Airworthiness Directives; Airbus Model A330 and A340 Series Airplanes
airworthiness · Rule · Final rule. · Published 1999-11-12 · Effective 1999-12-17 · 64 FR 61485
Document
Document number
99-29327
Federal Register citation
64 FR 61485
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A330 and A340 Series
Publication date
1999-11-12
Effective date
1999-12-17
FAA docket
Docket No. 99-NM-184-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A330 and A340 series airplanes, that requires repetitive detailed visual inspections to detect cracking of the vertical flange of the inboard Z-stiffeners of the centerline panel of the fuselage belly fairing; and corrective actions, if necessary. This amendment also provides for optional terminating action for the repetitive inspections. 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 fatigue cracking of the vertical flange of the inboard Z-stiffeners of the centerline panel of the fuselage belly fairing, which could result in reduced structural integrity of the belly fairing.