# Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-400F, 747SR, and 747SP Series Airplanes
> **Rule** · Final rule. · Published 2006-01-12 · Effective 2006-02-16 · 71 FR 1947
## Document
- **Document number:** 06-183
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 1947
- **Publication date:** 2006-01-12
- **Effective date:** 2006-02-16
- **FAA docket:** Docket No. FAA-2005-22289
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-100, 747-100B, 747-200B, 747-200C, 747-200F, 747-400F, 747SR, and 747SP series airplanes, without a stretched upper deck or stretched upper deck modification. This AD requires detailed and high-frequency eddy current inspections for cracks of each affected tension tie and of the surrounding structure, and related investigative and corrective actions if necessary. This AD results from a report of a crack in the tension tie at the body station 820 frame connection, and cracks found on the Boeing 747SR fatigue-test airplane in both the tension ties and frames at the tension tie to frame connections at body stations 800, 820, and 840. We are issuing this AD to find and fix cracks in the tension ties, which could lead to cracks in the skin and body frame and result in rapid in-flight depressurization of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/01/12/06-183/airworthiness-directives-boeing-model-747-100-747-100b-747-200b-747-200c-747-200f-747-400f-747sr-and)
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