What was found
AT C-CHECK, WING CENTER SECTION INTERIOR UPPER STIFFENER ATTACH ANGLE CRACKED LBL 24, BS 740. REMOVED AND REPLACED ANGLE PER SRM 51-30-2, 3 BY 3.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, WING CENTER SECTION INTERIOR UPPER STIFFENER ATTACH ANGLE CRACKED LBL 24, BS 740. REMOVED AND REPLACED ANGLE PER SRM 51-30-2, 3 BY 3.5.