## ^A300-600

AIRBUS INDUSTRIE PRODUCT SUPPORT DIRECTORATE 1 ROND POINT MAURIC E BELLONT E 3170 7 BLAGNAC CEDEXFRANC E TeL . : (33 ) 61-93-33-3 3 Telex: AIRBU530526 F SERVICE BULLETINCHANGE NOTICE S.B . No . A300-57-601 1 REV. 2 DATED; Dec 17/8 6 MOD. N0.6661H103 3 TITLE : WINGS - AUXILIARYSTRUCTURE - T O INTRODUCE IMPROVED AFT HINGE BRACKETS

TO OUTERSHROUD BOX MODEL: AL L models Listed o n the S.B . DESCRIPTION! Thi s notice is issue d t o informthe affected operators tha t subject Servic e Bulleti nis changed a s stated below. Servic e Bulleti n Page 1 paragraph1.A.(2 ) read : Customer and Qtyo f Kit s

Fleet No . MSNA300-57-601 1 -A0 1 KE 501-50 3 361 , 365 , 35 8 3 KU101-10 3 327 , 332 , 34 4 3 LH 601-60 7 380 , 391 , 401 , 405 , 408 , 411 , 41 4 7 R F 001,05 1 354 , 37 4 2 S V 001-01 1 284 , 294 , 301 , 307 , 312 , 317 , 32 1

336 , 341 , 348 , 35 1 11 TG051-05 6 368 , 371 , 377 , 384 , 395 , 39 8 6 XQ-00 1 25 2 1 AA-05 0 42 3 1 instead of : Customer and Qtyo f Kit s

Fleet No . MSNA300-57-601 1 -A0 1 KE501-50 3 361 , 365 , 35 8 3 KU101-10 3 327 , 332 , 34 4 3 LH601-60 7 380 , 391 , 401 , 405 , 408 , 411 , 41 4 7 RF001 , 05 1 354 , 37 4 2 SV001-01 1 284 , 294 , 301 , 307 , 312 , 317 , 321 ,

336 , 341 , 348 , 35 1 11 TG051-05 6 368 , 371 , 377 , 384 , 395 , 39 8 6 XX252 , 42 3 This change wil l be incorporated inthe next revision o f thi s Servic e Bulletin ; however n o revision is planned at the present time. FILINGINSTRUCTIONS Fil e thi s Chang e Notic e i n fron t o fthi s Servic e Bulletin. SERVIC E BULLETIN No: A300-57-6011 7 DATE : Mar20/90 CHANGE NOTICE No.:2 A Printe d i n France

## @A300-600

AIRBUS INDUSTRIE PRODUCT SUPPORT DIRECTORATE 1 ROND POINT MAURIC E BELLONTE 3170 7 BLAGNAC CEDEXFRANC E SERVICE BULLETIN TeL (33)61-93-33-3 3 REVISIONTRANSMITTAL SHEET TelexAIRBU53052 6 F

MODIFICATION No: 6661H1033 AT ASYSTEM : 57
TITLE : WINGS - AUXILIAR YSTRUCTURE - TO INTRODUCE IMPROVED AFT HINGE

BRACKETS TO OUTERSHROUD BOX . Fin dherewit hRevisio nNo. 2 o f SB.A300-57-6011 . N o additiona l work is required bythi s revision. REASON To informOperators o f revised clearances when installin g newhing e brackets. SUMMAR Y Pag e 1 - Inclusion o f Change Notices 1Aand IB . Revisio nNo. 2 added, SERVICE BULLETIN Page 1 - Inclusion o f Change Notice 1B , Revisio nNo. 2 added. Pag e 2 - Inclusion o f Change Notice 1A . DESCRIPTIONsub-par a (3 5

revised. Revisio nNo. 2 added. Pag e 5 - Paragraph2.A.(1)(c ) revised. Revision No. 2 added. Page 7- 8 - Paragraph2.C.(2 ) revised. Revisio nNo. 2 added. Pag e 11-12 - Drawin g change. Revision No. 2 added. FILINGINSTRUCTIONS 1 . Remove and destroypage 1 o f the Summaryand pages 1,2,5,7- 8 and 11-12 . 2 . Inser t page 1 o f the Summaryand pages 1,2,5,7- 8 and 11-12 a t Revisio n No.2 . REVISIONSEQUENCE ORIGINAL - DEC 17/8 6 REVISIONN0. 1 - MA R19/8 7 REVISIONN0. 2 -

