What was found
FOUND 46 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FORWARD OF PANEL 571CT. APPLIED FIBERGLASS REPAIR PER BOEING SRM 51-40-09, FIGURE 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND 46 INCH CRACK IN TRAILING EDGE FIBERGLASS PANEL FORWARD OF PANEL 571CT. APPLIED FIBERGLASS REPAIR PER BOEING SRM 51-40-09, FIGURE 10.