What was found
FUSELAGE SKIN HAS SUBSURFACE CRACK ALONG THE CHEM-MILL EDGE 1.25"IN LENGTH LWR SIDE OF RIVET ROW STA 537 STR 12R.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS SUBSURFACE CRACK ALONG THE CHEM-MILL EDGE 1.25"IN LENGTH LWR SIDE OF RIVET ROW STA 537 STR 12R.