What was found
CRACK ON SUPPORT ANGLE LOCATED ON INTERNAL AREA OF ACCESS PANEL 5835R AT LEVEL OF WBL 188 FIXED TRAILING EDGE STRUCTURE RT WING. REPLACED SUPPORT ANGLE IAW SRM AND DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE LOCATED ON INTERNAL AREA OF ACCESS PANEL 5835R AT LEVEL OF WBL 188 FIXED TRAILING EDGE STRUCTURE RT WING. REPLACED SUPPORT ANGLE IAW SRM AND DWG.