What was found
PANEL 424AR, AFT STIFFENER IS CRACKED. REMOVED STIFFENER AND INSTALLER NEW IAW SRM 51-42-05-02-01. TREATED AND PAINTED IAW SRM 51-25-05-02-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 424AR, AFT STIFFENER IS CRACKED. REMOVED STIFFENER AND INSTALLER NEW IAW SRM 51-42-05-02-01. TREATED AND PAINTED IAW SRM 51-25-05-02-01.