As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER PORTION OF LAV "E" IS CORRODED AROUND TIE DOWN AREAS (AFT SIDE). MFG END WALL FITTING IAW ESO 25-34. ALODINED FITTING IAW MM 51-21-04. PRIMED FITTING IAW MM 51-21-10. INSTALLED HELICOILS IAW SOPM 20-50-22 REV 5 INSTALLED END WALL FITTINGS IAW CMM 25-40-81, PG 629. LAYED UP AND CURED FIBERGLASS .