What was found
AT C-CHECK, LEFT WING CENTER L/E INTERIOR MID UPPER SECTION FOUND 2 INCH CRACK ON STRUCTURAL STIFFENER. REMOVED CRACKED ANGLE, FABRICATED ANGLE PER SRM 51-1-8, 2 X 1.75. INSTALLED PER SRM 51-1-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, LEFT WING CENTER L/E INTERIOR MID UPPER SECTION FOUND 2 INCH CRACK ON STRUCTURAL STIFFENER. REMOVED CRACKED ANGLE, FABRICATED ANGLE PER SRM 51-1-8, 2 X 1.75. INSTALLED PER SRM 51-1-2.