7 DATE : DEC 17/86 SERVIC E BULLETIN No: A300-57-6011 REVISION NO: 2 JU|..
. 10/8 9 PfM. d I n Fr.nc
. pAGE : 1 Of 1

## ^A300-600

AIRBUS INDUSTRIE PRODUCT SUPPORT DIRECTORATE 1 ROND POINT MAURIC E BELLONTE SERVICE BULLETIN 3170 7 BLAGNAC CEDEXFRANC E SUMMAR Y TeL (33)61-93-33-3 3 TelexAIRBU53052 6 F

Thi s summaryis fo r informatio nonlyand is no t D.G.A.C . approved for modificatio no f the aircraf t MODIFICATIONNo : 6661H103 3 ATASYSTEM: 5 7 TITLE : WINGS - AUXILIAR YSTRUCTURE - TO INTRODUCE IMPROVED AF T HINGE

BRACKETS TO OUTERSHROUD BOX REASON Crackin g o f hing e bracket assemblies, whic hare situated o n th e outer shroud boxand formthe rear attachmen t between the inner and outer shroud boxes, has been discovered durin g routine maintenanc e checks o n some in-service A30 0 aircraf t whic hhad accumulate d between 1515 0 and 2038 0 flight s and 1407 0 t o 1874 0 fligh t hours. Failur e o f the bracket would allo wvertica l movement o f the inner shroud boxstructure inthe immediat e area and probable fouling o f the inboard fla p top skin. Additionally , th e loads carried throughthi s bracket wil l be transferred t o the remainin g supports whic hmayeventuall ycrack; extensive structural damag e could then result. Inspection Service Bulleti n(ISB ) A300-57-601 0 detail s methods o f detecting cracked brackets. Embodiment o f thi s modificatio nrenders further complianc e wit hIS B A300-57-601 0 unnecessary. This Service Bulleti nintroduces newSteel Brackets t o replace the existin g aluminiu malloybrackets inorder t o improve the fatigue life. This Service Bulleti nis subject t o airworthines s authoritie s monitoring. ACTION At eachwing the No. 1 inner airbrak e is removed. Th e inner shroud box attachment bolts are removed and the shroud boxi s raised t o allowremoval o f th e existin g aluminiu malloybracket assembly. Anew , steel bracket assemblyis installed. The inner airbrak e is reinstalled and functio n tested. EFFECTIVITY Thi s modificatio n is applicabl e byServic e Bulletin on th e followin g A300-600 aircraft: - 252,284,294,301,307,312,317,321,327,332,336,341,344, 348,351,354,358,361,365,368,371,374,377,380,384,391,395,398,401,405,408,411 and 423. Embodied prio rt o deliver yon aircraf t MSN 388,417,420,459 and subsequent. COMPLIANCE Recommended

7 DATE : DEC 17/86 SERVIC E BULLETIN REF:A300-57-6011 Printe dI nFr«nc « REVISIO N NO: 2 -:H) l 10/R 9 PAGE : 1 of2AIRBUS ( % MDUSTR

C
A300-60 0 SERVIC E BULLETIN

SUMMAR Y MANPOWE R Ki t NO.A300-57-60TI-A01 Manhours : 26.75 Elapse d tim e (hours , 2 fitters ) 13.75 MATERIA LINFORMATION Kit No.A300-57-6011-A01 2 Hinge Bracke t Assemblies , 1 8 Cotte rpins, 20 Nuts
.



