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Airworthiness directives › 2004-25-10

AD 2004-25-10 Airworthiness Directives; Boeing Model 767-300 and -400ER Series Airplanes

2005-01-13
2004-12-09
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Airframe
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Models named: 767-300 series, 767-400ER series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model 767-300 series airplanes, as listed in Boeing Alert Service Bulletin 767-38A0062, dated August 15, 2002; and Model 767-400ER series airplanes, as listed in Boeing Alert Service Bulletin 767-38A0063, dated August 15, 2002; certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To prevent failure of the main deck floor stanchions and consequent collapse of the main floor during an emergency landing, which could result in passenger injury and impede passenger evacuation from the airplane, accomplish the following: Replacement and Related Investigative and Corrective Actions and Retrofit Action (a) Within 18 months after the effective date of this AD: Replace the four tie rods for the waste tank cradle with new tie rods and do all applicable related investigative actions, corrective actions, and special retrofit actions by accomplishing all the actions in the Accomplishment Instructions of Boeing Alert Service Bulletins 767-38A0062 (for Model 767-300 series airplanes) and 767-38A0063 (for Model 767-400ER series airplanes), both dated August 15, 2002; as applicable. Do the actions in accordance with the applicable service bulletin except as provided by paragraph (b) of this AD. Accomplish any related investigative, corrective, or special retrofit action before further flight. (b) If any deformation, crack, or other damage is found during any related investigative action required by paragraph (a) of this AD, and the bulletin specifies contacting Boeing for appropriate action: Before further flight, perform the special retrofit action per a method approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA. For a retrofit method to be approved by the Manager, Seattle ACO, as required by this paragraph, the Manager's approval letter must specifically refer to this AD. Parts Installation (c) As of the effective date of this AD, no person may install any tie rod for the waste tank cradle having part number 251T0100-1401, 251T0100-1402, 251T0100-1403, or 251T0100-1404, on any airplane to which this AD applies. Alternative Methods of Compliance (d) In accordance with 14 CFR 39.19, the Manager, Seattle ACO, FAA, is authorized to approve alternative methods of compliance (AMOCs) for this AD. Incorporation by Reference (e) Unless otherwise specified in this AD, the actions shall be done in accordance with Boeing Alert Service Bulletin 767-38A0062, dated August 15, 2002; and Boeing Alert Service Bulletin 767-38A0063, dated August 15, 2002; as applicable. 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 Boeing Commercial Airplanes, PO Box 3707, Seattle, Washington 98124-2207. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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. Effective Date (f) This amendment becomes effective on January 13, 2005. Issued in Renton, Washington, on November 30, 2004. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 04-26917 Filed 12-8-04; 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