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Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Models TB 9, TB 10, TB 20, TB 21, and TB 200 Airplanes

airworthiness · Rule · Final rule. · Published 2003-02-19 · Effective 2003-04-07 · 68 FR 7900

Document

Document number
03-3614
Federal Register citation
68 FR 7900
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-02-19
Effective date
2003-04-07
FAA docket
Docket No. 2002-CE-43-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to all SOCATA--Groupe AEROSPATIALE (Socata) Models TB 9, TB 10, TB 20, TB 21, and TB 200 airplanes. This AD requires you to repetitively inspect the aileron control gimbal joint for correct alignment and correct operation, and replace any misaligned or defective gimbal joint. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to prevent failure of the aileron control gimbal joint. Such failure could lead to loss of control of the airplane.

Source

Authoritative
Federal Register document
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