What was found
WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RT (O/B) ACTUATOR ATTACH POINT RIB FLANGE IS CRACKED COMMON TO COVE PANEL LOWER ATTACHMENT STRINGER. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RT (O/B) ACTUATOR ATTACH POINT RIB FLANGE IS CRACKED COMMON TO COVE PANEL LOWER ATTACHMENT STRINGER. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9.