What was found
RT WING O/B FORE FLAP I/B LEADING EDGE CHAFED FROM CONTACT WITH CAVITY PANEL. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND DOUBLER IAW B737 400 SRM 51 53 01 FIG 201 AND INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT WING O/B FORE FLAP I/B LEADING EDGE CHAFED FROM CONTACT WITH CAVITY PANEL. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS AND DOUBLER IAW B737 400 SRM 51 53 01 FIG 201 AND INSTALLED.