27 Flight Controls
TTP B1-L3 ATA 27 Beech 90 Series B2-L2 Flight Controls INTRODUCTION The aircraft uses co n v entional three-axis flight controls; ailerons, el ev ators, and a r udde r . T w o electr i cal l y dr i v en flaps are on each wing. Ground steering is accomplished b y the r udder pedals through a mechanical steering rod attached to the nose landing gea r . GENERAL LJ-1 AND AFTER; L W-1 AND AFTER Flight-control m o v ement is accomplished through single non-redundant ca b les, push rods, and bell cranks, and are non-p o w ered (with the e xception of the r udder boost). The ailerons and el ev ators are controlled b y co n v entional control columns interconnected to a T -column behind the inst r ument panel. The r udder is operated with co n v entional r udd...