# Airworthiness Directives; Reims Aviation S.A. Model F406 Airplanes; Correction
> **Rule** · Final rule; correction. · Published 2001-11-28 · Effective 2002-01-07 · 66 FR 59357
## Document
- **Document number:** 01-29492
- **Category:** airworthiness
- **Manufacturer:** Reims Aviation S.A. Model F406
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 66 FR 59357
- **Publication date:** 2001-11-28
- **Effective date:** 2002-01-07
- **FAA docket:** Docket No. 99-CE-28-AD
## Abstract

This document makes a correction to Airworthiness Directive (AD) 2001-23-07, which was published in the Federal Register on November 15, 2001 (66 FR 57364), and concerns certain Reims Model F406 airplanes. The FAA incorrectly referenced the AD number as "AD 2001- 01-07" instead of "AD 2001-23-07." This AD requires repetitive inspections of the canted rib upper cap in the center wing carry-through area for cracks, and, if cracks are found, immediate repair of the cracks or modification of this area depending on the extent of any cracks found. This AD also requires modifying the canted rib upper cap at a certain time period as terminating action for the repetitive inspections. This action corrects the AD to reflect the correct AD number.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2001/11/28/01-29492/airworthiness-directives-reims-aviation-sa-model-f406-airplanes-correction)
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