Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2006-06-16 · Effective 2006-07-03 · 71 FR 34811
Document
Document number
06-5430
Federal Register citation
71 FR 34811
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2006-06-16
Effective date
2006-07-03
FAA docket
Docket No. FAA-2006-25030
Abstract
The FAA is superseding an existing airworthiness directive (AD) that applies to certain Boeing Model 737-100, -200, -200C, -300, - 400, and -500 series airplanes. The existing AD currently requires initial and repetitive inspections of the elevator tab assembly to find any damage or discrepancy; and corrective actions if necessary. This new AD adds certain new inspections and removes certain existing inspections. This AD results from additional reports of airframe vibrations of the elevator tab during flight on airplanes inspected per the existing AD; subsequently, considerable damage was done to the elevator tab, elevator, and horizontal stabilizer. In several incidents, a portion of the elevator tab separated from the airplane. We are issuing this AD to prevent excessive in-flight vibrations of the elevator tab, which could lead to loss of the elevator tab and consequent loss of controllability of the airplane.