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Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes

airworthiness · Rule · Final rule. · Published 1999-08-23 · Effective 1999-09-27 · 64 FR 45868

Document

Document number
99-21365
Federal Register citation
64 FR 45868
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-08-23
Effective date
1999-09-27
FAA docket
Docket No. 96-NM-29-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A319, A320, and A321 series airplanes, that requires repetitive inspections to detect wear of the inboard flap trunnions, and to detect wear or debonding of the protective half-shells; and corrective actions, if necessary. 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 chafing and resultant wear damage on the inboard flap drive trunnions or on the protective half-shells, which could result in failure of the trunnion primary load path; this would adversely affect the fatigue life of the secondary load path and could lead to loss of the flap.

Source

Authoritative
Federal Register document
Machine
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