What was found
(CAN) A CRACK FOUND ON THE JOINT ASSEMBLY TOP WHICH IS INSTALLED AT THE TOP END OF THE AXLE STRUT. AD CF-69-12 AND SB 3/12 BOLT INSPECTION ARE RELEVANT. ALSO SB 3/32 LANDING GEAR ATTACHMENT TORQUE LOADING.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) A CRACK FOUND ON THE JOINT ASSEMBLY TOP WHICH IS INSTALLED AT THE TOP END OF THE AXLE STRUT. AD CF-69-12 AND SB 3/12 BOLT INSPECTION ARE RELEVANT. ALSO SB 3/32 LANDING GEAR ATTACHMENT TORQUE LOADING.