# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - GENERAL- ACTIVATE STOP RUDDER INPUT WARNING DEVICE MODIFICATION No.: 13593S22853 This page transmits Revision No.01 of Service Bulletin No.A310-22-2064 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 issued to add aircraft for operator FDX. CHANGES SUMMARY MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE UPDATED R EFFECTIVITY OPERATOR LIST UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Configuration definition CONF 001 CONFIGURATION DEFINITION UPDATED R Material Effectivity MATERIAL EFFECTIVITY UPDATED MATERIAL SET UPDATED R MANPOWER MANPOWER UPDATED R WEIGHT AND BALANCE Minor editorial or document structure change R REFERENCES REFERENCED DOCUMENTATION UPDATED R PUBLICATION AFFECTED PUBLICATIONS AFFECTED UPDATED R MATERIAL INFORMATION MATERIAL - PRICE AND AVAILABILITY

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 1 5

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# @A310 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Procurement Addresses PROCUREMENT ADDRESSES UPDATED MATERIAL SET UPDATED R LIST OF COMPONENTS Kit 222064A01R01 PART MATERIAL SET UPDATED MATERIAL SET LABEL UPDATED QUANTITY UPDATED R
ACCOMPLISHMENT INSTRUCTIONS TASK 222064- 831-801-001-Modification Subtask 222064-941-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R
Subtask 222064-831-001-001 SUBTASK SOLUTION UPDATED QUANTITY UPDATED CONFIGURATION UPDATED FIGURE REFERENCE UPDATED MATERIAL LIST UPDATED R

Subtask 222064-831-002-001 SUBTASK SOLUTION UPDATED MATERIAL LIST UPDATED R Subtask 222064-700-001-001 SUBTASK SOLUTION UPDATED R Subtask 222064-942-001-001 SUBTASK SOLUTION UPDATED REFERENCED DOCUMENTATION UPDATED REFERENCES UPDATED R Fig. A-FBAAA FIGURE SOLUTION UPDATED R Fig. A-FBAAA Sheet 01 SHEET UPDATED R Fig. A-FBAAA Sheet 02 SHEET UPDATED R FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS No previous revision REVISION SEQUENCE ORIGINAL: Nov 18/11 REVISION No. : 01 - May 31/12

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 2 5

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# @A310 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - GENERAL- ACTIVATE STOP RUDDER INPUT WARNING DEVICE **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 13593S22853 MINOR None NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES This Service Bulletin is issued further to an operator’s request. Following report of events of excessive rapid alternating and large rudder pedal inputs that resulted in high vertical stabilizer loads, this service bulletin provides increased protection by improvement of the cockpit crew awareness in case of excessive rudder reversal control input. This is achieved by activation of a warning red light "STOP" on rudder input panels in front of each pilot which is reinforced by an aural warning "Stop rudder input". This Service Bulletin installs on Captain and First Officer (F/O) side new 510VU including a red lighted push-button and activates the function. Aircraft have to be previously equipped with : - System and mechanical provision - Flight Warning Computer (FWC) STD S17 P/N 35-0B5-3008-320 - Flight Control Computer (FCC) P/N B470ADM03 Accomplishment of this Service Bulletin will satisfy the operator’s request.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 1 5

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# @A310 SERVICE BULLETIN SUMMARY The Operational/Maintenance Consequences of this Service Bulletin are covered by the update of the affected publications detailed in PLANNING INFORMATION NOTE: Accomplishment of this Service Bulletin requires previously a crew training to familiarize flight crew with the warning and the associated procedures. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED YES RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1): Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit222064A01R01 1 See SB Panels, Contacts EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

99Y FDX NOTE: This Service Bulletin is written for the operators listed above. The modification in this Service Bulletin can be done by other operators. If other operators want to do this modification, use the RFC/RMO procedure and write to : AIRBUS CUSTOMER SERVICES DIRECTORATE SC Department 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletins : Service Bulletin No. A310-22-2063 A310-22-2065 A310-31-2144 NOTE: Accomplishment of this Service Bulletin requires previously a crew training to familiarize flight crew with the warning and the associated procedures.

