What was found
DURING A04 CHK, LT WING INBOARD SLAT FILLET CHAFING AT WING FUSELAGE FAIRING. SLAT I/B RIB CRACKED & FAIRING RIB CRACKED. REMOVED AND REPLACED NR 1 SLAT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A04 CHK, LT WING INBOARD SLAT FILLET CHAFING AT WING FUSELAGE FAIRING. SLAT I/B RIB CRACKED & FAIRING RIB CRACKED. REMOVED AND REPLACED NR 1 SLAT.