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Airworthiness Directives; Schweizer Aircraft Corporation Model 269C, C-1, and D Helicopters

airworthiness · Rule · Final rule; request for comments. · Published 2005-05-18 · Effective 2005-06-02 · 70 FR 28415

Document

Document number
05-9764
Federal Register citation
70 FR 28415
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Schweizer
Publication date
2005-05-18
Effective date
2005-06-02
FAA docket
Docket No. FAA-2005-21217

Abstract

This amendment adopts a new airworthiness directive (AD) for the Schweizer Aircraft Corporation (Schweizer) Model 269C, C-1, and D helicopters. This action requires inspecting, modifying, and testing the lateral control trim actuator assembly on certain serial-numbered helicopters. This amendment is prompted by three reported incidents of the inner spring tube separating from the lateral trim control housing resulting in a lateral cyclic control restriction. The actions specified in this AD are intended to prevent separation of the inner spring tube from the lateral trim control housing and the associated loss of trim control, increased local resistance to right cyclic stick movement, and an emergency landing or subsequent loss of control of the helicopter.

Source

Authoritative
Federal Register document
Machine
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