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 2 5

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# @A310 SERVICE BULLETIN SUMMARY REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT YES HARD NO SOFT NO OBRM NO MANPOWER Task 222064-831-801-001: Modification TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 4.00 APPENDICES Appendix 01

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 3 5

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

FR1 FR20
190VT MODIFICATION OF THE WIRING IN 80VU

MODIFICATION OF 13VU
B_SB_222064_5_SAAA_01_00 Figure A-FSAAA - Sheet 01

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 4 5

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# @A310 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - GENERAL- ACTIVATE STOP RUDDER INPUT WARNING DEVICE MODIFICATION No.: 13593S22853 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY (1) Models 310-203 310-221 310-222 310-304 310-308 310-324 (2) Effectivity by MSN 0162 0201 0217 0230 0233 0237 0241 0245 0248 0251 0254 0264 0267 0278 0281 0283 0288 0297 0313 0316 0318 0326 0331 0333 0335 0339 0343 0345-0346 0353 0355-0356 0359 0362 0364 0369 0378 0394 0439 0449 0452 0454 0456-0458 0467 0489 0492 0500 0534 0539 0542 0549 0552 0593 0638 (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 99Y 0489
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 1 5

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# @A310 SERVICE BULLETIN

OPERATOR MSN FDX 0162 0201 0217 0230 0233 0237 0241 0245 0248 0251 0254 0264 0267 0278 0281 0283 0288 0297 0313 0316 0318 0326 0331 0333 0335 0339 0343 0345 0346 0353 0355 0356 0359 0362 0364 0369 0378 0394 0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539 0542 0549 0552 0593 0638 (4) Configuration by MSN MSN CONFIGURATION 0162 0201 0217 0230 0233 0237 0241 0245 0248 0251 0254 0264 0267 0278 0281 0283 0288 0297 0313 0316 0318 0326 0331 0333 0335 0339 0343 0345 0346 0353 0355 0356 0359 0362 0364 0369 0378 0394 0439 0449 0452 0454 0456 0457 0458 0467 0489 0492 0500 0534 0539 0542 0549 0552 0593 0638 001

(5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Kit222064A01R01 1 B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletins : Service Bulletin No. A310-22-2063 A310-22-2065 A310-31-2144 NOTE: Accomplishment of this Service Bulletin requires previously a crew training to familiarize flight crew with the warning and the associated procedures. C. REASON (1) History This Service Bulletin is issued further to an operator’s request. (2) Objective/Action Following report of events of excessive rapid alternating and large rudder pedal inputs that resulted in high vertical stabilizer loads, this service bulletin provides increased protection by improvement of the cockpit crew awareness in case of excessive rudder reversal control input.

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 2 5

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# @A310 SERVICE BULLETIN This is achieved by activation of a warning red light "STOP" on rudder input panels in front of each pilot which is reinforced by an aural warning "Stop rudder input". This Service Bulletin installs on Captain and First Officer (F/O) side new 510VU including a red lighted push-button and activates the function. Aircraft have to be previously equipped with : - System and mechanical provision - Flight Warning Computer (FWC) STD S17 P/N 35-0B5-3008-320 - Flight Control Computer (FCC) P/N B470ADM03 (3) Advantages Accomplishment of this Service Bulletin will satisfy the operator’s request. (4) Operational/Maintenance Consequences The Operational/Maintenance Consequences of this Service Bulletin are covered by the update of the affected publications detailed in PLANNING INFORMATION NOTE: Accomplishment of this Service Bulletin requires previously a crew training to familiarize flight crew with the warning and the associated procedures. D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 222064-831-801-001: Modification (1) Modify the Wiring in the Avionics Compartment. (2) Modify the Equipment in the Glareshield Panel 13VU. E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA) will be issued to confirm this classification. The accomplishment timescale, which has not yet been defined, will be given in the AD. F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 3 5

