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

airworthiness · Rule · Final rule. · Published 2009-02-20 · Effective 2009-03-27 · 74 FR 7804

Document

Document number
E9-3276
Federal Register citation
74 FR 7804
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2009-02-20
Effective date
2009-03-27
FAA docket
Docket No. FAA-2008-0657

Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A300, A310, and A300-600 series airplanes. That AD currently 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 new AD reduces the threshold and repetitive intervals for the detailed inspection for certain airplanes and reduces the applicability of the existing AD. This AD results from issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. We are issuing this AD 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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