Airworthiness Directives; Airbus Industrie Model A300-600 Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-09-24 · Effective 1998-10-29 · 63 FR 50981
Document
Document number
98-25354
Federal Register citation
63 FR 50981
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Industrie Model A300-600 Series
Publication date
1998-09-24
Effective date
1998-10-29
FAA docket
Docket No. 98-NM-82-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A300-600 series airplanes, that requires repetitive inspections to detect fatigue cracking of the wing top skin at the front spar joint; and a follow-on eddy current inspection and repair, if necessary. 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 detect and correct fatigue cracking of the wing top skin at the front spar joint, which could result in reduced structural integrity of the airplane.