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# @A310 SERVICE BULLETIN If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 222064-831-801-001: Modification Get Access 1.00 On Aircraft Modify the Wiring in the Avionics Compartment. 2.00 Modify the Equipment in the Glareshield Panel 13VU. 1.00 Tests 1.00 Close-Up 1.00 TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 4.00 NOTE: For detailed concerning the elapsed time assumptions, refer to Appendix 01 . H. WEIGHT AND BALANCE The weight and balance estimates given in this Service Bulletin are based on the Manufacturer’s Empty Weight (MEW) and do not include operator item’s. For the definition of MEW and operator’s items refer to Weight and Balance Manual (WBM) Chapter 1-00-07. Manufacturers Empty Weight +2.850 KG (+6.2831 LB) Effect on Balance +26.163 KGM (+189.236 LB.FT ) I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-31-53 06-41-00 06-41-52 06-41-53 20-21-12 21-21-00 22-10-00 22-18-34 22-27-00 22-40-00 24-00-00 24-31-11 24-41-00 31-51-00 33-12-00 33-13-00 33-14-00 52-10-00 52-30-00 Elec. Std. Practices Manual (ESPM) 20-25-51 20-52-10 20-55-00 Service Bulletin (SB) A310-22-2063 A310-22-2065 A310-31-2144
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 4 5

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# @A310 SERVICE BULLETIN
Standards Manual (SM) Weight and Balance Manual (WBM) Weight and Balance Manual (WBM) Chapter 1-00-07 K. PUBLICATION AFFECTED

Flight Crew Operating Manual (FCOM) Flight Manual (FM) Master Minimum Equipment List This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in advance, in case you need your operational documentation to be amended by a revision priorto Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to: SEDOR4 - AIRBUS Customer Services Technical Data Fax No.: (33) 5 61 93 28 06 E-mail: sb.reporting@airbus.com SB Reporting service is accessible on-line through AIRBUSWorld from : My on-line services’ section, available on all AIRBUSWorld pages The Maintenance and Engineering Community, in : - Modify and Upgrade page - Access SB and VSB section. These amendments will be confirmed by the next normal revision of operational documentation, once your Service Bulletin accomplishment report has been sent, as usual, to our Customer Services Aircraft In-Service Data (SEDOR4). L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 5 5

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# @A310 SERVICE BULLETIN

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# @A310 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit222064A01R01 The AIRBUS material is included in the commercial offer of the Letter Agreement, and as such will be supplied by AIRBUS Upgrade Services. To facilitate the material reception, Airline Customers are requested to send a Customer Purchase Order to: AIRBUS Upgrade Services Attn Key Account Manager (KAM) (2) Price and Availability Sales terms must be agreed between the Customer and AIRBUS in accordance with the RFC (or RFC/RMO) procedure. B. INDUSTRY SUPPORT INFORMATION Refer to the paragraph : ’Price and Availability’. C. LIST OF COMPONENTS Kit 222064A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 2 A9550051000195 1 PANEL 3 A9550051000295 1 PANEL E0171LA1202 2 CONTACT EN3155-016M2018 6 CONTACT EN3155-018M2018 2 CONTACT NOTE: If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. D. LIST OF MATERIALS - OPERATOR SUPPLIED None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 7 5

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# @A310 SERVICE BULLETIN
F. TOOLING None

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 8 5

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# @A310 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 222064-831-801-001 - Modification WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION: ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 120 210 Modified FIN 511VC2A 512VC2A 510VU1 510VU2 Access Door 132AZ 811 831 841 Manpower TOTAL MANHOURS 6.00 ELAPSED TIME (HOURS) 4.00 A. GENERAL (1) Subtask 222064-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. (2) Subtask 222064-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 9 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-31-53, Page Block 001 06-41-00, Page Block 001 20-21-12, Page Block 001 Elec. Std. Practices Manual (ESPM) 20-25-51 (a) For the Frame (FR) identification (Refer to AMM 06-31-53, Page Block 001). (b) For the identification of access panels (Refer to AMM 06-41-00, Page Block 001). (c) Do a continuity test of the modified wires (Refer to ESPM 20-25-51). B. PREPARATION (1) Subtask 222064-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 24-00-00, Page Block 301 24-31-11, Page Block 401 52-10-00, Page Block 001 52-30-00, Page Block 001 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platforms in position at the level of door 831 or 841 and 811. (c) Open the FWD passenger/crew door 831 or 841 (Refer to AMM 52-10-00, Page Block 001 and AMM 06-41-52, Page Block 001). (d) Open the FWD cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (e) Open the door 132AZ (Refer to AMM 06-41-53, Page Block 001). (f) Make sure that the external connector(s) is (are) not connected to the aircraft receptacle(s) EXT PW. (g) Make sure that there is (are) warning notice(s) on external power receptacle to tell persons not to connect an external power source. (h) Make sure that the EMER EXIT LT pushbutton switch on 436VU is on DISARM position. (i) In the cockpit, on the overhead panel 424VU release BAT pushbutton switches. (j) Put a warning notice on panel 424VU to tell persons not to operate the batteries.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 10 5

