Airworthiness directives › 2006-02-01
AD 2006-02-01 Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, Model A340-200 and -300 Series Airplanes, and Model A340-541 and A340-642 Airplanes
Models named: A330-201, -202, -203, -223, -243, -301, -321, -322, -323, -341. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to all Airbus Model A330-201, -202, -203, -223, -243, -301, -321, -322, -323, -341, -342, and -343 airplanes; and Model A340-211, -212, -213, -311, -312, -313, -541, and -642 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. Airplane Flight Manual (AFM) Revision (f) Within 10 days after the effective date of this AD, revise the Limitations section of the A330/A340 AFM to include the information in the applicable temporary revision (TR) listed in Table 1 of this AD. Thereafter, operate the airplane according to the limitations and procedures in the applicable TR. Table 1.—Airbus AFM Temporary Revisions Affected airplane models/series AFM TR TR approval date A330-201, -202, -203, -223, and -243 airplanes 4.02.00/31 October 19, 2005. A330-301, -321, -322, -323, -341, -342, and -343 airplanes 4.02.00/32 October 19, 2005. A340-211, -212, -213, -311, -312, and -313 airplanes 4.02.00/46 October 19, 2005. A340-541 airplanes 4.02.00/48 October 19, 2005. A340-642 airplanes 4.02.00/47 October 19, 2005. Note 1: The action required by paragraph (f) of this AD may be done by inserting into the AFM a copy of the applicable TR listed in Table 1 of this AD. When this TR has been included in the general revisions of the AFM, the general revisions may be inserted into the AFM, provided the relevant information in the general revision is identical to that in the applicable TR listed in Table 1 of this AD. Alternative Methods of Compliance (AMOCs) (g)(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 (h) French airworthiness directives F-2005-195 and F-2005-196, both dated December 7, 2005, also address the subject of this AD. Material Incorporated by Reference (i) You must use the documents listed in Table 2 of this AD to perform the actions that are required by this AD, unless the AD specifies otherwise. (The TR approval date is identified only on the first page of each TR; no other page of these documents contains the approval date.) The Director of the Federal Register approved the incorporation by reference of these documents 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_federal_regulations/ibr_locations.html . Table 2.—Material Incorporated by Reference Airbus temporary revisions to the Airbus A330/A340 airplane flight manual Temporary revision approval date 4.02.00/31 October 19, 2005. 4.02.00/32 October 19, 2005. 4.02.00/46 October 19, 2005. 4.02.00/47 October 19, 2005. 4.02.00/48 October 19, 2005. Issued in Renton, Washington, on January 9, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06-450 Filed 1-18-06; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD results from a determination that, once a fuel leak is detected, fuel management procedures are a critical factor in limiting the consequences of the leak. We are issuing this AD to ensure that the flightcrew, in the event of a fuel leak, is advised of appropriate procedures to follow, such as isolating the fuel tanks, stopping any fuel transfers, and landing as soon as possible. Failure to follow these procedures could result in excessive fuel loss that could cause the engines to shut down during flight.
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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