What was found
INSPECTION TYPE:C2 RIGHT L/E LOWER RIB IS CRACKED AT XFS 347.750. REMOVED EXISTING REPAIR ANGLE, NDT VERIFIED CRACK IS TERMINATED AT STOPDRILL, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C2 RIGHT L/E LOWER RIB IS CRACKED AT XFS 347.750. REMOVED EXISTING REPAIR ANGLE, NDT VERIFIED CRACK IS TERMINATED AT STOPDRILL, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.