# Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR Series Airplanes
> **Rule** · Final rule. · Published 2006-12-07 · Effective 2006-06-07 · 71 FR 70857
## Document
- **Document number:** E6-20618
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 70857
- **Publication date:** 2006-12-07
- **Effective date:** 2006-06-07
- **FAA docket:** Docket No. FAA-2006-25327
## Abstract

The FAA is revising an existing airworthiness directive (AD) that applies to certain Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR series airplanes. That AD currently requires repetitive inspections to detect cracking of certain lower lobe fuselage frames, and repair if necessary. This new AD specifies appropriate service information for certain corrective actions. This AD results from reports indicating that fatigue cracks were found in lower lobe frames on the left side of the fuselage. We are issuing this AD to detect and correct fatigue cracking of certain lower lobe fuselage frames, which could lead to fatigue cracks in the fuselage skin, and consequent rapid decompression of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/12/07/E6-20618/airworthiness-directives-boeing-model-747-100-747-100b-747-100b-sud-747-200b-747-300-747-400)
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