What was found
DURING C-CHECK, FOUND THE ATTACH ANGLE ON BOTTOM OF TRAP PANEL IN LEFT WHEEL WELL CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND THE ATTACH ANGLE ON BOTTOM OF TRAP PANEL IN LEFT WHEEL WELL CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2 AND 51-30-5.