Airworthiness Directives; Boeing Model 747 Airplanes
airworthiness · Rule · Final rule. · Published 2006-10-27 · Effective 2006-12-01 · 71 FR 62904
Document
Document number
E6-17941
Federal Register citation
71 FR 62904
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747
Publication date
2006-10-27
Effective date
2006-12-01
FAA docket
Docket No. FAA-2006-24119
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747 airplanes. This AD requires repetitive mid- and low-frequency eddy current inspections for cracks in the overlapped skin panels in the fuselage skin lap joints in sections 41, 42, 44, and 46, and corrective actions if necessary. This AD results from a report indicating that an operator found multiple small cracks in the overlapped skin panels in the fuselage skin lap joints. We are issuing this AD to detect and correct cracks in the overlapped skin panels, which could join together and result in reduced structural capability in the skin and consequent rapid decompression of the airplane.