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Cessna Service Bulletin SB09-24-03

November 24, 2009

 

Effectivity:

 

182T     18281198 thru 18282045

 

T182T   T18208001 thru T18208806

 

206H     20608001 thru 20608291

 

T206H   T20608001 thru T20608738

 

Reason:  It has been determined that on some airplanes, vibration, bends, and torsional stress on the alternator power cable may cause cracks and fractures of the alternator ring terminal.

 

Compliance:  Mandatory; shall be accomplished at the next 100-hour or 12-month (annual) type inspection, whichever occurs first.

CREDIT:  26 Oct 2010

 

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