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Airworthiness Directives; Airbus Model A320 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-09-08 · Effective 1998-10-13 · 63 FR 47423

Document

Document number
98-23738
Federal Register citation
63 FR 47423
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A320 Series
Publication date
1998-09-08
Effective date
1998-10-13
FAA docket
Docket No. 98-NM-18-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 of the front spar vertical stringers on the wings; and repair, 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 front spar vertical stringers on the wings, which could result in reduced structural integrity of the airframe.

Source

Authoritative
Federal Register document
Machine
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