What was found
INSPECTION TYPE:SV, RT NLG WW AFT CORNER SKIN PANEL BS 400, 1EA FASTENER HOLE FOUND CRACKED APPROX .1250" IN LENGTH AT THE SPLICE PLATE LAYER SURFACE IN 9 O/C DIRECTION. SPLICE PLATE REPLACED AND INSTALLED IAW RI 53-11-10245, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:SV, RT NLG WW AFT CORNER SKIN PANEL BS 400, 1EA FASTENER HOLE FOUND CRACKED APPROX .1250" IN LENGTH AT THE SPLICE PLATE LAYER SURFACE IN 9 O/C DIRECTION. SPLICE PLATE REPLACED AND INSTALLED IAW RI 53-11-10245, REV A.