What was found
DURING OK TO INSTALL PANEL 623BB, FOUND CRACK AT THE FWD UPPER RADIUS OF PANEL CUTOUT, DOT 55-006. INSTALLED REFORCING PLATE IAW SRM 57-41-12-227.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OK TO INSTALL PANEL 623BB, FOUND CRACK AT THE FWD UPPER RADIUS OF PANEL CUTOUT, DOT 55-006. INSTALLED REFORCING PLATE IAW SRM 57-41-12-227.