Airworthiness Directives; Boeing Model 747 Airplanes
airworthiness · Rule · Final rule. · Published 2009-05-07 · Effective 2009-06-11 · 74 FR 21249
Document
Document number
E9-9925
Federal Register citation
74 FR 21249
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747
Publication date
2009-05-07
Effective date
2009-06-11
FAA docket
Docket No. FAA-2008-1239
Abstract
We are adopting a new airworthiness directive (AD) for certain Boeing Model 747 airplanes. This AD requires repetitive external surface high frequency eddy current inspections to detect cracks in the radius detail of the upper lobe doubler on both sides of the airplane, and applicable corrective action. This AD results from reports of cracks in the radius detail of the upper lobe doublers. We are issuing this AD to detect and correct cracks in the upper lobe doublers. Such cracks could result in significant degradation of the fuselage structure and reduce its ability to carry flight loads from the vertical stabilizer, which could adversely affect the controllability of the airplane.