# nA

OUTER SHROUD BOX

DATE: DE C 17/86 SERVIC E BULLETI N REF:A300-57-6011 REVISION NO : ?„„,. , i
. F,,nc. PAGE: 2 o f2

## ^A300~600
AIRBUS INDUSTRIE PRODUCTSUPPORTDIRECTORAT E 1 ROND POIN TMAURICE BELLONTE 3170 7 BLAGNAC CEDE XFRANC E A300-600 SERVIC E BULLETIN Te L(33)61-93-33-33 Tele xAIRBU 530526 F MODIFICATION No: 6661H1033 AT ASYSTEM : 57 TITLE : WINGS - AUXILIAR YSTRUCTUR E - TO INTRODUCE IMPROVED AF THINGE

BRACKET S TO OUTER SHROUD BOX 1.PLANNING INFORMATION A.EFFECTIVIT Y (1) Aircraf t Models : B4-601 , B4-602, B4-602R, B4-602 B4-621R, C4-620. (2 ) Aircraf t Custome rand MSN Qt yo fKit s Fleet No
. A300-57-6011 -A01 KE501-503 361 , 365, 358 3 KU101-10 3 327 , 332, 344 3 LH601-607 380 , 391 , 401 , 405, 408, 411 , 414 7 RF001, 051 354, 37 4 2 SV001-011 284 , 294, 301 , 307 , 312 , 317 , 321 ,

336 , 341 , 348, 351 1 1 TG051-056 368 , 371 , 377 , 384 , 395 , 398 6 X X252, 423 Thi s modificatio n is embodied prio rto deliver yon aircraf t MSN 388,417,420,459 and subsequent. The above effectivit yand ki t allocatio n is base d on aircraf t modificatio n statu s and deliver y and subsequent Airbu s Servic e Bulleti n accomplishmen t reporte d t o Airbu s Industrie. (3) Spares None. B.REASO N Crackin g o fhinge bracke t assemblies , whic h ar e Situate d on th e oute r shroud bo xand for m th e rea rattachmen t betwee n th e innerand oute r shroud boxes , ha s been discovere d during routine maintenanc e check s on some in-servic e A300 aircraf t whic h had accumulate d betwee n 15150 and 20380 flight s and 14070 t o 18740 fligh t hours. Failur e o fth e bracke t woul d allo wvertica l movement o fth e innershroud boxstructur e i n th e immediat e are a and probable fouling ofth e inboard fla p top skin
. Additionally , th e load s carrie d throug h thi s bracke t wil l be transferre d t o th e remainin g support s whic h mayeventuall ycrack ; extensiv e structura l damage coul d the n result
.

7 DATE : DEC 17/86 SERVIC E BULLETIN No: A300-57-6011 REVISIO N No : 2 :il.l l 10/6 " pf ""• d l n Ff • nc • PAGE : 1 of1 3

# '^y/^^fvu-auu

Inspection Service Bulleti n(ISB ) A300-57-601 0 detail s methods o f detecting cracked brackets. Embodiment o f thi s modificatio nrenders further complianc e wit hIS B A300-57-601 0 unnecessary. This Service Bulleti nintroduces newSteel Brackets t o replace the existin g aluminiu mbrackets inorder t o improve the fatigue Life. This Servic e Bulleti nis subject t o airworthiness authoritie s monitoring. C.DESCRIPTION 

### Accomplishmen t o f thi s Service Bulleti nconsists o f : - AIRCRAF T Ki t NO.A300-57-6011-A01 . Al l aircraf t Liste dinPara.1.A.(2) . (1 ) Removin g inner airbrak e No.1 , LH and RH. (2 ) Removin g access panels. (3 ) Checkin g fo r equal clearance between the bearing and bracket faces o f the forward attachment bracket. (4 ) Removing 4 2 bolts attachin g landing gear baytop panel t o inner shroud box . (5 ) Removing inner shroud boxattachin g bolts. (6 ) Raisin g inner shroud boxsufficient t o gain access t o hing e bracket. (7 ) Removing existing af t hing e bracket. (8 ) InstaLLin g newsteeL Hinge Brackets at existin g positions. (9 ) Re-installin g inner shroud boxes. (10 ) Re-installin g and function testing inner airbrakes. (11 ) Closing up al l access panels. D.APPROVAL Thi s Servic e Bulleti nis approved byDirectio nGenerale de L'Aviatio n Civil e - FRANC E (D.G.A.C.) .

7 DATE : DEC 17/86 SERVIC E BULLETIN No: A300-57-6011 Printe d I n Ffnc* ..,.,.. - - , REVISIO N No: 23UL
. 10/8 9 PAGE: 2AIRBU S ( % INDUSTR

C

A300-60 0 SERVIC E BULLETIN E. MANPOWER Manhours pe r aircraf t Gain access Remova l o f Bracket s InstaLLatio no f newBracket s Close up and tes t TOTAL MANHOUR S ELAPSED TIME (HOURS ) ( 2 FITTERS) Ki t NO.A300-57-6011- A01 9.25 1.0 0 6.50 10.00 2677 ^ 13.75 NOTE : Thi s Servic e BuLLeti nassumes tha t the aircraf t has been place d in a maintenanc e status. The manhours/eLapse d tim e d o not includ e preparatio nfor the modification , non-productive elapsed tim e o r administrativ e functions. F . MATERIA L - COST AN D AVAILABILIT Y Refe r t o Paragrap h3 - MATERIA L INFORMATION. G . TOOLING- COST AN D AVAILABILIT Y None. H . WEIGHT AN D BALANC E ME W+ 0.7 2 kg ( + 1.5 8 Lb) Momen t + 23. 5 kg.m( + 169.9 2 Lbft ) I . REFERENCE S Aircraf t Maintenanc e Manua l (AMM ) 06-41-57 , 27-61-54 , 20-31-0 0 Inspection Servic e Bulleti n(ISB ) A300-57-601 0 J. PUBLICATIONS AFFECTE D Illustrate d Parts Catalo g (IPC ) 57-51-1 1 Structura l Repai r Manua l (SRM ) 57-51-1 1

DATE : SERVIC E BULLETIN No: A300-57-6011 REVISIO N NO: 1 MAR 19/8 7 Prinf O I n Fr.ne
. DACF
. 7- A

## ^A300-600

2.ACCOMPLISHMENT INSTRUCTIONS AIRCRAF T A.GENERAL WARNING: BEFOR E PROCEEDINGWITH MAINTENANCE WOR K ONORNEA R

MECHANICA L FLIGHT CONTROLS ORPRIMAR YFLIGHT CONTROL SURFACES, LANDINGGEARS, ASSOCIATED DOORS ORAN YMOVING COMPONENT MAK E CERTAINTHAT GROUND SAFETIES AND/O RWARNIN G NOTICES AR E I NCORREC T POSITIONT O PREVENT INADVERTEN T OPERATIONOF CONTROLS . The followin g instruction s are applicabl e t o bothL H and RH wings. (1 ) Jobse t up (a ) Refer t o Aircraf t Maintenanc e Manual (AMM27-61-5 4 page bloc k 401 . Remove and retaininner airbrak e No.1 . (b ) Refer t o AM M06-41-57 .

- Lower flap deflector panels 572AB , 572CB , 572GB , 672AB , 672CB and 672GB .

- Remove and retainaccess panel A5724098 0 fromthe inboard aft edge o f eachouter shroud boxa s showninfigure 1 , vie wA .

- Remove and retainwin g t o fuselage fairin g panels 577CT , 577DT , 677C

T and 677DT . (c ) Refer t o Figure 1 Vie wAand Figure 2 Detai l E .

- Gainaccess t o the forward attachment point whic hconnects the inner shroud boxt o the outer shroud box.

- Using a suitable ligh t source and mirro r mak e sure that an equal gap exists between the bearing and the bracket faces a s shown inFigur e 2 . Detail E .

- I f a gap exists METHOD ONE (op.B.(3 ) refers ) ca n be use d t o instal l the ne' waft hing e bracket.

- I f there is n o gap at al l METHOD TWO (op.B.(4 ) refers ) must be use d t o instal l the ne waft hing e bracket. (d ) Refer t o Figure 1 , Vie wA .

- Place suitabl e supports beneaththe inner shroud boxt o prevent excessive movement whenthe shroud boxi s released fromthe wing.

- Remove and retai nthe 4 2 bolts attachin g the landin g gear baytop panel t o the forward edge o f th e inner shroud box.

- Remov e and discar d the cotter pin s fromeachof th e bolts at th e mai nattachmen t points denoted 'C* .

