AD 2008-25-02 Airworthiness Directives; Airbus Model A330 Airplanes; and Model A340-200 and -300 Airplanes

Models named: A330, A340-200, A340-300. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to all Airbus Model A330, A340-200, and A340-300 airplanes, all certified models, all serial numbers, certificated in any category.

Unless already done, do the actions in paragraphs (f)(1), (f)(2), (f)(3), (f)(4), and (f)(5) of this AD for the applicable airplanes identified in Table 1 of this AD. Table 1—Applicable Paragraphs by Model These airplane models— Except airplanes— Are affected by these paragraphs of this AD— Model A330, A340-200, and A340-330 airplanes On which Airbus Modification 47634 has been embodied in production (f)(1).   • On which both Airbus Modifications 49135 and 49630 have been embodied in production (f)(2)(i), except as provided by paragraphs (f)(2)(ii) and (f)(2)(iii) of this AD.   • Both Airbus Modifications 51825 and 55118 have been embodied in production   • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A330-28-3082, Revision 04, including Appendix 01, dated August 3, 2007, or Revision 05, including Appendix 1, dated May 27, 2008; and Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006   • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007; and Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007 Model A330 airplanes on which the actions specified in Airbus Service Bulletin A330-28-3082, dated June 14, 2004, have been accomplished before the effective date of this AD; and Model A340-200 and A340-300 airplanes on which the actions specified in Airbus Service Bulletin A340-28-4097, dated June 14, 2004, Revision 01, dated March 3, 2005, or Airbus Mandatory Service Bulletin A340-28-4097, Revision 02, dated August 16, 2006, have been accomplished before the effective date of this AD • On which both Airbus Modifications 49135 and 49630 have been embodied in production • Both Airbus Modifications 51825 and 55118 have been embodied in production • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A330-28-3082, Revision 04, including Appendix 01, dated August 3, 2007, or Revision 05, including Appendix 1, dated May 27, 2008; and Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006 (f)(2)(ii) and (f)(2)(iii).   • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007, and Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007 Model A340-200 and A340-300 airplanes that have the ACT embodied in production or in service (Airbus Modification 42612, 44002, or 44005) That have been modified in service by Airbus Mandatory Service Bulletin A340-28-4078, Revision 01, dated January 25, 2007 (f)(3). Model A340-200 and A340-300 airplanes • On which Airbus Modification 44252 has been embodied in production (f)(4)(i), except as provided by paragraph (f)(4)(ii) of this AD.   • That have been modified in-service in accordance with Airbus Service Bulletin A340-55-4017, dated August 20, 1996; Revision 1, dated February 12, 2007; or Revision 02, dated March 16, 2007 Model A330-301, -321, -322, -341, -342 airplanes • On which Airbus Modification 44252 has been embodied in production (f)(4)(i), except as provided by paragraph (f)(4)(ii) of this AD.   • That have been modified in-service in accordance with Airbus Service Bulletin A330-55-3016, dated August 20, 1996; Revision 1 dated February 12, 1997; or Revision 02, dated March 16, 2007 Model A330-301, -321, -322, -341, -342 airplanes; and Model A340-200 and A340-300 airplanes On which the improvement of the THS lightning strike protection has already been performed before the effective date of this AD in accordance with Airbus A330/A340 All Operators Telex 55-03, dated August 22, 1996 (“solution A”), mandated by Direction Générale de l'Aviation Civile (DGAC) Airworthiness Directive F-1996-178-049(B) R1, and DGAC Airworthiness Directive F-1996-177-038(B), with a compliance time of November 15, 1996 (f)(4)(ii). Model A340-200 and A340-300 airplanes • On which Airbus Modification 46142 has been embodied in production (f)(5).   • That have been modified in-service in accordance with Airbus Mandatory Service Bulletin A340-28-4073, Revision 02, dated March 8, 2007 (1) Within 24 months after the effective date of this AD, do a detailed visual inspection of the P-clips in the wings and center fuel tanks, and apply the applicable corrective actions, in accordance with the applicable instructions of Airbus Mandatory Service Bulletin A330-28-3092, Revision 01, dated December 14, 2005; or Airbus Mandatory Service Bulletin A340-28-4107, Revision 01, dated December 14, 2005. (2) Do the requirements of paragraphs (f)(2)(i), (f)(2)(ii), and (f)(2)(iii) of this AD, as applicable, at the times specified in those paragraphs. (i) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 24 months after the effective date of this AD, modify the electrical bonding of the equipment installed in fuel tanks, in accordance with both Airbus Mandatory Service Bulletin A330-28-3082, Revision 05, including Appendix 1, dated May 27, 2008, and Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006; or both Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007, and Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007; as applicable. (ii) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 24 months after the effective date of this AD, modify the electrical bonding of the equipment installed in fuel tanks, in accordance with Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006; or Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007; as applicable. (iii) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 48 months after the effective date of this AD, do the additional work specified in Airbus Mandatory Service Bulletin A330-28-3082, Revision 05, including Appendix 1, dated May 27, 2008; or Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007; in accordance with the accomplishment instructions of those service bulletins, as applicable. (3) Within 24 months after the effective date of this AD, modify the electrical bonding in the ACT in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A340-28-4078, Revision 01, dated January 25, 2007. (4) Within 24 months after the effective date of this AD, do the requirements of paragraphs (f)(4)(i) and (f)(4)(ii), as applicable. (i) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 24 months after the effective date of this AD, increase the distance between metallic parts on the THS trim tank in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A330-55-3016, Revision 02, March 16, 2007; or Airbus Mandatory Service Bulletin A340-55-4017, Revision 02, dated March 16, 2007; as applicable. (ii) For airplanes affected by this paragraph, as specified in Table 1 of this AD: At the first THS removal from the aircraft done for any reason after the effective date of this AD (e.g., fuselage stress jacking, and repair) when the airplane is on a support tool (lifting and resting point fittings must be installed), or at the time of the first maintenance task that requires the use of THS lifting and resting point fittings, whichever occurs earlier, increase the distance between metallic parts on the THS trim tank in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A330-55-3016, Revision 02, March 16, 2007; or Airbus Mandatory Service Bulletin A340-55-4017, Revision 02, dated March 16, 2007; as applicable. (5) Within 24 months after the effective date of this AD, install a bonding lead between the bonding tags on the jettison valve actuator and drive assembly in accordance with the instructions of Airbus Mandatory Service Bulletin A340-28-4073, Revision 02, dated March 8, 2007. (6) Actions done before the effective date of this AD in accordance with the service bulletins listed in Table 2 of this AD are acceptable for compliance with the corresponding requirements of this AD. Table 2—Credit Service Bulletins Airbus Service information Revision level Date Corresponding paragraphs Mandatory Service Bulletin A330-28-3082 02 August 11, 2006 (f)(2)(i) of this AD. Mandatory Service Bulletin A330-28-3082 03 November 15, 2006 (f)(2)(i) and (f)(2)(iii) of this AD. Mandatory Service Bulletin A330-28-3082 04 August 3, 2007 (f)(2)(i) and (f)(2)(iii) of this AD. Mandatory Service Bulletin A330-28-3101 Original June 5, 2006 (f)(2)(i) and (f)(2)(ii) of this AD. Mandatory Service Bulletin A340-28-4118 Original June 5, 2006 (f)(2)(i) and (f)(2)(ii) of this AD. Mandatory Service Bulletin A340-28-4118 01 October 11, 2006 (f)(2)(i) and (f)(2)(ii) of this AD. Service Bulletin A330-28-3082 01 March 2, 2005 (f)(2)(i) of this AD. Service Bulletin A330-55-3016 Original August 20, 1996 (f)(4)(i) and (f)(4)(ii) of this AD. Service Bulletin A330-55-3016 1 February 12, 1997 (f)(4)(i) and (f)(4)(ii) of this AD. Service Bulletin A340-28-4073 Original May 14, 1998 (f)(5) of this AD. Service Bulletin A340-28-4073 01 October 9, 1998 (f)(5) of this AD. Service Bulletin A340-28-4078 Original March 17, 2000 (f)(3) of this AD. Service Bulletin A340-55-4017 Original August 20, 1996 (f)(4)(i) and (f)(4)(ii) of this AD. Service Bulletin A340-55-4017 1 February 12, 1997 (f)(4)(i) and (f)(4)(ii) of this AD. FAA AD Differences Note 