<p><strong><font color = "blue">2007-09-02  REIMS AVIATION S.A.:</font></strong> Amendment 39-15032; Docket No. FAA-2006-26690; Directorate Identifier  2006-CE-088-AD.</p>
<p><strong>[Docket No.  FAA-2006-26690 Directorate Identifier 2006-CE-088-AD; Amendment 39-15032; AD  2007-09-02] RIN 2120-AA64 </strong></p>
<p><strong>Airworthiness  Directives; REIMS AVIATION S.A. Model F406 Airplanes </strong></p>
<p><strong>AGENCY:</strong> Federal Aviation  Administration (FAA), Department of Transportation (DOT).</p>
<p><strong>ACTION:</strong> Final rule.</p>
<p><strong>SUMMARY:</strong> We are adopting a new  airworthiness directive (AD) for the products listed above. This AD results  from mandatory continuing airworthiness information (MCAI) issued by an  aviation authority of another country to identify and correct an unsafe  condition on an aviation product. The MCAI describes the unsafe condition as:</p>
<p>During maintenance,  cracks have been discovered about the left and right rib at the connection of  the center wing and the fuselage localized at the fuselage station FS160.80.  Cracks spread in the rib could result in structural failure.</p>
<p><strong>DATES:</strong> This AD becomes  effective May 31, 2007.</p>