What was found
CRACK - ANGLE, C/T WING TO BODY FAIRING SUPPORT STRUCTURE STA Y=1361, RT FUSELAGE L=1". REPLACED WITH NEW ANGLE IAW MD-11 SRM 51-33-01 AND SRM 51-35-01 REV 41. COND CHECK NORMAL AND JOB COMPLETED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK - ANGLE, C/T WING TO BODY FAIRING SUPPORT STRUCTURE STA Y=1361, RT FUSELAGE L=1". REPLACED WITH NEW ANGLE IAW MD-11 SRM 51-33-01 AND SRM 51-35-01 REV 41. COND CHECK NORMAL AND JOB COMPLETED.