Airworthiness Directives; Airbus Model A300 and A300-600 Series Airplanes
airworthiness · Rule · Final rule. · Published 1998-02-02 · Effective 1998-03-09 · 63 FR 5224
Document
Document number
98-2285
Federal Register citation
63 FR 5224
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300 and A300-600 Series
Publication date
1998-02-02
Effective date
1998-03-09
FAA docket
Docket No. 97-NM-178-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300 and A300-600 series airplanes, that requires inspections to detect cracks in Gear Rib 5 of the main landing gear (MLG) attachment fittings at the lower flange, and repair, 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 fatigue cracking of the MLG attachment fittings, which could result in reduced structural integrity of the airplane.