What was found
MAIN CABIN FUSELAGE, STRINGER 16R CRACKED AT BS 780+24. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM 51-40-02 & DWG 143N3110, DWG 143N3800.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
MAIN CABIN FUSELAGE, STRINGER 16R CRACKED AT BS 780+24. REMOVED AND REPLACED THE STRINGER SECTION IAW SRM 51-40-02 & DWG 143N3110, DWG 143N3800.