What was found
DURING ROUTINE C-CHECK, FOUND 3RD STIFFENER AFT OF LEFT WING LEADING EDGE AT WS 92.8 CRACKED AT UPPER END. STOP DRILLED CRACK FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK, FOUND 3RD STIFFENER AFT OF LEFT WING LEADING EDGE AT WS 92.8 CRACKED AT UPPER END. STOP DRILLED CRACK FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M)