What was found
DUE TO EXCESSIVE CORROSION ON CRACKED CUSP WEB BETWEEN BS 826 AND 845, RBL 54 - 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-16, 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 CRACKED CUSP WEB BETWEEN BS 826 AND 845, RBL 54 - 60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-16, 51-10-3 PAR 14 AND 21, 51-30-2.