As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SEVERAL AREAS OF CORROSION AT STRINGER 23P AND FORWARD AND AFT OF FRAME BS 488. FOUND LIGHT CORROSION AT AREAS INDICATED. BLENDED, ALODINED AND EPOXY PRIMED AREA IAW -8 SRM 55-20-11, 51-20-16 AND 51-20-36 AND CORROSION PREVENTION CONTROL MANUAL, CHAPTER 4.