2590-01-302-1247
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A device for maintaining control of an aircraft about its pitch and roll axis. It consists of a control wheel, aircraft mounted at the upper end of a lever, the wheel being turned to control the aircraft about its roll axis, the lever being pushed forward or pulled back to control the aircraft about its pitch axis, excludes:operation of trim tabs or the like.
2590-01-302-1247, no name available
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