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Airworthiness directives › 2005-20-17

AD 2005-20-17 Airworthiness Directives; Airbus Model A319-100 Series Airplanes; Model A320-111 Series Airplanes; Model A320-200 Series Airplanes; and Model A321-100 and -200 Series Airplanes

2005-11-09
2005-10-05
39-14311
FAA-2005-20874
Airframe
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Models named: A319-111, -112, -113, -114, -115, -131, -132, -133, A320-111, -211. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211 and -231 airplanes; certificated in any category; except those modified in production by Airbus Modification 30062.

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. Modification (f) Within 52 months after the effective date of this AD: Modify the parking brake system by accomplishing all the actions specified in the Accomplishment Instructions of Airbus Service Bulletin A320-32-1201, Revision 02, dated February 1, 2005. Modifications Accomplished Per Previous Issue of Service Information (g) Modifications accomplished before the effective date of this AD in accordance with Airbus Service Bulletin A320-32-1201, Revision 01, dated May 29, 2002; are considered acceptable for compliance with the corresponding modification required by paragraph (f) of this AD. 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 14 CFR 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-2004-137, dated November 10, 2004, also addresses the subject of this AD. Material Incorporated by Reference (j) You must use Airbus Service Bulletin A320-32-1201, Revision 02, dated February 1, 2005, 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 26, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-19874 Filed 10-4-05; 8:45 am] BILLING CODE 4910-13-P

Unsafe condition

This AD was prompted by a report of failure of the parking brake while the airplane was on the holding point of the runway before takeoff, leading to a runway departure. We are issuing this AD to ensure normal braking is available to prevent possible runway departure in the event of failure of the parking brake.

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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