NPRM 2000-CE-34-AD

Became AD 2000-22-17

Proposed airworthiness directive · Airworthiness Directives; SOCATA-Groupe AEROSPATIALE Models MS 880B, MS 885, MS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 894E, Rallye 100S, Rallye 150T, Rallye 150ST, Rallye 235C, and Rallye 235E Airplanes

Published
September 11, 2000 · 65 FR 54820
Comments due
October 11, 2000
Action
Notice of proposed rulemaking (NPRM)
Docket
2000-CE-34-AD
FR document
00-23209

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 MS 880B, MS 885, MS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 894E, Rallye 100S, Rallye 150T, Rallye 150ST, Rallye 235C, and Rallye 235E airplanes. The proposed AD would require you to repetitively inspect, and, if necessary, replace elevator clevis and rudder governor control clevis that are too thin. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in the proposed AD are intended to correct rudder and elevator control clevis that are too thin because of abnormal wear, with consequent failure of the rudder and elevator clevis. Such failure could lead to loss of directional or pitch control.

The resulting AD

Notices in this docket · 1