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Airworthiness Directives; Airbus Model A320-111 and -211 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 1998-07-16 · Effective 1998-07-31 · 63 FR 38290

Document

Document number
98-18769
Federal Register citation
63 FR 38290
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Airbus Model A320-111 and -211 Series
Publication date
1998-07-16
Effective date
1998-07-31
FAA docket
Docket No. 97-NM-160-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A320-111 and -211 series airplanes. This action requires repetitive inspections to detect fatigue cracking of the frames of the sliding windows in the cockpit, 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 fatigue cracking of the frames of the sliding windows in the cockpit, which could result in reduced structural integrity of the pressure vessel of the fuselage of the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown