As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD FUSELAGE SKIN CHAFED BETWEEN FRAMS 8/9 AND STRINGERS 21R/22R. (C-CHECK RO 7/16/2021) REPAIRED FORWARD FUSELAGE SKIN CHAFED DAMAGE BETWEEN FRAMS 8/9 AND STRINGERS 21R/22R.BY CUT OUT, FILLER AND DOUBLER FABRICATION REPAIR DOUBLER AND FILLER WEIGHT=20 GRAMS NO CHANGE TO THE WEIGHT AND BALLANCE NEEDED REF SRM 53-10-01/REPAIR 02P