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Airworthiness Directives; The New Piper Aircraft Corporation Model PA-38-112 Airplanes

airworthiness · Rule · Final rule. · Published 1998-02-11 · Effective 1998-03-16 · 63 FR 6839

Document

Document number
98-2776
Federal Register citation
63 FR 6839
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
The New Piper
Publication date
1998-02-11
Effective date
1998-03-16
FAA docket
Docket No. 96-CE-53-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to The New Piper Aircraft Corporation (Piper) Model PA-38-112 airplanes. This action requires repetitively replacing the upper rudder hinge bracket. Reports of fatigue cracks occurring on the upper rudder hinge bracket, and the manufacture of a new upper rudder hinge bracket with a life limited improved design prompted this action. The actions specified by this AD are intended to prevent cracks in the upper rudder hinge bracket, which could result in separation of the rudder from the airplane and loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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