What was found
AT C CHECK, INNER STRUCTURE SUPPORT ANGLE IS CRACKED AT NR 2 L/E SLAT INNER NOSE BETWEEN L/E SLAT ACTUATOR AND ANTI-ICE DUCT. STOP DRILLED CRACK, HFEC STOP DRILL. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 BY 1 BY 17.5, N/R 1090.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, INNER STRUCTURE SUPPORT ANGLE IS CRACKED AT NR 2 L/E SLAT INNER NOSE BETWEEN L/E SLAT ACTUATOR AND ANTI-ICE DUCT. STOP DRILLED CRACK, HFEC STOP DRILL. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 BY 1 BY 17.5, N/R 1090.