^A310

SERVICE BULLETIN

REVISION TRANSMITTA L SHEET

AIRBUS INDUSTRIE

CUSTOMER SERVICE S DIRECTORAT E

1 Rond Point Mauric e BELLONTE

31707 BLAGNAC CEDEX FRANC E

T eL : (33 ) 5 61 93 33 33

TeLex : AIRBU 530526F

F ax : (33 ) 5 61 93 41 06 '

A TA SYSTEM : 28

TITLE : FUEL - QUANTITY INDICATING - INSPECT FQI PROBES FOR STRUCTURAL CLEARANCE S

MODIFICATIO N No. : None

Thi s page transmit s Revisio n No . 01 of the Servic e Bulleti n No . A310-28-214S

ADDITIONA L MORK

No additiona l work is require d by thi s revisio n for aircraf t modifie d by any

previous issue .

REASO N

Thi s revisio n is issued to infor m operators tha t thi s Servic e Bulleti n is

rendered mandatory by Airworthines s Directiv e (Consign e de navigabilite ) No .

2002-170(8) and chang e the illustration s Figur e 1 and 4, P/N of the item 12/

and to correct P/N of the rivet s ite m 7 .

CHANGE S

SUMMAR Y

- Text updated followin g Service Bulleti n body changes . EVALUATIO N TABLE

updated/ complianc e becomes Mandatory/ Airworthines s Directiv e (Consign e de

NavigabiLite ) No . 2002-170(B)

SERVICE BULLETIN

- COMPLIANC E

- Classificatio n

. RECOMMENDE D becomes MANDATORY .

- Accomplishmen t Timescal e

. Airworthines s Directiv e No . 2002-170(B) (AD ) added .

- REFERENCE S

. Airworthines s Directiv e No . 2002-170(8) (AD ) added .

- MATERIA L - PRICE AND AVAILABILITY

- Pric e and Availabilit y

. Standard sentence added

- LIST OF COMPONENTS

. P/N of the support (LH ) ite m 12 changed .

. P/N of the fastener ite m 7 changed .

- REPAIR .

LO DATE : Aug 21/01 SERVICE BULLETIN No . : A310-28-2145

REVISION NO . : 01 - MAB04/03 PAGE : 1 of 2

Printed in France
^A310

SERVICE BULLETIN

REVISION TRANSMITTAL SHEET

. Para (1).tb) . P/N changed , note added .

. Para (2) . Text modified .

. Para <2).(a) . Text and P/N' s added .

. Para (2).(b) . 2 . P/N changed/ note added .

Para (3) . (b) . P/N changed , note added .

- ILLUSTRATIONS

. Figur e 1/ Sheet 1 and Figur e 4/ Sheet 1 modified .

FILING INSTRUCTIONS

Thi s Servic e Bulleti n has been generated eLectronicaLly , and is reissued as a

complet e document . Replac e the complet e document .

Put thi s Revisio n Transmitta l Sh'eet in front of the Servic e Bulletin .

REVISION SEQUENCE

ORIGINA L : Aug 21/01

REVISION No . : 01-

DATE : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 - MAB04/03 p^E : 3

Printed in Franc e ^k
A310

SERVIC E BULLETIN

SUMMAR Y

AIRBUS INDUSTRIE

CUSTOMER SERVICES DIRECTORAT E

1 Rond Point Mauric e BELLONTE

31707 BLAGNA C CEDEX FRANC E

T el : (33 ) 5 6 1 93 33 33

Telex : AIRBU 530526F

F ax : (33 ) 5 61 93 41 06

Thi s summar y is for informatio n only and is

not approved for modificatio n of the aircraf t

A T A SYSTE M : 28

TITLE : FUE L - QUANTITY INDICATING - INSPECT FQI PROBES FOR STRUCTURAL CLEARANCE S

MODIFICATIO N No. : None

REASON/DESCRIPTION/OPERATIONA L CONSEQUENCES

To ensure adequate protectio n in the event of Lightnin g strikes . Airbu s Industrie

has carrie d out investigation s of the clearances between the FQI probes and any

adjacen t structur e or metalli c components in the LK and RH wing fuel tanks whic h

could create a conductiv e pat h to the mai n structure .

T he investigation s have been carrie d on t e n A 3 0 0 aircraft . Seven aircraf t had FQI

probes tha t di d not have the minimu m clearance . Three aircraf t had no findings .

