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Airworthiness Directives; Airbus Model A320-111 Series Airplanes

airworthiness · Rule · Direct final rule; confirmation of effective date. · Published 1998-06-03 · Effective 1998-06-18 · 63 FR 30124

Document

Document number
98-14609
Federal Register citation
63 FR 30124
Type
Rule
Action
Direct final rule; confirmation of effective date.
Category
airworthiness
Manufacturer
Airbus Model A320-111 Series
Publication date
1998-06-03
Effective date
1998-06-18
FAA docket
Docket No. 98-NM-22-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Airbus Model A320-111 series airplanes. This amendment requires repetitive inspections to detect cracking around the attachment holes for the access panels in the lower skin of the wing; and repair, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to detect and correct such cracking, which could result in reduced structural integrity of the airplane.

Source

Authoritative
Federal Register document
Machine
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