What was found
DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 11-12 AND STRINGERS 20-21R. MAINTENANCE R & R THE SKIN IAW SRM 51-20-01. ACFT APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK THE FORWARD FUSELAGE II SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 11-12 AND STRINGERS 20-21R. MAINTENANCE R & R THE SKIN IAW SRM 51-20-01. ACFT APPROVED FOR RETURN TO SERVICE.