As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN AT FR34 STRINGERS 43L AND 43R IS CHAFED FROM BODY FAIRING SCREWS. ORIGINAL SKIN THICKNESS .084". AREAS BLENDED AND MAX MATERIAL LOSS IS .011". WITHIN SRM 53-21-11 DIA 105 SHEET 1. 13%. VERIFIED CRACK-FREE PER NTM51-10-08. THIS SRM REFERS TO SRI 53-21-11-1-003-00 TABLE 104 TO RE-INSPECT AT 60000C. CURRENT PTC 17186C.