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Airworthiness Directives; Airbus Model A300-600 Series Airplanes

airworthiness · Rule · Final rule. · Published 2000-04-14 · Effective 2000-05-19 · 65 FR 20078

Document

Document number
00-8987
Federal Register citation
65 FR 20078
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300-600 Series
Publication date
2000-04-14
Effective date
2000-05-19
FAA docket
Docket No. 98-NM-78-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 cracking of the doubler angle and discrepancies of the fasteners that connect the doubler angle and the bottom panel of the center wing box, and corrective actions, 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 in the doubler angle and discrepancies of the fasteners that connect the doubler angle and the bottom panel of the center wing box. Such cracking and discrepancies could result in reduced structural integrity of the airplane.

Source

Authoritative
Federal Register document
Machine
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