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Airworthiness Directives; Airbus Model A300, A310, and A300-600 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-07-31 · Effective 1998-09-04 · 63 FR 40816

Document

Document number
98-20434
Federal Register citation
63 FR 40816
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
1998-07-31
Effective date
1998-09-04
FAA docket
Docket No. 98-NM-116-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300, A310, and A300-600 series airplanes, that requires repetitive detailed visual inspections to detect cracks in the pylon thrust and sideload fitting of the wing, and replacement of any cracked pylon thrust and sideload fitting with a new fitting. 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 cracks in the pylon thrust and sideload fitting of the wing, which could result in reduced structural integrity of the airplane.

Source

Authoritative
Federal Register document
Machine
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