As a result of these investigation s thi s Servic e Bulleti n has also been issued

for A310 aircraf t for a one off inspection of the tri m fuel tanks FQI probes to

make sure tha t there is a minimu m clearanc e of 3. 0 mm (0.11 8 in ) between the ends

of the FQI probes and any adjacen t structure . Any FQI probe tha t does not have

thi s minimu m clearanc e is to be adjusted .

Thi s Servic e Bulleti n is rendered mandator y by Airworthines s Directiv e (Consign e

de NavigabiLite ) No . 2002-170CB).

EVALUATION TABLE

COMPLIANC E

POTENTIAL AD

RELIABILIT Y AFFECTE D

COST SAVING

STRUCTURA L LIFE EXTN

KIT PRICE (USD )

Mandatory

2002-170(8)

No

No

No

No Ki t

CANCEL S INSPECTION SB

A /C OPERATION AFFECTE D

PAX COMFOR T AFFECTE D

ETOPS AFFECTE D

VENDOR SB INVOLVED

No

No

No

No

NO

EFFECTIVIT Y

This Servic e Bulleti n is applicabl e to these operators :

62Z A1 L ACI AF L AIB AIC AJ M AMV ANG AW W BBC CFC CNW CSA CYP DGA DLH EUH F21 FDX

G8E GAF HLF 12L.IC B IRA IRM IWD IYE KAC KZK KZW LLB MGL MPD MWA P2C PIA PIC QAF

QSC R1T RJ A ROT RZO SIA TAP THY TSC UAE UZB

CONCURREN T REQUIREMENTS

None

LO DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-38-214 5

REVISION No. : MAB 04/03 PAGE : 1 of 2

Printed in Franc e
A310

SERVICE BULLETIN

SUMMAR Y

REFERENCES/REPERCUSSION S

T FU ; None

OEB : None

AOT : None

SIL . : None

LIF E LIMIT : None

LINE MAINTENANC E AFFECTE D : None

OTHERS : None

NATUR E OF THE WORK :

AIRCRAF T : Yes

 !i EQUIPMENT : No \

HARD : No

SOFT : No

OBRM : NO

MANPOWE R |

^

Inspection |

I

TOTAL MANHOUR S 8.00

t

ELAPSED TIME (HOURS ) 4.00

NOTE : The above hours do not includ e any repai r manhours .

MATERIA L INFORMATIO N

AIRCRAF T DATA

None

APPENDICES

None

DAT E : Au g 21/01 SERVIC E BULLETI N No . : A310-28-2145

REVISIO N No . : 01 -MAR04/03 p^g g ; 3

Printed in Franc e
A310

SERVICE BULLETIN

AIRBUS INDUSTRIE

CUSTOMER SERVICES DIRECTORAT E

1 Rond Point Mauric e BELLONTE

31707 BLAGNAC CEDEX FRANC E

Tel : (33) 5 61 93 33 33

TeLex : AIRBU 530526F

F ax : (33 ) 5 61 93 41 06

A TA SYSTEM : 28

TITLE : FUE L - QUANTITY INDICATIN G - INSPECT FQI PROBES FOR STRUCTURA L CLEARANCE S

MODIFICATIO N No. : None

Thi s document contains AIRBUS INDUSTRIE PROPRIETAR Y INFORMATIO N and shal l at al l

time s remai n the property of AIRBUS INDUSTRIE ; no intellectua l property righ t or

Licenc e is granted by AIRBUS INDUSTRIE in connectio n wit h any informatio n

contained in it . It is delivere d on the express co'ndition that said document and

t he informatio n containe d in i t shal l be treated as confidential , shal l not be

used for any purpose other than that for whic h it is hereby delivered . It shal l

not be disclosed in whol e or in part to thir d partie s and shal l not be duplicate d

in any manner (excep t for the purposes of performin g the tasks described

hereunder an provide d tha t any recipien t of such document shal l comply wit h the

condition s herein) , withou t AIRBU S INDUSTRIE' S prio r writte n consent .

1 . PLANNING INFORMATIO N

A . EFFECTIVIT Y , .

