What was found
COVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
COVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0.