What was found
LT O/B WING AFT FLAP L/E DEEP CHAFE WITH CRACK AT O/B ROLLERS. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS SKIN & SPLICE IAW SRM 57-53-01 FIG 204.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT O/B WING AFT FLAP L/E DEEP CHAFE WITH CRACK AT O/B ROLLERS. REMOVED DAMAGE, FABED AND INSTALLED REPAIR PARTS SKIN & SPLICE IAW SRM 57-53-01 FIG 204.