( 1 ) Models

310-304 310-308 310-322 310-324 310-325

( 2 ) Aircraf t

( a ) Effectivit y by MSN

Thi s Servic e Bulleti n is applicabl e to aircraf t MSN :

0378 0392 0399 0404 0406 0407 0409 0410 0412 0413 0416 0418

0421 0422 0425 0428 0429

0431-0437 0439-0449 0451-0453 0455-0458 0467 0472 0473 0475

0476 0478 0480-0485 0488-0504 0519 0520 0522-0524 0526 0527

0531 0534 0535 0537-0539 0541 0542 0544 0545 0547-0552 0562

0564 0565 056^ 0568 0570 0571 0573 0574 0576

0585-0595 0597-0600 0620 0622 0624 0634 0636 0638 0640 0642

0644 0646-0654 0656 0658 0660 0661 0663 0665 0667 066 9 0671

0672 0674 0676 0678 0680 0682 0684 0686 0687 0689 0691 0693

0695 0697 0698 0700 0702 0704 0706

t b ) Effectivit y by Operator

The Operator/MSN relationshi p is provided for informatio n only

and is correct at the tim e of issue in accordance wit h the

informatio n availabl e to AIRBUS INDUSTRIE . Any future changes

resultin g from transfer of an aircraf t from one operator to

another wil l not be reflected in thi s Lis t unless the Servic e

Bulleti n is revised for another reason .

OPERATOR MSN

62Z 0431

A 1L 0648

LO DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION NO. : 01 " MAB04/03 PAGE : 1

Printed 1 n Franc e
>A310

SERVIC E BULLETI N

OPERATOR MSN

A C ! 0672

J

A F L 0442 0453 0472 0475 0592 0593 0622 0646 0660 0687

0689

AIB 0404 0456 0492 0502 0598 0695

A IC 0392 0406 0407 0413 0428 0429 0447 0481 0501 0519

0538 0544 0548

A J M 0676 0678 0682 0686

A MV 0437

A NG 0378

AUU 0409 0410

BBC 0433 0650 0698 0700

C F C 0425 0441 0444 0446 0482

CSA 0564 0567

D GA 0418 0421 0422

D LH 0488 0524 0527 0547 0595 0599

EUH 0432

F21 0550 0551 0638

F DX 0539 0542

G8E 0435 0440 0448

G AF 0434 0484 0498 0499 0503 0522 0523

H LF 0485

12L 0504 0642

ICB 0552

I RA 0436

IRM 0586

IWD 0594 ,

IYE 0535 0568 0702 0704

K AC 0647 0649 0663

KZK 0399 0412

K2W 0439 0449 0452 0457 0458 0467 0674

LLB 0562

HGL 0526,

MPD 0443 0451 0455 0489 0520 0624 0640

DATE : Aug 21/01 SERVICE BULLETIN No . : A310-28-2145

REVISION No . : 01 -MAB04/03 PAGE ; 2

Printed In France

t
®A310

SERVIC E BULLETIN

OPERATOR MSN

M WA 0652 0671

P2C 0500 0534

PIA 0585 0587 0590 0653 0656 0691

PIC 0549

Q AF 0473

QSC 0620

R 1T 0591

R J A 0416 0445 0490 0491 0531 0573 0661

ROT 0636 0644

RZO 0571 0651

SIA 0493 0570 0589 0634 0654 0665 066 9 0680 0684 0693

0697

TAP 0483 0494 0495 0541 0565

THY 0476 0478 0480 0496 0497 0537

TSC 0545 0588 0597 0600 0658

U AE 0667

UZB 0574 0576 0706

NOTE : Thi s Servic e Bulleti n is not applicabl e to A/C havin g

M OD 12278 accomplishe d in Production .

(c) . Effectivit y by MSN and Kit/Configuratio n

None

( 3 ) Spares

None

B . CONCURREN T REQUIREMENT S

None

C . REASON

( 1 ) Hi story

To ensure adequate protectio n in the event of Lightnin g strikes /

Airbu s Industrie has carrie d out investigation s of the clearance s

between the FQI probes and any adjacen t structur e or metalli c

components in the LH and RH wing fue l tanks whic h could create a

conductiv e path to the mai n structure .

The investigation s have been carrie d on ten A300 aircraft . Seven

aircraf t had FQI probes tha t di d not have the minimu m clearance .

Three aircraf t had no findings .

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAR04/03 PAGE : 3

Pr'inted in F ranee
A310

SERVIC E BULLETIN

( 2 ) Objective/Actio n

This Service Bulleti n has been issued for A310 aircraf t for a one

off inspection of the tri m fuel tanks FQI probes to make sure that :

- There is a minimu m clearanc e of 3. 0 nun (0-11 8 in ) between the ends

of the FQI probes and any adjacen t structure .

