federal_register: 2015-30008

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document_number title type abstract publication_date pub_year pub_month html_url pdf_url agency_names agency_ids excerpts regulation_id_numbers
2015-30008 Airworthiness Directives; The Boeing Company Airplanes Proposed Rule We propose to supersede Airworthiness Directive (AD) 2011-23- 05, which applies to certain The Boeing Company Model 737-300, -400, and -500 series airplanes. AD 2011-23-05 currently requires repetitive inspections for cracking of the 1.04-inch nominal diameter wire penetration hole, and applicable related investigative and corrective actions. Since we issued AD 2011-23-05, an evaluation by the design approval holder (DAH) indicates that the fuselage frames and frame reinforcements are subject to widespread fatigue damage (WFD). This proposed AD would add new inspection areas, a modification that terminates certain inspections, post-modification inspections, and repair if necessary. We are proposing this AD to detect and correct fatigue cracking of the fuselage frames and frame reinforcements, which could result in reduced structural integrity of the airplane. 2015-11-27 2015 11 https://www.federalregister.gov/documents/2015/11/27/2015-30008/airworthiness-directives-the-boeing-company-airplanes https://www.govinfo.gov/content/pkg/FR-2015-11-27/pdf/2015-30008.pdf Transportation Department; Federal Aviation Administration 492,159 We propose to supersede Airworthiness Directive (AD) 2011-23- 05, which applies to certain The Boeing Company Model 737-300, -400, and -500 series airplanes. AD 2011-23-05 currently requires repetitive inspections for cracking of the 1.04-inch nominal... 2120-AA64

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