What was found
INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT L-1 DOOR FWD UPPER CORNER STA 25 BETWEEN LONG 10L-11L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C1 FUSELAGE SKIN CRACKED AT L-1 DOOR FWD UPPER CORNER STA 25 BETWEEN LONG 10L-11L. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0 FIG 15.