As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK DISCREPANCY AS FOLLOWS, LT WING LEADING EDGE AT LEADING EDGE STA 130 IS CRACKED. REMOVED EXISTING FASTENERS TO GAIN ACCESS TO THE REPAIR AS PER B-727 SRM 51-30-2. CUT DAMAGED AREA AS PER B-727 SRM 51-40-3 FIG 1. FABRICATED REPAIR ANGLES MATERIAL USED P/N 60-18001. PO 3077124 SIZES 11 X 1 INCH AND 8.5 X 1 INCH. TREATED AND PRIMED AS PER B-727 SRM 51-10-2. INSTALLED REPAIR ANGLES AS PER B-727 SRM 51-30-2.