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Gfa ad 485 issue 1

CRACKING OF CONTROL SYSTEM COMPONENTS

During static load testing the cracks were found in the longitudinal control coupling. This design is similar to four other components and it is possible that these may also crack. This AD is applicable to the Stemme S10 Serial Numbers 10-03 to 10-64, Stemme S10-V Serial Numbers 14-002 to 14-030 and converted aircraft from 14-012M to 14-063M and Stemme S10-VT Serial Numbers 11-001, 11-004 to 11-015 and 11-015. Stemme Service Bulletin A31-10-032 forms part of this AD.