Airworthiness directives › 2005-16-01
AD 2005-16-01 Airworthiness Directives; Boeing Model 747-200B, 747-300, 747-400, and 747-400D Series Airplanes
Models named: 747-200B, 747-300 series, 747-400, 747-400D series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to the Boeing airplanes, certificated in any category, specified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD. (1) Model 747-200B and 747-300 series airplanes identified in Boeing Special Attention Service Bulletin 747-53-2497, dated November 4, 2004. (2) Model 747-200B and 747-300 series airplanes on which Boeing Service Bulletins 747-25-2716, 747-25-2724, and 747-25-2784 have been done. (3) Model 747-400 and 747-400D series airplanes identified in Boeing Special Attention Service Bulletin 747-53-2481, dated October 24, 2002.
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. Model 747-200B and 747-300: Modification (f) Within 60 months after the effective date of this AD, modify the lateral shear beam for the Door 5 crew rest by accomplishing all of the actions specified in the Accomplishment Instructions of Boeing Special Attention Service Bulletin 747-53-2497, dated November 4, 2004. Model 747-400 and 747-400D: Modification and Replacement (g) Within 60 months after the effective date of this AD, modify the lateral shear beam for the Door 5 crew rest, replace the Zone E tie rods, and modify the Zone E stowbin ladder, by accomplishing all of the actions specified in the Accomplishment Instructions of Boeing Special Attention Service Bulletin 747-53-2481, dated October 24, 2002. Alternative Methods of Compliance (AMOCs) (h) The Manager, Seattle Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. Material Incorporated by Reference (i) You must use Boeing Special Attention Service Bulletin 747-53-2481, dated October 24, 2002; or Boeing Special Attention Service Bulletin 747-53-2497, dated November 4, 2004; as applicable, 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 these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207, 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 July 21, 2005. Kevin M. Mullin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-15017 Filed 8-1-05; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD was prompted by a report that the lateral shear beam for the Door 5 crew rest does not meet the 9G forward loading requirement. We are issuing this AD to prevent the structural support for the Door 5 crew rest and Zone E stowbins from failing, which could result in the crew rest or stowbins falling during an emergency and consequent injury to crew and passengers.
Read the original on the Federal Register →
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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