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federal_register: 2010-31992

All Federal Register documents (rules, proposed rules, notices, presidential documents) from 1994 to present.

Data license: Public Domain (U.S. Government data) · Data source: Federal Register API & Regulations.gov API

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document_number title type abstract publication_date pub_year pub_month html_url pdf_url agency_names agency_ids excerpts
2010-31992 Airworthiness Directives; The Boeing Company Model 747-200C, -200F, -400, -400D, and -400F Series Airplanes Rule The FAA is superseding an existing airworthiness directive (AD), which applies to certain Model 747-200C, -200F, -400, -400D, and -400F series airplanes. That AD currently requires repetitive inspections for cracks in the overlapping (upper) skin of the upper fastener row of the lap joints of the fuselage skin in sections 41, 42, and 46; and related investigative and corrective actions, if necessary. This new AD expands the inspection area in the existing AD, and adds a modification of certain lap joints and certain post-repair inspections of the lap joints. Accomplishing the modification would end the repetitive inspections required by the existing AD for the length of lap joint that is modified. This AD results from a structural review of affected skin lap joints for widespread fatigue damage. We are issuing this AD to prevent fatigue cracking in certain lap joints, which could result in rapid depressurization of the airplane. 2010-12-28 2010 12 https://www.federalregister.gov/documents/2010/12/28/2010-31992/airworthiness-directives-the-boeing-company-model-747-200c--200f--400--400d-and--400f-series https://www.govinfo.gov/content/pkg/FR-2010-12-28/pdf/2010-31992.pdf Transportation Department; Federal Aviation Administration 492,159 The FAA is superseding an existing airworthiness directive (AD), which applies to certain Model 747-200C, -200F, -400, -400D, and -400F series airplanes. That AD currently requires repetitive inspections for cracks in the overlapping (upper) skin of...

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