Airworthiness Directives; Boeing Model 737-200, -200C, -300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule. · Published 2004-09-08 · Effective 2004-10-13 · 69 FR 54206
Document
Document number
04-20120
Federal Register citation
69 FR 54206
Type
Rule
Action
Final rule.
Category
airworthiness
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.