What was found
LW #3 LEADING EDGE SLAT SKIN (ACTUATOR RIB ATTACH POINT) - FOUND 2EA FASTENER HOLES TO BE CRACKED IN SKIN. MARKED LOCATIONS.<[01] #3 L/E SLAT REMOVED; REPLACED; AND ADJUSTED PER AMM 27-81-21-400-801.;[02] VERIFIED CORRECTIVE ACTION #1
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LW #3 LEADING EDGE SLAT SKIN (ACTUATOR RIB ATTACH POINT) - FOUND 2EA FASTENER HOLES TO BE CRACKED IN SKIN. MARKED LOCATIONS.<[01] #3 L/E SLAT REMOVED; REPLACED; AND ADJUSTED PER AMM 27-81-21-400-801.;[02] VERIFIED CORRECTIVE ACTION #1