What was found
CENTER FUSELAGE I REINFORCEMENT PLATE IS CRACKED BETWEEN FR14 AND FR 15 AND Y = .32". REMOVED AND REPLACED REINFORCEMENT PLATE AT CENTER FUSELAGE BETWEEN FR 14 AND FR 15 AND Y = .32"
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CENTER FUSELAGE I REINFORCEMENT PLATE IS CRACKED BETWEEN FR14 AND FR 15 AND Y = .32". REMOVED AND REPLACED REINFORCEMENT PLATE AT CENTER FUSELAGE BETWEEN FR 14 AND FR 15 AND Y = .32"