What was found
DURING ROUTINE C-CHECK, FOUND 4TH STIFFENER AFT OF LEADING EDGE OF LEFT WINGS AT WS 92.8, CRACKED AT LOWER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER REPAIR 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 4TH STIFFENER AFT OF LEADING EDGE OF LEFT WINGS AT WS 92.8, CRACKED AT LOWER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-3. (M)