What was found
A CRACK THROUGH RIVET ON VERTICAL STIFFENER BETWEEN NR 3 AND 4 HORIZONTAL BEAMS RT SIDE OF FRONT PRESSURE BULKHEAD FORWARD SIDE. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A CRACK THROUGH RIVET ON VERTICAL STIFFENER BETWEEN NR 3 AND 4 HORIZONTAL BEAMS RT SIDE OF FRONT PRESSURE BULKHEAD FORWARD SIDE. CRACK NOTED DURING C-CHECK. CRACK REPAIRED I/A/W SRM.