# 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
> **Rule** · Final rule. · Published 2000-11-14 · Effective 2000-12-29 · 65 FR 68065
## Document
- **Document number:** 00-28439
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 68065
- **Publication date:** 2000-11-14
- **Effective date:** 2000-12-29
- **FAA docket:** Docket No. 2000-CE-34-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that applies 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. This AD requires you to repetitively inspect, and, if necessary, replace elevator clevis and rudder governor control clevis that are too thin. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified in this 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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/11/14/00-28439/airworthiness-directives-socata-groupe-aerospatiale-models-ms-880b-ms-885-ms-892a-150-ms-892e-150-ms)
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