What was found
ANGLE HAS .25 INCH CRACK AT BOTTOM OF LEFT WING UPPER TRAILING EDGE PANEL, 5 FT FORWARD OF LEFT INBOARD AILERON INBOARD LEADING EDGE. REMOVED ANGLE AND FABICATED NEW ANGLE IAW 51-10-1 PAGE 2. INSTALLED ANGLE IAW 51-10-2 PAGE 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ANGLE HAS .25 INCH CRACK AT BOTTOM OF LEFT WING UPPER TRAILING EDGE PANEL, 5 FT FORWARD OF LEFT INBOARD AILERON INBOARD LEADING EDGE. REMOVED ANGLE AND FABICATED NEW ANGLE IAW 51-10-1 PAGE 2. INSTALLED ANGLE IAW 51-10-2 PAGE 1. (M)