Airworthiness Directives; Airbus Model A300 Series Airplanes
airworthiness · Rule · Final rule. · Published 1997-05-23 · Effective 1997-06-27 · 62 FR 28325
Document
Document number
97-12859
Federal Register citation
62 FR 28325
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300 Series
Publication date
1997-05-23
Effective date
1997-06-27
FAA docket
Docket No. 96-NM-43-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to all Airbus Model A300 series airplanes, that requires inspections of the lower door surrounding structure to detect cracks and corrosion, and repair, if necessary. This amendment also requires inspections to detect cracking of the holes of the corner doublers, the fail-safe ring, and the door frames of the door structures; and repair, if necessary. In addition, this amendment will also require modification of the passenger/crew door frames, which, when accomplished, terminates certain inspections. This amendment is prompted by reports indicating that corrosion was found behind the scuff plates at exit and cargo doors, and fatigue cracks originated from certain fastener holes located in adjacent structure. The actions specified by this AD are intended to detect and correct such corrosion and fatigue cracking, which could result in reduced structural integrity of the door surroundings.