What was found
NR 4 SLAT OUTBOARD SIDE OF ACTUATOR ROD END ATTACH POINT INTERNAL WEB CRACKED. *S/D* REPAIRED RIB IN ACCORDANCE WITH OVERHAUL MANUAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 4 SLAT OUTBOARD SIDE OF ACTUATOR ROD END ATTACH POINT INTERNAL WEB CRACKED. *S/D* REPAIRED RIB IN ACCORDANCE WITH OVERHAUL MANUAL.