• - There is a minimu m clearanc e of 3. 0 mm (0.11 8 in ) between the FQI

probes harness connector blocks and any adjacen t structure .

NOTE : Any adjacen t structure includes :

- Support structur e

-Stringer s

- Tank structur e

-Adjacen t fasteners

-Pipe s

- Bond i ng Leads

- Any other adjacen t metalli c component whic h could create a

conductiv e path to the mai n structure .

Any tri m fuel tank FQI probe that does not have this minimu m

clearanc e is to be adjuste d by eithe r movin g the probe up or down in

i ts support bracket or by the installatio n of modifie d support

brackets . '

( 3 ) Advantages

The accomplishmen t of thi s Servic e Bulleti n makes sure tha t there is

adequate protectio n agains t the effects of lightnin g strikes .

( 4 ) Operational/Maintenanc e Consequences

None

D . DESCRIPTION

To accomplis h thi s Servic e Bulleti n it is necessary to :

( 1 ) Defuel and ventilat e the aircraf t tri m fuel tanks .

( 2) Get access to al l the FQI probes in the tri m fuel tanks .

( 3 ) Do an inspectio n to make sure there is a minimu m 3. 0 mm (0.11 8 in )

clearanc e around the ends of the FQI probes .

( 4 ) If the clearance is between 2. 5 mm (0.09 8 in ) and 3. 0 mm (0.11 8 in) /

loosen the FQI probe atta chment screws and adjus t the probe to get

t he require d minimu m 3. 0 mm (0.11 8 in ) clearance .

( 5 ) If the clearanc e is less than 2. 5 mm (0.09 8 in ) / remove the FQI

probe(s ) and instal l new FQI probe supports to get the required

minimu m 3. 0 mm (0.11 8 in ) clearance .

( 6 ) Instal l the FQI probe(s) .

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAB 04/03 PAGE : 4

Printe d 1n France
'A310

SERVIC E BULLETIN

( 7 ) Close up .

( 8 ) Test (onl y require d if a FQI probe was disconnected) .

E . COMPLIANC E

(^Classificatio n

I MANDATOR Y

( 2 ) Accomplishmen t TimescaL e

Thi s Service Bulleti n is rendered mandatory by Airworthines s

Directiv e (Consign e the NavigabiLite ) No . 2002-170(6) .

Accomplis h thi s Servic e Bulleti n withi n 4000 fligh t hours from the

effectiv e date of the Airworthines s Directiv e No . 2002-170(8).

F . APPROVA L

The technica l c.ontent of thi s Servic e Bulleti n has been approved under

t he authorit y of the DGAC Design Organizatio n Approva l No . F.JA.02 .

If an aircraf t Liste d in the effectivit y has a modificatio n or repai r

embodied tha t is not Airbu s origin / and whic h affects the content of thi s

Servic e Bulletin , the operator is responsible for obtainin g approval by

i ts airworthines s authorit y for any adaptatio n necessary before

incorporatio n of the Servic e Bulletin .

G . HANPOtiER

Thi s Servic e Bulleti n is writte n for an aircraf t in maintenanc e status .

The man-hours/elapsed tim e estimate s do not includ e the tim e to prepare

for the modification / non-productive elapsed tim e or administration .

Gainacces s 2.00

Inspection 5.00

Close-up 1.5 0

TOTAL MANHOUR S 8.00

ELAPSED TIME (HOURS ) 4.00

NOTE : The above hours do not includ e any repai r manhours .

H . WEIGHT AND BALANC E

None

I . ELECTRICA L LOAD DATA

None

J . REFERENCE S

Aircraf t Maintenanc e Manua l (AMM ) : 20-21-00 24-00-00 28-10-00

28-11-28 28-11-33 28-42-00

28-42-51

Structura l Repai r Manual (SRM ) : 51-40-00

| Airworthines s Directiv e (AD ) : 2002-170 (B )

DATE : Aug 21/01 SERVICE BULLETIN No . : A310-28-2145

REVISION No . : 01 -MAR04/Q3 PAGE : 5

Pr1nted i n F ranee
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SERVICE BULLETIN

