As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:SV, FUSELAGE STA 400 LT HOSE WHEEL AFT CORNER SKIN PANEL 1 EA FASTENER HOLE FOUND CRACKED APPROX .1250" LENGTH AT THE 3RD LAYER LOWER SURFACE FROM BOTTOM IN 9 O/C DIRECTION REFER NDT TEST REPORT FX STA 400 LT NLG WW AFT CORNER SKIN PANEL ATTACH ANGLE REPAIRED IAW HX RI-53-11-10244 REV A & EO B747-5330-51345-A. REPAIR CLASSIFIED AS MAJOR.