What was found
DURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT FWD ENTRY DOOR AREA, THE FUSELAGE SKIN WITH CRACK AT THE SILL LOWER AFT CORNER. DUE TO THIS SITUATION THE SKIN WAS REPAIRED AS PER SRM 53-10-01 REPAIR 12 FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING THE CURRENT MAINTENANCE PROCESS IT WAS FOUND AT FWD ENTRY DOOR AREA, THE FUSELAGE SKIN WITH CRACK AT THE SILL LOWER AFT CORNER. DUE TO THIS SITUATION THE SKIN WAS REPAIRED AS PER SRM 53-10-01 REPAIR 12 FIGURE 201.