What was found
RIGHT O/B FORE FLAP L EADING EDGE CHAFED. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-53-01 FIG 201 REPAIR 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT O/B FORE FLAP L EADING EDGE CHAFED. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-53-01 FIG 201 REPAIR 1.