<p><strong><font color = "blue">2007-09-01  CESSNA AIRCRAFT COMPANY:</font></strong> Amendment 39-15031; Docket No.<br>
  FAA-2007-27786;  Directorate Identifier 2007-CE-031-AD.</p>
<p><strong>Airworthiness  Directives; Cessna Aircraft Company Models 182H, 182J, 182K, 182L, 182M, 182N,  182P, 182Q, and 182R Airplanes </strong></p>
<p><strong>AGENCY:</strong> Federal Aviation  Administration (FAA), DOT.</p>
<p><strong>ACTION:</strong> Final rule; request for  comments.</p>
<p><strong>SUMMARY:</strong> The FAA is adopting a  new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna)  Model 182 series airplanes that are equipped with Air Plains Services  Corporation Supplemental Type Certificate (STC) SA00152WI. This AD requires you  to disconnect or remove the electrical cable between the forward ground power  relay and the starter relay, install a placard, inspect the fuel line between  the auxiliary electric fuel pump and the engine-driven fuel pump for chafing,  and replace the fuel line if chafing is found. This AD results from a report of  an in-flight and post-landing engine compartment fire. We are issuing this AD  to detect and correct interference between the ground power electrical cable,  the fuel strainer cable, and the fuel line between the auxiliary electric fuel  pump and the engine-driven fuel pump. This condition could lead to a fire in  the engine compartment.</p>
<p><strong>DATES:</strong> This AD becomes effective on April 25, 2007.</p>
<p><strong>Applicability </strong><br>
  (c)     This  AD applies to Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R  airplanes, all serial numbers, that:<br>
  (i)         Have Air  Plains Services Corporation Supplemental Type Certificate (STC) SA00152WI  installed;     <br>
  (ii)        Have a  ground power receptacle mounted on the firewall (forward ground power  receptacle); and     <br>
  (iii)       Are  certificated in any category.</p>
<p><strong>Unsafe Condition </strong><br>
  (d)     This AD results from a report of an  in-flight and post-landing engine compartment fire. We are issuing this AD to  detect and correct interference between the ground power electrical cable, the  fuel strainer cable, and the fuel line between the auxiliary electric fuel pump  and the engine-driven fuel pump. This condition could lead to a fire in the  engine compartment.</p>