What was found
INITIAL INSPECTION: CRACK IN RECEPTACLE PLATE AT FUSELAGE. (FUS)SUMMARY: RECEPTACLE PLATE AT FUSELAGE WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01
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: RECEPTACLE PLATE AT FUSELAGE WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01