A test stop^ utilizing a split ring which grips a 3/8- 

 inch diameter cable through the liner by means of three 

 socket-head cap-screws i, was accordingly designed and manu- 

 factured. For tests, operating conditions were simulated by 

 loading the fairing and simultaneously exerting a load on the 

 cable. The stop was tested to a load of only 400 poxinds, 

 however « due to the limitations of the test fixture. 



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