K . PUBLICATIONS AFFECTE D

Aircraf t Maintenanc e Manua l (AMM ) : 28-42-51

Illustrate d Parts Catalog (IPC ) : 28-42-51

L . INTERCHANGEABILITY/MIXABILIT Y

None

DATE : Aug 21/01 SERVICE BULLETIN No . : A310-28-2145

REVISION No . : 01 - MAW 04/03 PAGE : 6

Printed 1n France
^A3W

SERVICE BULLETIN

2 . MATERIA L INFORMATION

A . MATERIA L - PRICE AND AVAILABILIT Y

( 1 ) Materia l

Customers wit h aircraf t shown in the effectivit y of thi s Service

Bulleti n should send a purchase order to AIRBUS INDUSTRIE . Quote the

number of thi s Servic e Bulletin . The address is :

AIRBUS INDUSTRIE

MATERIE L SUPPORT CENTER

P.O . Box 630262

22312 HAMBURG

GERMAN Y

( 2 ) Pric e and Availabilit y

I

No AIRBU S INDUSTRIE ki t wil l be provided . Parts require d to

accomplis h thi s Servic e Bulleti n are to be purchased by a Spares

Purchase Order .

B . INDUSTRY SUPPORT INFORMATIO N

i

To make the inspectio n easier it is recommended to use a 3. 0 mm .

(0.1 1 8 i n . ) suitabl e gage to measure the minimu m clearanc e between the F Q I

probes and the surroundin g structure/components . Refer to Figur e 2, for

detai Is .

C . LIST OF COMPONENTS

ITEM NEW PART No . QTY UM KEYWOR D ITEM OLD PART No . INT INST DISP

9 R2822D00500000 1 Support(LH )

9 R2822000600000 1 Support(RH )

| 12 R2822030600000 1 Support(LH )

12 R2822000300000 1 Support(RH )

14 R2822000100000 1 Support(LH )

14 R2822000100100 1 Support(RH )

16 R2822018500000 1 Support(LH )

1 6 R2822018500100 1 Support(RH )

18 R2822018600000 1 Support(LH )

18 R2822018600100 1 Support(RH )

| 7 MS20470AD5-10 12 Rivet s

NOTE : Materia l require d for accomplishmen t of thi s Servic e Bulleti n

shal l be obtained by means of a Spares Purchase Order .

D . LIST OF MATERIAL S - OPERATOR SUPPLIED

DESCRIPTION REFERENC E TO CML QTY PER A/C INST/DISP

MAT . No .

CLeaningagen t Mat . No . 11-026 As required

Sealant Mat . No . 09-005 As required

E . PARTS TO BE RE-IDENTIFIED BY THE OPERATOR

None

F . TOOLING - PRICE AND AVAILABILIT Y

None

DATE : Aug 21/01 SERVIC E BULLETIN No . : A310-28-2145

REVISION No . ; 01 -MAR04/Q3 PAGE : 7

Printe d in France
>A310

SERVIC E BULLETIN

G . SPECIAL TOOLS

None

DATE : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAR 04/03 p^GE : 8

Printed in France
^A310

SERVICE BULLETIN

3 . ACCOMPLISHMEN T INSTRUCTIONS

A . GENERAL

WARNIN G : MAKE SURE THAT YOU OBEY ALL THE WARNINGS / CAUTIONS AND NOTES IN

THE REFERENCE D MANUALS .

WARNIN G : LANDING GEA R - MAKE CERTAIN GROUND SAFETIES AN D CHOCKS AR E IN

POSITION.

WARNIN G : DO NOT DO ANY WORK IN THE FUEL TANKS UNTIL THE VAPOR

CONCENTRATIO N IS BELOW 207. OF THE LOWER EXPLOSION LIMIT (LED .

( 1 ) Preparation

( a ) Make sure tha t the aircraf t is eLectricalL y grounded . Refer to

A MM 24-00-00 Page block 301.

( b ) Instal l access platform s to gai n access at the THS area in

zones Z333 (Z343) .

( c ) Make sure the Elevato r and THS are set to a neutra l position .

( d ) Defuel and ventilat e the aircraf t tri m fuel tank . Refer to AMM

28-10-00 Page block 301 .

( e ) Remove the manhol e covers 333BB/ (343BB) / 333CB and

(343CB)/333EB and (343EB) . Refe r to AM M 28-11-28 Page block 401

Refer to Figur e 1

( f ) If i t is necessary to remove the probes . Refer to AM M 28-42-51

Page block 401.

( 2 ) Standard Practices

( a ) Clea n the work area wit h cleanin g agent (Mat . No . 11-026 )

( b ) For informatio n on tighte n torques for standard fasteners .

