# Proposed AD 97-CE-77-AD: SOCATAGroupe AEROSPATIALE Models TB9, TB10, TB20, TB21, and TB200 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 98-04-03
- Action: Notice of proposed rulemaking (NPRM).
- Published: November 7, 1997, 62 FR 60189
- Comments due: December 15, 1997
- Became: [AD 98-04-03](https://openairdocs.org/ad/98-04-03)
- Docket: 97-CE-77-AD
- FR document: 97-29422
- Official PDF: https://openairdocs.org/files/sha256/c5/37/c5376ce9b46d719c0f279b9efda4976f002d8623cf0d869cde884400b26e72e9 (from https://www.govinfo.gov/content/pkg/FR-1997-11-07/pdf/97-29422.pdf)
- Federal Register: https://www.federalregister.gov/documents/1997/11/07/97-29422/airworthiness-directives-socatagroupe-aerospatiale-models-tb9-tb10-tb20-tb21-and-tb200-airplanes
- Page: https://openairdocs.org/proposed/97-CE-77-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain SOCATA--Groupe AEROSPATIALE (Socata) Models TB9, TB10, TB20, TB21, and TB200 airplanes. The proposed AD would require inspecting the bolts and spacers of the upper attachments of the front belts for cracks, dents, etc. (damage); replacing any damaged bolts or spacers; incorporating a front belts upper attachment reinforcement kit; and reconditioning the belts. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by the proposed AD are intended to prevent failure of the upper seat belt attachment caused by excessive loads on the upper attachment of the belt, which could result in bodily injury to the occupants during landing.

## Notices in this docket

- Nov 7, 1997: Notice of proposed rulemaking (NPRM). (first notice), FR document 97-29422, comments due Dec 15, 1997 (https://www.federalregister.gov/documents/1997/11/07/97-29422/airworthiness-directives-socatagroupe-aerospatiale-models-tb9-tb10-tb20-tb21-and-tb200-airplanes)

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