What was found
REAR FUSELAGE INTERNAL FOUND 1 RIB CRACKED AT FR86 STR32R. REMOVED THE CRACKED RIB. FABRICATED A NEW RIB FOR REPLACEMENT IAW SRM 51-72-10 AND IAW DWG A53986743205.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
REAR FUSELAGE INTERNAL FOUND 1 RIB CRACKED AT FR86 STR32R. REMOVED THE CRACKED RIB. FABRICATED A NEW RIB FOR REPLACEMENT IAW SRM 51-72-10 AND IAW DWG A53986743205.