As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CHAFED APPROX 13 INCHES LONB BY FORWARD RIGHT WING ROOT FAIRING BETWEEN FRAMES 25/26. REF W/C 6075 FOR BLEND AND NDT. FIT EXTERNAL PATCH OVER CHAFED AREA UNDER RT WING ROOT FAIRING ON FUSELAGE SKIN BETWEEN FRAMES 25/26 PER SRM 53-00-12 FIGURE 201 INC STRINGERS ABOVE AND BELOW CHAFE PER FAX REF DJH/RJO248-98. (M)