Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes
airworthiness · Rule · Final rule. · Published 1999-12-08 · Effective 2000-01-12 · 64 FR 68623
Document
Document number
99-31471
Federal Register citation
64 FR 68623
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1999-12-08
Effective date
2000-01-12
FAA docket
Docket No. 98-NM-284-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A319, A320, and A321 series airplanes, that requires a one-time inspection of the forward engine mount assembly of the left and right engines to verify that the part number on each assembly is correct; re-identification of the forward engine mount assembly; and follow-on 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 prevent structural failure of the secondary load path of the forward engine mount, which, if combined with failure of the primary load path, could result in separation of the engine from the airplane.