What was found
SUPPORT ANGLE CRACKED AT INTERNAL AREA OF ACCESS PANEL NÏ¿½ 5757L ON STRUT TORQUE BOX OTBD SIDE NR 1 ENGINE. R&R ANGLE IAW SRM & DRAWING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SUPPORT ANGLE CRACKED AT INTERNAL AREA OF ACCESS PANEL NÏ¿½ 5757L ON STRUT TORQUE BOX OTBD SIDE NR 1 ENGINE. R&R ANGLE IAW SRM & DRAWING.