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# @A310 SERVICE BULLETIN (k) Put a warning notice on the refuel/defuel panel 110VU to tell persons not to operate the NORMAL BATTERY switch. (l) Put a warning notice in the cockpit to tell persons not to start the APU. (m) Put a warning notice in the cockpit to tell persons not to start the ENG 1 and 2. (n) Battery disconnection : - For Job Set-up, refer to the removal of the Batteries (Refer to AMM 24-31-11, Page Block 401). - Turn the knurled nut a quarter turn. - Disconnect the connectors. - Put blanking caps on the disconnected electrical connectors. C. PROCEDURE (1) Subtask 222064-831-001-001 - Modify the Wiring in the Avionics Compartment. Work Zones and Access Panels Zone Access/Work location 120 Access Door 132AZ, Door 811 Manpower Resources Manhours 2.00 Minimum number of person 2 Subtask elapsed time 1.00 Skills ELECTRICAL Material necessary to do the job Kit 222064A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES E0171LA1202 2 CONTACT EN3155-016M2018 6 CONTACT EN3155-018M2018 2 CONTACT References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 Fig. A-FHAAA Hook-up Chart of the Modification of the Wiring in the Avionics Compartment. Sheet 01
Fig. A-FHBAA Hook-up Chart of the Modification of the Wiring in 80VU. Sheet 01

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# @A310 SERVICE BULLETIN

References Fig. A-FWAAA Modification of the Wiring in the Avionics Compartment. Sheet 01 Sheet 02 Fig. A-FWBAA Modification of the Wiring in 80VU. Sheet 01 Sheet 02 (a) Remove the Flight Control Computers 301CA1 and 301CA2 (Refer to AMM 22-18-34, Page Block 401). (b) Remove the wires as shown on the wiring diagram Fig. A-FWBAA Sheet 01 and as given in the Hook-up Chart lines: - 1 and 2 (Refer to Fig. A-FHBAA Sheet 01). (c) Modify the wiring as shown in the wiring diagrams Fig. A-FWAAA Sheet 01, Fig. AFWAAA Sheet 02, Fig. A-FWBAA Sheet 01 and Fig. A-FWBAA Sheet 02, and as given in the hook-up chart lines : - 1 thru 8 (Refer to Fig. A-FHAAA Sheet 01), - 6 thru 13 (Refer to Fig. A-FHBAA Sheet 01). (d) If necessary, use : 6 Contact EN3155-016M2018 2 Contact EN3155-018M2018 2 Contact E0171LA1202 (e) Install the Flight Control Computers 301CA1 and 301CA2 (Refer to AMM 22-18-34, Page Block 401) removed for access. (2) Subtask 222064-831-002-001 - Modify the Equipment in the Glareshield Panel 13VU. Work Zones and Access Panels Zone Access/Work location 210 Access Door 831, Door 841 Work location Electrical panel 13VU Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills ELECTRICAL

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 12 5

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# @A310 SERVICE BULLETIN
Material necessary to do the job Kit 222064A01R01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 A9550051000195 1 PANEL 3 A9550051000295 1 PANEL References Fig. A-FBAAA Modification of the Equipment on the Glareshield Panel 13VU Sheet 01 Sheet 02 (a) On the glareshield panel 13VU : 1 Remove (Refer to Fig. A-FBAAA Sheet 01) : 2 Rest Plate A9251134100000 Item (1) Discard 2 Disconnect the connectors 511VC1A and 511VC2A from the LH rest plate item 1 and the connectors 512VC1A and 512VC2A from the RH rest plate item 1. 3 Install (Refer to Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02) : FIN 510VU1 1 Panel A9550051000195 Item 2 FIN 510VU2 1 Panel A9550051000295 Item 3 4 Connect the connectors 511VC1A and 511VC2A to the panel 510VU1 item 2 and the connectors 512VC1A and 512VC2A to the panel 510VU2 item 3. D. TEST (1) Subtask 222064-700-001-001 - Testing Manpower Resources Skills NON SPECIFIC

