# Proposed AD 2000-CE-34-AD: 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

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2000-22-17
- Action: Notice of proposed rulemaking (NPRM).
- Published: September 11, 2000, 65 FR 54820
- Comments due: October 11, 2000
- Became: [AD 2000-22-17](https://openairdocs.org/ad/2000-22-17)
- Docket: 2000-CE-34-AD
- FR document: 00-23209
- Official PDF: https://openairdocs.org/files/sha256/1a/42/1a42aa3fa73b338966baf74d212c3278d736e172b87aa181ceb76c7cb9357d2c (from https://www.govinfo.gov/content/pkg/FR-2000-09-11/pdf/00-23209.pdf)
- Federal Register: https://www.federalregister.gov/documents/2000/09/11/00-23209/airworthiness-directives-socata-groupe-aerospatiale-models-ms-880b-ms-885-ms-892a-150-ms-892e-150-ms
- Page: https://openairdocs.org/proposed/2000-CE-34-AD

## 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.

## Notices in this docket

- Sep 11, 2000: Notice of proposed rulemaking (NPRM). (first notice), FR document 00-23209, comments due Oct 11, 2000 (https://www.federalregister.gov/documents/2000/09/11/00-23209/airworthiness-directives-socata-groupe-aerospatiale-models-ms-880b-ms-885-ms-892a-150-ms-892e-150-ms)

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