What was found
C-CHECK, FUSELAGE SKIN CRACKED 1.25 AT L-2 DOOR FWD LOWER CORNER. STOP DRILLED CRACK, FABRICATED REPAIR PARTS, TREATED AND PRIMED PARTS, INSTALLED REPAIR IAW B737 SRM 53-60-01 FIG 203.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-CHECK, FUSELAGE SKIN CRACKED 1.25 AT L-2 DOOR FWD LOWER CORNER. STOP DRILLED CRACK, FABRICATED REPAIR PARTS, TREATED AND PRIMED PARTS, INSTALLED REPAIR IAW B737 SRM 53-60-01 FIG 203.