What was found
INSPECTION FOUND A .5 CRACK AT FASTENER HOLE OF NLG WHEEL WELL TOP CENTER PANEL, STA 290, LBL 2. THE CRACKED AREA WAS CUT OUT. A DOUBLER 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 A .5 CRACK AT FASTENER HOLE OF NLG WHEEL WELL TOP CENTER PANEL, STA 290, LBL 2. THE CRACKED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.