AD 2009-19-06

Active

Unsafe Condition

Key Information
2009-19-06
Active
October 12, 2010
September 23, 2010
FAA-2010-0950
39-16460
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
747-100 Series 747-100B Series 747-100B SUD Series 747-200B Series 747-200F Series 747-300 Series 747-400 Series 747-400D Series 747SP Series 747SR Series
Summary

This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) 2009-19-06 that was sent previously by individual notices to the known U.S. owners and operators of affected airplanes identified above. This AD requires installing certain equipment on the flight deck door. This AD was prompted by reports that the current design of the flight deck door is defective. We are issuing this AD to prevent failure of this equipment, which could jeopardize flight safety.

Action Required

Final rule; request for comments.

Regulatory Text

2009-19-06 The Boeing Company: Amendment 39-16460. Docket No. FAA- 2010-0950; Directorate Identifier 2009-NM-194-AD. \n\nEffective Date \n\n\t(a) This AD becomes effective October 12, 2010, to all persons except those persons to whom it was made immediately effective by AD 2009-19-06, issued on September 9, 2009, which contained the requirements of this amendment. \n\nAffected ADs \n\n\t(b) None. \n\nApplicability \n\n\t(c) This AD applies to Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200F, 747-300, 747-400, 747-400D, 747SP, and 747SR series airplanes, certificated in any category; as identified in Boeing Service Bulletin 747-52-2293, dated September 4, 2009. \n\nSubject \n\n\t(d) Air Transport Association (ATA) of America Code 52: Doors. \n\nUnsafe Condition \n\n\t(e) This AD was prompted by reports that the current design of the flight deck door is defective. We are issuing this AD to prevent failure of this equipment, which could jeopardize flight safety. \n\nCompliance(f) Comply with this AD within the compliance times specified, unless already done. \n\nDoor Equipment Installation \n\n\t(g) Within 30 days after the effective date of this AD, install certain equipment associated with the flight deck door, in accordance with Boeing Service Bulletin 747-52-2293, dated September 4, 2009. \n\nAlternative Methods of Compliance (AMOCs) \n\n\t(h)(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 Robert Kaufman, 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) 917-6433; fax (425) 917-6590. Or e-mail information to 9-ANM- Seattle-ACO-AMOC-Requests@faa.gov. \n\n\t(2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR39.19. 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 refer to this AD. \n\nIncorporation by Reference \n\n\t(i) You must use Boeing Service Bulletin 747-52-2293, dated September 4, 2009, to do the actions required by this AD, unless the AD specifies otherwise. \n\n\t(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. \n\n\t(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. \n\n\t(3) You mayreview 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. \n\n\t(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.

Supplementary Information

On September 9, 2009, we issued AD 2009-19- 06, which applies to certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200F, 747-300, 747-400, 747-400D, 747SP, and 747SR series airplanes. \n\nBackground \n\n\tWe have received a report indicating that the current design of the flight deck door is defective. This condition, if not corrected, could jeopardize flight safety. \n\nRelevant Service Information \n\n\tWe reviewed Boeing Service Bulletin 747-52-2293, dated September 4, 2009. The service bulletin describes procedures for installing certain equipment associated with the flight deck door. \n\nFAA's Determination and Requirements of This AD \n\n\tSince the unsafe condition described is likely to exist or develop on other airplanes of the same type design, we issued AD 2009-19-06 to prevent failure of the flight deck door, which could jeopardize flight safety. The AD requires accomplishing the actions specified in the service information previously described. \n\n\tWe have determined that notice and opportunity for prior public comment on AD 2009-19-06 were contrary to the public interest, and good cause existed to make the AD effective immediately by individual notices issued on September 9, 2009, to the known U.S. owners and operators of certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747- 200B, 747-200F, 747-300, 747-400, 747-400D, 747SP, and 747SR series airplanes. These conditions still exist, and the AD is hereby published in the Federal Register as an amendment to section 39.13 of the Federal Aviation Regulations (14 CFR 39.13) to make it effective to all persons. \n\nComments Invited \n\n\tThis AD is a final rule that involves requirements affecting flight safety, and we did not provide you with notice and an opportunity to provide your comments before it becomes effective. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSESsection. Include "Docket No. FAA-2010-0950; Directorate Identifier 2009-NM-194-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD because of those comments. \n\n\tWe will post all comments we receive, without change, to http:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. \n\nAuthority for This Rulemaking \n\n\tTitle 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII, Aviation Programs, describes in more detail the scope of the Agency's authority. \n\n\tWe are issuing this rulemaking under the authority described in subtitle VII, part A, subpart III, section44701, "General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. \n\nRegulatory Findings \n\n\tThis AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. \n\n\tFor the reasons discussed above, I certify that this AD: \n\n\t(1) Is not a "significant regulatory action'' under Executive Order 12866, \n\n\t(2) Is not a "significant rule'' under DOT Regulatory Policies and Procedures(44 FR 11034, February 26, 1979), and \n\n\t(3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. \n\n\tYou can find our regulatory evaluation and the estimated costs of compliance in the AD Docket. \n\nList of Subjects in 14 CFR Part 39 \n\n\tAir transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. \n\nAdoption of the Amendment \n\nAccordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n1. The authority citation for part 39 continues to read as follows: \n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\nSec. 39.13 (Amended) \n\n2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD):

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Contact Information

Robert Kaufman, Aerospace Engineer, Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle ACO, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 917-6433; fax (425) 917-6590.

References
(Federal Register: October 7, 2010 (Volume 75, Number 194))
--- - Part 39
(Page 61985-61987)
FAA Documents