What was found
INSPECTION FOUND A 0.3 CRACK IN TOP LT PANEL OF NLG WHEEL WELL. THE AREA WAS REPAIRED 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 0.3 CRACK IN TOP LT PANEL OF NLG WHEEL WELL. THE AREA WAS REPAIRED IAW SRM 51-40-2.