What was found
CRACK ON VERTICAL ANGLE AT STRUT TORQUE BOX ACCESS PANEL 5858R ENGINE 2. REPLACED ANGLE IAW SRM AND DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON VERTICAL ANGLE AT STRUT TORQUE BOX ACCESS PANEL 5858R ENGINE 2. REPLACED ANGLE IAW SRM AND DWG.