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Airworthiness Directives; Fairchild Aircraft, Inc. SA226 and SA227 Series Airplanes

airworthiness · Rule · Final rule. · Published 1997-05-13 · Effective 1997-07-08 · 62 FR 26223

Document

Document number
97-12517
Federal Register citation
62 FR 26223
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fairchild
Publication date
1997-05-13
Effective date
1997-07-08
FAA docket
Docket No. 96-CE-65-AD

Abstract

This amendment supersedes Airworthiness Directive (AD) 96-21- 05, which currently requires the following on certain Fairchild Aircraft, Inc. (Fairchild) SA226 and SA227 series airplanes that do not have a certain elevator torque tube installed: drilling inspection access holes in the elevator torque tube arm, inspecting the elevator torque tube for corrosion, replacing any corroded elevator torque tube, and applying a corrosion preventive compound. AD 96-21-05 resulted from several reports of corrosion found in the elevator torque tube area on the affected airplanes. This AD retains the actions required by AD 96- 21-05, and adds certain Fairchild Model SA227-BC airplanes to the Applicability section of that AD. The actions specified by this AD are intended to prevent failure of the flight control system caused by a corroded elevator torque tube, which could result in loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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