7 DATE : DEC 17/86 SERVIC E BULLETIN No: A300-57-6011 Prinli dI nFf»nc « REVISIO N No: 2 JU L10/8 9 PAGE : 5AIR BUS INDUSTRI E A300-600 SERVIC E BULLETIN

- Remov e and retai n nuts, washer s and specia l bolt s (Qty.5 ) fro m th e attachmen t points
.

- Remov e and retai n the slidin g bush fro m th e af t innert o oute r shroud boxattachment
. (e ) Carefull yrais e th e af t edge o fth e innershrou d boxjus t sufficien t to gain acces s to the af t hinge bracke t sit'-ate d o th e inboard edge o fthe outershroud box, as show n i n Figure 1 , Vie wB
. NOTE : Movementofth e inne rshroud boxis severel yrestricte d by electrica l looms and hydrauli cpipes
. When raisin g th e shrou d boxensure tha t the looms orpipes ar e no t strained
. Remova l o f'P'-clip s wil l allo wincrease d movement o fth e shrou d box
. B
. MODIFICATIO N Ki t NO.A300-57-6011-A01 (1) Mar k

around the outlin e o fth e existin g af t hinge bracke t on th e oute r shroud boxusing a sharpene d pencil
. (2 ) Remov e and discar d th e existin g hinge bracke t fro m th e oute rshrou d box takin g note ofth e directio n o finstallatio n and positio n o fal l th e attachin g bolts
. Retai n bolt s and washers ; discar d nuts
. (3 ) METHOD ONE. Refe rt o Figur e 1 , Vie wB. (a ) Positio n th e ne wHinge Bracke t Assembl yA5724664100095, Ite m 1 , LH , (A5724864100195, Item 2 , RH) t o th e penci l outlin e on th e shrou d bo x an d clamp
. (b ) Ensure sufficien t hole landings and tha t dimensions show n ar e correct
. Mar k the positio n o fhole s t o be drille d in-th e hinge bracke t fro m th e existin g vacan t bolt hole s i n the shrou d box
. (c ) Remove the hinge bracke t assembl yfro m th e shrou d bo xand drill/rea m sixtee n holes 0.190/0.192 in
. (4.83/4.8 8 mm) dia. a t position s previousl ymarked
. (d) Spotfac e te n hole s denoted 'D ' 0.562 5 in
. (14. 3 mm) dia. (spotfac e corne rradius t o be 0.0625 in
. (1.53 mm))
. Spotfac e t o minimum depth t o provide correc t nu t seating
. Deburral l holes
. Ensure corne r radius of0.015/0.025 in
. (0.38/0.6 3 mm) is achieve d on thre e hole s a s show n t o allo wbolt heads t o sea t correctly
. Thoroughl yclea n spotface s wit h Genklene (Mat.No.11-004). Restor e protectiv e treatmen t using Prime r(Mat.No.16-006) and Polyurethan e finis h (Mat.No.16-018) (e ) Instal l newAncho rNuts NAS1067C 3 t o bracke t assembl ya s show n wit h Sealan t PR1431-G (Mat.No.09-005 ) using ne wRivet s L21217024008DCA
. (f ) Install newBracke t Assembl yt o shrou d boxusing bolt s retaine d i n op.B.d) wit h ne wNuts H19200C-3 Item 6 using Secan t PR1431-G (Mat
. No. 09-005) o n interfayin g sur-foces , nuts ci d bolts
. DATE : DE C 17/86 SERVIC E BULLETIN No: A300-57-6011 REVISIO N NO: Prinf d In Franc *