Refer to AMM 20-21-00

( c ) For informatio n on dril l data . Refer to SRM 51-40-00

( d ) Appl y interfac e sealant (Mat . No . 09-005)to the matin g

surfaces and to the rivet s before installation .

( e ) For materia l informatio n (Mat . No . )give n in thi s Servic e

Bu L Let i n refer to CML .

B . INSPECTION

NOTE : Only the LH side is described the RH is similar .

( 1 ) Check the clearanc e between the lower and upper end of the probe/

item d) / (10) / (15 ) and any adjacen t metalli c structure includin g

supports/ pipes/ bonding Leads or any other metaLLi c component that

couLd create a conductiv e path to the mai n structure . Refer to

Figur e 2 Figur e 4 and Figur e 6

Use a suitabL e tool/ operator supplied / to check the clearance .

( a ) If the clearance is between 2. 5 mm (0.09 8 in ) and 3. 0 mm (0.11 8

i n ) Loose the probe screws and move the probe up and down to

get the require d minimu m gap of 3. 0 mm (0.11 8 in) .

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAB04/03 PAG E : 9

Printed in France
A310

SERVICE BULLETIN

( b ) If the clearanc e is less than 2. 5 mm (0.09 8 in) / remove the FQI

probe(s ) and instal l new FQI probe supports/ to get the

require d minimu m 3. 0 mm (0.11 8 in ) clearance . Refer to para . C .

REPAIR .

( c ) If the clearanc e is 3. 0 mm (0-11 8 in ) or more/ no further

actio n is required . Refer to para . E . CLOSE UP .

C . REPAIR

NOTE : Only the LH side is described the RH is similar .

( 1 ) For FQI probe/ ite m (1) . If the clearanc e is Less than 2. 5 mm (0.09 8

i n ) to get the require d minimu m gap/ exchange the support/ item (8 )

of the probe item / (1) . Refer to Figur e 2 and Figur e 3

( a ) Remove the support/ ite m (8 ) and the probe/ item (1) . Refer to

Figur e 3 . Follo w instruction s give n in AMM 28-42-51to remove

theprobe/itemd) .

1 Probe Item (1 ) Reta i n

1 Screw Item (2 ) Retai n

3 Washers Item (3 ) Retai n

1 Screw Item (4 ) Retai n

1 Washer Item <5 ) Retai n

2 Screws Item (6 ) Retai n

2 Rivet s Item (7 ) Discar d

1 Support Item (8 ) Discar d

( b ) Instal l the new support/ item 9 in the same position as the

previou s ite m (8) . Use ;

1 Support (LH ) R2822000500000 Item 9

1 Support (RH ) R2822000600000 Item 9

2 Rivet s • MS20470AD5-10 Item 7

NOTE : The rivet s ite m 7 should be cut to the appropriat e

Length .

( c ) Instal l the retained probe/ ite m (1) . Refer to Figur e 3 .

Follo w instruction s give n in AMM 28-42-51 to instal l the probe/

item (1) . Use :

1 Probe Item (1 ) Retaine d

1 Screw Item (2 ) Retaine d

3 Washers Item (3 ) Retaine d

1 Screw Item (4 ) Retained

1 washer Item (5 ) Retained

2 Screws Item (6) Retained

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAR04/03 PAGE : 1 0

Printed In F ranee
^A310

SERVIC E BULLETIN

( d ) Before tightenin g the screws , items (2) / (4 ) and <6 ) check that

t he minimu m clearance of 3. 0 mm (0.11 8 in ) is achieved .

( e ) Tighte n the screws/ item s (2) / (4 ) and (6) .

I (2 ) For FQI probe/ 1'tem (10) . Refer to Figur e 4

( a ) If the clearanc e in the hi-Lok / ite m (19 ) and the collar / item

(20 ) is less than 3. 0 mm (0.11 8 in ) remove it/ and instal l a

new one hi-lok / item 1 9 wit h the collar / item 20 to the

opposite side/ or if i t is in th e h i - L o k / ite m (21 ) and the

collar / item (22 ) remove it , and instal l a new one rivet/ ite m

2 3 . Refer to Figur e 4 detai l D .

