# Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
> **Rule** · Final rule; correction. · Published 2004-10-26 · Effective 2004-11-01 · 69 FR 62399
## Document
- **Document number:** 04-23928
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 69 FR 62399
- **Publication date:** 2004-10-26
- **Effective date:** 2004-11-01
- **FAA docket:** Docket No. 2003-NM-90-AD
## Abstract

This document corrects a typographical error that appeared in airworthiness directive (AD) 2004-19-10 that was published in the Federal Register on September 27, 2004 (69 FR 57632). The typographical error resulted in the omission of the AD number in one location of the document. This AD is applicable to certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections for corrosion and cracking of the pivot hinge pins of the horizontal stabilizer, certain follow-on inspections, and replacement of the hinge pins with new or serviceable pins if necessary.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2004/10/26/04-23928/airworthiness-directives-boeing-model-737-100--200--200c--300--400-and--500-series-airplanes)
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