Airworthiness Directives; Airbus Model A300-600 Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-12-10 · Effective 1999-01-14 · 63 FR 68167
Document
Document number
98-32623
Federal Register citation
63 FR 68167
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300-600 Series
Publication date
1998-12-10
Effective date
1999-01-14
FAA docket
Docket No. 97-NM-153-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 cracks in the angle fitting at frame 40 of the center wing box, and corrective actions, if necessary; and eventual modification of that angle fitting, which terminates the repetitive inspections. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent cracks in the center wing box angle fitting, which could result in the failure of the center wing box at frame 40, and consequent reduced structural integrity of the airplane.