What was found
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT INBD FLAP UPPER SKIN CENTER PANEL SURFACE CORROSION, AND CRACK WS108-192. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, FIG 57-70-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-10 CHECK AND CENTER WING REPLACEMENT, FOUND LT INBD FLAP UPPER SKIN CENTER PANEL SURFACE CORROSION, AND CRACK WS108-192. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, FIG 57-70-01.