What was found
CENTER FUSELAGE 1 AT FRAME 23 WEB INTERCOSTAL OUTBOARD ANGLE CORRODED AND INBOARD ANGLE RIVET LOOSE. OUTBOARD ANGLE REPLACED AS PER SRM 51-40-02 AND LOOSE RIVETS REPLACED ON INBOARD ANGLE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CENTER FUSELAGE 1 AT FRAME 23 WEB INTERCOSTAL OUTBOARD ANGLE CORRODED AND INBOARD ANGLE RIVET LOOSE. OUTBOARD ANGLE REPLACED AS PER SRM 51-40-02 AND LOOSE RIVETS REPLACED ON INBOARD ANGLE.