What was found
DURING INSPECTION WHILE REMOVING LT WINGLET, AN IMPACT OCCURRED ON THE WINGLET PLUG ASSEMBLY CAUSING A 3.100 LONG CRACK ON RIB INBOARD SIDE ROOT RADIUS & A BENT ON LEADING EDGE SKIN. REPAIRED PER ERA 588666-14.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION WHILE REMOVING LT WINGLET, AN IMPACT OCCURRED ON THE WINGLET PLUG ASSEMBLY CAUSING A 3.100 LONG CRACK ON RIB INBOARD SIDE ROOT RADIUS & A BENT ON LEADING EDGE SKIN. REPAIRED PER ERA 588666-14.