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Airworthiness Directives; Aerospatiale Model ATR42-500 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 1998-04-10 · Effective 1998-04-27 · 63 FR 17670

Document

Document number
98-9343
Federal Register citation
63 FR 17670
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Aerospatiale Model ATR42-500 Series
Publication date
1998-04-10
Effective date
1998-04-27
FAA docket
Docket No. 98-NM-107-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Aerospatiale Model ATR42-500 series airplanes. This action requires a one-time inspection to verify the installation of certain stringer clips at the junction of frame 34 and stringer 6, and installation of stringer clips, 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 prevent fatigue cracking in the skin of the fuselage, which could result in loss of pressure inside the airplane.

Source

Authoritative
Federal Register document
Machine
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