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70 FR 74641 - Airworthiness Directives; Boeing Model 777-200 and -300 Series Airplanes

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Publication TitleMouse over help for Publication Title says The title of the publication. Individual Federal Register documents can be searched using the title field operator. Search field operator example is title:california volume:73 issue:25. Federal Register Volume 70, Issue 241 (December 16, 2005)
CategoryMouse over help for Category says The category to which the collection belongs. Search field operator example is category:"regulatory information". Regulatory Information
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GS 4.107:
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SectionMouse over help for Section says The section under which the rule, notice, proposed rule, or presidential document was published. Search field operator example is section:prorule. Rules and Regulations
ActionMouse over help for Action says The action being taken by the agency such as proposed rule, notice, or request for comments, etc. Search field operator example is action:"reopening of comment period".Final rule.
DatesMouse over help for Dates says Full text field which identifies the dates important to the regulation, such as the effective date, deadlines for comments, etc. Search field operator example is dates:effective.This AD becomes effective January 20, 2006.
ContactMouse over help for Contact says Contact information for more information about the notice or rule. Search field operator example is contact:fax.Gary Oltman, Aerospace Engineer, Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 917-6443; fax (425) 917-6590.
SummaryMouse over help for Summary says Summary of the rule or notice. Search field operator example is summary:airworthiness.The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 777-200 and -300 series airplanes. This AD requires repetitive detailed inspections of the forward lugs of the power control unit (PCU), yoke assembly, and forward attachment hardware of the left inboard, left outboard, right inboard, and right outboard flaperon PCUs; and other specified/corrective actions if necessary. For certain airplanes, this AD also requires other related concurrent actions. This AD results from reports indicating that operators have found worn, fretted, and fractured bolts that attach the yoke assembly to the flaperon PCU. We are issuing this AD to prevent damage and eventual fracture of the yoke assembly, pin assembly, and attachment bolts that connect the inboard and outboard PCUs to a flaperon, which could lead to the flaperon becoming unrestrained and consequently departing from the airplane. Loss of a flaperon could result in asymmetric lift and reduced roll control of an airplane. A departing flaperon could also cause damage to the horizontal and vertical stabilizers, which could result in loss of control of the airplane if damage is significant.
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Federal Aviation Administration
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Federal Register CitationMouse over help for Federal Register Citation says The Federal Register citation in the form of (volume) FR (page number). Search field operator example is citation:"71 fr 65732". 70 FR 74641 
RIN NumberMouse over help for RIN Number says The Regulation ID number associated with the rule or notice. Search field operator example is rinnumber:"1290-AA23".2120-AA64
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Document in Context
This is part of Federal Register Volume 70, Issue 241 (December 16, 2005)
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