What was found
DROOP L/E HAS CHAFED AT LEADING INBD AND OTBD SIDES AND CRACK ON THE UPPER SKIN AT RT WING. REPAIR CRACK UPPER SKIN WITH A 0.100" 301-50 STAINLESS STEEL DOUBLER IAW SRM 57-10-00 FIG 55, MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DROOP L/E HAS CHAFED AT LEADING INBD AND OTBD SIDES AND CRACK ON THE UPPER SKIN AT RT WING. REPAIR CRACK UPPER SKIN WITH A 0.100" 301-50 STAINLESS STEEL DOUBLER IAW SRM 57-10-00 FIG 55, MAJOR REPAIR.