1 Hi-lo k HST756CB-5-5 Item (19 ) Discard

1 Colla r HST1087-5 Item (20 ) Discar d

1 Hi-Lo k HST11AZ-5-5 Item (21 ) Discar d

1 Colla r HST681-5 Item (22 ) Discar d

1 Hi-Lo k HST756CB-5-5 Item 1 9

1 Colla r HST1087-5 Item 20

1 Rive t ASNA2051DEJ040 Item 23

( b ) If th e clea r a'nce in the adjacen t areas is lees tha n 2. 5 mm

(0.09 8 in ) to get the required minimu m gap/ exchange the

support/ ite m (11 ) of the probe , ite m (10) . Refer to Figur e 4

and Figur e 5

j. Remov e the support/ ite m (11 ) and the probe , ite m (10) .

Refer to Figur e 5 . Follo w instruction s give n in AM M

28-42-51 to remove the probe/ item (10) .

1 Probe Item (10 ) Retai n

1 Support Item (13 ) Discard

1 Support Item (11)Discar d

1 Screw Item (2 ) Retai n

3 Washers Item (3) Retai n

1 Screw Item (4 ) Retai n

1 washer Item (5 ) Retai n

2 Screws Item (6 ) Retai n

2 Rivet s Item (7 ) Discard

.2. Instal l the new support/ ite m 12 in the same positio n as the

previous/ ite m (11) . Use :

| 1 Support (LH ) R2822030600000 Item 12

1 Support (RH ) R2822000300000 Item 12

| 2 Rivet s MS20470AD5-10 Item 7

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -M4B04/03 , PAQE : 1 1

Printed in Franc e
'A310

SERVICE BULLETIN

NOTE : The rivet s ite m 7 should be cut to the appropriat e

Length .

,3. Insert the probe/ ite m (10 ) in the new support , ite m 14 and

instal l it . Refer to Figur e 5

1 Support (LH ) R2822000100000 Item 14

1 Support (RH ) R2822000100100 Item 14

1 Probe Item (10)Retaine d

2 Screws Item • (6 ) Retaine d

1 Washer Item . (5 ) Retaine d

1 Screw , Item (4 ) Retaine d

3 Washers Item (3 ) Retained

1 Screw . Item (2 ) Retaine d

.4. Before tightenin g the screws/ ite m (2) / (4 ) and (6) check

tha t the minimu m clearanc e of 3. 0 mm (0.11 8 in ) is achieved .

.5. Tighte n the screws/ item s (2 ) / (4 ) and (6) .

( 3 ) For FQI probe , ite m (15) . If the clearanc e is Less tha n 2. 5 mm

(0.09 8 in ) to get the require d minimu m gap/ exchange the Support/

item (17 ) of the probe/ ite m (15) . Refer to Figur e 6 and F i g u r e 7

( a ) Removeth e support/ ite m ( 1 7) a n d the probe/ item (15).Refe r

to Figur e 7 . Follo w instruction s give n in AMH 28-42-51to

remove the probe/ ite m (15) .

1 Probe Item (15 )

1 Support Item (13 )

1 Support Item (17 )

1 Screw Item (2 )

3 Washers Item (3 )

1 Screw Item <4 )

1 Washer Item (5 )

2 Screws Item (6)

2 Rivet s Item (7)

( b ) Instal l the new support/ item 18 in the same positio n as the

previous/ item (17/ . Use :

1 Support (LH ) R2822018600000 Item 18

1 Support (RH ) R2822018600100 Item 18

2 Rivet s MS20470AD5-10 Item 7

NOTE : The rivets/ item 7 should be cut to the appropriat e

length .

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. ; A310-28-214 5

REVISION No. : 01 -MAR04/03 PAGE : 1 2

Printed 1 n Franc e
A310

SERVIC E BULLETIN

( c ) Insert the probe/ ite m (15 ) in the new support , ite m 1 6 and

instal l it . Refer to Figur e 7 .Follo w instruction s give n in

A HM 28-42-51to instal l the probe . Use :

1 Support (LH ) R2822018500000 Item 1 6

1 Support (RH ) R2822018500100 Item 1 6

1 Probe Item (15 ) Retained

2 Screws Item (6 ) Retained

1 Washer Item <5 ) Retained

1 Screw Item (4 ) Retained

3 Washers Item (3 ) Retaine d

1 Screw Item . (2 ) Retaine d

( d ) Before tightenin g the screws/, ite m (2) / (4 ) and (6 ) check that

t he minimu m clearanc e of 3. 0 mm (0.11 8 in ) is achieved .

( e ) Tighte n the screws , ite m (2) , (4 ) and (6) .

