# Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes
> **Rule** · Final rule; correction. · Published 2007-02-16 · Effective 2004-12-23 · 72 FR 7581
## Document
- **Document number:** E7-2754
- **Category:** airworthiness
- **Manufacturer:** Raytheon
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 72 FR 7581
- **Publication date:** 2007-02-16
- **Effective date:** 2004-12-23
- **FAA docket:** Docket No. 2003-CE-51-AD
## Abstract

This document makes a correction to Airworthiness Directive (AD) 2004-23-02, which was published in the Federal Register on November 9, 2004 (69 FR 64842), and applies to all Raytheon Aircraft Company (Raytheon) 65, 90, 99, 100, 200, and 1900 series airplanes and Models 70 and 300 airplanes. AD 2004-23-2 requires repetitive inspections of the nose landing gear (NLG) fork for cracks with replacement if cracks are found (replacement terminates repetitive inspections). Current language in paragraph (e)(3) of AD 2004-23-02 references Part III of the Accomplishment Instructions of the service bulletin instead of Part II. This document corrects that paragraph by changing the reference from Part III to Part II.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2007/02/16/E7-2754/airworthiness-directives-raytheon-aircraft-company-65-90-99-100-200-and-1900-series-airplanes-and)
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