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 13 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 21-21-00, Page Block 501 22-10-00, Page Block 501 22-27-00, Page Block 501 22-40-00, Page Block 501 24-31-11, Page Block 401 24-41-00, Page Block 301 31-51-00, Page Block 501 33-12-00, Page Block 501 33-13-00, Page Block 501 33-14-00, Page Block 501 Elec. Std. Practices Manual (ESPM) 20-52-10 (a) Job Set-up 1 Battery re-connection - For Job Set-up, refer to the installation of the Batteries (Refer to AMM 24-31-11, Page Block 401). - Remove the blanking cap from the electrical connectors. - Make sure that the electrical connectors are clean and in correct condition. - Connect the connector on the battery. - Turn the knurled nut a quarter turn. 2 Remove all warning notices. 3 Restore the systems and the aircraft to normal operating condition. (b) Procedure 1 Preliminary Tests NOTE: If the aircraft is operated in CAT3 conditions, you must also do the LAND test (Refer to AMM 22-40-00, Page Block 501).
a On each connector which was disconnected : - Do the checks as defined by ESPM 20-52-10. NOTE: The functional test and/or operational test requested by this ESPM procedure is given hereafter. b Do the operational test of the Annunciator Light Test (Refer to AMM 33-14-00, Page Block 501).
c Do the operational test of the General Illumination (Refer to AMM 33-12-00, Page Block 501).

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 14 5

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# @A310 SERVICE BULLETIN
d Do the operational test of the Instrument and Panel Integral Lighting (Refer to AMM 33-13-00, Page Block 501).
e Make certain that the ventilation system operates correctly (Refer to AMM 21-21-00, Page Block 501). f Do the Automatic Flight System Test (Refer to AMM 22-40-00, Page Block 501, para 1.A) g Do the operational test of Electronic Centralized Aircraft Monitoring / Electronic Flight Instrument System Display Test (Refer to AMM 31-51-00, Page Block 501). h Do the operational test FWC1 and FWC2 (Refer to AMM 31-51-00, Page Block 501). 2 Test of the equipments (301CA1 and 301CA2)
a Do a detailed visual inspection of the autotrim function (Refer to AMM 22-27-00, Page Block 501, para 1.H). b Do the autopilot operational test (Refer to AMM 22-10-00, Page Block 501, para 1.D Check of Pitch Trim Autotrim circuits). 3 Check the correct activation of the stop rudder input warning device as follows : a Job Set-up : <1> Energize the aircraft electrical network (Refer to AMM 24-41-00, Page Block 301). <2> Make certain that electronic racks ventilation is correct. <3> Make sure that the following circuit breakers are closed : PANEL DESIGNATION FIN LOCATION SEE NOTES 21VU AFS/AP1-FD1/FCC1/28VDC 306CA1 Ref. AMM 24-50-10 21VU AFS/AP2-FD2/FCC2/28VDC 306CA2 Ref. AMM 24-50-10 21VU ECAM/FWC1 7WW Ref. AMM 24-50-10 21VU ECAM/FWC2 32WW Ref. AMM 24-50-10 b Procedure : ACTION RESULT 1. On overhead C/B panel 21VU : - Open FCC2 circuit breaker 306CA2 and open

FWC2 circuit breaker 32WW. DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 15 5

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# @A310 SERVICE BULLETIN

ACTION RESULT 2. On CAPT panel 510VU1 : - Press STOP pushbutton switch. On the glareshield panel 13VU : - Check that CAPT and F/O lights are illuminated.

Aural warning message "stop rudder input" is repeated two times. 3. On CAPT panel 510VU1 : - Release STOP pushbutton switch. On the glareshield panel 13VU : - Check that both lights go off. 4. On overhead C/B panel 21VU : - Close FWC2 circuit breaker 32WW and open

FWC1 circuit breaker 7WW. 5. On CAPT panel 510VU1 : - Press STOP pushbutton switch. On the glareshield panel 13VU : - Check that CAPT and F/O lights are illuminated.

