What was found
FUSELAGE FRAME AT FS 333.00 HAS LIGHT CORROSION, BETWEEN STRINGER 25L - 26R. REPAIRED LIGHT SURFACE CORROSION ON FRAME AT FS 333.00, BETWEEN STRINGER 25L - 26R IAW SRM 51-21-06. COMPLIED WITH DT CHECKLIST 15 - 27.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE FRAME AT FS 333.00 HAS LIGHT CORROSION, BETWEEN STRINGER 25L - 26R. REPAIRED LIGHT SURFACE CORROSION ON FRAME AT FS 333.00, BETWEEN STRINGER 25L - 26R IAW SRM 51-21-06. COMPLIED WITH DT CHECKLIST 15 - 27.