Airworthiness Directives; Boeing Model 737-200C Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2000-02-24 · Effective 2000-03-10 · 65 FR 9215
Document
Document number
00-4116
Federal Register citation
65 FR 9215
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Boeing Model 737-200C Series
Publication date
2000-02-24
Effective date
2000-03-10
FAA docket
Docket No. 99-NM-352-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Boeing Model 737-200C series airplanes. This action requires repetitive inspections to detect cracking in the lower skin at the stringer 4R lap joint, and certain fuselage frames; and corrective actions, if necessary. This amendment also provides for optional terminating action for the repetitive inspections. This amendment is prompted by a report of a fractured frame located at body station (BS) 480. The actions specified in this AD are intended to detect and correct cracking in certain frames, which, in conjunction with multiple site cracking in the lower skin of the lap joint, could result in failure of certain lap joints, and consequent rapid decompression of the airplane fuselage.