# Airworthiness Directives; Boeing Model 737-200, -200C, -300, -400, and -500 Series Airplanes
> **Rule** · Final rule. · Published 2004-09-08 · Effective 2004-10-13 · 69 FR 54206
## Document
- **Document number:** 04-20120
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 69 FR 54206
- **Publication date:** 2004-09-08
- **Effective date:** 2004-10-13
- **FAA docket:** Docket No. 2001-NM-246-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 737-200, -200C, -300, -400, and -500 series airplanes, that requires repetitive inspections to find fatigue cracking of certain upper and lower skin panels of the fuselage, and follow-on and corrective actions, if necessary. This amendment also includes terminating action for the repetitive inspections of certain modified or repaired areas only. This action is necessary to find and fix fatigue cracking of the skin panels, which could result in sudden fracture and failure of the skin panels of the fuselage, and consequent rapid decompression of the airplane. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2004/09/08/04-20120/airworthiness-directives-boeing-model-737-200--200c--300--400-and--500-series-airplanes)
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