## ^A300-600
(4 ) METHOD TWO . Refer t o Figure 1 Vie wA , and Figur e 2 . (a ) Refer t o Figure 2 Detai l 'F' . Bolt the newHinge Bracket AssemblyA5724864100095 , Item1 , LH (A5724864100195 , Item2 , RH) t o the inner shroud boxoutboard aft attachmen t bracket using the appropriate bolts retained inop.2.A.(1)(d ) together wit hslidin g bush. (b ) Temporarilyreinstal l the inner shroud boxt o the remainin g mai nattachment points and suitabl ysupport. (c ) Refer t o Detai l 'E' . Reinstal l two bolt s denoted "G " s o that the threads are just engaged, t o th e landin g gear baytop panel. (d ) Refer t o Figur e 2 Detai l 'F' . Clam p newHing e Bracket Assembly, Item1 L H (item2 RH) t o th e outer shroud box ensuring that a minimu mgap o f 0.00 8 in. (0.20 mm) exist s between th e flange o f the fixe dbearing andthe washer. (e ) Mark th e position o f holes to be drille dinthe newHinge Bracket fromth e existin g vacant bolt holes. Ensure tha t sufficient hole landing exists. (f ) Support inner shroud box , remove andretainal l bolts installe da t op.2.B.(4)(b ) and(c) . (g ) Refer t o Figure 1 , ViewB . Remove the newHinge Bracket Assembly, Ite m1 LH (Ite m2 RH) fromthe inner shroud box ; retainth e bolts and slidin g bushinstalle dat op.2.B.(4)(a) , (h ) Performop.2.B.(3)(c ) t o 2.B.(3)(f) . C.CLOS E U P AN D TES T (1 ) Carefullylower the inner shroud boxt o its origina l position linin g up wit hattachment points. (2 ) Reinstal l slidin g busht o the aft inner t o outer shroud box attachment. Install special bolts wit hnuts and washers retained inop.A.(1)(d ) and newCotter Pins MS24665-304 , Item3 (Qty.3 ) and MS24665-155 , Item4 (Qty.2) , t o attachment points. (3 ) Reinstal l attachin g bolts retained inop.2.A.(1)(d ) into the landing gear bayto p panel using Sealant PR1431- G(Mat . No.09-005) . (4 ) Refe r t o AM M27-61-5 4 page bloc k 401 . Re-instal l inner airbrak e No. 1 retained at op.A.(1)(a ) using newCotter Pins MS24665-304 , Item3 , (Qty.2 ) and MS24665-374 , Item5 , (Qty.2) . Performrelevant tests a s detailed . (5 ) Ensure work areas are clean andclear o f tools and miscellaneou s item s o f equipment. (6 ) Re-instal l al l access panels removed or opened inop.A.(1)(b) .

7 DATE : DEC 17/86 SERVIC E BULLETIN No: A300-57-6011 Printed I n Fr.nc* REVISIO N No: 2 JU L10 8 9 PA6E : 7 - 8AIRBU S ^NDUSTR C i A300-60 D SERVIC E BULLETIN I ! 

# • A

_ _i OUT'B D ^

/''I$~' -

^ : f:: ^^^^?^^^^^^^^? =::=s: ^ ^ ' T SE E FIGURE 2 J ^ :=:=:::=: -^^:^'*^L^^——^^^_ :::::: ^^^^^^^^^^.^ ^ No.l INBOAR D SPOILER DETAI LF .^,^--——-= : ====:^^^^^^^^^^^ ' I ATTACHMEN TPOINTS \ ^CESS PANEL >^'^\

/ ~~~~ ———— = —^ ^ \ \ | /^^-^^ \ A572-40980
\ \ /

(REF) 1

- 381 ^ 4—————^

Q

40 IN
. ! ^———J ^^^^
. ^^^^^^^f^\ / \ \ / I <35.05mm ) ,,•_, , '(REF ) ia h ________L____________^rn^^rh__________^^i C
. \ / VJ 

# ^ 1 ...__ - ^^ , % B ^> N , ' / r-iD-Dra-E/^D.-Kt—f ^ I ' ^ .^ ' ' 

# • , . 0.5 0 IN
. /// ^-J.-.'^-^yZT^Y 7 """"""" / 'i it;

-<'-•' / '^^(IZ./Omm ) / 7 , u , / \0.6 D IN
. / 1 / / .A - '--J^ ^

(15.24mm)'"I" I l / l^^

"' , L- P ' < ^ I INNER SHROUD /.^ i

tI--------- X 7 ! I BOX SEE dGURE 2 /^-^^ ^ ^ i

^ \ (^ ^\-^ , // ; i DETAI LE / ^^S^^^LLj"'"'/ " - - -- - - V • ' REMOVE AND RETAI N BOLTS \ / D/ Dr^~^7^~=E^5~-=^./ , ~~~------_ / i I (QT Y42) SECURING LANDING \ l ENSURE CORNE R RADIU S ON / Dr^gT^^r^^, , \ : \\ GEAR BA YTOP PANEL TO V - ~ , HOLES (ST Y3) o-f0.015/O.U25IN
. / ul

