Airworthiness Directives; Boeing Model 747-100, -100B, -100B SUD, -200B, and -300 Series Airplanes; and Model 747SR and 747SP Series Airplanes
airworthiness · Rule · Final rule. · Published 2005-03-21 · Effective 2005-04-25 · 70 FR 13353
Document
Document number
05-5386
Federal Register citation
70 FR 13353
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-03-21
Effective date
2005-04-25
FAA docket
Docket No. FAA-2004-19495
Abstract
The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747-100, -100B, -100B SUD, -200B, and -300 series airplanes; and Model 747SR and 747SP series airplanes. That AD currently requires repetitive inspections to detect fatigue cracking in the upper deck floor beams located at certain body stations, and repair, if necessary. This new AD lowers the threshold for the existing inspections and requires new repetitive inspections of previously repaired areas, and repair if necessary. This AD is prompted by the results of an additional detailed analysis that indicate fatigue cracks can initiate sooner than has previously been observed. We are issuing this AD to prevent failure of the upper deck floor beams at certain body stations due to fatigue cracking, which could result in rapid decompression and reduced controllability of the airplane.