NPRM 2002-CE-43-AD

Became AD 2003-04-03

Proposed airworthiness directive · Socata--Groupe Aerospatiale

Published
November 15, 2002 · 67 FR 69154
Comments due
January 3, 2003
Action
Notice of proposed rulemaking (NPRM)
Docket
2002-CE-43-AD
FR document
02-29004
Products
Aircraft

A proposal is not in force. If adopted, it becomes an AD, usually with changes. Only the Federal Register edition is official.

Summary

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

The resulting AD

Notices in this docket · 1