What was found
VERTICAL STIFFINER ON CENTER WING AFT WEB AFT SIDED CRACKED APPROX 4 INCHES AT UPPER END STA 868 RBL 40 WL 190. REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STIFFINER ON CENTER WING AFT WEB AFT SIDED CRACKED APPROX 4 INCHES AT UPPER END STA 868 RBL 40 WL 190. REMOVED STIFFENER AND INSTALLED NEW STIFFENER PER SRM 51-10-1.