# Proposed AD 2002-CE-43-AD: SOCATA--Groupe AEROSPATIALE Models TB 9, TB 10, TB 20, TB 21, and TB 200 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2003-04-03
- Products: Socata--Groupe Aerospatiale
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: November 15, 2002, 67 FR 69154
- Comments due: January 3, 2003
- Became: [AD 2003-04-03](https://openairdocs.org/ad/2003-04-03)
- Docket: 2002-CE-43-AD
- FR document: 02-29004
- Official PDF: https://openairdocs.org/files/sha256/29/4d/294dce21d93c4443117df51279aa1674f9d011710303b02707921f7279ebf90d (from https://www.govinfo.gov/content/pkg/FR-2002-11-15/pdf/02-29004.pdf)
- Federal Register: https://www.federalregister.gov/documents/2002/11/15/02-29004/airworthiness-directives-socata-groupe-aerospatiale-models-tb-9-tb-10-tb-20-tb-21-and-tb-200
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A3223B391AC4C8B086256C7200537901.0001
- Page: https://openairdocs.org/proposed/2002-CE-43-AD

## 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.

## Notices in this docket

- Nov 15, 2002: Notice of proposed rulemaking (NPRM). (first notice), FR document 02-29004, comments due Jan 3, 2003 (https://www.federalregister.gov/documents/2002/11/15/02-29004/airworthiness-directives-socata-groupe-aerospatiale-models-tb-9-tb-10-tb-20-tb-21-and-tb-200)

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