# Proposed AD 95-CE-72-AD: SOCATAGroupe AEROSPATIALE Models TB9 and TB10 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 98-16-03
- Action: Notice of proposed rulemaking (NPRM).
- Published: May 22, 1998, 63 FR 28299
- Comments due: June 25, 1998
- Became: [AD 98-16-03](https://openairdocs.org/ad/98-16-03)
- Docket: 95-CE-72-AD
- FR document: 98-13653
- Official PDF: https://openairdocs.org/files/sha256/45/c9/45c92dab7021183a2a05a4109c885c870e269bd4a669b94b654c7c0653ef9ff2 (from https://www.govinfo.gov/content/pkg/FR-1998-05-22/pdf/98-13653.pdf)
- Federal Register: https://www.federalregister.gov/documents/1998/05/22/98-13653/airworthiness-directives-socatagroupe-aerospatiale-models-tb9-and-tb10-airplanes
- Page: https://openairdocs.org/proposed/95-CE-72-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain SOCATA--Groupe AEROSPATIALE (Socata) Models TB9 and TB10 airplanes. The proposed AD would require repetitively inspecting the wing front attachments on the wing and fuselage sides for cracks, and repetitively incorporating a certain modification kit (type of kit and time of incorporation depends on whether cracks are found during the inspection). 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 structural failure of the wing front attachments caused by fatigue cracking, which could result in the wing separating from the airplane if the airplane is operated with cracked wing front attachments over an extended period of time.

## Notices in this docket

- May 22, 1998: Notice of proposed rulemaking (NPRM). (first notice), FR document 98-13653, comments due Jun 25, 1998 (https://www.federalregister.gov/documents/1998/05/22/98-13653/airworthiness-directives-socatagroupe-aerospatiale-models-tb9-and-tb10-airplanes)

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