What was found
PANEL 423AL HAS A CRACK (BETWEEN 3" TO 4" LONG) DOT 129-001 (GE-129) INSTALLED RIB AT PYLON #2 WITH EXISTING FASTENERS IAW A300-600 SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PANEL 423AL HAS A CRACK (BETWEEN 3" TO 4" LONG) DOT 129-001 (GE-129) INSTALLED RIB AT PYLON #2 WITH EXISTING FASTENERS IAW A300-600 SRM 51-40-21.