Airworthiness Directives; Airbus Model A300 B2 and B4 Series Airplanes
airworthiness · Rule · Final rule. · Published 1999-12-21 · Effective 2000-01-25 · 64 FR 71282
Document
Document number
99-32736
Federal Register citation
64 FR 71282
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus Model A300 B2 and B4 Series
Publication date
1999-12-21
Effective date
2000-01-25
FAA docket
Docket No. 98-NM-248-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300 B2 and B4 series airplanes, that requires repetitive inspections to detect cracking of the inner skin panel of the longitudinal lap joint; and repair, or modification and new repetitive inspections, 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 stress corrosion cracking of the inner skin panel of the longitudinal lap joint, which could result in rapid depressurization of the airplane.