What was found
LT OB FORE FLAP IB LEADING EDGE IS CHAFED. REMOVED DAMAGED AREA FABRICATED HEAT TREATED AND INSTALLED REPLACEMENT SKIN IAW SOPM 20 50 01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT OB FORE FLAP IB LEADING EDGE IS CHAFED. REMOVED DAMAGED AREA FABRICATED HEAT TREATED AND INSTALLED REPLACEMENT SKIN IAW SOPM 20 50 01.