Cessna Service Bulletin SB07-25-01
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.