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AD AD 2004-23-02

Airworthiness Directives; Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 Airplanes

Summary

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.

Directive Details

AD Number

AD 2004-23-02

Document Number

E7-2754

Type

Rule

Publication Date

February 16, 2007

Effective Date

December 23, 2004

Affected Manufacturer

Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300

Criticality

routine

Emergency

No

Docket ID

Docket No. 2003-CE-51-AD

Official Documents

View all ADs for Raytheon Aircraft Company 65, 90, 99, 100, 200, and 1900 Series Airplanes, and Models 70 and 300 →

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