Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule; correction. · Published 2004-10-26 · Effective 2004-11-01 · 69 FR 62399
Document
Document number
04-23928
Federal Register citation
69 FR 62399
Type
Rule
Action
Final rule; correction.
Category
airworthiness
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.