What was found
FUSELAGE SKIN BELOW THE L2 DOOR WAS CORRODED, BULGING AND CRACKED AT FRAME 68, STRINGER 28L. THE AIRCRAFT WAS GROUNDED. REPAIRED THE SKIN IAW SRM 53-41-11-300-018.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN BELOW THE L2 DOOR WAS CORRODED, BULGING AND CRACKED AT FRAME 68, STRINGER 28L. THE AIRCRAFT WAS GROUNDED. REPAIRED THE SKIN IAW SRM 53-41-11-300-018.