What was found
"INITIAL INSPECTION: CRACK IN RECEPTACLE PLATE AT FUSELAGE. (FUS) ""SUMMARY: DAMAGED IN RECEPTACLE PLATE AT FUSELAGE WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR.6
"
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
"INITIAL INSPECTION: CRACK IN RECEPTACLE PLATE AT FUSELAGE. (FUS) ""SUMMARY: DAMAGED IN RECEPTACLE PLATE AT FUSELAGE WAS REPLACED PER SRM 51-42-06-001-001-A01 PAR.6
"