What was found
CENTER FUSELAGE BETWEEN FRAME 23 AND 24 LOWER WEB ANGLE CORRODED. THE ANGLE WAS REPLACED IAW SRM 53-22-10 AND SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CENTER FUSELAGE BETWEEN FRAME 23 AND 24 LOWER WEB ANGLE CORRODED. THE ANGLE WAS REPLACED IAW SRM 53-22-10 AND SRM 51-40-02.