What was found
FRAME 19/20, STR 29-31 RT DAMAGED FUSELAGE SKIN AT ACCESS DOOR CONTROL PNL CORNERS. BLEND OUT DAMAGE IAW THE REFERENCED DWG EFW 632-99 & PROTECT SURFACE AP SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FRAME 19/20, STR 29-31 RT DAMAGED FUSELAGE SKIN AT ACCESS DOOR CONTROL PNL CORNERS. BLEND OUT DAMAGE IAW THE REFERENCED DWG EFW 632-99 & PROTECT SURFACE AP SRM.