What was found
CRACKED RIGHT MAIN CABIN FUSELAGE TO FLOOR STIFFENER BETWEEN BS 2129 AND 2150, NEAR STRINGER 27R. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED RIGHT MAIN CABIN FUSELAGE TO FLOOR STIFFENER BETWEEN BS 2129 AND 2150, NEAR STRINGER 27R. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02-06.