What was found
DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD ANGLE CORRODED BETWEEN BS 947.5 TO BS 1006, STR 17R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 16Y CHECK, FOUND INNER CHORD ANGLE CORRODED BETWEEN BS 947.5 TO BS 1006, STR 17R. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.