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Airworthiness Directives; Aerospatiale Model ATR42-300 and ATR42- 320 Series Airplanes

airworthiness · Rule · Final rule. · Published 1999-08-31 · Effective 1999-10-05 · 64 FR 47384

Document

Document number
99-22389
Federal Register citation
64 FR 47384
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Aerospatiale Model ATR42-300 and ATR42- 320 Series
Publication date
1999-08-31
Effective date
1999-10-05
FAA docket
Docket No. 98-NM-201-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Aerospatiale Model ATR42-300 and ATR42-320 series airplanes, that requires a one-time inspection for cracking of a fastener hole located on the lower surface of the outer wing, and repair, if necessary; and cold working of the hole and installation of a new fastener in the hole. 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 prevent fatigue damage on the outer wing and consequent reduced structural integrity of the wing.

Source

Authoritative
Federal Register document
Machine
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