What was found
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK NOSE WHEEL WELL, NOSE GEAR ACTUATOR SUPPORT STRUCTURE ANGLE. REPLACED GUSSET AND ACTUATOR MOUNT PER BOEING DRAWING 65-45819. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK NOSE WHEEL WELL, NOSE GEAR ACTUATOR SUPPORT STRUCTURE ANGLE. REPLACED GUSSET AND ACTUATOR MOUNT PER BOEING DRAWING 65-45819. (M)