# Airworthiness Directives; Boeing Model 747 Series Airplanes
> **Rule** · Final rule. · Published 2004-12-23 · Effective 2005-01-27 · 69 FR 76839
## Document
- **Document number:** 04-27508
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 747 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 69 FR 76839
- **Publication date:** 2004-12-23
- **Effective date:** 2005-01-27
- **FAA docket:** Docket No. 2001-NM-179-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 747 series airplanes, that requires repetitive inspections for cracking of the top and side panel webs and panel stiffeners of the nose wheel well (NWW), and corrective actions if necessary. This action is necessary to detect and correct fatigue cracks in the top and side panel webs and stiffeners of the NWW, which could compromise the structural integrity of the NWW and could lead to the rapid depressurization of the airplane. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2004/12/23/04-27508/airworthiness-directives-boeing-model-747-series-airplanes)
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