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Airworthiness Directives; Airbus Airplanes

airworthiness · Rule · Final rule. · Published 2015-11-20 · Effective 2015-12-28 · 80 FR 72569

Document

Document number
2015-28895
Federal Register citation
80 FR 72569
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2015-11-20
Effective date
2015-12-28
FAA docket
Docket No. FAA-2014-1043

Abstract

We are adopting a new airworthiness directive (AD) for all Airbus Model A330-200, A330-200 Freighter, and A330-300 series airplanes; and Model A340-200 and A340-300 series airplanes. This AD was prompted by reports of cracked support strut body ends at a certain frame location of the trimmable horizontal stabilizer (THS). This AD requires repetitive inspections for cracking of the strut ends of the THS support located at a certain frame in the tail cone, and replacement if necessary; and reinstallation or installation of reinforcing clamps on certain strut ends. We are issuing this AD to detect and correct cracked support strut body ends of the THS, which could lead to the loss of all four THS support struts, making the remaining structure unable to carry limit loads, resulting in the loss of the horizontal tail plane.

Source

Authoritative
Federal Register document
Machine
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