What was found
PANEL 513AB CRACKED AT NUTPLATE HOLE. CLEANED AREA AROUND CRACK AND REMOVED FASTENERS IAW A300-600 SRM 53-15-63 STEP 5.TREATED AND PRIMED DOUBLERS IAW A300-600 SRM 51-21-10 AND 51-75-10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 513AB CRACKED AT NUTPLATE HOLE. CLEANED AREA AROUND CRACK AND REMOVED FASTENERS IAW A300-600 SRM 53-15-63 STEP 5.TREATED AND PRIMED DOUBLERS IAW A300-600 SRM 51-21-10 AND 51-75-10.