What was found
THE LEFT OUTBOARD FLAP HAS A 1.50 INCH CRACK ON THE LEADING EDGE. STOP DRILLED AND INSTALLED DOUBLER IAW AMWA T.O. 1900-27-00-0001. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THE LEFT OUTBOARD FLAP HAS A 1.50 INCH CRACK ON THE LEADING EDGE. STOP DRILLED AND INSTALLED DOUBLER IAW AMWA T.O. 1900-27-00-0001. (X)