Aural warning message "stop rudder input" is repeated two times. 6. On CAPT panel 510VU1 : - Release STOP pushbutton switch. On the glareshield panel 13VU : - Check that both lights go off. 7. On overhead C/B panel 21VU : - Close FCC2 circuit breaker 306CA2 and open

FCC1 circuit breaker 306CA1. 8. On F/O panel 510VU2 : - Press STOP pushbutton switch. On the glareshield panel 13VU : - Check that CAPT and F/O lights are illuminated.

Aural warning message "stop rudder input" is repeated two times. 9. On F/O panel 510VU2 : - Release STOP pushbutton switch. On the glareshield panel 13VU : - Check that both lights go off. 10. On overhead C/B panel 21VU : - Close FWC1 circuit breaker 7WW and open

FWC2 circuit breaker 32WW. 11. On F/O panel 510VU2 : - Press STOP pushbutton switch. On the glareshield panel 13VU : - Check that CAPT and F/O lights are illuminated.

Aural warning message "stop rudder input" is repeated two times. 12. On F/O panel 510VU2 : - Release STOP pushbutton switch. On the glareshield panel 13VU : - Check that both lights go off. 13. On overhead C/B panel 21VU : - Close FWC2 circuit breaker 32WW and open

FCC1 circuit breaker 306CA1.

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 16 5

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# @A310 SERVICE BULLETIN

4 Close-up :
a De-energize the aircraft electrical network (Refer to AMM 24-41-00, Page Block 301). E. CLOSE-UP (1) Subtask 222064-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-52, Page Block 001 06-41-53, Page Block 001 52-10-00, Page Block 001 52-30-00, Page Block 001 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Close the door 132AZ (Refer to AMM 06-41-53, Page Block 001). (c) Close the FWD cargo compartment door 811 (Refer to AMM 52-30-00, Page Block 001). (d) Close the FWD passenger/crew door 831 841 (Refer to AMM 52-10-00, Page Block 001 and AMM 06-41-52, Page Block 001). (e) Remove the access platforms. (f) Restore the system and the aircraft to the normal operating condition.

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 17 5

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# @A310 SERVICE BULLETIN

**CONF ALL



## BEFORE

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## A **A B**  **A B** 

(1)

B_SB_222064_5_BAAA_01_01 Figure A-FBAAA - Sheet 01 Modification of the Equipment on the Glareshield Panel 13VU
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 18 5

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# @A310 SERVICE BULLETIN

**CONF ALL


## AFTER

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B 3 RH 2LH

STOP RUDDER INPUTS

B_SB_222064_5_BAAA_02_03 Figure A-FBAAA - Sheet 02 Modification of the Equipment on the Glareshield Panel 13VU
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 19 5

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# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 01 Modification of the Wiring in the Avionics Compartment.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 20 5

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# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FWAAA - Sheet 02 Modification of the Wiring in the Avionics Compartment.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 21 5

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# @A310 SERVICE BULLETIN

**CONF ALL

END1 LEAD END2 Instructions Zone or

Panel Elec.Ident. Term Terminal P/N Wire Ident. Co Rte Gauge Lenght mm Inch Zone or Panel Elec.Ident. Term Terminal P/N L i n e 1 122 190VT 24G 3313−0611 R 2M PF18 122 371LF−A H M1O 2 122 190VT 34G EN3155−016M2018 3313−0611 R 2M PF18 122 371LF−A H M1N 3 122 190VT 1F 3313−0612 B 2M PF18 122 371LF−A J M1O 4 122 190VT 35F EN3155−016M2018 3313−0612 B 2M PF18 122 371LF−A J M1N 5 122 190VT WS 3313−1660 2M CF18 122 190VT 34K M1O 6 122 190VT 24G EN3155−016M2018 3313−1660 2M CF18 122 190VT 34K M1N 7 122 190VT WS 3313−1661 2M CF18 122 190VT 35K M1O 8 122 190VT 1F EN3155−016M2018 3313−1661 2M CF18 122 190VT 35K M1N 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25

M1O = OLD HOOK−UP ON END 1 M1N = NEW HOOK−UP ON END 1
Figure A-FHAAA - Sheet 01 Hook-up Chart of the Modification of the Wiring in the Avionics Compartment.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 22 5

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# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FWBAA - Sheet 01 Modification of the Wiring in 80VU.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 23 5

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# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FWBAA - Sheet 02 Modification of the Wiring in 80VU.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 24 5

