What was found
AT C-CHECK, FUSELAGE INTERIOR NOSE W/W BOX CORROSION AT STA 308. REMOVED STIFFENERS AND CUT OUT SKIN, INSTALLED NEW SKIN PER SRM 51-40-2, REINSTALLED STIFFENERS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, FUSELAGE INTERIOR NOSE W/W BOX CORROSION AT STA 308. REMOVED STIFFENERS AND CUT OUT SKIN, INSTALLED NEW SKIN PER SRM 51-40-2, REINSTALLED STIFFENERS.