What was found
CRACK- ONE CLIP CRACKED ABOUT .5 INCH, Y=1401, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY =1. REPLACED WITH NEW CLIP IAW MD11 SRM 51-35-01 FIG 2 AND SRM 51-33-01 FIG 2 REV 41.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK- ONE CLIP CRACKED ABOUT .5 INCH, Y=1401, L31L, LEFT UPPER FUSELAGE TO WING FAIRING SUPPORT QTY =1. REPLACED WITH NEW CLIP IAW MD11 SRM 51-35-01 FIG 2 AND SRM 51-33-01 FIG 2 REV 41.