Airworthiness Directives; Airbus Model A300-600 Series Airplanes
airworthiness · Rule · Final rule. · Published 1997-09-25 · Effective 1997-10-30 · 62 FR 50251
Document
Document number
97-25164
Federal Register citation
62 FR 50251
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300-600 Series
Publication date
1997-09-25
Effective date
1997-10-30
FAA docket
Docket No. 96-NM-170-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300-600 series airplanes, that requires repetitive inspections to detect fatigue cracking in the left and right wings in the area where the top skin attaches to the center spar; and repair or modification of this area, if necessary. This amendment is prompted by a report from the manufacturer indicating that, during full-scale fatigue testing of the airframe, fatigue cracking was detected in this area. The actions specified by this AD are intended to detect and correct this cracking, which could reduce the residual strength of the top skin of the wings, and consequently affect the structural integrity of the airframe.