What was found
CRACK FOUND AT OPEN HOLE OF LT WING FR 40 LOWER RADIUS, CRACK NOTED AT FIRST LAYER FWD LAYER, 6 O'CLOCK POSITION, CRACK DEPTH FROM FWD TO AFT AT 5MM. INSTALLED REINFORCING SKIN AND STIFFENER UNDER IAW SRM 51-40-21 .
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND AT OPEN HOLE OF LT WING FR 40 LOWER RADIUS, CRACK NOTED AT FIRST LAYER FWD LAYER, 6 O'CLOCK POSITION, CRACK DEPTH FROM FWD TO AFT AT 5MM. INSTALLED REINFORCING SKIN AND STIFFENER UNDER IAW SRM 51-40-21 .