What was found
LEFT WING TE INBD MAIN FLAP, UPPER SURFACE TE WEDGE PANEL HAS SPOTS OF CORROSION AT MID OTBD SECTION. REPAIRED LT WING INBD MAIN FLAP UPPER SURFACE BY HOT BONDING FILLER & DOUBLER IAW SRM 57-53-01-2R FIG 201 & SRM 51-70-10-2R PARA 20.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TE INBD MAIN FLAP, UPPER SURFACE TE WEDGE PANEL HAS SPOTS OF CORROSION AT MID OTBD SECTION. REPAIRED LT WING INBD MAIN FLAP UPPER SURFACE BY HOT BONDING FILLER & DOUBLER IAW SRM 57-53-01-2R FIG 201 & SRM 51-70-10-2R PARA 20.