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Airworthiness Directives; Airbus Model A320 Series Airplanes

airworthiness · Rule · Final rule. · Published 1999-01-08 · Effective 1999-02-12 · 64 FR 1116

Document

Document number
99-181
Federal Register citation
64 FR 1116
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A320 Series
Publication date
1999-01-08
Effective date
1999-02-12
FAA docket
Docket No. 98-NM-356-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A320 series airplanes, that requires repetitive inspections to detect fatigue cracking in certain areas of the fuselage; and corrective action, if necessary. This amendment also provides for an optional terminating action for 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 detect and correct fatigue cracking of the fuselage, which could result in reduced structural integrity of the airplane.

Source

Authoritative
Federal Register document
Machine
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