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Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters

airworthiness · Rule · Final rule. · Published 2020-12-18 · Effective 2021-01-22 · 85 FR 82305

Document

Document number
2020-27808
Federal Register citation
85 FR 82305
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Airbus
Publication date
2020-12-18
Effective date
2021-01-22
FAA docket
Docket No. FAA-2020-0572

Abstract

The FAA is superseding Airworthiness Directive (AD) 2007-26-51 which applied to certain Airbus Helicopters Deutschland GmbH Model EC135 helicopters. AD 2007-26-51 required inspecting the tail rotor control rod (control rod) and ball pivot and, depending on findings, replacing those parts. This new AD requires inspecting certain ball pivots, applying corrosion preventative compound on the ball pivot, and corrective action, as applicable. This AD also requires replacing the control rod with a newly developed control rod. This AD was prompted by the manufacturer's development of a new control rod, which the FAA has determined must be installed in order to address the identified unsafe condition. The actions of this AD are intended to address an unsafe condition on these products.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown