What was found
LT WING T/E CAVITY UPPER PANEL EDGE CRACKED AT XCW 109. THE PANEL WAS REPAIRED IAW SRM 57-09, FIG 42.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING T/E CAVITY UPPER PANEL EDGE CRACKED AT XCW 109. THE PANEL WAS REPAIRED IAW SRM 57-09, FIG 42.