What was found
INSPECTION FOUND A .5 INCH CRACK IN NOSE WHEEL WELL STIFFENER AT STA 234, LBL 20. THE STIFFENER WAS REPAIRED IAW SRM 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN NOSE WHEEL WELL STIFFENER AT STA 234, LBL 20. THE STIFFENER WAS REPAIRED IAW SRM 51-10-2.