What was found
DURING BRIDGE CHECK + 4C CHECK, EGAT MECH FOUND ANGLE OF LT WING FIXED L/E CRACK AT STA XORS=488. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A57B-1301 REV 00 AND EI W2008A57B-1301 REV 01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING BRIDGE CHECK + 4C CHECK, EGAT MECH FOUND ANGLE OF LT WING FIXED L/E CRACK AT STA XORS=488. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A57B-1301 REV 00 AND EI W2008A57B-1301 REV 01.