AD 2011-17-09 Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes

Models named: A330-201, -202, -203, -223, -223F, -243, -243F, A330-301, -302, -303. Read the applicability below — it usually turns on serial or part numbers too.

This AD applies to Airbus Model A330-201, -202, -203, -223, -223F, -243, and -243F airplanes, and Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes, certificated in any category, all manufacturer serial numbers. Note 1: This AD requires revisions to certain operator maintenance documents to include new inspections. Compliance with these inspections is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (j)(1) of this AD. The request should include a description of changes to the required inspections that will ensure the continued operational safety of the airplane.

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Restatement of Requirements of Paragraph (f)(2) of AD 2006-09-07: Airworthiness Limitations Revision (g) For Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes: Within 3 months after June 7, 2006 (the effective date of AD 2006-09-07 (71 FR 25919, May 3, 2006)), revise the ALS of the Instructions for Continued Airworthiness by incorporating Section 9-1 “Life limit/Monitored parts,” Revision 05, dated April 7, 2005, of the Airbus A330 Maintenance Planning Document, into the ALS. New Requirements of This AD Revise the Maintenance Program (h) Within 3 months after the effective date of this AD: Revise the maintenance program by incorporating Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 05, dated July 29, 2010. Comply with all Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 05, dated July 29, 2010, at the times specified therein. Accomplishing the revision in this paragraph ends the requirements in paragraph (g) of this AD. Alternative Intervals or Limits (i) Except as provided by paragraph (j)(1) of this AD, after accomplishing the actions specified in paragraph (h) of this AD, no alternatives to the maintenance tasks, intervals, or limitations specified in paragraph (h) of this AD may be used. FAA AD Differences Note 2: This AD differs from the MCAI and/or service information as follows: (1) Although the applicability in the MCAI also identifies Airbus Model A340-200, -300, -500, and -600 series airplanes, this AD only applies to Airbus Model A330-200 and -300 series airplanes. FAA AD 2011-04-06, Amendment 39-16606 (76 FR 8610, February 15, 2011), addresses Model A340-200, -300, -500, and -600 series airplanes. (2) The applicability in the MCAI does not specify Model A330-223F and -243F airplanes. Those models are listed in the applicability of this AD. (3) The MCAI requires incorporating Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 04, dated January 28, 2010; however, this AD requires incorporating Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 05, dated July 29, 2010, which adds the airworthiness limitation items for Model A330-223F and -243F airplanes. Other FAA AD Provisions (j) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1138; fax (425) 227-1149. Information may be e-mailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov . Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD. (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. Related Information (k) Refer to MCAI EASA Airworthiness Directive 2010-0253, dated December 3, 2010; Section 9-1 “Life limit/Monitored parts” Revision 05, dated April 7, 2005, of the Airbus A330 Maintenance Planning Document; and Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 05, dated July 29, 2010; for related information. Material Incorporated by Reference (l) You must use Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 05, dated July 29, 2010; and Airbus A330 ALS Section 9-1 “Life limit/Monitored parts” Revision 05, dated April 7, 2005, of the Airbus A330 Maintenance Planning Document; as applicable; to do the actions required by this AD, unless the AD specifies otherwise. The revision level of Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 05, dated July 29, 2010, is indicated only on the title page and in the Record of Revisions of this document; the revision date of this document is not indicated on the title page of this document. (1) The Director of the Federal Register approved the incorporation by reference of Airbus A330 ALS Part 1, “Safe Life Airworthiness Limitation Items,” Revision 05, dated July 29, 2010, under 5 U.S.C. 552(a) and 1 CFR part 51. (2) The Director of the Federal Register previously approved the incorporation by reference of Section 9-1 “Life limit/Monitored parts,” Revision 05, dated April 7, 2005, of the Airbus A330 Maintenance Planning Document, on June 7, 2006 (71 FR 25919, May 3, 2006). (3) For service information identified in this AD, contact Airbus SAS—Airworthiness Office—EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80, e-mail airworthiness.A330-A340@airbus.com; Internet http://www.airbus.com. (4) You may review copies of the service information 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. (5) You may also review copies of the service information that is incorporated by reference 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/ code_of_federal_regulations/ibr_locations.html. Issued in Renton, Washington, on August 2, 2011. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2011-21625 Filed 8-25-11; 8:45 am] BILLING CODE 4910-13-P