What was found
DURING C CHECK FOUND CRACK ON FRAME 10 RHS INNER FLANGE AT TOP FORWARD RIVET AT ATTACHMENT TO WINDOW SILL STRUCTURE. MAINTENANCE REPLACED FRAME 10 RHS INNER FLANGE IAW SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C CHECK FOUND CRACK ON FRAME 10 RHS INNER FLANGE AT TOP FORWARD RIVET AT ATTACHMENT TO WINDOW SILL STRUCTURE. MAINTENANCE REPLACED FRAME 10 RHS INNER FLANGE IAW SRM 51-40-02.