What was found
RT WING O/B FOREFLAP LEADING EDGE IS CHAFED AT O/B CORNER REMOVED DAMAGE FROM SKIN ON L/E. FABRICATED DRILLED AND INSTALLED A REPAIR DOUBLER IAW SRM 57-53-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING O/B FOREFLAP LEADING EDGE IS CHAFED AT O/B CORNER REMOVED DAMAGE FROM SKIN ON L/E. FABRICATED DRILLED AND INSTALLED A REPAIR DOUBLER IAW SRM 57-53-01 FIG 201.