What was found
1/4IN CRACK AT NO.4 L/E SLAT LWR COVE SKIN ANGLE AT O/B STOP PAD REPAIRED PER MM 57-54-000-8
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
1/4IN CRACK AT NO.4 L/E SLAT LWR COVE SKIN ANGLE AT O/B STOP PAD REPAIRED PER MM 57-54-000-8