What was found
DURING C-CHECK THE CENTRAL FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED AT FRAME 21, STRINGERS 21L AND 21R. MAINTENANCE R & R THE SKIN IAW EC5330-02895. THE ACFT WAS 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 CENTRAL FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED AT FRAME 21, STRINGERS 21L AND 21R. MAINTENANCE R & R THE SKIN IAW EC5330-02895. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.