Airworthiness directives › 2005-20-10
AD 2005-20-10 Airworthiness Directives; Airbus Model A330-243, -341, -342, and -343 Airplanes
Models named: A330-243, -341, -342, -343. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Airbus Model A330-243, -341, -342, and -343 airplanes, certificated in any category.
Compliance
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. AFM Revision (f) Within 10 days after the effective date of this AD, revise the Normal Procedures section of the Airbus A330 Airplane Flight Manual (AFM) by inserting a copy of Airbus Temporary Revision (TR) 4.03.00/24, dated April 2, 2004, into the AFM. (g) When the information in Airbus TR 4.03.00/24, dated April 2, 2004, is included in the general revisions of the AFM, the general revisions may be inserted in the AFM, and this TR may be removed. Alternative Methods of Compliance (AMOCs) (h)(1) The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (i) French airworthiness directive F-2004-081, dated June 9, 2004, also addresses the subject of this AD. Material Incorporated by Reference (j) You must use Airbus Temporary Revision 4.03.00/24, dated April 2, 2004, to the Airbus A330 Airplane Flight Manual to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of this document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the 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 September 20, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-19436 Filed 10-3-05; 8:45 am] BILLING CODE 4910-13-U
Unsafe condition
This AD results from reports of damage to the engine blades of the first stage of the intermediate pressure compressor due to ice accumulation. We are issuing this AD to prevent engine damage due to ice accumulation, which could result in an engine shutdown and cause the flightcrew to divert to the nearest available airport.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1