As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE AFT CARGO COMPARTMENT, BETWEEN STRINGER 27R & 28R & BETWEEN FRAME 81 & 83, FUSELAGE SKIN INNER SURFACE CORRODED. REPAIR HAS BEEN ACCOMPLISHED UNDER ETD2015-190-077564 REV A INSTRUCTIONS & APPROVED UNDER F-200-06G FORM RCE 2009C06-28.