In a message dated 5/29/2003 9:22:28 AM Eastern Daylight Time, [email protected] writes:
> now the bias Perhaps I'm missing the point. If the pivot for the elevator and the pivot for the aileron is attached at the same point, as mine are, the elevator cables will try to twist forward of the aft spar mounted pulley assembly, any time the stick is moved for aileron input. As the stick is pulled for and aft, the aileron cable or push/pull rod set will move for and aft. In both cases, the stick movement in one direction does not affect the movement of the other control surface. I guess I fail to see how the bias is induced. Help me out Orma AKA AviationMech KR-2 N110LR 1984 to Present www.members.aol.com/aviationmech -------------- next part -------------- An HTML attachment was scrubbed... URL: http://mylist.net/private/krnet/attachments/20030530/76f6ff1a/attachment.htm
