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