As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN BULGES WITH .50 INCH CRACK IN OUTER SKIN AT FR 23 BS 7654.7 BETWEEN STR 20L AND STR 21L. ALSO, A .50 INCH CRACK BETWEEN STR 21L AND STR 21R, BS 7654.7. THIS CORROSION IS A RESULT OF THE DIRECT CONTACT BETWEEN THE FUSELAGE SKIN PANEL AND THE TITANIUM STRAP AT THIS FRAME. C/W EMB120 SB 120-53-0065 AFTER APPLICABLE REPAIRS ARE COMPLETED. (X)