1: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, ANM-116, International Branch, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Tim Backman, Aerospace Engineer, ANM-116, International Branch, Transport Airplane Directorate, FAA, 1601 Lind Ave. SW., Renton, Washington, 98057-3356, telephone (425) 227-2797; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI European Aviation Safety Agency (EASA) Airworthiness Directive 2007-0278, dated November 5, 2007 [Corrected: November 8, 2007], and the service bulletins in Table 3 of this AD, for related information. Table 3—Related Service Bulletins Airbus Mandatory Service Bulletin Revision level Date A330-28-3082, including Appendix 1 05 May 27, 2008. A330-28-3092, excluding Appendix 01 01 December 14, 2005. A330-28-3101 01 October 11, 2006. A330-55-3016 02 March 16, 2007. A340-28-4073 02 March 8, 2007. A340-28-4078 01 January 25, 2007. A340-28-4097, including Appendix 01 03 July 3, 2007. A340-28-4107, excluding Appendix 01 01 December 14, 2005. A340-28-4118 02 July 10, 2007. A340-55-4017 02 March 16, 2007. Material Incorporated by Reference (i) You must use the service information specified in Table 4 of this AD to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Airbus SAS—Airworthiness Office—EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; fax +33 5 61 93 45 80, e-mail airworthiness.A330-A340@airbus.com; Internet http://www.airbus.com. (3) You may review copies of the service information that is incorporated by reference at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (4) You may also review copies of the service information at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Table 4—Material Incorporated by Reference Airbus Mandatory Service Bulletin Revision level Date A330-28-3082, including Appendix 1 05 May 27, 2008. A330-28-3092, excluding Appendix 01 01 December 14, 2005. A330-28-3101 01 October 11, 2006. A330-55-3016 02 March 16, 2007. A340-28-4073 02 March 8, 2007. A340-28-4078 01 January 25, 2007. A340-28-4097, including Appendix 01 03 July 3, 2007. A340-28-4107, excluding Appendix 01 01 December 14, 2005. A340-28-4118 02 July 10, 2007. A340-55-4017 02 March 16, 2007. Issued in Renton, Washington, on November 26, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-29076 Filed 12-10-08; 8:45 am] BILLING CODE 4910-13-P

Unless already done, do the actions in paragraphs (f)(1), (f)(2), (f)(3), (f)(4), and (f)(5) of this AD for the applicable airplanes identified in Table 1 of this AD. Table 1—Applicable Paragraphs by Model These airplane models— Except airplanes— Are affected by these paragraphs of this AD— Model A330, A340-200, and A340-330 airplanes On which Airbus Modification 47634 has been embodied in production (f)(1).   • On which both Airbus Modifications 49135 and 49630 have been embodied in production (f)(2)(i), except as provided by paragraphs (f)(2)(ii) and (f)(2)(iii) of this AD.   • Both Airbus Modifications 51825 and 55118 have been embodied in production   • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A330-28-3082, Revision 04, including Appendix 01, dated August 3, 2007, or Revision 05, including Appendix 1, dated May 27, 2008; and Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006   • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007; and Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007 Model A330 airplanes on which the actions specified in Airbus Service Bulletin A330-28-3082, dated June 14, 2004, have been accomplished before the effective date of this AD; and Model A340-200 and A340-300 airplanes on which the actions specified in Airbus Service Bulletin A340-28-4097, dated June 14, 2004, Revision 01, dated March 3, 2005, or Airbus Mandatory Service Bulletin A340-28-4097, Revision 02, dated August 16, 2006, have been accomplished before the effective date of this AD • On which both Airbus Modifications 49135 and 49630 have been embodied in production • Both Airbus Modifications 51825 and 55118 have been embodied in production • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A330-28-3082, Revision 04, including Appendix 01, dated August 3, 2007, or Revision 05, including Appendix 1, dated May 27, 2008; and Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006 (f)(2)(ii) and (f)(2)(iii).   • That have been modified in-service in accordance with both Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007, and Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007 Model A340-200 and A340-300 airplanes that have the ACT embodied in production or in service (Airbus Modification 42612, 44002, or 44005) That have been modified in service by Airbus Mandatory Service Bulletin A340-28-4078, Revision 01, dated January 25, 2007 (f)(3). Model A340-200 and A340-300 airplanes • On which Airbus Modification 44252 has been embodied in production (f)(4)(i), except as provided by paragraph (f)(4)(ii) of this AD.   • That have been modified in-service in accordance with Airbus Service Bulletin A340-55-4017, dated August 20, 1996; Revision 1, dated February 12, 2007; or Revision 02, dated March 16, 2007 Model A330-301, -321, -322, -341, -342 airplanes • On which Airbus Modification 44252 has been embodied in production (f)(4)(i), except as provided by paragraph (f)(4)(ii) of this AD.   • That have been modified in-service in accordance with Airbus Service Bulletin A330-55-3016, dated August 20, 1996; Revision 1 dated February 12, 1997; or Revision 02, dated March 16, 2007 Model A330-301, -321, -322, -341, -342 airplanes; and Model A340-200 and A340-300 airplanes On which the improvement of the THS lightning strike protection has already been performed before the effective date of this AD in accordance with Airbus A330/A340 All Operators Telex 55-03, dated August 22, 1996 (“solution A”), mandated by Direction Générale de l'Aviation Civile (DGAC) Airworthiness Directive F-1996-178-049(B) R1, and DGAC Airworthiness Directive F-1996-177-038(B), with a compliance time of November 15, 1996 (f)(4)(ii). Model A340-200 and A340-300 airplanes • On which Airbus Modification 46142 has been embodied in production (f)(5).   • That have been modified in-service in accordance with Airbus Mandatory Service Bulletin A340-28-4073, Revision 02, dated March 8, 2007 (1) Within 24 months after the effective date of this AD, do a detailed visual inspection of the P-clips in the wings and center fuel tanks, and apply the applicable corrective actions, in accordance with the applicable instructions of Airbus Mandatory Service Bulletin A330-28-3092, Revision 01, dated December 14, 2005; or Airbus Mandatory Service Bulletin A340-28-4107, Revision 01, dated December 14, 2005. (2) Do the requirements of paragraphs (f)(2)(i), (f)(2)(ii), and (f)(2)(iii) of this AD, as applicable, at the times specified in those paragraphs. (i) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 24 months after the effective date of this AD, modify the electrical bonding of the equipment installed in fuel tanks, in accordance with both Airbus Mandatory Service Bulletin A330-28-3082, Revision 05, including Appendix 1, dated May 27, 2008, and Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006; or both Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007, and Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007; as applicable. (ii) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 24 months after the effective date of this AD, modify the electrical bonding of the equipment installed in fuel tanks, in accordance with Airbus Mandatory Service Bulletin A330-28-3101, Revision 01, dated October 11, 2006; or Airbus Mandatory Service Bulletin A340-28-4118, Revision 02, dated July 10, 2007; as applicable. (iii) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 48 months after the effective date of this AD, do the additional work specified in Airbus Mandatory Service Bulletin A330-28-3082, Revision 05, including Appendix 1, dated May 27, 2008; or Airbus Mandatory Service Bulletin A340-28-4097, Revision 03, including Appendix 01, dated July 3, 2007; in accordance with the accomplishment instructions of those service bulletins, as applicable. (3) Within 24 months after the effective date of this AD, modify the electrical bonding in the ACT in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A340-28-4078, Revision 01, dated January 25, 2007. (4) Within 24 months after the effective date of this AD, do the requirements of paragraphs (f)(4)(i) and (f)(4)(ii), as applicable. (i) For airplanes affected by this paragraph, as specified in Table 1 of this AD: Within 24 months after the effective date of this AD, increase the distance between metallic parts on the THS trim tank in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A330-55-3016, Revision 02, March 16, 2007; or Airbus Mandatory Service Bulletin A340-55-4017, Revision 02, dated March 16, 2007; as applicable. (ii) For airplanes affected by this paragraph, as specified in Table 1 of this AD: At the first THS removal from the aircraft done for any reason after the effective date of this AD (e.g., fuselage stress jacking, and repair) when the airplane is on a support tool (lifting and resting point fittings must be installed), or at the time of the first maintenance task