As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FOUND UPPER L/E WING SKIN AT PYLON LOAD FITTING NR 1 ENGINE MARKED. CONTACT PLANNING TO ISSUE WC 5724-01005-10. REMOVED PANEL 511PT FOR MX ACCESS . C/W UPPER LINK FUSE PIN REMOVAL IAW AMM 54-51-03-004-001, PARA F6. REMOVED FASTENER. INSTALLED PANEL 511 PT. C/W PRI 514854-14AD, REV 0 THROUGH REV 5 AND WC 5724-01005-10. C/W ERA 514854-14 AD.