What was found
AT D-CHECK, RIGHT WING L/E INTERIOR, RIB FLANGE CRACKED AT SLAT 238.5 BETWEEN NR 6 AND NR 7 SLATS. STOP DRILLED BOTH ENDS OF CRACK, NDT, REMOVED FASTENERS, INSTALLED DOUBLER REPAIR PER SRM 51-40-3 8 BY 1 BY 1.5 N/R 2535.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT D-CHECK, RIGHT WING L/E INTERIOR, RIB FLANGE CRACKED AT SLAT 238.5 BETWEEN NR 6 AND NR 7 SLATS. STOP DRILLED BOTH ENDS OF CRACK, NDT, REMOVED FASTENERS, INSTALLED DOUBLER REPAIR PER SRM 51-40-3 8 BY 1 BY 1.5 N/R 2535.