What was found
INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF NOSE WHEEL WELL GUSSET AT AFT END OF NLG ACTUATOR SUPPORT FITTING, NWW STA 251, BL 0. THE GUSSET WAS REPLACED IAW SRM 51-10-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF NOSE WHEEL WELL GUSSET AT AFT END OF NLG ACTUATOR SUPPORT FITTING, NWW STA 251, BL 0. THE GUSSET WAS REPLACED IAW SRM 51-10-02.