What was found
AFTER REMOVING A DAMAGED STIFFENER, FOUND A CRACK ON PANEL 171CL. REMOVED AND REPLACED THE PANEL IAW SRM 51-40-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVING A DAMAGED STIFFENER, FOUND A CRACK ON PANEL 171CL. REMOVED AND REPLACED THE PANEL IAW SRM 51-40-11.