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Cessna Service Bulletin SB07-25-01

January 29, 2007

Cessna Service Bulletin SB07-25-01, Title: Inflatable Seat Restraints Wiring Connector Strain Relief Installation.

Effectivity:

 Model  S/N
 172R  17280001 thru 17281272
172S 172S8001 thru 172S10102
182S 18280001 thru 18280944
182T 18280945 thru 18281741
 T182T  T18208001 thru T18208540
206H 20608001 thru 20608257
T206H T20608001 thru T20608594
      
Description:  AMSAFE has developed a more robust strain relief which should be installed at the base of FCI connectors found on the Cable Interface Assemblies and the End-Rlease Buckle Assemblies.

Compliance:  Recommended:  should be accomplished at the next scheduled airplane inspection, not to exceed 100 hours of operation or 12 months, whichever occurs first.
 

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