As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND CORROSION ON FORWARD AND AFT FACE OF CIRCUMFERENTIAL AT LOWER FORWARD NOSE COMPARTMENT, BS 219 BETWEEN STRINGER 24R AND 26R. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2.