What was found
DURING A C-CHECK, THE FUSELAGE SKIN WAS CRACKED AT FRAME 78 STRINGERS 4 - 5R. REPAIRED THE SKIN IAW SRM 53-32-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A C-CHECK, THE FUSELAGE SKIN WAS CRACKED AT FRAME 78 STRINGERS 4 - 5R. REPAIRED THE SKIN IAW SRM 53-32-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.