Airworthiness Directives; Fairchild Aircraft, Inc. SA26, SA226, and SA227 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1997-01-17 · Effective 1997-02-06 · 62 FR 2552
Document
Document number
97-814
Federal Register citation
62 FR 2552
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Fairchild
Publication date
1997-01-17
Effective date
1997-02-06
FAA docket
Docket No. 96-CE-64-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to Fairchild Aircraft, Inc. (Fairchild) SA26, SA226, and SA227 series airplanes. This action requires applying torque to the control column pitch bearing attaching nuts, inspecting for any looseness or movement of the bearing assembly, and inspecting the elevator control rod end bearing retainer/dust seals for creasing. If either of these problems are evident, this action requires replacing these parts, as well as installing a new bolt and washer to the elevator control rod end bearing assembly at the walking beam connection. Reports of Fairchild SA227 series airplanes losing pitch control in-flight prompted this action. The actions specified by this AD are intended to prevent loss of pitch control, which if not corrected, could result in loss of the airplane.