What was found
DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, RIGHT INBOARD AFT FLAP SKIN CRACKED AT OUTBOARD ATTACH POINT. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-50-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, RIGHT INBOARD AFT FLAP SKIN CRACKED AT OUTBOARD ATTACH POINT. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-50-4.