As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING INSPECTION CHANNEL FOUND CRACKED IN CUTOUT ,ON FWD R/H SIDE OF CHANNEL. CRACK EXTENDS FROM CUTOUT TO BOTTOM OF FWD FLANGE. CHANNEL LOCATED IN FUSELAGE ABOVE NOSE WHEEL WELL . BOLTS THRU CHANNEL HOLD NOSE LANDING GEAR ACTUATOR AFT ATTACHMENT. FAILURE OF BRACKET COULD COMPRIMIZE STRUCTURAL INTERGRITY OF NOSE LANDING GEAR. CRACKED BRACKET REPLACED WITH SERVICEABLE BRACKET.