As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH WING LEADING EDGE SKIN AREA CRACKED BETWEEN WS 150.5 AND 204.50 (#5 LEADING EDGE SLAT AREA ) PERFORMED TAP TEST ON LH WING L/E DELAMINATION FOUND DIM L= 18.5" W=15" OUT OF LIMIT IAW B757 SRM 57-41-01-1A FIG 101 SHEET 2 TABLE I NOTE A AND IAW B757 SRM 51-10-06-2R AND APPLIED PERMANENT REPAIR ON LH WING LEADING EDGE IAW B757 SRM 51-70-08-0G