Airworthiness Directives; Boeing Model 737-100, -200, -200C, - 300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1999-04-23 · Effective 1999-05-10 · 64 FR 19879
Document
Document number
99-9739
Federal Register citation
64 FR 19879
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1999-04-23
Effective date
1999-05-10
FAA docket
Docket No. 98-NM-337-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to all Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This action requires repetitive inspections to detect cracking in the web of the aft pressure bulkhead at body station 1016 at the aft fastener row attachment to the ``Y'' chord; and corrective actions, if necessary. This amendment is prompted by several reports of fatigue cracking found at that location on Model 737 series airplanes. The actions specified in this AD are intended to detect and correct such fatigue cracking, which could result in rapid decompression of the fuselage.