What was found
INSPECTION FOUND CRACK INDICATIONS AROUND SIX EACH FASTENERS IN TOP RIGHT PANEL OF NLG WHEEL WELL. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND CRACK INDICATIONS AROUND SIX EACH FASTENERS IN TOP RIGHT PANEL OF NLG WHEEL WELL. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.