What was found
INSPECTION FOUND COLLAR CRACKED THROUGH LOCKING BOLT HOLE AT PIN BETWEEN INBOARD END OF GEAR BEAM AND H-LINK IN LT WHEELWELL AREA. THE PIN RETAINER FLANGE WAS REMOVED AND REPLACED IAW SRM 57-40-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND COLLAR CRACKED THROUGH LOCKING BOLT HOLE AT PIN BETWEEN INBOARD END OF GEAR BEAM AND H-LINK IN LT WHEELWELL AREA. THE PIN RETAINER FLANGE WAS REMOVED AND REPLACED IAW SRM 57-40-0.