What was found
DUE TO EXCESSIVE CORROSION ON CUSP WEB X=-54 TO X=-60 BETWEEN BS 806 AND 817. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, FIG 131A-2, 51-10-3 PAR 14 AND 21, 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DUE TO EXCESSIVE CORROSION ON CUSP WEB X=-54 TO X=-60 BETWEEN BS 806 AND 817. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-13, FIG 131A-2, 51-10-3 PAR 14 AND 21, 51-30-2.