# Airworthiness Directives; Boeing Model 747-400F Series Airplanes
> **Rule** · Final rule. · Published 2004-03-26 · Effective 2004-04-30 · 69 FR 15663
## Document
- **Document number:** 04-6579
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 747-400F Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 69 FR 15663
- **Publication date:** 2004-03-26
- **Effective date:** 2004-04-30
- **FAA docket:** Docket No. 2002-NM-288-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747-400F series airplanes, that requires repetitive detailed and general visual inspections of the external fuselage skin for cracks; various inspections of the affected area where cracks are found to determine the extent of the damage; and repair of cracks. This action is necessary to detect and correct fatigue cracks in the fuselage skin and frame shear tie assemblies, which could propagate and result in possible in-flight decompression of the airplane. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2004/03/26/04-6579/airworthiness-directives-boeing-model-747-400f-series-airplanes)
---
*AI Analytics · CC0 1.0*