NPRM 2001-CE-41-AD

Became AD 2002-05-04

Proposed airworthiness directive · SOCATA--Groupe Aerospatiale

Published
December 17, 2001 · 66 FR 64928
Comments due
January 11, 2002
Action
Notice of proposed rulemaking (NPRM)
Docket
2001-CE-41-AD
FR document
01-30953
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 supersede Airworthiness Directive (AD) 77-15-06, which applies to all SOCATA--Groupe Aerospatiale (Socata) Models MS 892A-150, MS 892E-150, MS 893A, MS 893E, Rallye 150T, and Rallye 150ST airplanes. AD 77-15-06 currently requires you to repetitively inspect the engine mount assembly for cracks, repair any cracks found, and modify the brackets on airplanes with right angle engine mounts. This proposed AD is the result of the French airworthiness authority's determination that updated service information and additional aircraft should be added to the applicability of AD 77-15-06. This proposed AD would retain the inspection and repair requirements of the current AD and would add the information communicated by the French airworthiness authority. The actions specified by this proposed AD are intended to detect and correct cracks in the engine mount assembly. Such a condition could cause the engine mount assembly to fail, which could result in loss of control of the airplane.

The resulting AD

Notices in this docket · 1