Airworthiness directives › 2008-01-01
AD 2008-01-01 Airworthiness Directives; The Boeing Company Model 737-200, -300, -400, -500, -600, -700, -800, and -900 Series Airplanes; Model 747-400 Series Airplanes; Model 757-200 and 757-300 Series Airplanes; Model 767-200, 767-300, and 767-400ER Series Airplanes; and Model 777-200 Series Airplanes
Applicability*9
This AD applies to The Boeing Company airplanes identified in Table 1 of this AD, certificated in any category. Table 1—Applicability Model— Modified in accordance with Supplemental Type Certificate— As identified in Jamco Service Bulletin— (1)737-200, -300, -400, -500, -600, -700, -800, and -900 series airplanes ST01143SE 52-2295, Revision 1, dated October 10, 2007. (2) 747-400 series airplanes ST01194SE 52-2303, Revision 1, dated October 10, 2007. (3) 757-200 and -300 series airplanes ST01150SE 52-2304, Revision 2, dated November 1, 2007. (4) 767-200, -300, and -400ER series airplanes ST01121SE 52-2302, Revision 1, dated October 10, 2007. (5) 777-200 series airplanes ST01201SE 52-2305, Revision 1, dated October 10, 2007.
Compliance
Comply with this AD within the compliance times specified, unless already done. Replacement (g) Within 30 days after the effective date of this AD, replace a certain flight deck door feature and revise the modification record placard, in accordance with the Accomplishment Instructions of the applicable service bulletin identified in Table 1 of this AD. (h) Actions done before the effective date of this AD in accordance with Jamco Service Bulletin 52-2304, Revision 1, dated October 10, 2007, are acceptable for compliance with the corresponding requirements of paragraph (g) of this AD. Alternative Methods of Compliance (AMOCs) (i)(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 FR 39.19. Send information to Attn: Patrick Gillespie, 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) 917-6429; fax (425) 917-6590. Information may be e-mailed 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 (j) You must use the applicable service information contained in Table 2 of this AD 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 Jamco America, Inc., 1018 80th Street SW., Everett, WA 98203; telephone 425-347-4735, ext: 1192 (David Crotty); fax 425-353-2343; e-mail David_Crotty@jamco-america.com ; Internet http://jamco-america.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. (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. Table 2—Material Incorporated by Reference Document Revision Date Jamco Service Bulletin 52-2295 1 October 10, 2007. Jamco Service Bulletin 52-2302 1 October 10, 2007. Jamco Service Bulletin 52-2303 1 October 10, 2007. Jamco Service Bulletin 52-2304 2 November 1, 2007. Jamco Service Bulletin 52-2305 1 October 10, 2007. Issued in Renton, Washington, on June 18, 2010. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010-15655 Filed 6-30-10; 8:45 am] BILLING CODE 4910-13-P
Unsafe condition
This AD results from a report indicating that a feature of the flight deck door is defective. We are issuing this AD to prevent failure of this feature, which could jeopardize flight safety.
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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