As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING C-09 CHECK A 2 INCH CRACK WAS FOUND ON THE L-4 DOOR AREA CUSP INNER FRAME AT BS 1720, WL 208, LBL 70. MAINTENANCE WELDED CRACK AT THE INNER FRAME BS 1720 IAW AWA E.R. 19-5361-03035-SS2 . CAD PLATING WAS PERFORMED IAW E.O. 19-5361-03035-552, AND SOPM 20-42-10 PAGES 1-11. AREA WAS PRIMED AND PAINTED IAW SRM 51-20-01 PG 1.