What was found
FWD CABIN FLOOR PANEL 232AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-044<[01] RECEIVED FWD CABIN FLOOR PANEL 232AF WILL BE INSTALL ON ITEM TTG8Q00SCGXR;[02] VERIFIED STEP 1
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FWD CABIN FLOOR PANEL 232AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-044<[01] RECEIVED FWD CABIN FLOOR PANEL 232AF WILL BE INSTALL ON ITEM TTG8Q00SCGXR;[02] VERIFIED STEP 1