Airworthiness Directives; Airbus Model A300 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2000-02-07 · Effective 2000-02-22 · 65 FR 5756
Document
Document number
00-2467
Federal Register citation
65 FR 5756
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Airbus Model A300 Series
Publication date
2000-02-07
Effective date
2000-02-22
FAA docket
Docket No. 2000-NM-16-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Airbus Model A300 series airplanes. This action requires either a one-time ultrasonic inspection, or repetitive visual inspections and eventual ultrasonic inspection, to detect cracking of the longitudinal skin splice above the mid-passenger door panels, and corrective actions, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to detect and correct cracking of the longitudinal skin splice above the mid-passenger door panels, which could result in reduced structural integrity of the fuselage pressure vessel.