Airworthiness Directives; Boeing Model 747-200B, -200C, -200F, and -400F Series Airplanes
airworthiness · Rule · Final rule. · Published 2005-04-19 · Effective 2005-05-24 · 70 FR 20273
Document
Document number
05-7683
Federal Register citation
70 FR 20273
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-04-19
Effective date
2005-05-24
FAA docket
Docket No. FAA-2005-20136
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747 series airplanes. This AD requires repetitive detailed inspections for cracks in the crease beam and adjacent structure of the fuselage, and related investigative and corrective actions if necessary. This AD is prompted by fatigue cracks found in the crease beam during a follow-on inspection of a previously installed modification. We are issuing this AD to find and fix fatigue cracking of the fuselage frame, which could result in reduced structural integrity of the frame and consequent rapid decompression of the airplane.