Cessna Service Bulletin SB09-24-03
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