that requires the use of THS lifting and resting point fittings, whichever occurs earlier, increase the distance between metallic parts on the THS trim tank in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A330-55-3016, Revision 02, March 16, 2007; or Airbus Mandatory Service Bulletin A340-55-4017, Revision 02, dated March 16, 2007; as applicable. (5) Within 24 months after the effective date of this AD, install a bonding lead between the bonding tags on the jettison valve actuator and drive assembly in accordance with the instructions of Airbus Mandatory Service Bulletin A340-28-4073, Revision 02, dated March 8, 2007. (6) Actions done before the effective date of this AD in accordance with the service bulletins listed in Table 2 of this AD are acceptable for compliance with the corresponding requirements of this AD. Table 2—Credit Service Bulletins Airbus Service information Revision level Date Corresponding paragraphs Mandatory Service Bulletin A330-28-3082 02 August 11, 2006 (f)(2)(i) of this AD. Mandatory Service Bulletin A330-28-3082 03 November 15, 2006 (f)(2)(i) and (f)(2)(iii) of this AD. Mandatory Service Bulletin A330-28-3082 04 August 3, 2007 (f)(2)(i) and (f)(2)(iii) of this AD. Mandatory Service Bulletin A330-28-3101 Original June 5, 2006 (f)(2)(i) and (f)(2)(ii) of this AD. Mandatory Service Bulletin A340-28-4118 Original June 5, 2006 (f)(2)(i) and (f)(2)(ii) of this AD. Mandatory Service Bulletin A340-28-4118 01 October 11, 2006 (f)(2)(i) and (f)(2)(ii) of this AD. Service Bulletin A330-28-3082 01 March 2, 2005 (f)(2)(i) of this AD. Service Bulletin A330-55-3016 Original August 20, 1996 (f)(4)(i) and (f)(4)(ii) of this AD. Service Bulletin A330-55-3016 1 February 12, 1997 (f)(4)(i) and (f)(4)(ii) of this AD. Service Bulletin A340-28-4073 Original May 14, 1998 (f)(5) of this AD. Service Bulletin A340-28-4073 01 October 9, 1998 (f)(5) of this AD. Service Bulletin A340-28-4078 Original March 17, 2000 (f)(3) of this AD. Service Bulletin A340-55-4017 Original August 20, 1996 (f)(4)(i) and (f)(4)(ii) of this AD. Service Bulletin A340-55-4017 1 February 12, 1997 (f)(4)(i) and (f)(4)(ii) of this AD. FAA AD Differences Note 1: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, ANM-116, International Branch, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Tim Backman, Aerospace Engineer, ANM-116, International Branch, Transport Airplane Directorate, FAA, 1601 Lind Ave. SW., Renton, Washington, 98057-3356, telephone (425) 227-2797; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056. Related Information (h) Refer to MCAI European Aviation Safety Agency (EASA) Airworthiness Directive 2007-0278, dated November 5, 2007 [Corrected: November 8, 2007], and the service bulletins in Table 3 of this AD, for related information. Table 3—Related Service Bulletins Airbus Mandatory Service Bulletin Revision level Date A330-28-3082, including Appendix 1 05 May 27, 2008. A330-28-3092, excluding Appendix 01 01 December 14, 2005. A330-28-3101 01 October 11, 2006. A330-55-3016 02 March 16, 2007. A340-28-4073 02 March 8, 2007. A340-28-4078 01 January 25, 2007. A340-28-4097, including Appendix 01 03 July 3, 2007. A340-28-4107, excluding Appendix 01 01 December 14, 2005. A340-28-4118 02 July 10, 2007. A340-55-4017 02 March 16, 2007. Material Incorporated by Reference (i) You must use the service information specified in Table 4 of this AD to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Airbus SAS—Airworthiness Office—EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; fax +33 5 61 93 45 80, e-mail airworthiness.A330-A340@airbus.com; Internet http://www.airbus.com. (3) You may review copies of the service information that is incorporated by reference at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (4) You may also review copies of the service information at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call (202) 741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Table 4—Material Incorporated by Reference Airbus Mandatory Service Bulletin Revision level Date A330-28-3082, including Appendix 1 05 May 27, 2008. A330-28-3092, excluding Appendix 01 01 December 14, 2005. A330-28-3101 01 October 11, 2006. A330-55-3016 02 March 16, 2007. A340-28-4073 02 March 8, 2007. A340-28-4078 01 January 25, 2007. A340-28-4097, including Appendix 01 03 July 3, 2007. A340-28-4107, excluding Appendix 01 01 December 14, 2005. A340-28-4118 02 July 10, 2007. A340-55-4017 02 March 16, 2007. Issued in Renton, Washington, on November 26, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8-29076 Filed 12-10-08; 8:45 am] BILLING CODE 4910-13-P