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Airworthiness directives › 2004-06-02

AD 2004-06-02 Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes

2004-04-22
2004-03-18
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Airframe
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Models named: A319, A320, A321 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model A319, A320, and A321 series airplanes; certificated in any category; on which Airbus Modification 30821 has not been accomplished.

Compliance

Required as indicated, unless accomplished previously. To prevent failure of a lower guide rod fitting, which could cause a rear passenger door to jam during opening, delaying an emergency evacuation and resulting in injury to passengers or crew members, accomplish the following: Replacement (a) Within 22 months after the effective date of this AD, replace the lower guide rod fitting on each rear passenger door with an improved fitting by doing all actions in and per the Accomplishment Instructions of Airbus Service Bulletin A320-53-1154, Revision 2, dated March 7, 2003. Replacements Accomplished Previously (b) Replacements of the lower guide rod fitting accomplished before the effective date of this AD per the Accomplishment Instructions of Airbus Service Bulletin A320-53-1154, dated July 12, 2001; or Revision 1, dated August 28, 2002; are acceptable for compliance with the corresponding action required by this AD. Alternative Methods of Compliance (c) In accordance with 14 CFR 39.19, the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, is authorized to approve alternative methods of compliance for this AD. Incorporation by Reference (d) Unless otherwise specified in this AD, the actions shall be done in accordance with Airbus Service Bulletin A320-53-1154, Revision 2, dated March 7, 2003. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Note 1: The subject of this AD is addressed in French airworthiness directive 2001-634(B), dated December 26, 2001. Effective Date (e) This amendment becomes effective on April 22, 2004. Issued in Renton, Washington, on March 9, 2004. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-5847 Filed 3-17-04; 8:45 am] BILLING CODE 4910-13-P

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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