As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PANEL 194CL HAS CHAFING DAMAGE AT FWD I/B CORNER INNER SURFACE. ; / [01] IDENTIFIED PANEL 194CL IAW SRM 53-60-70-0I-1 FIGURE 2. TABLE 2. ITEM 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-60-70-1A-1 PARA. 4.B.(7). DAMAGE IS TO BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 53-60-70-2R-1 TABLE 202.