D . TEST

If you disconnected/reconnecte d the wirin g harness of a FQI probe/ do the

test of the applicabl e FQI probe , as give n in AM M 28-42-00 Page block 501

E- CLOSE UP

( 1 ) Make sure tha t the work area is clea n and clea r of tools and other

item s of equipment .

( 2 ) Instal l the removed manhol e covers 333BB, (343BB) / 333CB, (343CB) /

333EB and (343EB) . Refer to AM M 28-11-33 Page block 401.

( 3 ) Remove the access platform .

( 4 ) Restore the systems and the aircraf t to norma l operatin g condition .

f - DOCUMENTATIO N

Writ e in the applicabl e aircraf t records tha t you have done al l the work

give n in thi s Servic e Bullet.in .

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION NO. : 01 -MAR04/03 PAGE : 1 3

Printed in Franc e
4

1

®A310

SERVIC E BULLETIN

Location and access

Figur e 1 Sheet 1

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 —MAR04/03 PAGE : 1 4

Printed in Franc e
A310

SERVIC E BULLETIN

CD LOWER SKIN

Areas of inspectio n

Figur e 2 Sheet 1

DATE : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-2U5

REVISIO N No. : 01 - MAR04/03 PAGE : 1 5

Printed in Franc e
A310

SERVIC E BULLETIN

4

/^y^p A

[B] (3)(3)———^/^ ^

^^^ /^ (6)(6) ~^/ 7 l !

'^^y/ C./—(1)(1) i

(2)(2) "-/^< / (8)9

 VN/ l

.ReroovaL/instaLLatio n of the Probe and support

Figure 3 Sheet T

DATE : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAR04/03 PAGE : 1 6

Printed In Franc e
®A310

SERVIC E BULLETIN

Areas of inspectio n

Figur e 4 Sheet 1

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION NO. : 01 -MAR04/03 PAGE : 1 7

Printed in Franc e
'A310

SERVIC E BULLETIN

4

^

(4)(4)

RemovaL/instaLLatio n of the Probe and support

Figure 5 Sheet 1 JJ

DATE : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAR04/03 PAGE : 1 8 }

Printed In Franc e
A310

SERVICE BULLETIN

Areas of inspection

Figur e 6 Sheet 1

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. ; A310-28-214 5

REVISION No. : 01 -MAR04/03 p^g^ ; 1 9

Printed "in F ranee
^A310

SERVIC E BULLETIN

jRemovaL/instaLLatio n of the Probe and support

Figur e 7 Sheet !

DAT E : Aug 21/0 1 SERVIC E BULLETIN No. : A310-28-214 5

REVISION No. : 01 -MAB04/D3 pA6E ; ^0

Printed in Franc e
A310

SERVICE BULLETIN

REPORTING SHEET

TITLE : FUEL - QUANTITY INDICATING - INSPECT FQI PROBES FOR STRUCTURA L CLEARANCE S

MODIFICATIO N No. : None

PLease complete the appropriat e Item :

Planned for embodimen t YES/NO

Rejecte d YES/NO

Embodied on MSN :

From Airlin e : ...................................... .

Name/Title : ...................................... .

Signatur e : ................. . Date :

Importan t Info r_ma t i on :

Thi s SB wil l only be incorporate d in your maintenanc e and operationa l

documentatio n if thi s sheet is returned to Airbu s Industri e and signed by a dul y

authorise d representative . Wit h the next feasibl e revision / thi s wil l result in

updatin g of maintenanc e documentatio n to show pre and post SB data .

updatin g of maintenanc e and operationa l documentatio n to show post SB

data after embodiment .

If thi s SB requires previous or simultaneous accomplishmen t of other SBs, Airbus

Industri e shal l automaticall y includ e them in the manua l revisions .

Refer to SIL 00-037 for detaile d informatio n

Please return thi s compIeted sheet to :

AIRBU S INDUSTRI E

CUSTOMER SERVICE S DIRECTORAT E

1 Rond Point Mauric e BELLONTE

31707 BLAGNA C CEDEX FRANC E

Att n : AI/SE-D32 Technica l Data and Documentatio n Services

F A X : (+33 ) 5 61 93 28 06

or vi a your Resident Customer Support Office .

Alternatively , SB List s vi a letters or fax are also accepted .

LO DATE ; Aug 21/0 1 SERVIC E BULLETIN No. i A310-28-214 5

REVISION No. : 01 -MAR04/03 PAGE : 1 of 1

printed in Franc e