AD 54-26-02 addresses the wear of cables at the control quadrant. It states that any one of four FAA approved modifications listed would satisfy the AD. On this forum it was stated that the only approved modification was the installation of the new quadrant with a part number of 415-52137 which is the last method (of the four) listed in the AD. I have removed my column and the quadrant was manufactured by "Met-Co-Aire" which is the manufacturer listed in the AD for the first approved method. My question is: Is there any other directives that I do not have that eliminates all of the other three methods except the last? Or is the fourth method the only one currently available so therefore becomes by default the only approved method? .
Rich Blair N99997 4J6 St. Marys, Ga. --------------------------------- to unsubscribe send mailto:[EMAIL PROTECTED] ___________________________________________________________ T O P I C A The Email You Want. http://www.topica.com/t/16 Newsletters, Tips and Discussions on Your Favorite Topics
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