Airworthiness Directives; Boeing Model 737-100, -200, and -200C Series Airplanes
airworthiness · Rule · Final rule. · Published 2003-11-18 · Effective 2003-12-23 · 68 FR 64980
Document
Document number
03-28492
Federal Register citation
68 FR 64980
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-11-18
Effective date
2003-12-23
FAA docket
Docket No. 2002-NM-150-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 737-100, -200, and -200C series airplanes, that currently requires repetitive inspections to detect discrepancies in the upper and lower skins of the fuselage lap joint, and repair if necessary. This amendment adds new inspections, reduces the repetitive inspection intervals for certain airplanes, and mandates a terminating modification. The actions specified by this AD are intended to detect and correct discrepancies in the upper and lower skins of the fuselage lap joint and circumferential joint, which could result in sudden fracture and failure of a lap joint or circumferential joint and rapid decompression of the airplane fuselage. This action is intended to address the identified unsafe condition.