Airworthiness Directives; Airbus Model A340-211, -212, -213, - 311, -312, and -313 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1999-01-08 · Effective 1999-01-25 · 64 FR 1108
Document
Document number
99-51
Federal Register citation
64 FR 1108
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1999-01-08
Effective date
1999-01-25
FAA docket
Docket No. 98-NM-297-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A340-211, -212, -213, -311, -312, and - 313 series airplanes. This action requires repetitive operational tests to ensure proper operation of the actuator of the secondary locks of the thrust reversers; 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 in this AD are intended to prevent the inadvertent opening of a thrust reverser door in the event of failure of the primary and secondary locks of the thrust reverser. Such inadvertent opening could result in reduced controllability of the airplane.