Summary
We propose to remove AD 93-14-19, which applies to certain The Boeing Company Model 767-200 and -300 series airplanes. AD 93-14-19 requires inspections for disbonding of the trailing edge wedge of the leading edge slat; and repair, if necessary. Since we issued AD 93-14- 19, an updated stability and control analysis showed that the worst- case scenario of a trailing edge wedge disbond in-flight would not adversely affect the controllability of the airplane. Accordingly, we propose to remove AD 93-14-19.