptransmission shafts. Refer 10Figure 1 Refer 10Figure 2 (,)



### (bl



### (e)

DATE. Feb 17/06 Visually inspect the wiper rings inthe splined couplings of the flap transmission shafts. Make sure that the wiper rings inthe crown spline joints ofthe flap drive shafts are not damaged, protruding or missing, refer 10Figure 1, Sheet 2, Details 2 BM akndC.

# I'h h . .. I· .. II I II d· a esure

## I at t ewiper rings Inthe crown sp IneJOintsare correc y inSa 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 Dand 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) Ifdamage. missing or incorrect installation isfound 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 acomponent from the aircraft ifnoserviceable one is inslock.

- 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, 54172, 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 inworkshop 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, 54182, 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 toAMM 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©AIRBUS2008All 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 ofthe 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 oftools and other items of equipment. Close the access dOOr .(Referto 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 CliJsand 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 : Concernsl aircraft 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 301l. Remove the access platform(s). Remove the safety ba~riers. 

### F. DOCUMENTATION Write inthe applicable aircraft records that you have done alilhe work given inthis 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 ASERVICEABLE 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) IfYES, aircraft concerned (as per S8 effectivity bydefault) 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 .. .. Ifoperallonal documentation is affected (see ParaQraph 1.KofthiS S8): IfInformation ISneeded 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 ifthis 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 Ifthis 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 fordetailed 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



# , Orvia your Resident Customer Support Office. Alternatively, 58 lists via letters or faxare 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@AIRBUS2008Allrightsreserved

# 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' 1 

### 432 432 -Quality rating ofthe Illustrations Use this form 10tell uswhat isyour perception ofthe quality ofthis Service Bulletin,The reported dala thal ~ou provide uswill be used to analyse 

### areaslof difficulties and 10take 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 ascale 0jl to4, with 4 being the highest score) -Quality rating ofthis S8 -Quality rating ofthe Accomplish ent Instructions
-Isthis S8 easy Lounderstand? Y

### IN Ifyou have had difficulties inthe acco plishment ofthis 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 XTooling Instructions X Preparation X Mod/Inspection XTest 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 Orvia 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~

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