# Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes
> **Rule** · Final rule. · Published 2001-11-15 · Effective 2002-01-07 · 66 FR 57364
## Document
- **Document number:** 01-28571
- **Category:** airworthiness
- **Manufacturer:** Reims Aviation S.A. Model F406
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 66 FR 57364
- **Publication date:** 2001-11-15
- **Effective date:** 2002-01-07
- **FAA docket:** Docket No. 99-CE-28-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Reims Aviation S.A. (Reims) Model F406 airplanes. This AD requires you to repetitively inspect the canted rib upper cap in the center wing carry-through area for cracks, and, if cracks are found, immediately repair the cracks or modify this area depending on the extent of any cracks found. This AD also requires you to modify the canted rib upper cap at a certain time period as terminating action for the repetitive inspections. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for France. The actions specified by this AD are intended to detect and correct cracks in the canted rib upper cap in the center wing carry-through area, which could result in structural failure of the wing with possible loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2001/11/15/01-28571/airworthiness-directives-reims-aviation-sa-model-f406-airplanes)
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