What was found
VERTICAL STIFFENER WAS CRACKED ON THE LT WING T/E, BEHIND PANEL 541JB, AT XORS 433. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-31-01, AND SRM 51-33-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STIFFENER WAS CRACKED ON THE LT WING T/E, BEHIND PANEL 541JB, AT XORS 433. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-31-01, AND SRM 51-33-01.