What was found
DURING C-CHECK, FOUND FORWARD LOWER INBOARD CORNER ATTACH ANGLE CRACKED AT EDGE OF RIGHT WHEEL WELL STRUCTURE. REPLACED ANGLE IAW DC9 SRM 51-30-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND FORWARD LOWER INBOARD CORNER ATTACH ANGLE CRACKED AT EDGE OF RIGHT WHEEL WELL STRUCTURE. REPLACED ANGLE IAW DC9 SRM 51-30-1.