What was found
LEFT WING OTBD FLAP UPPER SURFACE SKIN XOF 563, HAS A 2.25 INCH CRACK. CONFIRMED BY HFEC. INSTALLED A FILLER AND DOUBLER IAW SRM 57-20-01, FIG 4, SHEET 2, VOL 1, AND SRM 51-35-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING OTBD FLAP UPPER SURFACE SKIN XOF 563, HAS A 2.25 INCH CRACK. CONFIRMED BY HFEC. INSTALLED A FILLER AND DOUBLER IAW SRM 57-20-01, FIG 4, SHEET 2, VOL 1, AND SRM 51-35-02.