Airworthiness directives › 2010-05-11
AD 2010-05-11 Airworthiness Directives; The Boeing Company Model 747-100, 747-200B, 747-300, and 747SR Series Airplanes
Models named: 747-100, 747-200B, 747-300, 747SR series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to The Boeing Company Model 747-100, 747-200B, 747-300, and 747SR series airplanes, certificated in any category; as identified in Boeing Service Bulletin 747-25A3368, Revision 2, dated June 12, 2008. Note 1: The affected airplanes are those that have been converted by Boeing to the Boeing Special Freighter configuration.
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. Install the Closeout Panel and Moisture Curtains (g) Within 24 months after the effective date of this AD, install the closeout panel and moisture curtains for the main equipment center, by accomplishing all of the applicable actions specified in the Accomplishment Instructions of Boeing Service Bulletin 747-25A3368, Revision 2, dated June 12, 2008. Credit for Actions Done According to Previous Issue of the Service Bulletin (h) Actions done before the effective date of this AD in accordance with the Accomplishment Instructions in Boeing Alert Service Bulletin 747-25A3368, dated August 25, 2005, are acceptable for compliance with the corresponding actions required by paragraph (g) of this AD, provided that the additional work specified in the Accomplishment Instructions of Boeing Alert Service Bulletin 747-25A3368, Revision 1, dated June 25, 2007; or Revision 2, dated June 12, 2008; is accomplished. The additional work required is to cap seal all rivets fastening the mounting base assembly to the moisture shroud as given in Figure 10 in Boeing Alert Service Bulletin 747-25A3368, Revision 2, dated June 12, 2008, and to fill any unused pilot holes in the mounting base assembly in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 747-25A3368, Revision 2, dated June 12, 2008; or cap seal all rivets fastening the mounting base assembly to the moisture shroud as given in Figure 10 of Boeing Alert Service Bulletin 747-25A3368, Revision 1, dated June 25, 2007, and to fill any unused pilot holes in the mounting base assembly in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 747-25A3368, Revision 1, dated June 25, 2007. (i) Actions done before the effective date of this AD in accordance with Boeing Alert Service Bulletin 747-25A3368, Revision 1, dated June 25, 2007, are acceptable for compliance with the corresponding actions required by paragraph (g) of this AD. Alternative Methods of Compliance (AMOCs) (j)(1) The Manager, Seattle Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Marcia Smith, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 917-6484; fax (425) 917-6590. Or, e-mail information to 9-ANM-Seattle-ACO-AMOC-Requests@faa.gov. (2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. The AMOC approval letter must specifically reference this AD. Material Incorporated by Reference (k) You must use Boeing Service Bulletin 747-25A3368, Revision 2, dated June 12, 2008, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; telephone 206-544-5000, extension 1; fax 206-766-5680; e-mail me.boecom@boeing.com; Internet https://www.myboeingfleet.com. (3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (4) You may also review copies of the service information that is incorporated by reference 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. Issued in Renton, Washington, on February 25, 2010. Jeffrey E. Duven, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010-4650 Filed 3-8-10; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD results from a report of water contamination in the electrical and electronic units in the main equipment center. We are issuing this AD to prevent the malfunction of one or more electrical and electronic units in the main equipment center, which could adversely affect the airplane's continued safe 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