What was found
DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING NR 1 SLAT II/B WEB FOR ACTUATOR ATTACH POINT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, ALODINED, AND PRIMED IAW SRM 51-40-3, 51-10-2, 51-30-2, 27-81-11, SPM 20-50-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING NR 1 SLAT II/B WEB FOR ACTUATOR ATTACH POINT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, ALODINED, AND PRIMED IAW SRM 51-40-3, 51-10-2, 51-30-2, 27-81-11, SPM 20-50-01.