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# @A310 SERVICE BULLETIN

**CONF ALL

END1 LEAD END2 Instructions Zone or

Panel Elec.Ident. Term Terminal P/N Wire Ident. Co Rte Gauge Lenght mm Inch Zone or Panel Elec.Ident. Term Terminal P/N L i n e 1 80VU 2297VC <C 2212−0014 W1M CF18 83VU 301CA1−AC 7 D 2 80VU 2616VC JJ 2212−0069 X2M CF18 84VU 301CA2−AC 7 D 3 4 5 6 80VU 2297VC WS 2212−0350 CF18 80VU 123VT 73B M1O 7 80VU 2297VC <C EN3155−018M2018 2212−0350 CF18 80VU 123VT 73B M1N 8 80VU 2616VC WS 2212−0365 X2M CF18 80VU 124VT 22B M1O 9 80VU 2616VC JJ EN3155−018M2018 2212−0365 X2M CF18 80VU 124VT 22B M1N 10 80VU 123VT WS 2212−0351 W1M CF18 83VU 301CA1−AC WS M1O+M2O 11 80VU 123VT 73A EN3155−016M2018 2212−0351 W1M CF18 83VU 301CA1−AC 7 E0171LA1202 M1N+M2N 12 80VU 124VT WS 2212−0366 X2M CF18 84VU 301CA2−AC WS M1O+M2O 13 80VU 124VT 22A EN3155−016M2018 2212−0366 X2M CF18 84VU 301CA2−AC 7 E0171LA1202 M1N+M2N 14 15 16 17 18 19 20 21 22 23 24 25

M1O = OLD HOOK−UP ON END 1 M1N+M2N= NEW HOOK−UP ON END 1 AND 2 M1N = NEW HOOK−UP ON END 1 D = DELETED WIRE M1O+M2O= OLD HOOK−UP ON END 1 AND 2 Figure A-FHBAA - Sheet 01 Hook-up Chart of the Modification of the Wiring in 80VU.
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 25 5

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# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FWCAA - Sheet 01 Modification of the Wiring in 510VU1 (for information only).
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 26 5

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# @A310 SERVICE BULLETIN

**CONF ALL

Figure A-FWDAA - Sheet 01 Modification of the Wiring in 510VU2 (for information only).
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 27 5

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# @A310 SERVICE BULLETIN

This Page Intentionally Left Blank

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 28 5

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# @A310 SERVICE BULLETIN Appendix 01 **CONF ALL For detail concerning the elapsed time assumptions, refer to the Gantt chart shown below :

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 1 5

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# @A310 SERVICE BULLETIN Appendix 01

**CONF ALL
**ELAPSED TIME ASSUMPTIONS SERVICE BULLETIN No. A310−22−2064**

TOTAL MANHOURS SB ELAPSED TIME 6.00 4.00

MH ET/S: PER MANHOURS ELAPSED TIME PER STEP NUMBER OF PERSONS 01 02

THIS CHART IS ONLY A PROPOSAL. OPERATORS MAY DETERMINE THAT ANOTHER WAY TO DO THE WORK IS MORE SUITABLE FOR THEM. MANHOURS GIVEN IN VENDOR SERVICE BULLETINS ARE NOT REFLECTED IN THIS GANTT CHART. 01
02 **NOTES:**

: : SB ELAPSED TIME (HOURS) MH PER ET/S STEPS

0 GET ACCESS 1.00 1.00 1

CLOSE−UP 1.00 1.00 1

4 5 MODIFICATION WIRING 2.00 1.00 2 AVIONICS COMPARTMENT

MODIFICATION EQUIPMENT 13VU 1.00 1.00 1

1.00 1.00 1 TEST

2 3 1

B_SB_222064_5_AAAA_01_00 Figure A-FAAAA - Sheet 01 Elapsed Time Assumption
DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 2 5

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# @A310 SERVICE BULLETIN REPORTING SHEET 

### TITLE: AUTO FLIGHT - GENERAL- ACTIVATE STOP RUDDER INPUT WARNING DEVICE MODIFICATION No.: 13593S22853 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 1 5

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# @A310 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Nov 18/11 SERVICE BULLETIN No.: A310-22-2064 REVISION No.: 01 - May 31/12 Page: 1 5

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