What was found
INSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN IS CRACKED AT STA 1660 LONG 11R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 16.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C2 R-2 DOOR UPPER AFT CORNER FUSELAGE SKIN IS CRACKED AT STA 1660 LONG 11R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 FIG 16.