^^^""--^ ^ ! A ' INNE R SHROUD BOX
. /p ! \ / I TO ALLO WBOLTHEAD S TO / i (•J^

___________

\__________________________________fe;;.'Ja g-^ W \ SEA TCORRECTL YWHE N INSTALLED. 1 (LH ) | C -^,. <,.o.,.oXo.,,ooooB.o..,o<iooooooB.o. o .A,", 7 | ";' / 2(RH )
___ i ^^
. \ | /

/ | Q | "^ ^ LANDING GEA R BAY^~---i^ / | P | | ^ \ TOP PANEL| | / ! ^"^-———————. I - |-————... ^__,___——~^_/OUTER SHROUD VIE WSHOWIN G POSITION O F AF T| |A| Box HING E BRACKE TO N OUTER SHROUD | ' • Bo xVIE WLOOKING DOWN ON INNER SHROUD BOXLH RH SIMILAR BU TOPPOSITE i 

# • I
InstaLLatio n o f ne wHing e Bracke t Assembl yi Figur e 1 ; DATE : D&C 17/8 6 SERVIC E BULLETIN No: A300-57-60n I REVISIO N NO: Printed m Franc e PAGE : 9-1 0 [A I R B U S (^INDUSTRI E
A300-60 0 SERVIC E BULLETIN

SLIDINGMIN. 0.00 8 IN . BUSH (REP ) (0.20MM ) FIXE D ,,_., . _- , BEARIN G ^^-ffl

LANDIN GGEA RBAY TO P PANE L

View s showin g clearance s whe n instaLLin g th e newHinge Bracke t

Figur e 2 DATE : DE C 17/8 6 SERVIC E BULLETI N No: A300-57-6011 REVISION NO: 2 JU L 10/8 9 printed i n France PAGE : 11-1 2AIRBUS^INOUSTR C A300-600 SERVIC E BULLETIN 3. MATERIA LINFORMATION A
. DAT ABASI S Quantit yspecifie d i n B.(1) ki t A01 i s peraircraf t Liste d i n para.1-A.(2)
. B
. MATERIAL S (1 ) Part s require d
ITE MNEWPART QT YPERKI T DESCRIPTIONOLD PART REMARK S No . No . A300-57-6011-A0 1 No . 1 A572486410009 5 1 Hing e Bracket A5724191700 0 A,B, C Assembl y(LH ) 2 A572486410019 5 1 Hing e Bracket A5724191700 1 A,B, C Assembly(RH ) 3 MS24665-30 4 1 0 Cotter pi n- A, C 4 MS24665-15 5 4 Cotter pi n- A, C 5 MS24665-37 4 4 Cotter pi n- A, C 6 H19200C- 3 2 0 Nut - A, C Remark s A- Ol dpart discarded . B - Hing e Bracke t Assemblie s are supplie d wit hanchor nuts and rivet s loose inbag. C - Newparts required t o accomplis hthi s Servic e Bulleti nare t o b e procured bySpares Purchas e Order from: AIRBU S INDUSTRIE SPARES SUPPORT CENTER WEGBEIMJAEGE R15 0 D200 0 HAMBUR G6 3 GERMAN Y (2 ) Specia l tools required None. (3 ) Material s require d(Operator supplied )
DESCRIPTIONREFERENC E QT Y AM M20-31-0 0 Genklene Mat.No.11-00 4 As required Epoxid e Prime r Mat.No.16-00 6 As require d Polyurethane Finis hMat.No.16-01 8 As require d Sealant PR1431- GMat.No.09-00 5 As require d C . PART S TO BE RE-IDENTIFIED BYOPERATO R None. DATE : SERVIC E BULLETIN No: A300-57-6011 REVISIO N NO: 1 MA R 19/8 7 PAGE : 1 3 Printe d In Frjnc *