As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C 44, CIRCUMFERENTIAL SKIN SPLICE PLATE FOUND CRACKED AT BOTH AFT CORNERS OF NOSE WHEEL WELL BS 400 STR 44L AND 44R. CRACK SPLICE PLATES REMOVED IAW SRM 51-30-02. NEW SPLICE PLATES DRILLED UP AND FITTED IAW SRM 51-30-02.