Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule. · Published 2005-09-27 · Effective 2005-11-01 · 70 FR 56361
Document
Document number
05-19143
Federal Register citation
70 FR 56361
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-09-27
Effective date
2005-11-01
FAA docket
Docket No. FAA-2005-18788
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD requires repetitive inspections of the intercostal webs, attachment clips, and stringer splice channels for cracks; and corrective action if necessary. This AD is prompted by reports of fatigue cracks on several Boeing Model 737-200 series airplanes. We are issuing this AD to detect and correct fatigue cracking of the intercostals on the forward and aft sides of the forward entry door, which could result in loss of the forward entry door and rapid decompression of the airplane.