# Airworthiness Directives; Boeing Model 747 Airplanes
> **Rule** · Final rule. · Published 2006-10-27 · Effective 2006-12-01 · 71 FR 62904
## Document
- **Document number:** E6-17941
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 747
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 62904
- **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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/10/27/E6-17941/airworthiness-directives-boeing-model-747-airplanes)
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